727 200 Performance Manual

Boeing 727-200 Performance Manual

727-200 / JT8D-15 FAA / Pounds

- All Rights Reserved -

June, 26th 2012 Issued by: Flight Operations Engineering Document Numer: PM.727.200/01

Boeing 727-200 INTRODUCTION Performance Manual

JUN 26, 2012 727-200/JT8D-15 0.1

CHAPTER 0 – INTRODUCTION

0.1 INTRODUCTION ................................................... 3 0.2 RECORD OF REVISIONS ............................................ 5 0.3 LIST OF EFFECTIVE PAGES ........................................ 7

INTRODUCTION Boeing 727-200 Performance Manual

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JUN 26, 2012 727-200/JT8D-15 0.3

0.1 INTRODUCTION The Boeing 727 Performance Manual has been prepared as the company performance manual for the Boeing 727-200 airplanes. It contains performance data, which are peculiar to the flight planning and operation of these airplanes. The Boeing 727 Performance Manual will be issued to pilots, copilot and flight engineers who fly this type of aircraft and to all offices which are involved in flight planning and flight preparation. Any suggestions for improvement and advise of errors or obsolescence will be appreciated and shall be forwarded to the operations department. For missing amendments or pages the distribution department shall be contacted. For easy reference the manual is divided into chapters which are broken down into sections. Each manual sheet bears an chapter reference on the bottom consisting of a group of two numerals, indicating the chapter and the page. The pages are numbered consecutively. Amendments to this manual will be issued when necessary and are numbered consecutively. Each amendment should be inserted immediately and entered in the Record of Amendments. Alterations to former pages will be identified by a strong vertical line, except when a whole chapter or section is revised. Each amendment contains a distribution list which indicates the amendment highlights. The Performance Manual is divided into the following chapters: Chapter 0 Introduction Chapter 1 General Performance Chapter 2 Flight Planning Chapter 3 Takeoff Chapter 4 Enroute Chapter 5 Landing


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JUN 26, 2012 727-200/JT8D-15 0.5

0.2 RECORD OF REVISIONS Revision No. Revision Date Date Inserted Inserted by


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0.3 LIST OF EFFECTIVE PAGES

PAGE DATE PAGE DATE COVER JUN 26, 2012

0.1 JUN 26, 2012 0.2 JUN 26, 2012 0.3 JUN 26, 2012 0.4 JUN 26, 2012 0.5 JUN 26, 2012 0.6 JUN 26, 2012 0.7 JUN 26, 2012 0.8 JUN 26, 2012 2.19 JUN 26, 2012

2.20 JUN 26, 2012 TAB CHAPTER 1 2.21 JUN 26, 2012

2.22 JUN 26, 2012 1.1 JUN 26, 2012 2.23 JUN 26, 2012 1.2 JUN 26, 2012 2.24 JUN 26, 2012 1.3 JUN 26, 2012 1.4 JUN 26, 2012 TAB CHAPTER 3 1.5 JUN 26, 2012 1.6 JUN 26, 2012 3.1 JUN 26, 2012 1.7 JUN 26, 2012 3.2 JUN 26, 2012 1.8 JUN 26, 2012 3.3 JUN 26, 2012 1.9 JUN 26, 2012 3.4 JUN 26, 2012 1.10 JUN 26, 2012 3.5 JUN 26, 2012 1.11 JUN 26, 2012 3.6 JUN 26, 2012 1.12 JUN 26, 2012 3.7 JUN 26, 2012

3.8 JUN 26, 2012 TAB CHAPTER 2 3.9 JUN 26, 2012

3.10 JUN 26, 2012 2.1 JUN 26, 2012 3.11 JUN 26, 2012 2.2 JUN 26, 2012 3.12 JUN 26, 2012 2.3 JUN 26, 2012 3.13 JUN 26, 2012 2.4 JUN 26, 2012 3.14 JUN 26, 2012 2.5 JUN 26, 2012 3.15 JUN 26, 2012 2.6 JUN 26, 2012 3.16 JUN 26, 2012 2.7 JUN 26, 2012 3.17 JUN 26, 2012 2.8 JUN 26, 2012 3.18 JUN 26, 2012 2.9 JUN 26, 2012 3.19 JUN 26, 2012 2.10 JUN 26, 2012 3.20 JUN 26, 2012 2.11 JUN 26, 2012 3.21 JUN 26, 2012 2.12 JUN 26, 2012 3.22 JUN 26, 2012 2.13 JUN 26, 2012 3.23 JUN 26, 2012 2.14 JUN 26, 2012 3.24 JUN 26, 2012 2.15 JUN 26, 2012 3.25 JUN 26, 2012 2.16 JUN 26, 2012 3.26 JUN 26, 2012 2.17 JUN 26, 2012 3.27 JUN 26, 2012 2.18 JUN 26, 2012 3.28 JUN 26, 2012

3.29 JUN 26, 2012


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PAGE DATE PAGE DATE CHAPTER 3 (CON’T)

3.30 JUN 26, 2012 TAB CHAPTER 4 3.31 JUN 26, 2012 3.32 JUN 26, 2012 4.1 JUN 26, 2012 3.33 JUN 26, 2012 4.2 JUN 26, 2012 3.34 JUN 26, 2012 4.3 JUN 26, 2012 3.35 JUN 26, 2012 4.4 JUN 26, 2012 3.36 JUN 26, 2012 4.5 JUN 26, 2012 3.37 JUN 26, 2012 4.6 JUN 26, 2012 3.38 JUN 26, 2012 4.7 JUN 26, 2012 3.39 JUN 26, 2012 4.8 JUN 26, 2012 3.40 JUN 26, 2012 4.9 JUN 26, 2012 3.41 JUN 26, 2012 4.10 JUN 26, 2012 3.42 JUN 26, 2012 4.11 JUN 26, 2012 3.43 JUN 26, 2012 4.12 JUN 26, 2012 3.44 JUN 26, 2012 4.13 JUN 26, 2012 3.45 JUN 26, 2012 4.14 JUN 26, 2012 3.46 JUN 26, 2012 3.47 JUN 26, 2012 TAB CHAPTER 5 3.48 JUN 26, 2012 3.49 JUN 26, 2012 5.1 JUN 26, 2012 3.50 JUN 26, 2012 5.2 JUN 26, 2012 3.51 JUN 26, 2012 5.3 JUN 26, 2012 3.52 JUN 26, 2012 5.4 JUN 26, 2012 3.53 JUN 26, 2012 5.5 JUN 26, 2012 3.54 JUN 26, 2012 5.6 JUN 26, 2012 3.55 JUN 26, 2012 5.7 JUN 26, 2012 3.56 JUN 26, 2012 5.8 JUN 26, 2012 3.57 JUN 26, 2012 5.9 JUN 26, 2012 3.58 JUN 26, 2012 5.10 JUN 26, 2012 3.59 JUN 26, 2012 5.11 JUN 26, 2012 3.60 JUN 26, 2012 5.12 JUN 26, 2012 3.61 JUN 26, 2012 5.13 JUN 26, 2012 3.62 JUN 26, 2012 5.14 JUN 26, 2012 3.63 JUN 26, 2012 5.15 JUN 26, 2012 3.64 JUN 26, 2012 5.16 JUN 26, 2012 3.65 JUN 26, 2012 3.66 JUN 26, 2012 3.67 JUN 26, 2012 3.68 JUN 26, 2012 3.69 JUN 26, 2012 3.70 JUN 26, 2012 3.71 JUN 26, 2012 3.72 JUN 26, 2012 3.73 JUN 26, 2012 3.74 JUN 26, 2012 3.75 JUN 26, 2012 3.76 JUN 26, 2012 3.77 JUN 26, 2012 3.78 JUN 26, 2012 3.79 JUN 26, 2012 3.80 JUN 26, 2012

Boeing 727-200 GENERAL PERFORMANCE Performance Manual

JUN 26, 2012 727-200/JT8D-15 1.1

CHAPTER 1 – GENERAL PERFORMANCE

1.1 DEFINITIONS .................................................... 3 1.1.1 Airspeeds................................................... 3 1.1.2 Temperature................................................. 4 1.1.3 Takeoff Path................................................ 4 1.1.4 Takeoff Flight Path ........................................ 5

1.2 AIRPLANE LIMITATIONS AND GENERAL PERFORMANCE................... 7 1.2.1 Stall Speeds................................................ 7 1.2.2 Temperature Conversion ..................................... 8 1.2.3 Altimeter and Airspeed Calibration ......................... 8

1.3 WEIGHT DEFINITIONS ............................................. 9 1.3.1 General..................................................... 9 1.3.2 Standard Weights .......................................... 10

1.4 WEIGHT LIMITATIONS ............................................ 11 1.4.1 Maximum Weights (AFM) ..................................... 11 1.4.2 Center of Gravity Limitations (AFM) ....................... 12

GENERAL PERFORMANCE Boeing 727-200 Performance Manual

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JUN 26, 2012 727-200/JT8D-15 1.3

1.1 DEFINITIONS

1.1.1 Airspeeds All airspeeds and Mach values in this manual are based on the normal static source position error and assume zero instrument error. Static Source Position error,Vp , is the error due to the location of the static port within the airplane pressure field. Indicated Airspeed, VI, IAS - Airspeed indicator reading, as installed in the airplane, uncorrected for static source position error (assumes zero instrument error). Calibrated Airspeed, Vc, CAS - Indicated airspeed corrected for static source position error (Vc = VI + Vp). Equivalent Airspeed, Ve, EAS - Calibrated airspeed corrected for compressibility (Ve = Vc - Vc), True Airspeed, VT , TAS - Equivalent airspeed corrected for

atmospheric density effects (VT = Ve/ ρ ). True Mach Number, M - Machmeter reading, as installed in the airplane, corrected for static source position error. Critical Engine Failure Speed, VEF - The speed at which, if the most critical engine fails, the engine failure is recognized at Vl, 1 second later. Takeoff Decision Speed, Vl - Following a failure of the critical engine at VEF, the speed from which a decision to continue the takeoff results in a takeoff distance to a height of 35 feet at V2 speed that will not exceed the usable takeoff distance and the speed at which the first action is taken to bring the airplane to a full stop will not exceed the accelerate-stop distance available. Vl must not be less than the minimum Vl for control on the ground Vl(MCG) or greater than the rotation speed, VR, or greater than the maximum brake energy speed, VMBE Rotation Speed, VR - The speed at which rotation from the three-point attitude to the takeoff attitude is initiated. Takeoff Decision Speed Ratio, Vl/VR - The ratio of the takeoff decision speed, V1, to the rotation speed, VR. Maximum Brake Energy Speed, VMBE - The highest takeoff decision speed from which the airplane may be brought to a stop without exceeding the maximum energy absorption capability of the brakes. Maximum Brake Energy Speed is compared in takeoff planning to Vl speed. Takeoff Safety Speed, V2 - The target speed to be attained at the 35 foot height, assuming recognition of an engine failure at or after Vl.


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Air Minimum Control Speed, VMCA - The minimum flight speed at which the airplane is controllable with a maximum of 5 degrees bank when the critical engine suddenly becomes inoperative with the remaining engine at takeoff thrust. Minimum V1 for Control on the Ground, Vl(MCG) - The minimum takeoff decision speed, Vl, at which, when Re-critical engine suddenly becomes inoperative at VEF with the remaining engine at takeoff thrust, it is possible to control the airplane with primary aerodynamic controls alone and continue the takeoff. Landing Reference Speed, VREF - The minimum speed at the 50 foot height in a normal landing. This speed is equal to 1.3 times the stall speed in the landing configuration. Design maneuvering Speed, VA - The maximum speed at which application of full available aileron, rudder or elevator will not overstress the airplane.

1.1.2 Temperature ISA - International Standard Atmosphere, as accepted by the International Civil Aviation Organization. OAT - Outside Air Temperature the free air static (ambient) temperature. SAT - Static Air Temperature outside air (ambient) temperature as computed from TAT (see temperature conversion chart this section). TAT - Total Air Temperature - static air temperature plus adiabatic compression (ram) rise as indicated on the Total Air Temperature indicator.

1.1.3 Takeoff Path The takeoff path assumes failure of the most critical engine at VEF and extends from a standing start to a point where the airplane is at least 1,500 feet above the takeoff surface and has achieved the enroute configuration and final climb speed. The performance charts divide the takeoff path into segments representing distinct changes in airplane configuration, airspeed, and engine thrust as defined below. Some of these definitions are abbreviated versions of those appearing in FAR Parts 1 and 25; the appropriate regulations should be consulted for complete details. Clearway - An obstacle-free area beyond the takeoff runway which can be used as a part of the takeoff distance available. Stopway - An area beyond the takeoff runway capable of supporting the airplane in an aborted takeoff which can be used as part of the accelerate-stop distance available.


JUN 26, 2012 727-200/JT8D-15 1.5

Takeoff Distance Required - The greater of: (1) the distance to takeoff and climb to a height of 35 feet with a failure of the critical engine at VEF, or (2) 115 percent of the distance to takeoff and climb to a height of 35 feet with all engines operating. Takeoff Run Required - The greater of: (1) the distance to takeoff and climb to a point equidistant between lift off and the 35 foot height point with a failure of the critical engine at VEF, or (2) 115 percent of the distance to takeoff and climb to a point equidistant between lift off and the 35 foot height point with all engines operating. Accelerate-Stop Distance Required - The greater of: (1) The sum of the distances required to accelerate with all engines operating and come to a complete stop assuming a critical engine failure at VEF, or (2) The sum of the distances required to accelerate with all engines operating and come to a complete stop with all engines still operating.

1.1.4 Takeoff Flight Path The takeoff flight path begins 35 feet above the takeoff surface at the end of the takeoff distance and extends to a point where the airplane is at least 1500 feet above the takeoff surface and has achieved the enroute configuration and final climb speed. Climb Gradient - The ratio, expressed as a percentage, of the change in geometric height divided by the horizontal distance travelled in a given time. Gross gradient is the actual calculated performance of the airplane under specified conditions, while Net gradient is the gross gradient reduced by an increment specified in the regulations. Gross Height - The geometric height attained at any point in the takeoff flight path using gross climb performance. Gross height is used for calculating actual pressure altitude at which obstacle clearance procedures and wing flap retraction are initiated, and level-off height scheduled. Net Height - The geometric height attained at any point in the takeoff flight path using net climb performance. Net height is used to determine the net flight path which must clear any obstacle by at least 35 feet to comply with the regulations. Reference Zero - A point on the runway or clearway plane at the end of the takeoff distance and 35 feet below the flight path to which the height and distance coordinates of other points in the takeoff flight path are referred. First Segment - Extends from the end of the takeoff distance to the point where the landing gear is assumed to be fully retracted, using takeoff thrust and takeoff flaps at a constant V2 speed.


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Second Segment - Extends from the gear up point to a gross height of at least 400 feet, using takeoff thrust and takeoff flaps at a constant V2 speed. Third Segment - The horizontal distance required to accelerate, at constant altitude using takeoff thrust, to the final climb speed while retracting flaps in accordance with the recommended speed schedule. Maximum Level-Off Height - The maximum height at which the third segment can be completed before the time limit on the use of takeoff thrust expires. Final Takeoff Segment - Extends from the end of the third segment to a gross height of at least 1500 feet, with flaps up, maximum continuous thrust and at final climb speed.


JUN 26, 2012 727-200/JT8D-15 1.7

1.2 AIRPLANE LIMITATIONS AND GENERAL PERFORMANCE

1.2.1 Stall Speeds These tables present the Stall Speeds and the Stick Shaker Speeds as a function of gross weight and flap setting.

Stall Speeds Flap Setting

Gross Weight up 5 15 25 30 40 pounds x 1000 Stall Speed KIAS

170 163 130 121 111 107 110 165 160 128 118 109 106 108 160 157 125 116 107 104 105 155 154 123 114 105 102 102 150 151 121 112 103 100 100 145 148 118 109 101 98 97 140 145 116 107 99 96 94 135 142 113 105 97 94 92 130 139 111 102 95 92 89 125 136 109 100 92 89 87 120 133 106 98 90 87 84 115 130 104 95 88 85 82 110 126 101 93 86 83 80 105 123 99 91 84 82 77 100 120 96 89 82 80 75

Stick Shaker Speeds Flap Setting

Gross Weight up 5 15 25 30 40 pounds x 1000 Stick Shaker Speed KIAS

170 175 143 134 125 124 118 165 173 141 132 123 122 116 160 170 139 130 121 120 114 155 167 137 128 119 117 112 150 164 134 126 117 115 109 145 162 132 124 115 113 107 140 159 130 122 113 110 105 135 156 127 120 111 108 103 130 153 125 117 109 106 100 125 150 123 115 107 103 98 120 147 120 113 105 101 96 115 144 118 111 102 98 94 110 141 115 108 100 96 91 105 138 112 106 98 93 89 100 134 110 103 95 90 86

Speeds applicable to takeoff and landing altitudes only. Values are based on most forward C.G.


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1.2.2 Temperature Conversion Use the table to convert Total Air Temperature (TAT) to Outside Air Temperature (OAT).

INDICATED MACH NUMBER .30 .40 .50 .60 .70 .76 .78 .80 .82 .84

IND TAT - °C TRUE OUTSIDE AIR TEMPERATURE - DEGREES C

70 47 39 34 33 31 29 28 65 49 42 35 30 28 27 25 23 60 50 44 38 30 25 24 22 21 19 55 49 45 39 33 26 21 19 18 16 14 50 44 40 35 28 21 17 15 13 12 10 45 39 35 30 24 17 12 10 9 7 6 40 34 30 25 19 12 8 6 4 3 1 35 30 25 20 14 7 3 2 0 -2 -3 30 25 21 16 10 3 -1 -3 -4 -6 -7 25 20 16 11 5 -2 -6 -7 -9 -10 -12 20 15 11 6 0 -6 -10 -12 -13 -15 -16 15 10 6 1 -4 -11 -15 -16 -18 -19 -21 10 5 1 -3 -9 -15 -19 -21 -22 -24 -25

5 0 -4 -8 -14 -20 -24 -25 -27 -28 -29 0 -5 -8 -13 -18 -24 -28 -30 -31 -32 -34

-5 -10 -13 -18 -23 -29 -33 -34 -35 -37 -38 -10 -15 -18 -23 -28 -33 -37 -39 -40 -41 -43 -15 -20 -23 -27 -32 -38 -42 -43 -44 -46 -47 -20 -24 -28 -32 -37 -43 -46 -47 -49 -50 -51 -25 -29 -33 -37 -42 -47 -51 -52 -53 -54 -56 -30 -34 -38 -42 -46 -52 -55 -56 -58 -59 -60 -35 -39 -42 -46 -51 -56 -60 -61 -62 -63 -64 -40 -44 -47 -51 -56 -61 -64 -65 -66 -68 -69

1.2.3 Altimeter and Airspeed Calibration Corrections due to static port position error are minimal for Captain, F/O, and auxiliary static ports. They are less than 1 knot, .001 Mach, or 20 feet of altitude for all flap positions between 1.2 VS and VMO, MMO or VFE as applicable. This is true with the landing gear retracted or extended, also in taxi attitude on the ground. Since these corrections are so minimal, desired speed and altitude will be flown at that indicated value.


JUN 26, 2012 727-200/JT8D-15 1.9

1.3 WEIGHT DEFINITIONS

1.3.1 General Maximum Taxi Weight (MTXW) The MTXW is a structual limit and is in no way influenced by operational conditions of the aircraft. Maximum Allowable Takeoff Weight (MATOW) The MATOW is the maximum weight at start of the takeoff-run (at brake release).

Maximum Zero Fuel Weight (MZFW) The MZFW must not be exceeded by the full loaded aircraft with fuel tanks empty. Maximum Landing Weight (MLAW) The MLAW is a structual limit. Any weight in excess of MLAW must be consists of disposable fuel. Due to insufficient runway length, high airfield altitude, etc. the MLAW may have to be restricted. Takeoff Fuel (TOF) The weight of the fuel on board at take-off. Operating Weight DOW + Takeoff Fuel Total Traffic Load (TTL) The weight of cargo loads, passengers and passenger bags including any non-revenue load. Zero Fuel Weight (ZFW) DOW + Total Traffic Load Trip Fuel The weight of the fuel necessary to cover the normal leg without reserves. Landing weight The weight at landing = Takeoff Weight (TOW) - Trip Fuel.


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1.3.2 Standard Weights The following Standard Weights are according to Advisory Circular 120-27D and are used for Weight and Balance calculations: FLIGHT CREW Flight Crew Member 190 LB Pilot Flight Bag 20 LB Roller Bag 30 LB CABIN CREW Cabin Attendant 170 LB Flight Attendant Kit 10 LB Roller Bag 30 LB PASSENGER WEIGHT The AC 120-27D specifies an average passenger weight of 195 LB which consists of a 179 LB passenger plus 16 LB carry-on baggage and personal items.


JUN 26, 2012 727-200/JT8D-15 1.11

1.4 WEIGHT LIMITATIONS

1.4.1 Maximum Weights (AFM) Maximum Taxi Weight (MTXW):...............185,800 pounds Maximum Takeoff Weight (MTOW):............184,800 pounds* Maximum Zero Fuel Weight (MZFW):..........138,000 pounds Maximum Landing Weight (MLAW): Flaps 30...........................154,500 pounds Flaps 40...........................142,500 pounds * for pressure altitudes of 2000 ft and below with a linear reduction of 125 lbs for each 1000 ft airport pressure altitude above 2000 ft. The above maximum allowable weights may be further reduced by field length, climb, tire speed and size, or breake energy limits, or obstacle clearance, enroute and landing requirements. The fuel on board at takeoff must exceed 14,903 lbs when the following conditions exists:

flaps 5 improved climb performance is used airport altitude is below 6500 ft actual takeoff weight is within 882 lbs of the flaps 5 improved

climb performance limit weight.


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1.4.2 Center of Gravity Limitations (AFM)

110

120

130

140

150

160

170

180

190

0 10 20 30 40 50Center of Gravity % MAC

Gro

ss W

eigh

t lbs

x100

0

Boeing 727-200 FLIGHT PLANNING Performance Manual

JUN 26, 2012 727-200/JT8D-15 2.1

CHAPTER 2 – FLIGHT PLANNING

2.1 DRY OPERATING WEIGHT AND INDEX ................................. 3 2.1.1 General..................................................... 3 2.1.2 Usage of the DOW/DOI data .................................. 4 2.1.3 Actual DOW and DOI Data .................................... 4

2.2 COMPARTMENTS ................................................... 5 2.2.1 Passenger Compartment ...................................... 5 2.2.2 Cargo Compartments ......................................... 5

2.3 LOADING INSTRUCTIONS ........................................... 6 2.3.1 General..................................................... 6 2.3.2 Distribution of Cargo ...................................... 6 2.3.3 Flight Kit.................................................. 6 2.3.4 Crew Baggage................................................ 6 2.3.5 Transportation of Live Animals ............................. 7

2.4 LOAD AND TRIM SHEET ............................................ 8 2.4.1 General..................................................... 8 2.4.2 Fuel Correction ............................................ 8 2.4.3 Loading Tables.............................................. 9 2.4.4 Index Conversion Chart .................................... 10 2.4.5 Manual Load and Trim Sheet ................................ 11

2.5 FUEL .......................................................... 13 2.5.1 General.................................................... 13 2.5.2 Fuel Type.................................................. 13 2.5.3 Refueling.................................................. 13

2.6 FLIGHT PLANNING ............................................... 20 2.6.1 Flight Planning Allowances ................................ 20 2.6.2 Optimum Altitude .......................................... 21 2.6.3 Holding.................................................... 22 2.6.4 Flight Time and Fuel Table ................................ 22

FLIGHT PLANNING Boeing 727-200 Performance Manual

2.2 727-200/JT8D-15 JUN 26, 2012



JUN 26, 2012 727-200/JT8D-15 2.3

2.1 DRY OPERATING WEIGHT AND INDEX

2.1.1 General Dry Operating Weight (DOW) The DOW is defined as the weight of the completely equipped aircraft, including all operational items, such as crew with their baggage, removable cabin equipment, meal and liquor service equipment, food and beverage, drinking and washing water, engine and auxiliary oil and unusable fuel. Not included in the DOW are fuel and payload, weight of pallets, igloos and nets and other tiedown equipment. Dry Operating Index (DOI) The DOI indicates the Center of Gravity position corresponding to the Dry Operating Weight. The DOI is defined by the following formula:

2080000

880ArmDOWDOI

Datum.....................................................Sta. 0 Leading Edge of MAC............................Sta. 860.2 inches Length of MAC.......................................180.0 inches Reference line for DOI and Balance Chart................Sta. 880


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2.1.2 Usage of the DOW/DOI data The DOW and DOI data shall be used in the following manner: 1) Enter the table with Tail Number and read seating version. 2) Select respective Group and read DOW and DOI data. 3) Correct obtained DOW/DOI data as indiacted in correction table. 4) Enter corrected DOW/DOI in Load and Trim Sheet.

2.1.3 Actual DOW and DOI Data ALL WEIGHTS IN POUNDS

Tail Number Version Group Crew DOW DOI

A 3/0 100704 43.7 B 3/4 101544 41.5 12/137 C 3/4 102144 39.9 A 3/0 100704 43.7 B 3/4 101544 41.5 12/137 C 3/4 102144 39.9

DOW/DOI Corrections DOW DOI

Flight without Flight Crew Baggage -90 -0.41 Flight without Cabin Crew Baggage -120 -0.80 Flight Kit* +120 +0.43 1st Observer Seat Occupied** +210 -1.94 2nd Observer Seat Occupied** +210 -1.84 * Must be loaded in AFT Compartment ** Flight Bag included, Baggage shall be treated as Passenger Baggage

Group Classification Operation Group

Flights without Pantry and Cabin Crew (Ferry/Training) A Flights with Cabin Crew and without Pantry (Ferry) B Normal Operation with Cabin Crew and Pantry C NOTE: Flight Crew Baggage must be loaded in FWD Compartment and Cabin Crew Baggage must be loaded in FWD Closet.


JUN 26, 2012 727-200/JT8D-15 2.5

2.2 COMPARTMENTS

2.2.1 Passenger Compartment

2.2.2 Cargo Compartments The forward and aft compartments are classified as FAR class “D” because they are so designed and constructed that a fire occuring therein will be completely confined without endangering the safety of the airplane or the occupants. Both compartments are pressurized. The following tabulation shows temperature within the forward and aft compartment for normal flight profiles. Temperatures apply to all locations except the door area, where the temperature are some degrees lower than given in the table.

Flight Time (hrs) Initial Temperature

°C 0.5 1.0 1.5 2.0 2.5 3.0-5.0 +30 +24 +20 +18 +16 +16 +15 +25 +21 +18 +17 +16 +15 +15 +20 +18 +17 +16 +15 +15 +15 +15 +15 +15 +15 +15 +15 +15 +10 +13 +14 +15 +15 +15 +15 +5 +10 +13 +14 +14 +15 +15 0 +8 +11 +13 +14 +15 +15 -5 +6 +8 +12 +13 +14 +15

Compartment Dimensions

Dimension Forward Compartment

Aft Compartment

Length (Inch) 320 316

Bulk Volume (ft³) 710 815


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Compartment Weight Limitations The weight limitations for both lower cargo compartments are as follows:

Forward Compartment Aft Compartment

9000 lbs 10000 lbs

Compartment Door Opening Sizes

Forward Compartment Aft Compartment

Width(In) 54 54

Height (In) 42 44

2.3 LOADING INSTRUCTIONS

2.3.1 General Loading instruction applies to loadmasters and handling agents who control the weight and distribution of the traffic load (e.g., passengers, cargo, baggage and mail). However, the Commander has the final authority concerning acceptance and placement of the traffic load.

2.3.2 Distribution of Cargo Normally the ground handling personnel will decide how to distribute the cargo between the compartments according to their instructions. The cargo shall be distributed evenly among compartments, taking into account weight and distribution of passenger and baggage.

2.3.3 Flight Kit The Flight Kit shall be loaded in the AFT Compartment. The following items are included in the Flight Kit:

Item Weight Spare Parts 75 LB Tool Kit Box 45 LB FLIGHT KIT TOTAL 120 LB

2.3.4 Crew Baggage Flight Crew baggage must be loaded in FWD compartment. Cabin Crew baggage must be loaded in FWD closet.


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2.3.5 Transportation of Live Animals The warmest temperatures will occur in the forward end of the forward compartment, so it is the recommended location for transport of coldsensitive animals. This table shows the quantity limits for loading live animals.

Maximum Quantity in Compartment Group Animal, example

FWD AFT

1 Chimpanzees, gibbons, monkey, apes 125 N/A

2 Tropical fish, fish No Limit N/A

3 Shrimps, reptiles, snakes, crabs, frogs, oysters

No Limit

4 Cats, dogs, mice, hamsters, pigs 125 N/A

5 Tropical birds, poultry, birds 125 N/A

6 Minks, squirrels, weasels 125 N/A 7 Chinchillas 125 N/A 8 Sea lions 100 N/A

Note 1: Maximum weights given are gross weights, except for

group 1 and 4, which indicates net weight. Note 2: NA indicates that no animals from that group can be

loaded. Note3: If other baggage is presented, reduce the animal

load in proportion to the compartment space taken by the luggage. For example, if 25% of the compartment is filled with luggage, the animal load should be reduced by 25%


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2.4 LOAD AND TRIM SHEET

2.4.1 General For each flight a load and trim sheet has to be used. For the calculation of the Load & Trim Sheet the passenger standard weight has been used.

2.4.2 Fuel Correction A fuel correction has to be applied to the DOI. The following table may be used to obtain the correction index. The table is based on the standard fuel distribution procedure.

Fuel Index Correction and Distribution

TOTAL TANK FUEL 1 2 3 LBS LBS

I.U.

3000 1000 1000 1000 +2.8 6000 2000 2000 2000 +5.8 9000 3000 3000 3000 +8.9

12000 4000 4000 4000 +12.1 15000 5000 5000 5000 +15.5 18000 6000 6000 6000 +18.9 21000 7000 7000 7000 +22.4 24000 8000 8000 8000 +26.0 27000 9000 9000 9000 +29.6 30000 10000 10000 10000 +33.3 33000 11000 11000 11000 +37.0 36000 12000 12000 12000 +40.8 39000 12000 15000 12000 +42.0 42000 12000 18000 12000 +43.3 45000 12000 21000 12000 +44.6 48000 12000 24000 12000 +45.8 51000 12000 27000 12000 +47.1 54000 12000 30000 12000 +48.4


JUN 26, 2012 727-200/JT8D-15 2.9

2.4.3 Loading Tables The following Loading Tables shall be used when using the Manual Load and Trim Sheet.

Cargo Loading Table

Weight I.U. lbs Fwd Aft

6000 +21.4 5000 -12.5 +17.9 4000 -10.0 +14.3 3000 -7.5 +10.7 2000 -5.0 +7.1 1000 -2.5 +3.6 900 -2.2 +3.2 800 -2.0 +2.9 700 -1.7 +2.5 600 -1.5 +2.1 500 -1.2 +1.8 400 -1.0 +1.4 300 -0.7 +1.0 200 -0.5 +0.7 100 -0.2 +0.4

Passenger Loading Table

PAX Weight I.U. Number lbs

Forward Compartment 5 850 -3.2

10 1700 -6.3 15 2550 -9.5 20 3400 -12.7 25 4250 -15.8 29 4930 -18.4

Aft Compartment 10 1700 +3.1 20 3400 +6.3 30 5100 +9.4 40 6800 +12.6 50 8500 +15.7 60 10200 +18.9 70 11900 +22.0 80 13600 +25.2 90 15300 +28.3

100 17000 +31.4 110 18700 +34.6 120 20400 +37.7 130 22100 +40.9 133 22610 +41.8


2.10 727-200/JT8D-15 JUN 26, 2012

2.4.4 Index Conversion Chart

0

20000

40000

60000

80000

100000

120000

140000

160000

180000

200000

0 20 40 60 80 100 120 140 160

Index Units

Gro

ss W

eigh

t [lb

s]

% MAC

5

10 15 20

25 30 35 40

Example:Gross Weight = 14800 lbsIndex Units = 84

Find: MAC = 32%


JUN 26, 2012 727-200/JT8D-15 2.11

2.4.5 Manual Load and Trim Sheet The Loadsheet consists of 3 copies (White - original, Yellow and Pink - copies), and shall always be signed by the Commander. Loadsheet pages are designated according to the following:

Original shall be kept onboard during flight, Yellow Copy shall be left in the departing airport, and be

filed there for 3 months, Pink Copy shall be kept on board in the case if a/c is forced

to use an alternate airfield and be filed there for 3 months. Procedure 1. Enter the DOW/DOI data. 2. Enter the Cargo and Passenger weights and the respective index. Read the respective index from the Loading Tables. 3. Add all weights and index numbers and enter the result in the Zero Fuel Weight box. 4. Add the Takeoff Fuel and enter the Fuel Index Correction. Add Takeoff Fuel and Zero Fuel Weight as well as the index at Zero Fuel Weight and the Fuel Index. 5. With the Takeoff Weight and the Index at Takeoff Weight enter Index Conversion Chart and read MAC. Enter MAC at Takeoff in the box. 6. From Takeoff Weight subtract the Trip Fuel to find the Landing Weight. Enter Landing Weight into respective box.


2.12 727-200/JT8D-15 JUN 26, 2012

Flight Date Plane Departure Station

Item Weight LBS Index DOW

FWD Passengers

AFT

FWD Cargo

AFT

ZERO FUEL WEIGHT

MAX 138,000

Takeoff Fuel

TAKEOFF WEIGHT

MAX

Trip Fuel

LANDING WEIGHT

MAX

Remarks

MAC at Takeoff Handling Agent Pilot in Command

Flight EXAMPLE

Date Plane Departure Station

Item Weight LBS Index

DOW 102404 38.2 FWD 4250 -15.8

Passengers AFT 20400 37.7 FWD 3000 -7.5

Cargo AFT 2000 7.1

ZERO FUEL WEIGHT 132054 59.7 MAX 138,000 Takeoff Fuel 21000 22.4 TAKEOFF WEIGHT 153054 82.1 MAX Trip Fuel 18000 LANDING WEIGHT 135054 MAX

Remarks

MAC at Takeoff 28%

Handling Agent Pilot in Command


JUN 26, 2012 727-200/JT8D-15 2.13

2.5 FUEL

2.5.1 General The primary purpose of fuel loading and fuel utilisation schedules is to ensure the best weight distribution along the wing span for all stages of flight, in order to protect the structural integrity of the aircraft at all times. Note that generally a “Fuel Quantity Check” must be made, using:

Remaining fuel + supply fuel = block fuel

2.5.2 Fuel Type

Designation Specification Usage Freezing Point °C

JET A1 ASTM D 1655 Normal Fuel -47 JET A ASTM D 1655 Alterante Fuel -40 (JP 5) (DERD 2498) Alternate Fuel -48 JET B (JP 4) ASTM D 1655 Should be used only in case none of the

a.m. fuel types are available. -60

The above fuels are approved by the engine manufacturer. They may be mixed in any proportion without affecting engine performance or operation.

2.5.3 Refueling Fuel Load Distribution 1. Load fuel equally in tanks 1, 2 and 3. 2. If the tanks 1 and 3 are full and additional fuel is required, continue to load center tank. Gage Reading The fuel indicating system shall be used as primary fuel quantity check for all tanks. Dripstick Reading The dripstick shall be used as secondary fuel quantity check. A dripstick reading is obtained by withdrawing the dripstick from the tank until a steady drip of fuel commences at the drain hole near the bas. When the dripstick is withdrawn from the tank, the drain hole should be directed downwind and away from personnel. Fuel Pressure Recommended maximum pressure is 50 psi. Overwing Fueling If pressure fueling facilities are not available overwing ports for tank 1 and 3 may be used. The tank 2 can be filled by transfering fuel from wing tanks.


2.14 727-200/JT8D-15 JUN 26, 2012

Fueling Order The Fueling Order & Monitoring Message shall be prepared in duplicate and shall be used for the order of the requested fuel quantity and to show the distribution of the fuel amongst the individual tanks. The original shall be carried on the aircraft the copy retained at the station of departure in the trip file.

Fueling Order Boeing 727-200 Requested Actual pounds pounds Tank 1 Center Tank 2 Block - Remaining = Supply Flight

Prepared:

Station Date

Approved:


JUN 26, 2012 727-200/JT8D-15 2.15

Responsibility of Fueling

Actions F/E GE Fuel Comp.

Preparation of Fueling Order and Sign-off at the space marked “Prepared”. X Disp./

F/E,GE

Determination of remaining fuel by cockpit gages and compare with the last flight-log-entry

X

Observe aircraft fueling X If required, determine exact remaining fuel by sticks X X

On request of flight crew check fuel density from fuel truck X

Open fueling station access door and remove fueling receptable caps

domestic X abroad X Connect ground wire and fuel hoses X Visual check ground wire/fuel hose connections X

Check for water contamination of fuel truck

first check X double check X X Open fuel valves domestic X abroad X Close fuel valves domestic X abroad X Check requested fuel by cockpit gages and enter in Fueling Order X X

If required, check requested fuel by sticks and enter in Fueling Order X X

If required, push in and lock sticks X Enter supplied fuel acc. to fuel truck gages in Fueling Order X

Disconnect fuel hoses and ground wire X Install fuel receptable caps and close fueling station access door

domestic X abroad X Add actual fuel gage indications (cockpit) and enter in the space marked “Block Actual”

X

Responsible for total fuel (cross-check “Actual/ Requested”), and completion of Fueling Order

X


2.16 727-200/JT8D-15 JUN 26, 2012

Fuel Distribution Table

Total Tank 1 Center Tank 3 Total Tank 1 Center Tank 3 Fuel Tank Fuel Tank Load 2 Load 2

3000 1000 1000 1000 27000 9000 9000 9000 3600 1200 1200 1200 27600 9200 9200 9200 4200 1400 1400 1400 28200 9400 9400 9400 4800 1600 1600 1600 28800 9600 9600 9600 5400 1800 1800 1800 29400 9800 9800 9800 6000 2000 2000 2000 30000 10000 10000 10000 6600 2200 2200 2200 30600 10200 10200 10200 7200 2400 2400 2400 31200 10400 10400 10400 7800 2600 2600 2600 31800 10600 10600 10600 8400 2800 2800 2800 32400 10800 10800 10800 9000 3000 3000 3000 33000 11000 11000 11000 9600 3200 3200 3200 33600 11200 11200 11200 10200 3400 3400 3400 34200 11400 11400 11400 10800 3600 3600 3600 34800 11400 12000 11400 11400 3800 3800 3800 35400 11400 12600 11400 12000 4000 4000 4000 36000 11400 13200 11400 12600 4200 4200 4200 36600 11400 13800 11400 13200 4400 4400 4400 37200 11400 14400 11400 13800 4600 4600 4600 37800 11400 15000 11400 14400 4800 4800 4800 38400 11400 15600 11400 15000 5000 5000 5000 39000 11400 16200 11400 15600 5200 5200 5200 39600 11400 16800 11400 16200 5400 5400 5400 40200 11400 17400 11400 16800 5600 5600 5600 40800 11400 18000 11400 17400 5800 5800 5800 41400 11400 18600 11400 18000 6000 6000 6000 42000 11400 19200 11400 18600 6200 6200 6200 42600 11400 19800 11400 19200 6400 6400 6400 43200 11400 20400 11400 19800 6600 6600 6600 43800 11400 21000 11400 20400 6800 6800 6800 44400 11400 21600 11400 21000 7000 7000 7000 45000 11400 22200 11400 21600 7200 7200 7200 45600 11400 22800 11400 22200 7400 7400 7400 46200 11400 23400 11400 22800 7600 7600 7600 46800 11400 24000 11400 23400 7800 7800 7800 47400 11400 24600 11400 24000 8000 8000 8000 48000 11400 25200 11400 24600 8200 8200 8200 48600 11400 25800 11400 25200 8400 8400 8400 49200 11400 26400 11400 25800 8600 8600 8600 49800 11400 27000 11400 26400 8800 8800 8800 50400 11400 27500 11400


JUN 26, 2012 727-200/JT8D-15 2.17

Drip Stick Table Tank 1 and 3 Inches pounds kilo US gal Liter Inches pounds kilo US gal Liter

2.6 872 396 128 494 12.6 4960 2250 730 2812 2.8 928 421 137 526 12.8 5080 2304 748 2880 3.0 976 443 144 553 13.0 5200 2359 765 2948 3.2 1032 468 152 585 13.2 5328 2417 784 3021 3.4 1096 497 161 621 13.4 5448 2471 802 3089 3.6 1144 519 168 649 13.6 5576 2529 821 3162 3.8 1208 548 178 685 13.8 5712 2591 841 3239 4.0 1264 573 186 717 14.0 5848 2653 861 3316 4.2 1320 599 194 748 14.2 5976 2711 880 3388 4.4 1376 624 203 780 14.4 6120 2776 901 3470 4.6 1440 653 212 816 14.6 6248 2834 920 3543 4.8 1496 679 220 848 14.8 6400 2903 942 3629 5.0 1552 704 228 880 15.0 6528 2961 961 3701 5.2 1616 733 238 916 15.2 6680 3030 983 3788 5.4 1672 758 246 948 15.4 6816 3092 1003 3865 5.6 1736 787 255 984 15.6 6950 3152 1023 3941 5.8 1800 816 265 1021 15.8 7104 3222 1046 4028 6.0 1864 846 274 1057 16.0 7248 3288 1067 4110 6.2 1936 878 285 1098 16.2 7400 3357 1089 4196 6.4 2000 907 294 1134 16.4 7544 3422 1110 4277 6.6 2064 936 304 1170 16.6 7688 3487 1131 4359 6.8 2128 965 313 1207 16.8 7840 3556 1154 4445 7.0 2208 1002 325 1252 17.0 8000 3629 1177 4536 7.2 2280 1034 336 1293 17.2 8160 3701 1201 4627 7.4 2352 1067 346 1334 17.4 8320 3774 1225 4717 7.6 2432 1103 358 1379 17.6 8480 3847 1248 4808 7.8 2520 1143 371 1429 17.8 8640 3919 1272 4899 8.0 2608 1183 384 1479 18.0 8808 3995 1296 4994 8.2 2696 1223 397 1529 18.2 8976 4071 1321 5089 8.4 2784 1263 410 1579 18.4 9144 4148 1346 5185 8.6 2880 1306 424 1633 18.6 9312 4224 1371 5280 8.8 2976 1350 438 1687 18.8 9480 4300 1395 5375 9.0 3064 1390 451 1737 19.0 9640 4373 1419 5466 9.2 2880 1306 424 1633 19.2 9808 4449 1444 5561 9.4 3256 1477 479 1846 19.4 9976 4525 1468 5656 9.6 3360 1524 495 1905 19.6 10144 4601 1493 5752 9.8 3448 1564 507 1955 19.8 10312 4677 1518 5847 10.0 3552 1611 523 2014 20.0 10472 4750 1541 5938 10.2 3648 1655 537 2068 20.2 10632 4823 1565 6028 10.4 3752 1702 552 2127 20.4 10792 4895 1588 6119 10.6 3848 1745 566 2182 20.6 10952 4968 1612 6210 10.8 3960 1796 583 2245 20.8 11112 5040 1635 6300 11.0 4064 1843 598 2304 21.0 11264 5109 1658 6387 11.2 4168 1891 613 2363 21.2 11408 5175 1679 6468 11.4 4280 1941 630 2427 21.4 11552 5240 1700 6550 11.6 4384 1989 645 2486 21.6 11680 5298 1719 6623 11.8 4496 2039 662 2549 21.8 11816 5360 1739 6700 12.0 4608 2090 678 2613 22.0 11952 5421 1759 6777 12.2 4728 2145 696 2681 12.4 4840 2195 712 2744


2.18 727-200/JT8D-15 JUN 26, 2012

Drip Stick Table (con’t) Tank 2 Inches pounds kilo US gal Liter Inches pounds kilo US gal Liter

2.6 720 327 106 408 12.6 8128 3687 1196 4609 2.8 824 374 121 467 12.8 8296 3763 1221 4704 3.0 936 425 138 531 13.0 8464 3839 1246 4799 3.2 1056 479 155 599 13.2 8624 3912 1269 4890 3.4 1176 533 173 667 13.4 8792 3988 1294 4985 3.6 1304 591 192 739 13.6 8960 4064 1319 5080 3.8 1432 650 211 812 13.8 9128 4140 1343 5176 4.0 1544 700 227 875 14.0 9296 4217 1368 5271 4.2 1696 769 250 962 14.2 9456 4289 1392 5362 4.4 1832 831 270 1039 14.4 9624 4365 1416 5457 4.6 1976 896 291 1120 14.6 9792 4442 1441 5552 4.8 2112 958 311 1197 14.8 9960 4518 1466 5647 5.0 2248 1020 331 1275 15.0 10128 4594 1491 5743 5.2 2392 1085 352 1356 15.2 10296 4670 1515 5838 5.4 2536 1150 373 1438 15.4 10464 4746 1540 5933 5.6 2680 1216 394 1520 15.6 10532 4777 1550 5972 5.8 2832 1285 417 1606 15.8 10792 4895 1588 6119 6.0 2976 1350 438 1687 16.0 10960 4971 1613 6214 6.2 3120 1415 459 1769 16.2 11128 5048 1638 6310 6.4 3264 1481 480 1851 16.4 11288 5120 1661 6400 6.6 3408 1546 502 1932 16.6 11468 5202 1688 6502 6.8 3560 1615 524 2019 16.8 11632 5276 1712 6595 7.0 3704 1680 545 2100 17.0 11792 5349 1736 6686 7.2 3848 1745 566 2182 17.2 11960 5425 1760 6781 7.4 4000 1814 589 2268 17.4 12128 5501 1785 6877 7.6 4152 1883 611 2354 17.6 12296 5577 1810 6972 7.8 4304 1952 633 2440 17.8 12456 5650 1833 7063 8.0 4456 2021 656 2527 18.0 12674 5749 1865 7186 8.2 4608 2090 678 2613 18.2 12792 5802 1883 7253 8.4 4768 2163 702 2703 18.4 12960 5879 1907 7348 8.6 4912 2228 723 2785 18.6 13128 5955 1932 7444 8.8 5064 2297 745 2871 18.8 13288 6027 1956 7534 9.0 5216 2366 768 2957 19.0 13456 6104 1980 7630 9.2 5368 2435 790 3044 19.2 13616 6176 2004 7720 9.4 5520 2504 812 3130 19.4 13784 6252 2029 7815 9.6 5672 2573 835 3216 19.6 13952 6329 2053 7911 9.8 5840 2649 860 3311 19.8 14120 6405 2078 8006 10.0 6000 2722 883 3402 20.0 14288 6481 2103 8101 10.2 6160 2794 907 3493 20.2 14448 6554 2126 8192 10.4 6320 2867 930 3583 20.4 14608 6626 2150 8283 10.6 6480 2939 954 3674 20.6 14776 6702 2175 8378 10.8 6632 3008 976 3760 20.8 14644 6642 2155 8303 11.0 6800 3084 1001 3856 21.0 15112 6855 2224 8568 11.2 6960 3157 1024 3946 21.2 15280 6931 2249 8664 11.4 7128 3233 1049 4042 21.4 15448 7007 2274 8759 11.6 7296 3309 1074 4137 21.6 15616 7083 2298 8854 11.8 7464 3386 1099 4232 21.8 15784 7160 2323 8949 12.0 7632 3462 1123 4327 22.0 15944 7232 2347 9040 12.2 7800 3538 1148 4423 22.2 16112 7308 2371 9135 12.4 7960 3611 1172 4513 22.4 16280 7385 2396 9231


JUN 26, 2012 727-200/JT8D-15 2.19

Drip Stick Table (con’t) Tank 2 Inches pounds kilo US gal Liter Inches pounds kilo US gal Liter

22.6 16448 7461 2421 9326 29.0 21472 9740 3160 12175 22.8 16680 7566 2455 9457 29.2 21600 9798 3179 12247 23.0 16768 7606 2468 9507 29.4 21728 9856 3198 12320 23.2 16936 7682 2493 9603 29.6 21856 9914 3217 12392 23.4 17104 7758 2517 9698 29.8 21984 9972 3236 12465 23.6 17272 7835 2542 9793 30.0 22104 10026 3253 12533 23.8 17440 7911 2567 9888 30.2 22216 10077 3270 12596 24.0 17603 7985 2591 9981 30.4 22328 10128 3286 12660 24.2 17776 8063 2616 10079 30.6 22440 10179 3303 12723 24.4 17936 8136 2640 10170 30.8 22541 10225 3317 12781 24.6 18104 8212 2664 10265 31.0 22648 10273 3333 12841 24.8 18272 8288 2689 10360 31.2 22760 10324 3350 12905 25.0 18440 8364 2714 10455 31.4 22864 10371 3365 12964 25.2 18608 8441 2739 10551 31.6 22968 10418 3380 13023 25.4 18768 8513 2762 10641 31.8 23072 10465 3396 13082 25.6 18928 8586 2786 10732 32.0 23168 10509 3410 13136 25.8 19089 8659 2809 10823 32.2 23272 10556 3425 13195 26.0 19249 8731 2833 10914 32.4 23360 10596 3438 13245 26.2 19500 8845 2870 11056 32.6 23456 10640 3452 13299 26.4 19557 8871 2878 11089 32.8 23544 10679 3465 13349 26.6 19720 8945 2902 11181 33.0 23632 10719 3478 13399 26.8 19872 9014 2925 11267 33.2 23720 10759 3491 13449 27.0 20024 9083 2947 11354 33.4 23800 10796 3503 13495 27.2 20176 9152 2969 11440 33.6 23880 10832 3515 13540 27.4 20328 9221 2992 11526 27.6 20480 9290 3014 11612 27.8 20632 9359 3037 11698 28.0 20776 9424 3058 11780 28.2 20928 9493 3080 11866 28.4 21068 9556 3101 11945 28.6 12203 5535 1796 6919 28.8 21330 9675 3139 12094


2.20 727-200/JT8D-15 JUN 26, 2012

2.6 FLIGHT PLANNING This chapter contains flight planning data to determine trip fuel/time, and reserve fuel. The data includes engine bleed effects for normal air conditioning operation.

2.6.1 Flight Planning Allowances Simplified Flight Planning charts enable rapid determination of estimated trip time and fuel from brake release to landing. Additional flight planning information including maneuver allowances is summarized below. Fuel can be saved by minimizing APU utilization. Average APU fuel flow rates under normal operation are 230 lbs per hour on the ground. Taxi fuel allowance is approximately 500 lbs.


JUN 26, 2012 727-200/JT8D-15 2.21

2.6.2 Optimum Altitude Optimum altitude for best fuel mileage is presented for .78M speed schedule.

25

27

29

31

33

35

37

39

41

100 110 120 130 140 150 160 170 180

Gross Weight - 1000 lbs

Alti

tude

- 10

00 fe

et


2.22 727-200/JT8D-15 JUN 26, 2012

2.6.3 Holding This table provides total fuel flow information necessary for planning holding and reserve fuel requirements. The table is based on a racetrack pattern in clean configuration and minimum drag airspeed.

Pressure Zero Fuel Weight - pounds x 1000 Altitude 140 130 120 110

ft Total Holding Fuel Flow- lbs/hr 9000 6784 6630 6508 6376 8000 6850 6702 6568 6442 7000 6920 6776 6634 6512 6000 6992 6852 6706 6586 5000 7068 6930 6786 6664 4000 7148 7010 6870 6746 3000 7230 7090 6960 6834 2000 7318 7174 7056 6924 1000 7406 7258 7158 7018

0 7500 7344 7266 7116

2.6.4 Flight Time and Fuel Table A Flight Time and Fuel Table is provided for .78M speed schedule at constant altitudes to determine trip time and trip fuel from brake release to touchdown. APU usage, taxi, inflight flaps down maneuvering (other than straight in approach) and reserve fuel should be added to the trip fuel obtained from the table to obtain the total fuel required. These fuel allowances are presented under Flight Planning Allowances. Additional fuel for extended inflight traffic delays should be determined from the holding table. Example: Segment Distance = 800 NM Flight Level = 330 Wind in FL 330 = 35 kts HW Landing Weight = 130,000 lbs Find: TAS in FL 330 = 454 kts Still Air Dist = 867 NAM Flight Fuel from table = 18,253 lbs, LW correction = 800 lbs. Flight Fuel = 19,053 lbs Flight Time = 2:00 hrs


JUN 26, 2012 727-200/JT8D-15 2.23

Flight Time & Fuel Table

STILL AIR FLIGHT LEVEL and TAS DISTANCE 90 110 130 150 170 190 210 230 250 270 290 310 330 350 370 390

(NAM) 285 407 419 431 444 456 470 474 470 466 462 458 454 450 447 447 100 0:24 0:20 0:22 0:24 0:27 0:29 0:30 0:33 0:36 0:38 0:41 0:44 0:50 0:56 0:54 0:52

4.37 4.24 4.60 5.09 5.58 5.85 6.34 6.95 7.43 7.93 8.43 9.16 10.24 10.90 9.65 9.08 200 0:45 0:35 0:34 0:33 0:33 0:32 0:32 0:33 0:36 0:38 0:41 0:44 0:50 0:56 0:54 0:52

6.59 6.78 6.70 7.24 6.63 6.50 6.60 6.95 7.43 7.93 8.43 9.16 10.24 10.90 9.65 9.08 300 1:06 0:49 0:48 0:47 0:46 0:46 0:45 0:44 0:45 0:45 0:45 0:45 0:50 0:56 0:54 0:52

8.83 9.43 9.25 10.41 8.96 8.75 8.76 8.83 8.81 8.87 8.98 9.24 10.24 10.90 9.65 9.08 400 1:27 1:04 1:03 1:01 1:00 0:59 0:57 0:57 0:57 0:58 0:58 0:58 0:59 0:59 0:59 0:59

11.07 12.09 11.80 13.60 11.30 11.00 10.93 10.93 10.77 10.69 10.67 10.82 11.18 11.22 10.20 9.74 500 1:48 1:19 1:17 1:15 1:13 1:12 1:10 1:10 1:10 1:11 1:11 1:11 1:12 1:12 1:12 1:12

13.32 14.76 14.36 16.81 13.65 13.26 13.10 13.03 12.73 12.52 12.37 12.41 12.67 12.63 11.58 11.09 600 2:09 1:34 1:31 1:29 1:27 1:25 1:23 1:22 1:23 1:23 1:24 1:24 1:25 1:25 1:26 1:26

15.59 17.45 16.94 20.03 16.01 15.53 15.29 15.15 14.71 14.37 14.09 14.02 14.18 14.06 12.97 12.46 700 2:30 1:48 1:46 1:43 1:40 1:38 1:36 1:35 1:36 1:36 1:37 1:37 1:38 1:39 1:39 1:39

17.87 20.14 19.52 23.27 18.38 17.81 17.49 17.27 16.70 16.23 15.81 15.64 15.70 15.51 14.39 13.84 800 2:51 2:03 2:00 1:57 1:54 1:51 1:48 1:48 1:48 1:49 1:50 1:51 1:51 1:52 1:53 1:53

20.16 22.85 22.11 26.52 20.76 20.10 19.69 19.41 18.70 18.10 17.55 17.27 17.23 16.98 15.82 15.24 900 3:12 2:18 2:14 2:11 2:07 2:04 2:01 2:00 2:01 2:02 2:03 2:04 2:05 2:05 2:06 2:06

22.47 25.57 24.72 29.80 23.15 22.39 21.91 21.55 20.72 19.98 19.30 18.92 18.78 18.46 17.26 16.66 1000 3:33 2:33 2:29 2:25 2:21 2:18 2:14 2:13 2:14 2:15 2:16 2:17 2:18 2:19 2:20 2:19

24.78 28.30 27.33 33.09 25.55 24.69 24.13 23.70 22.75 21.87 21.06 20.58 20.35 19.96 18.73 18.10 1100 3:54 2:47 2:43 2:39 2:34 2:31 2:27 2:26 2:27 2:28 2:29 2:30 2:31 2:32 2:33 2:33

27.11 31.05 29.95 36.39 27.96 27.01 26.37 25.87 24.78 23.78 22.83 22.26 21.94 21.49 20.21 19.56 1200 4:15 3:02 2:57 2:53 2:48 2:44 2:39 2:38 2:39 2:41 2:42 2:43 2:44 2:45 2:46 2:46

29.45 33.80 32.59 39.72 30.38 29.32 28.62 28.04 26.83 25.70 24.62 23.95 23.54 23.02 21.72 21.03 1300 4:36 3:17 3:12 3:07 3:01 2:57 2:52 2:51 2:52 2:54 2:55 2:56 2:58 2:59 3:00 3:00

31.80 36.57 35.23 43.06 32.81 31.65 30.87 30.23 28.90 27.63 26.42 25.65 25.15 24.58 23.24 22.52 1400 4:57 3:32 3:26 3:20 3:15 3:10 3:05 3:04 3:05 3:06 3:08 3:09 3:11 3:12 3:13 3:13

34.17 39.35 37.88 46.41 35.25 33.98 33.14 32.42 30.97 29.57 28.23 27.37 26.79 26.16 24.78 24.03 1500 5:18 3:46 3:40 3:34 3:28 3:23 3:18 3:16 3:18 3:19 3:21 3:22 3:24 3:25 3:27 3:27

36.54 42.14 40.55 49.79 37.69 36.33 35.42 34.62 33.06 31.52 30.05 29.10 28.43 27.75 26.33 25.56 1600 5:39 4:01 3:55 3:48 3:42 3:37 3:31 3:29 3:31 3:32 3:34 3:35 3:37 3:39 3:40 3:40

38.93 44.94 43.22 53.18 40.15 38.68 37.70 36.84 35.16 33.49 31.88 30.85 30.10 29.36 27.91 27.11 1700 6:00 4:16 4:09 4:02 3:56 3:50 3:43 3:42 3:43 3:45 3:47 3:48 3:50 3:52 3:54 3:53

41.33 47.76 45.90 56.59 42.62 41.04 40.00 39.06 37.27 35.47 33.73 32.61 31.78 30.99 29.50 28.67 1800 6:21 4:31 4:23 4:16 4:09 4:03 3:56 3:54 3:56 3:58 4:00 4:02 4:04 4:05 4:07 4:07

43.74 50.59 48.60 60.01 45.10 43.40 42.30 41.30 39.39 37.46 35.59 34.38 33.47 32.64 31.11 30.25 1900 6:43 4:45 4:38 4:30 4:23 4:16 4:09 4:07 4:09 4:11 4:13 4:15 4:17 4:19 4:20 4:20

46.16 53.43 51.30 63.46 47.59 45.78 44.62 43.54 41.52 39.46 37.46 36.17 35.19 34.30 32.74 31.85 2000 7:04 5:00 4:52 4:44 4:36 4:29 4:22 4:20 4:22 4:24 4:26 4:28 4:30 4:32 4:34 4:34

48.60 56.28 54.01 66.92 50.09 48.16 46.95 45.79 43.67 41.48 39.34 37.97 36.91 35.99 34.38 33.47

Based on: Landing Weight = 110,000 lbs If actual landing weight is above 110,000 lbs, ADD a fuel burn correction of 200 lbs for each 5,000 lbs increament of additional landing weight. CLIMB: 250 / 300 / M.78 Still Air Distance: CRUISE: 250 / 350 / M.78

DESCENT: 280 / M.78

Example: 600 1:25 - Flight Time from start of takeoff roll to landing (h:m) 14.06 - Flight Fuel from start of takeoff roll to landing (1000 lbs)

WTAS

TAS

VVVNMSAD


2.24 727-200/JT8D-15 JUN 26, 2012


Boeing 727-200 TAKEOFF Performance Manual

JUN 26, 2012 727-200/JT8D-15 3.1

CHAPTER 3 - TAKEOFF

3.1 GENERAL TAKEOFF PERFORMANCE .................................... 3 3.1.1 Introduction................................................ 3 3.1.2 Performance Limited Takeoff Weight ......................... 3 3.1.3 Altimeter Setting To Station Pressure ...................... 3 3.1.4 Wind Component.............................................. 3

3.2 PERFORMANCE LIMITED TAKEOFF WEIGHT DETERMINATION............... 6 3.2.1 Takeoff Field Corrections .................................. 7 3.2.2 Takeoff Field Limit ........................................ 7 3.2.3 Takeoff Climb Limit ........................................ 7 3.2.4 Tire Speed Limited Weight .................................. 7

3.3 SLUSH/STANDING WATER TAKEOFF .................................. 18 3.4 Takeoff Speeds ................................................ 19 3.5 Takeoff EPR and N1 ............................................ 21 3.6 Anti-Skid Inoperative ......................................... 22 3.7 Dispatch with Tailskid Extended ............................... 22 3.8 Stab Trim Setting ............................................. 22 3.9 RUNWAY WEIGHT CHARTS .......................................... 24

TAKEOFF Boeing 727-200 Performance Manual

3.2 727-200/JT8D-15 JUN 26, 2012



JUN 26, 2012 727-200/JT8D-15 3.3

3.1 GENERAL TAKEOFF PERFORMANCE

3.1.1 Introduction This chapter contains data to determine takeoff performance limitations, based on engine bleed effects for normal air conditioning operation and antiice off, i.e., two packs on, one pack bleed from each engine. The data is presented in simplified form and is therefore conservative. In the event of any conflict between data presented in this section and those contained in the Approved Airplane Flight Manual, the Airplane Flight Manual shall always take precedence.

3.1.2 Performance Limited Takeoff Weight The Performance Limited Takeoff Weight (PTOW) is the least of the field length, climb, and tire speed limit weights.

3.1.3 Altimeter Setting To Station Pressure The determination of thrust setting and takeoff/landing performance generally requires station pressure altitude. If station pressure or station pressure altitude are not available, enter the chart with altimeter setting (QNH) and read the pressure altitude adjustment. Apply this adjustment to the station elevation to obtain station pressure altitude. For boundary QNH values, read the midpoint between tabulated adjustments to elevation, e.g., for QNH of 29.66 inches (1004 mb), the elevation adjustment is 250 ft. Alternatively, station pressure altitude may be determined by setting the cockpit altimeter to 29.92 inches (1013.2 mb); the altimeter will then read station pressure altitude.

3.1.4 Wind Component The Wind Component chart provides crosswind and head/tail wind components, appropriate to the runway headings, reported wind velocity and direction. To use the chart, find the intersection between reported wind velocity in knots (circular lines) and the angle in degrees between reported wind direction and the runway (radial lines). Then read head/tail wind component to the left and crosswind component from the bottom scale.


3.4 727-200/JT8D-15 JUN 26, 2012

ALTIMETER SETTING TO STATION PRESSURE

QNH IN. HG. Correction to Elevation for

Pressure Altitude QNH MILLIBARS

28.81 to 28.91 1000 976 to 979

28.91 to 29.02 900 979 to 983

29.02 to 29.12 800 983 to 986

29.12 to 29.23 700 986 to 990

29.23 to 29.34 600 990 to 994

29.34 to 29.44 500 994 to 997

29.44 to 29.55 400 997 to 1001

29.55 to 29.66 300 1001 to 1004

29.66 to 29.76 200 1004 to 1008

29.76 to 29.87 100 1008 to 1012

29.87 to 29.97 0 1012 to 1015

29.97 to 30.08 -100 1015 to 1019

30.08 to 30.19 -200 1019 to 1022

30.19 to 30.30 -300 1022 to 1026

30.30 to 30.41 -400 1026 to 1030

30.41 to 30.52 -500 1030 to 1034

30.52 to 30.63 -600 1034 to 1037

30.63 to 30.74 -700 1037 to 1041

30.74 to 30.85 -800 1041 to 1045

30.85 to 30.96 -900 1045 to 1048

30.96 to 31.07 -1000 1048 to 1052

Example : Elevation = 1600 FT QNH = 29.48 IN.HG. Correction = 400 FT Pressure Altitude = 2000 FT


JUN 26, 2012 727-200/JT8D-15 3.5

WIND COMPONENT


3.6 727-200/JT8D-15 JUN 26, 2012

3.2 PERFORMANCE LIMITED TAKEOFF WEIGHT DETERMINATION

PERFORMANCE LIMITED TAKEOFF WEIGHT DETERMINATION PROCEDURE 1. With Wind, Slope, and Field Length Available enter Field Length

Correction Chart and obtain Corrected Field Length. 2. With QNH and Field Elevation enter Altimeter Setting to Station

Pressure Table and obtain Pressure Altitude. 3. With Corrected Field Length (step 1), OAT, and Pressure Altitude

(step 2) enter Takeoff Field Limit Chart and obtain Field Length Limited Takeoff Weight. Adjust for Bleed Configuration.

4. With OAT and Pressure Altitude (step 2) enter Takeoff Climb Limit Chart and obtain Climb Limited Takeoff Weight. Adjust for Bleed Configuration.

5. With OAT and Pressure Altitude (step 2) enter Tire Speed Limited Weight Chart and obtain Tire Speed Limited Weight. Adjust obtained weight for wind.

6. Compare the obtained limiting weights from steps 3, 4, and 5. Use the SMALLER one as the Performance Limited Takeoff Weight.

Atmospheric Conditions: - QNH - OAT - Wind

Runway Characteristics: - Field Length Available - Slope - Field Elevation


JUN 26, 2012 727-200/JT8D-15 3.7

3.2.1 Takeoff Field Corrections Enter the chart with field length available and correct for slope and wind.

3.2.2 Takeoff Field Limit Maximum field length limited brake release weights are presented for all certified takeoff flap settings. The field length available is the amount of paved surface which may be used to accelerate to the decision speed and either stop at the end of the runway or climb to 35 ft. The field limited weight does not account for clearway or stopway. The reference takeoff condition is flap position 15, zero slope, and zero wind. To determine the field length limit brake release weight, enter the chart with OAT, move horizontally to airport pressure altitude and project a line vertically down. Now enter the chart with the Field Length corrected for wind and slope and move horizontally until the vertically line from the airport pressure altitude is intersected. At the intersection of both lines read the Field Length Limited Weight. Adjust the field length limit weight according to the notes below the chart to account for the appropriate engine bleed configuration.

3.2.3 Takeoff Climb Limit Maximum climb limited brake release weights are presented for all certified takeoff flap settings. The weights are limited by second segment climb performance and do not account for obstacles. To determine the climb limit weight, enter the chart with OAT, move vertically to airport pressure altitude. Move horizontally and read the climb limit weight to the left. Adjust the climb limit weight according to the notes below the chart to account for the appropriate engine bleed configuration.

3.2.4 Tire Speed Limited Weight Maximum Tire Speed Limited Weights are presented for one certified takeoff flap setting. The weights are limited by tire speed limit and are based on zero slope and zero wind conditions. To determine the tire speed limit weight, enter the chart with OAT, move vertically to airport pressure altitude. Move horizontally and read the tire speed limit weight to the left. Adjust the tire speed limit weight according to the notes below the chart to account for wind and different tires.


3.8 727-200/JT8D-15 JUN 26, 2012

FIELD LENGTH CORRECTION

4000

6000

8000

10000

12000

14000

16000

18000

20000

22000

24000

26000

28000

30000

32000

34000

36000

38000

40000

42000

44000

46000

48000

0 2000 4000 6000 8000 10000 12000 14000 16000

Fiel

d Le

ngth

Ava

ilabl

e - f

eet

0

10000

20000

30000

40000

50000

60000

70000

80000

90000

100000

110000

120000

130000

140000

Cor

rect

ed F

ield

Len

gth

- fee

t

Runway Slope - %

+ 2 (Uphill)

0 - 2 (Downhill)

0Wind Component - knots

-10 (TW)

20 (HW)

40 (HW)

14000

13000

12000

11000

10000

9000

8000

7000

6000

5000

Example:Field Length Available = 6700 ft, Runway Slope = 1% downhill, and Wind Component = 0 kts. Find: Corrected Field Length = 7000 ft


JUN 26, 2012 727-200/JT8D-15 3.9

TAKEOFF FIELD LIMIT FLAPS 5

3000

4000

5000

6000

7000

8000

9000

10000

11000

12000

13000

14000

15000

16000

17000

18000

19000

20000

21000

22000

23000

24000

25000

26000

27000

28000

29000

30000

60 80 100 120 140 160 180

Cor

rect

ed F

ield

Len

gth

- fee

t

-50

-45

-40

-35

-30

-25

-20

-15

-10

-5

0

5

10

15

20

25

30

35

40

45

50

OAT

- °C

& below

2000 4000 6000 80000

Pressure Altitude - feet

BASED ON:- Anti-skid operative- A/C bleed ON- Autopack Trip Operative- Engine Failure Warning System Operative

CORRECTIONS:For Anti-Ice System ON reduce weight 1000 lb

130

140

150

160

170

180

190195

Gro

ss W

eigh

t - 1

000

LBSL

BS

FLAPS 5


3.10 727-200/JT8D-15 JUN 26, 2012


3000

4000

5000

6000

7000

8000

9000

10000

11000

12000

13000

14000

15000

16000

17000

18000

19000

20000

21000

22000

23000

24000

25000

26000

27000

28000

29000

30000

-50

-45

-40

-35

-30

-25

-20

-15

-10

-5

0

5

10

15

20

25

30

35

40

45

50

Cor

rect

ed F

ield

Len

gth

- fee

t

2000 4000 6000 8000Pressure Altitude - feet 0

Gro

ss W

eigh

t - 1

000

LBSL

BS

130

140

150

160

170

180

190195

OAT

- °C

FLAPS 15

Example: For 25°C OAT, 2000 ft pressure altitude and 7000 ft Corrected Field Length, the Runway Limited Takeoff Weight is 160,000 lb.



&below


JUN 26, 2012 727-200/JT8D-15 3.11


3000

4000

5000

6000

7000

8000

9000

10000

11000

12000

13000

14000

15000

16000

17000

18000

19000

20000

21000

22000

23000

24000

25000

26000

27000

28000

29000

30000

40 50 60 70 80 90 100 110 120 130 140

Cor

rect

ed F

ield

Len

gth

- 100

0 FT

-50

-45

-40

-35

-30

-25

-20

-15

-10

-5

0

5

10

15

20

25

30

35

40

45

50

OAT

- °C

& below

2000 4000 6000 80000




FLAPS 20130

140

150

160

170

180

190

195

Gro

ss W

eigh

t - 1

000

LBSL

BS


3.12 727-200/JT8D-15 JUN 26, 2012


3000

4000

5000

6000

7000

8000

9000

10000

11000

12000

13000

14000

15000

16000

17000

18000

19000

20000

21000

22000

23000

24000

25000

26000

27000

28000

29000

30000

40 50 60 70 80 90 100 110 120 130 140

Cor

rect

ed F

ield

Len

gth

- 100

0 FT

-50

-45

-40

-35

-30

-25

-20

-15

-10

-5

0

5

10

15

20

25

30

35

40

45

50

OAT

- °C

& below

2000 4000 6000 80000




FLAPS 25130

140

150

160

170

180190

195

Gro

ss W

eigh

t - 1

000

LBS

LBS


JUN 26, 2012 727-200/JT8D-15 3.13

TAKEOFF CLIMB LIMIT FLAPS 5

130

135

140

145

150

155

160

165

170

175

180

185

190

195

200

10 15 20 25 30 35 40 45 50

OAT - °C

Gro

ss W

eigh

t - 1

000

LBS

FLAPS 52nd Segment Weight Limitation


0

1000

2000

3000

4000

5000

6000

7000

8000BASED ON:- A/C bleed ON- Autopack Trip Operative- Engine Failure Warning System Operative


& below


3.14 727-200/JT8D-15 JUN 26, 2012


130

135

140

145

150

155

160

165

170

175

180

185

190

195

200

10 15 20 25 30 35 40 45 50


Gro

ss W

eigh

t - 1

000

LBS

OAT - °C

Pressure Altitude - feet 0

100020003000

4000

5000

6000

7000

8000

Example: For 25°C OAT and 2000 feet pressure altitude, the 2nd Segment Limited Weight is 196,800 lb.

BASED ON:- A/C bleed ON- Autopack Trip Operative- Engine Failure Warning System Operative


& below


JUN 26, 2012 727-200/JT8D-15 3.15


130

135

140

145

150

155

160

165

170

175

180

185

190

195

200

10 15 20 25 30 35 40 45 50

OAT - °C

Gro

ss W

eigh

t - 1

000

LB



0

1000

2000

3000

4000

5000

6000

7000

8000



& below


3.16 727-200/JT8D-15 JUN 26, 2012


120

130

140

150

160

170

180

190

200

10 15 20 25 30 35 40 45 50

OAT - °C

Gro

ss W

eigh

t - 1

000

LBS



0

1000

2000

3000

4000

5000

6000

7000

8000



& below


JUN 26, 2012 727-200/JT8D-15 3.17

TIRE SPEED LIMITED WEIGHT

150

160

170

180

190

200

210

220

230

240

250

10 15 20 25 30 35 40 45 50OAT - °C

Tire

Spe

ed L

imite

d W

eigh

t - 1

000

LB

& below

FLAPS 15Tire Speed Weight Limitation

210 MPH TIRES

BASED ON:- Zero Wind- 210 MPH Tires

CORRECTIONS:-2000 lb/1kt TW+1500 lb/kt HW for 200 MPH Tires: -20000 lbfor 225 MPH Tires: +20000 lbfor Flaps 5: -18960 lb

Flap Positions 20 and 25 are NEVER Tire Speed Limited


0

1000

2000

3000

4000

5000

6000

7000

8000

Example: For 25°C OAT, zero wind and 2000 feet pressure altitude, the Tire Speed Limited Weight is 222,000 lb.


3.18 727-200/JT8D-15 JUN 26, 2012

3.3 SLUSH/STANDING WATER TAKEOFF Experience has shown that aircraft performance may deteriorate significantly on runways covered with snow, slush, standing water, or ice. Therefore a reduction in dry field length/obstacle limited takeoff weight and revised takeoff speeds is necessary. The information provided is intended for guidance in accordance with advisory material. The performance is based on an engine failure at the critical point during takeoff and a 15 ft. screen height at the end of the runway. Tables are provided for dispatch with all three thrust reversers operative. The entire runway is assumed to be completely covered by a contaminant of uniform thickness and density. Therefore this information is conservative when operating under typical colder weather conditions where patches of slush exist and some degree of sanding is common. Takeoffs in slush depths greater than 13mm (0.5 inches) are not recommended because of possible airplane damage as a result of slush impingement on the airplane structure. Maximum depths for slush, snow and standing water covering an appreciable part of the runway are as follows: Takeoff Landing Slush or wet snow 0.5 inch (12 mm) 1 inch (25 mm) Standing water 0.25 inch (6 mm) 1 inch (25 mm) Dry snow 3.5 inch (90 mm) 3.5 inch (90 mm) The use of assumed temperature method for reduced thrust is not allowed on contaminated runways. Interpolation for slush/standing water depths between the values shown is permitted. Instructions for Using Tables: Determine the field limit weight for the takeoff flap setting. Enter the Weight Adjustment table with the pressure altitude and the corrected runway length to obtain the weight reduction for the slush/standing water depth. Reduce the field limit weight by the reduction shown. Takeoff speeds determination: Determine takeoff speeds V1, VR and V2 for actual brake release weight using the Takeoff Speeds table in this section. Enter the Weight Adjustment table with the pressure altitude and the corrected runway length to obtain the speed reduction for the slush/standing water depth. Reduce the V1 by the reduction shown.


JUN 26, 2012 727-200/JT8D-15 3.19

SLUSH/STANDING WATER TAKEOFF

1/4 Inch Slush Corrections

Weight Reduction - pounds V1 Reduction - KTS Flaps 5 Flaps 15 Flaps 20,25 Flaps 5,15 Flaps 20,25

Runway Length

FT S.L. 4000 S.L. 4000 S.L. 4000 S.L. 4000 S.L. 4000 5000 12000 12000 15000 14000 16000 15000 33 33 32 31 7000 15000 13000 17000 16000 19000 18000 30 29 29 28 9000 17000 15000 20000 18000 21000 20000 29 27 27 27 11000 18000 16000 22000 20000 24000 22000 28 27 26 26 13000 20000 18000 24000 22000 - - 26 25 - -

1/2 Inch Slush Corrections Weight Reduction - pounds V1 Reduction - KTS

Flaps 5 Flaps 15 Flaps 20,25 Flaps 5,15 Flaps 20,25 Runway Length

FT S.L. 4000 S.L. 4000 S.L. 4000 S.L. 4000 S.L. 4000 5000 20000 20000 22000 21000 24000 22000 29 27 27 26 7000 22000 22000 26000 24000 28000 26000 26 25 25 25 9000 25000 23000 28000 26000 30000 28000 26 25 25 24 11000 27000 25000 30000 28000 32000 30000 26 25 25 24 13000 29000 27000 32000 30000 - - 26 26 - -

3.4 TAKEOFF SPEEDS The speeds presented in the Takeoff Speeds table can be used for all performance conditions except where adjustments must be made to V1 for clearway, stopway, brake deactivation, improved climb, contaminated runway situations, unbalanced for brake energy or obstacle clearance with unbalanced V1. These speeds may be used for weights less than or equal to the performance limited weight. Normal takeoff speeds, V1, VR, and V2, with anti-skid on, are read from the table by entering with takeoff flap setting, brake release weight, and appropriate column.


3.20 727-200/JT8D-15 JUN 26, 2012

Press

Alt 1000 ft

OAT

°F -65 to -14 -13 to 33 34 to 86 9 to 10

°C -54 to -26 -25 to 0 1 to 30 °F - 65 to -36 -35 to 112 13 to 75 76 to 100

7 to 9 °C -54 to -38 -37 to -11 -10 to 24 25 to 38 °F 65 to 2 3 to 40 41 to 96 97 to 109

5 to 7 °C -54 to -17 -16 to 4 5 to 35 36 to 42 °F -65 to 32 33 to 88 89 to 112

3 to 5 °C -54 to 0 1 to 31 32 to 44 °F -65 to 84 85 to 104 105 to 120

1 to 3 °C -54 to 29 30 to 40 41 to 49 °F -65 to 100 101 to 120

-1 to 1 °C -54 to 38 39 to 49

WEIGHT FLAPS

lb V1 = VR V2 V1 = VR V2 V1 = VR V2 V1 = VR V2

210000 165 175 167 175 200000 159 170 161 170 190000 154 166 156 166 158 166 180000 148 161 150 161 152 161 5 170000 142 157 144 157 146 156 148 156 160000 137 151 138 151 140 156 142 150 150000 131 146 132 146 133 145 136 144 140000 128 143 129 143 129 142 131 142 130000 125 141 126 141 127 140 129 140 120000 119 136 120 135 121 134 122 133 210000 155 166 157 166 200000 150 161 152 161 190000 145 157 147 157 149 157 180000 139 152 141 152 143 152

15 170000 134 148 136 148 138 147 140 147 160000 129 143 130 143 132 143 134 142 150000 123 138 124 138 126 137 128 137 140000 121 137 122 136 123 135 125 134 130000 118 134 119 133 120 132 122 132 120000 112 128 113 128 114 127 115 126 210000 150 161 152 161 200000 145 157 147 157 190000 140 152 142 152 144 152 180000 135 148 137 148 139 148

20 170000 130 144 131 144 133 143 135 143 160000 125 139 126 139 128 138 130 138 150000 119 134 120 134 122 133 124 133 140000 116 131 117 131 118 130 120 130 130000 114 129 115 129 116 128 118 128 120000 109 124 109 124 110 123 111 122 210000 143 155 146 155 200000 141 152 143 152 190000 136 148 138 148 139 148 180000 130 144 132 144 134 144

25 170000 125 139 127 139 129 139 131 139 160000 120 135 122 135 124 134 125 134 150000 115 130 116 130 118 130 120 129 140000 112 128 113 127 114 127 116 127 130000 110 126 111 125 112 125 114 125 120000 105 121 106 120 106 120 107 119

SPEEDS NOT VALID WHEN WEIGHTS ARE PREDICATED ON USE OF CLEARWAY, STOWAY, IMPROVED CLIMB OR ARE LIMITED BY BRAKE ENERGY.


JUN 26, 2012 727-200/JT8D-15 3.21

3.5 TAKEOFF EPR AND N1

TAKEOFF EPR PRESS OAT

°F -4 5 14 23 32 41 50 59 68 77 86 95 104 113 120

ALT °C -20 -15 -10 -5 0 5 10 15 20 25 30 35 40 45 49

-1000 1 & 3 2.04 2.04 2.04 2.04 2.04 2.04 2.04 2.04 2.04 2.04 2.04 2.04 2.03 1.99 1.94 1.91

2 2.06 2.06 2.06 2.06 2.06 2.06 2.06 2.06 2.06 2.06 2.06 2.06 2.05 2.00 1.96 1.92

S.L. 1 & 3 2.10 2.10 2.10 2.10 2.10 2.10 2.10 2.10 2.10 2.10 2.10 2.08 2.03 1.99 1.94 1.91

2 2.11 2.11 2.11 2.11 2.11 2.11 2.11 2.11 2.11 2.11 2.11 2.10 2.05 2.00 1.96 1.92

1000 1 & 3 2.15 2.15 2.15 2.15 2.15 2.15 2.15 2.13 2.12 2.12 2.11 2.08 2.03 1.99 1.94 1.91

2 2.16 2.16 2.16 2.16 2.16 2.16 2.16 2.15 2.13 2.13 2.12 2.10 2.05 2.00 1.96 1.92

2000 1 & 3 2.21 2.21 2.21 2.21 2.21 2.20 2.17 2.14 2.14 2.14 2.11 2.08 2.03 1.99 1.94 1.91

2 2.22 2.22 2.22 2.22 2.22 2.21 2.18 2.16 2.16 2.15 2.12 2.10 2.05 2.00 1.96 1.92

3000 1 & 3 2.26 2.26 2.26 2.25 2.23 2.20 2.17 2.14 2.14 2.14 2.11 2.08 2.03 1.99 1.94 1.91

2 2.28 2.28 2.28 2.27 2.24 2.21 2.18 2.16 2.16 2.15 2.12 2.10 2.05 2.00 1.96 1.92

3856 & 1 & 3 2.31 2.29 2.27 2.25 2.23 2.20 2.17 2.14 2.14 2.14 2.11 2.08 2.03 1.99 1.94 1.91

ABOVE 2 2.32 2.31 2.29 2.27 2.24 2.21 2.18 2.16 2.16 2.15 2.12 2.10 2.05 2.00 1.96 1.92

EPR BLEED CORRECTIONS ENG 1 & 3 ENG 2

AIR CONDITIONING OFF +.04 -

ENGINE A/I ON ZERO -0.3

IN SHADED AREA COLDER

THAN 0°F (-18°C) -0.3 -0.6

MOD 'A' INLET - 0.1

TAKEOFF N1

PRESS OAT - °C

ALT -40 -35 -29 -23 -18 -12 -7 -1 4 10 16 18 21 24 27 29 32 35 38 41 43 49

-1000 82.2 83.2 84.2 85.1 86.1 87.0 87.9 88.8 89.7 90.6 91.5 92.0 92.4 92.8 93.2 93.7 94.1 94.2 93.7 93.3 92.9 92.0

S.L. 83.5 84.5 85.5 86.5 87.4 88.3 89.3 90.2 91.1 92.0 93.0 93.4 93.9 94.3 94.7 95.0 94.6 94.2 93.7 93.3 92.9 92.0

1000 85.4 86.4 87.3 88.3 89.2 90.2 91.1 92.0 92.9 93.3 93.0 93.4 93.9 94.3 94.7 95.0 94.6 94.2 93.7 93.3 92.9 92.0

2000 68.8 87.8 88.9 89.9 90.9 91.9 92.8 93.8 93.6 93.3 93.0 93.4 93.9 94.3 94.7 95.0 94.6 94.2 93.7 93.3 92.9 92.0

3000 88.4 89.5 90.5 91.5 92.5 93.5 94.0 93.8 93.6 93.3 93.0 93.4 93.9 94.3 94.7 95.0 94.6 94.2 93.7 93.3 92.9 92.0

4000 90.1 91.2 92.3 93.3 94.0 94.0 94.0 93.8 93.6 93.3 93.0 93.4 93.9 94.3 94.7 95.0 94.6 94.2 93.7 93.3 92.9 92.0

5000 92.0 93.1 93.7 93.9 94.0 94.0 94.0 93.8 93.6 93.3 93.0 93.4 93.9 94.3 94.7 95.0 94.6 94.2 93.7 93.3 92.9 92.0

5660 93.2 93.5 93.7 93.9 94.0 94.0 94.0 93.8 93.6 93.3 93.0 93.4 93.9 94.3 94.7 95.0 94.6 94.2 93.7 93.3 92.9 92.0

ADJUSTMENTS:

ENGINE ANTI-ICE ON -No. 1&3 + 0.7% - No. 2 + 0.2%


3.22 727-200/JT8D-15 JUN 26, 2012

3.6 ANTI-SKID INOPERATIVE For antiskid inoperative, the runway limited maximum takeoff weight at breake release and the V1 speed must be reduced to allow for the effect on accelerate stop performance as detailed in the FAA Approved Airplane Flight Manual. Enter the table with flap setting and read weight reduction. Enter table with flap setting and runway length and read speed reduction.

Flap Setting Weight Reduction – pounds 5° 4000

15° 6300 20° 8500 25° 10000

Flap Setting Runway Length - FT V1 Reduction – KTS

10000 13 5° 12000 14 6000 21 7000 18 8000 17 9000 16

15°

10000 15 7000 18 8000 16 9000 16 20°

10000 15 6000 21 7000 18 25° 8000 16

3.7 DISPATCH WITH TAILSKID EXTENDED In order to compensate for the increased drag resulting from an extended tail skid, the following adjustments are recommended. Increase climb time, fuel and distance to cruise altitude by 25 percent. Increase cruise fuel flows by 10 Percent (range reduction 10 percent). Reduce thrust limited cruise weights by 20,000 lb.

3.8 STAB TRIM SETTING To find takeoff stabilizer trim setting, enter the Stab Trim Setting table with flap setting and center of gravity (C.G. % MAC) and read required stabilizer trim units.


JUN 26, 2012 727-200/JT8D-15 3.23

STABILZER TRIM SETTING

FLAPS

5 15 / 20 25 CG % UNITS AIRPLANE NOSE UP

10 6 3/4 7 1/2 8 1/4 12 6 1/2 7 1/4 8 14 6 1/4 7 7 3/4 16 6 6 3/4 7 1/2 18 5 3/4 6 1/2 7 20 5 1/2 6 6 1/2 22 5 5 3/4 6 1/4 24 4 3/4 5 1/4 5 3/4 26 4 1/2 4 3/4 5 1/4 28 4 4 1/2 4 3/4 30 3 3/4 4 4 1/4 32 3 1/2 3 3/4 4 34 3 1/4 3 1/4 3 1/2 36 2 3/4 3 3 38 2 1/2 2 1/2 2 1/2 40 2 1/2 2 1/2 2 1/2 42 2 1/2 2 1/2 2 1/2


3.24 727-200/JT8D-15 JUN 26, 2012

3.9 RUNWAY WEIGHT CHARTS The Maximum-Takeoff-Weight limitation for the particular combination of airport, flap setting, temperature, runway and winds, is the LESSER of the weights determined in Steps A and B below. The Climb Limit (Step A) and the Runway Limit (Step B) are calculated separately because they are two different distinctly limitations (but neither one may be exceeded). If the runway selected does not permit sufficient take-off weight, consider the possibility of using a different runway. This will involve repeating Step B for the new choice of runway (including revision of wind component if the runway direction is different).

A. Second Segement Limit Weight – The 2nd Segment Limit Weight is the maximum allowable take-off weight for the altitude (of the airport) and the temperature (at the time of takeoff). Determine the 2nd Segement Limit Weight by entering the airport chart with the Outside Air Temperature (OAT in degrees Celsius). Follow the line to its intersection with the column labeled 2nd Segment and read the 2nd Segment Limit Weight.

NOTE: The 2nd Segment Limit Weight is independand of the runway length and the actual takeoff weight MUST NEVER EXCEED this limitation or the Structural Maximum Takeoff Wieght no matter how long a runway is.

B. Runway Limit – The next weight to be determined is the maximum

takeoff weight for the particular runway to be used; including limitations due to obstacles beyond the runway, whell brake energy limitations, tire speed limitations, etc. Again, enter the airport chart with the OAT. Proceed along the temperature line to its intersection with the column identified by the number of the runway to be used. Read the ZERO WIND runway limited weight. This weight must now be corrected for winds (if any) as follows:

Determine the wind component parallel to the runway (from the reported wind by using the “Wind Component” chart in this section).


JUN 26, 2012 727-200/JT8D-15 3.25

(1) For a Headwind (a) MULTIPLY the headwind component by the HEAD ADD shown on the chart. This product is the headwind correction. (b) ADD the headwind correction to the (zero wind) runway limited weight obtained above. The result is the RUNWAY LIMITED WEIGHT. (2) For a Tailwind (a) MULTIPLY the tail wind component by the TAIL SUB shown on the chart. This product is the tailwind correction. (b) SUBTRACT the tailwind correction from the (zero wind) runway limited weight obtained above. The result is the RUNWAY LIMITED WEIGHT.


3.26 727-200/JT8D-15 JUN 26, 2012



JUN 26, 2012 727-200/JT8D-15 3.27

15° FLAPS ALBUQUERQUE INTL, NEW MEX

ELEVATION 5355 OAT ZERO WIND RUNWAY LIMIT (1000 LBS) 2nd OAT OAT °C SEGMENT °C °F 03 21 08 26 12 30 LIMIT

40 162.8F 163.8F 181.4F 183.0F 124.6F 124.6F 158.2 40 104

38 164.3F 165.2F 182.9F 184.4F 125.8F 125.8F 160.5 38 100

36 165.7F 166.6F 184.3F 185.9F 127.1F 127.1F 162.9 36 97

34 167.1F 168.1F 185.7F 187.3F 128.3F 128.3F 172.6 34 93

32 168.6F 169.5F 187.2F 188.7F 129.6F 129.6F 172.6 32 90

30 170.0F 170.9F 188.6F 190.1F 130.8F 130.8F 172.6 30 86

28 171.4F 172.4F 190.0F 191.5F 132.0F 132.0F 172.6 28 82

26 172.9F 173.8F 191.5F 193.0F 133.3F 133.3F 172.6 26 79

24 174.3F 175.2F 192.9F 194.4F 134.5F 134.5F 172.6 24 75

22 175.7F 176.7F 194.3F 195.8F 135.8F 135.8F 172.6 22 72

20 177.2F 178.1F 195.8F 197.2F 137.0F 137.0F 172.6 20 68

18 178.6F 179.6F 197.2F 198.6F 138.2F 138.2F 172.6 18 64

16 180.0F 181.0F 198.6F 200.1F 139.5F 139.5F 172.6 16 61

14 181.5F 182.4F 200.1F 201.5F 140.7F 140.7F 172.6 14 57

12 182.9F 183.9F 201.5F 202.9F 142.0F 142.0F 172.6 12 54

10 184.3F 185.3F 203.0F 204.3F 143.2F 143.2F 172.6 10 50

8 185.8F 186.7F 204.4F 205.8F 144.5F 144.5F 172.6 8 46

6 187.2F 188.2F 205.8F 207.2F 145.7F 145.7F 172.6 6 43

4 188.6F 189.6F 207.3F 208.6F 146.9F 146.9F 172.6 4 39

2 190.1F 191.0F 208.7F 210.0F 148.2F 148.2F 172.6 2 36

0 191.5F 192.5F 210.1F 211.4F 149.4F 149.4F 172.6 0 32

-2 192.9F 193.9F 211.6F 212.4T 150.7F 150.7F 172.6 -2 28

-4 194.4F 195.3F 213.0F 213.3T 151.9F 151.9F 172.6 -4 25

-6 195.8F 196.8F 214.3T 214.3T 153.2F 153.2F 172.6 -6 21

-8 197.2F 198.2F 215.2T 215.2T 154.4F 154.4F 172.6 -8 18

-10 198.6F 199.6F 216.1T 216.1T 155.6F 155.6F 172.6 -10 14

-12 200.1F 201.1F 217.0T 217.0T 156.9F 156.9F 172.6 -12 10

-14 201.5F 202.5F 218.0T 218.0T 158.1F 158.1F 172.6 -14 7

-16 202.9F 203.9F 218.9T 218.9T 159.4F 159.4F 172.6 -16 3

-18 204.4F 205.4F 219.8T 219.8T 160.6F 160.6F 172.6 -18 0

-20 205.8F 206.8F 220.8T 220.8T 161.9F 161.9F 172.6 -20 -4

-22 207.2F 208.3F 221.7T 221.7T 163.1F 163.1F 172.6 -22 -8

-24 208.7F 209.7F 222.6T 222.6T 164.3F 164.3F 172.6 -24 -11

-26 210.1F 211.1F 223.5T 223.5T 165.6F 165.6F 172.6 -26 -15

-28 211.5F 212.6F 224.5T 224.5T 166.8F 166.8F 172.6 -28 -18

-30 213.0F 214.0F 225.4T 225.4T 168.1F 168.1F 172.6 -30 -22

-32 214.4F 215.4F 226.3T 226.3T 169.3F 169.3F 172.6 -32 -26

-34 215.8F 216.9F 227.2T 227.2T 170.6F 170.6F 172.6 -34 -29

-36 217.3F 218.3F 228.2T 228.2T 171.8F 171.8F 172.6 -36 -33

-38 218.7F 219.7F 229.1T 229.1T 173.0F 173.0F 172.6 -38 -36

-40 220.1F 221.2F 230.0T 230.0T 174.3F 174.3F 172.6 -40 -40

LENGTH (FT) 10000 10000 13793 13793 6000 6000 LIMITATIONS SLOPE (%) +0.10 -0.10 +0.30 -0.30 0.00 0.00 RUNWAY LENGTH F LIMITATION OBSTACLE * HEAD ADD 285 280 165 115 70 70 BRAKE ENERGY BE TAIL SUB 990 1000 830 990 1000 1000 TIRE SPEED T


3.28 727-200/JT8D-15 JUN 26, 2012

15° FLAPS ALBUQUERQUE INTL, NEW MEX

ELEVATION 5355 OAT ZERO WIND RUNWAY LIMIT (1000 LBS) 2nd OAT OAT °C SEGMENT °C °F 17 35 LIMIT

40 163.3F 163.3F 158.2 40 104

38 164.8F 164.8F 160.5 38 100

36 166.2F 166.2F 162.9 36 97

34 167.6F 167.6F 172.6 34 93

32 169.1F 169.1F 172.6 32 90

30 170.5F 170.5F 172.6 30 86

28 171.9F 171.9F 172.6 28 82

26 173.4F 173.4F 172.6 26 79

24 174.8F 174.8F 172.6 24 75

22 176.2F 176.2F 172.6 22 72

20 177.7F 177.7F 172.6 20 68

18 179.1F 179.1F 172.6 18 64

16 180.5F 180.5F 172.6 16 61

14 182.0F 182.0F 172.6 14 57

12 183.4F 183.4F 172.6 12 54

10 184.8F 184.8F 172.6 10 50

8 186.3F 186.3F 172.6 8 46

6 187.7F 187.7F 172.6 6 43

4 189.1F 189.1F 172.6 4 39

2 190.6F 190.6F 172.6 2 36

0 192.0F 192.0F 172.6 0 32

-2 193.5F 193.5F 172.6 -2 28

-4 194.9F 194.9F 172.6 -4 25

-6 196.3F 196.3F 172.6 -6 21

-8 197.8F 197.8F 172.6 -8 18

-10 199.2F 199.2F 172.6 -10 14

-12 200.6F 200.6F 172.6 -12 10

-14 202.1F 202.1F 172.6 -14 7

-16 203.5F 203.5F 172.6 -16 3

-18 204.9F 204.9F 172.6 -18 0

-20 206.4F 206.4F 172.6 -20 -4

-22 207.8F 207.8F 172.6 -22 -8

-24 209.2F 209.2F 172.6 -24 -11

-26 210.7F 210.7F 172.6 -26 -15

-28 212.1F 212.1F 172.6 -28 -18

-30 213.5F 213.5F 172.6 -30 -22

-32 215.0F 215.0F 172.6 -32 -26

-34 216.4F 216.4F 172.6 -34 -29

-36 217.8F 217.8F 172.6 -36 -33

-38 219.3F 219.3F 172.6 -38 -36

-40 220.7F 220.7F 172.6 -40 -40

LENGTH (FT) 10000 10000 LIMITATIONS SLOPE (%) 0.00 0.00 RUNWAY LENGTH F LIMITATION OBSTACLE * HEAD ADD 285 285 BRAKE ENERGY BE TAIL SUB 990 990 TIRE SPEED T


JUN 26, 2012 727-200/JT8D-15 3.29

15° FLAPS BELLINGHAM INTL, WASH


40 163.2F 164.1F 190.0 40 104

38 163.9F 164.8F 192.5 38 100

36 164.6F 165.5F 195.1 36 97

34 165.4F 166.3F 196.2 34 93

32 166.1F 167.0F 196.2 32 90

30 166.8F 167.7F 196.2 30 86

28 167.5F 168.4F 196.2 28 82

26 168.3F 169.2F 196.2 26 79

24 169.0F 169.9F 196.2 24 75

22 169.7F 170.6F 196.2 22 72

20 170.4F 171.4F 196.2 20 68

18 171.2F 172.1F 196.2 18 64

16 171.9F 172.8F 196.2 16 61

14 172.6F 173.5F 196.2 14 57

12 173.3F 174.3F 196.2 12 54

10 174.1F 175.0F 196.2 10 50

8 174.8F 175.7F 196.2 8 46

6 175.5F 176.4F 196.2 6 43

4 176.2F 177.2F 196.2 4 39

2 177.0F 177.9F 196.2 2 36

0 177.7F 178.6F 196.2 0 32

-2 178.4F 179.4F 196.2 -2 28

-4 179.1F 180.1F 196.2 -4 25

-6 179.9F 180.8F 196.2 -6 21

-8 180.6F 181.5F 196.2 -8 18

-10 181.3F 182.3F 196.2 -10 14

-12 182.0F 183.0F 196.2 -12 10

-14 182.8F 183.7F 196.2 -14 7

-16 183.5F 184.4F 196.2 -16 3

-18 184.2F 185.2F 196.2 -18 0

-20 184.9F 185.9F 196.2 -20 -4

-22 185.7F 186.6F 196.2 -22 -8

-24 186.4F 187.3F 196.2 -24 -11

-26 187.1F 188.1F 196.2 -26 -15

-28 187.8F 188.8F 196.2 -28 -18

-30 188.6F 189.5F 196.2 -30 -22

-32 189.3F 190.3F 196.2 -32 -26

-34 190.0F 191.0F 196.2 -34 -29

-36 190.7F 191.7F 196.2 -36 -33

-38 191.5F 192.4F 196.2 -38 -36

-40 192.2F 193.2F 196.2 -40 -40

LENGTH (FT) 6701 6701 LIMITATIONS SLOPE (%) +0.10 -0.10 RUNWAY LENGTH F LIMITATION OBSTACLE * HEAD ADD 150 160 BRAKE ENERGY BE TAIL SUB 1170 1180 TIRE SPEED T


3.30 727-200/JT8D-15 JUN 26, 2012



JUN 26, 2012 727-200/JT8D-15 3.31

15° FLAPS BEND REDMONT, OREG

ELEVATION 3077 OAT ZERO WIND RUNWAY LIMIT (1000 LBS) 2nd OAT OAT °C SEGMENT °C °F 04 22 10 28 LIMIT

40 125.3F 122.8F 121.5F 125.7F 168.4 40 104

38 127.0F 124.4F 123.2F 127.4F 169.9 38 100

36 128.6F 126.1F 124.8F 129.0F 171.4 36 97

34 130.3F 127.8F 126.5F 130.7F 172.9 34 93

32 132.0F 129.4F 128.1F 132.4F 174.5 32 90

30 133.6F 131.1F 129.8F 134.0F 176.0 30 86

28 135.3F 132.7F 131.4F 135.7F 177.5 28 82

26 137.0F 134.4F 133.1F 137.4F 179.1 26 79

24 138.7F 136.1F 134.8F 139.1F 180.6 24 75

22 140.3F 137.7F 136.4F 140.7F 182.1 22 72

20 142.0F 139.4F 138.1F 142.4F 183.7 20 68

18 143.7F 141.1F 139.8F 144.1F 185.2 18 64

16 145.4F 142.8F 141.4F 145.8F 186.8 16 61

14 147.1F 144.4F 143.1F 147.5F 188.4 14 57

12 148.7F 146.1F 144.8F 149.1F 189.9 12 54

10 150.4F 147.8F 146.4F 150.8F 191.5 10 50

8 152.1F 149.5F 148.1F 152.5F 193.0 8 46

6 153.8F 151.1F 149.8F 154.2F 194.6 6 43

4 155.5F 152.8F 151.5F 155.9F 196.2 4 39

2 157.2F 154.5F 153.2F 157.6F 197.8 2 36

0 158.9F 156.2F 154.8F 159.3F 199.3 0 32

-2 160.6F 157.9F 156.5F 161.0F 200.9 -2 28

-4 162.3F 159.6F 158.2F 162.7F 202.5 -4 25

-6 164.0F 161.3F 159.9F 164.4F 204.1 -6 21

-8 165.7F 163.0F 161.6F 166.1F 205.7 -8 18

-10 166.8F 164.0F 162.7F 167.2F 206.1 -10 14

-12 167.6F 164.9F 163.5F 168.1F 206.1 -12 10

-14 168.5F 165.8F 164.4F 168.9F 206.1 -14 7

-16 169.4F 166.7F 165.3F 169.8F 206.1 -16 3

-18 170.3F 167.6F 166.2F 170.7F 206.1 -18 0

-20 171.2F 168.4F 167.1F 171.6F 206.1 -20 -4

-22 172.1F 169.3F 168.0F 172.5F 206.1 -22 -8

-24 172.9F 170.2F 168.8F 173.3F 206.1 -24 -11

-26 173.8F 171.1F 169.7F 174.2F 206.1 -26 -15

-28 174.7F 172.0F 170.6F 175.1F 206.1 -28 -18

-30 175.6F 172.9F 171.5F 176.0F 206.1 -30 -22

-32 176.5F 173.7F 172.4F 176.9F 206.1 -32 -26

-34 177.3F 174.6F 173.2F 177.8F 206.1 -34 -29

-36 178.2F 175.5F 174.1F 178.6F 206.1 -36 -33

-38 179.1F 176.4F 175.0F 179.5F 206.1 -38 -36

-40 180.0F 177.3F 175.9F 180.4F 206.1 -40 -40

LENGTH (FT) 7040 7040 7000 7000 LIMITATIONS SLOPE (%) -0.30 +0.30 +0.50 -0.50 RUNWAY LENGTH F LIMITATION OBSTACLE * HEAD ADD 380 375 375 380 BRAKE ENERGY BE TAIL SUB 1060 1050 1040 1070 TIRE SPEED T


3.32 727-200/JT8D-15 JUN 26, 2012



JUN 26, 2012 727-200/JT8D-15 3.33

15° FLAPS CONCORD REG, CALIF


40 165.4F 172.0F 186.7 40 104

38 166.2F 172.8F 189.2 38 100

36 167.0F 173.6F 191.8 36 97

34 167.8F 174.4F 193.8 34 93

32 168.6F 175.2F 193.8 32 90

30 169.4F 176.1F 193.8 30 86

28 170.1F 176.9F 193.8 28 82

26 170.9F 177.7F 193.8 26 79

24 171.7F 178.5F 193.8 24 75

22 172.5F 179.3F 193.8 22 72

20 173.3F 180.2F 193.8 20 68

18 174.1F 181.0F 193.8 18 64

16 174.9F 181.8F 193.8 16 61

14 175.7F 182.6F 193.8 14 57

12 176.5F 183.4F 193.8 12 54

10 177.3F 184.2F 193.8 10 50

8 178.1F 185.1F 193.8 8 46

6 178.9F 185.9F 193.8 6 43

4 179.7F 186.7F 193.8 4 39

2 180.5F 187.5F 193.8 2 36

0 181.3F 188.3F 193.8 0 32

-2 182.1F 189.2F 193.8 -2 28

-4 182.9F 190.0F 193.8 -4 25

-6 183.7F 190.8F 193.8 -6 21

-8 184.5F 191.6F 193.8 -8 18

-10 185.3F 192.4F 193.8 -10 14

-12 186.1F 193.2F 193.8 -12 10

-14 186.9F 194.1F 193.8 -14 7

-16 187.7F 194.9F 193.8 -16 3

-18 188.5F 195.7F 193.8 -18 0

-20 189.3F 196.5F 193.8 -20 -4

-22 190.1F 197.3F 193.8 -22 -8

-24 190.9F 198.2F 193.8 -24 -11

-26 191.7F 199.0F 193.8 -26 -15

-28 192.5F 199.8F 193.8 -28 -18

-30 193.3F 200.6F 193.8 -30 -22

-32 194.1F 201.4F 193.8 -32 -26

-34 194.9F 202.2F 193.8 -34 -29

-36 195.7F 203.1F 193.8 -36 -33

-38 196.5F 203.9F 193.8 -38 -36

-40 197.3F 204.7F 193.8 -40 -40



3.34 727-200/JT8D-15 JUN 26, 2012



JUN 26, 2012 727-200/JT8D-15 3.35

15° FLAPS FRESNO INTL, CALIF

ELEVATION 336 OAT ZERO WIND RUNWAY LIMIT (1000 LBS) 2nd OAT OAT °C SEGMENT °C °F 11R 29L 11L 29R LIMIT

40 168.9F 168.9F 190.0F 190.0F 189.0 40 104

38 169.7F 169.7F 190.8F 190.8F 191.5 38 100

36 170.4F 170.4F 191.6F 191.6F 194.1 36 97

34 171.2F 171.2F 192.4F 192.4F 195.5 34 93

32 172.0F 172.0F 193.3F 193.3F 195.5 32 90

30 172.7F 172.7F 194.1F 194.1F 195.5 30 86

28 173.5F 173.5F 194.9F 194.9F 195.5 28 82

26 174.2F 174.2F 195.7F 195.7F 195.5 26 79

24 175.0F 175.0F 196.5F 196.5F 195.5 24 75

22 175.8F 175.8F 197.3F 197.3F 195.5 22 72

20 176.5F 176.5F 198.1F 198.1F 195.5 20 68

18 177.3F 177.3F 199.0F 199.0F 195.5 18 64

16 178.1F 178.1F 199.8F 199.8F 195.5 16 61

14 178.8F 178.8F 200.6F 200.6F 195.5 14 57

12 179.6F 179.6F 201.4F 201.4F 195.5 12 54

10 180.3F 180.3F 202.2F 202.2F 195.5 10 50

8 181.1F 181.1F 203.0F 203.0F 195.5 8 46

6 181.9F 181.9F 203.8F 203.8F 195.5 6 43

4 182.6F 182.6F 204.7F 204.7F 195.5 4 39

2 183.4F 183.4F 205.5F 205.5F 195.5 2 36

0 184.1F 184.1F 206.3F 206.3F 195.5 0 32

-2 184.9F 184.9F 207.1F 207.1F 195.5 -2 28

-4 185.7F 185.7F 207.9F 207.9F 195.5 -4 25

-6 186.4F 186.4F 208.7F 208.7F 195.5 -6 21

-8 187.2F 187.2F 209.5F 209.5F 195.5 -8 18

-10 188.0F 188.0F 210.4F 210.4F 195.5 -10 14

-12 188.7F 188.7F 211.2F 211.2F 195.5 -12 10

-14 189.5F 189.5F 212.0F 212.0F 195.5 -14 7

-16 190.2F 190.2F 212.8F 212.8F 195.5 -16 3

-18 191.0F 191.0F 213.6F 213.6F 195.5 -18 0

-20 191.8F 191.8F 214.4F 214.4F 195.5 -20 -4

-22 192.5F 192.5F 215.2F 215.2F 195.5 -22 -8

-24 193.3F 193.3F 216.1F 216.1F 195.5 -24 -11

-26 194.0F 194.0F 216.9F 216.9F 195.5 -26 -15

-28 194.8F 194.8F 217.7F 217.7F 195.5 -28 -18

-30 195.6F 195.6F 218.5F 218.5F 195.5 -30 -22

-32 196.3F 196.3F 219.3F 219.3F 195.5 -32 -26

-34 197.1F 197.1F 220.1F 220.1F 195.5 -34 -29

-36 197.9F 197.9F 220.9F 220.9F 195.5 -36 -33

-38 198.6F 198.6F 221.8F 221.8F 195.5 -38 -36

-40 199.4F 199.4F 222.6F 222.6F 195.5 -40 -40

LENGTH (FT) 7200 7200 9200 9200 LIMITATIONS SLOPE (%) 0.00 0.00 0.00 0.00 RUNWAY LENGTH F LIMITATION OBSTACLE * HEAD ADD 200 200 295 295 BRAKE ENERGY BE TAIL SUB 1180 1180 1130 1130 TIRE SPEED T


3.36 727-200/JT8D-15 JUN 26, 2012



JUN 26, 2012 727-200/JT8D-15 3.37

15° FLAPS HOLLYWOOD-BURBANK, CALIF


40 133.7F 122.6F 142.2F 132.3F 182.2 40 104

38 135.3F 124.2F 143.8F 133.9F 183.8 38 100

36 137.0F 125.9F 145.5F 135.6F 185.4 36 97

34 138.6F 127.5F 147.2F 137.2F 187.0 34 93

32 140.3F 129.1F 148.9F 138.9F 188.6 32 90

30 141.9F 130.7F 150.5F 140.5F 190.2 30 86

28 143.6F 132.4F 152.2F 142.2F 191.8 28 82

26 145.2F 134.0F 153.9F 143.8F 193.4 26 79

24 146.9F 135.7F 155.6F 145.5F 195.0 24 75

22 148.5F 137.3F 157.3F 147.1F 196.6 22 72

20 150.2F 138.9F 158.9F 148.8F 198.2 20 68

18 151.9F 140.6F 160.6F 150.4F 199.8 18 64

16 153.5F 142.2F 162.3F 152.1F 201.4 16 61

14 155.2F 143.9F 164.0F 153.7F 203.1 14 57

12 156.8F 145.5F 165.7F 155.4F 204.7 12 54

10 158.3F 147.0F 167.2F 156.9F 206.0 10 50

8 159.2F 147.9F 168.1F 157.8F 206.0 8 46

6 160.1F 148.7F 169.0F 158.7F 206.0 6 43

4 161.0F 149.6F 169.8F 159.5F 206.0 4 39

2 161.9F 150.5F 170.7F 160.4F 206.0 2 36

0 162.7F 151.4F 171.6F 161.3F 206.0 0 32

-2 163.6F 152.3F 172.5F 162.2F 206.0 -2 28

-4 164.5F 153.2F 173.4F 163.1F 206.0 -4 25

-6 165.4F 154.0F 174.3F 164.0F 206.0 -6 21

-8 166.3F 154.9F 175.1F 164.8F 206.0 -8 18

-10 167.2F 155.8F 176.0F 165.7F 206.0 -10 14

-12 168.0F 156.7F 176.9F 166.6F 206.0 -12 10

-14 168.9F 157.6F 177.8F 167.5F 206.0 -14 7

-16 169.8F 158.4F 178.7F 168.4F 206.0 -16 3

-18 170.7F 159.3F 179.5F 169.2F 206.0 -18 0

-20 171.6F 160.2F 180.4F 170.1F 206.0 -20 -4

-22 172.4F 161.1F 181.3F 171.0F 206.0 -22 -8

-24 173.3F 162.0F 182.2F 171.9F 206.0 -24 -11

-26 174.2F 162.9F 183.1F 172.8F 206.0 -26 -15

-28 175.1F 163.7F 184.0F 173.7F 206.0 -28 -18

-30 176.0F 164.6F 184.8F 174.5F 206.0 -30 -22

-32 176.9F 165.5F 185.7F 175.4F 206.0 -32 -26

-34 177.7F 166.4F 186.6F 176.3F 206.0 -34 -29

-36 178.6F 167.3F 187.5F 177.2F 206.0 -36 -33

-38 179.5F 168.1F 188.4F 178.1F 206.0 -38 -36

-40 180.4F 169.0F 189.2F 178.9F 206.0 -40 -40

LENGTH (FT) 5800 5800 6890 6890 LIMITATIONS SLOPE (%) -0.60 +0.60 -1.20 +1.20 RUNWAY LENGTH F LIMITATION OBSTACLE * HEAD ADD 355 345 385 370 BRAKE ENERGY BE TAIL SUB 990 970 1060 1020 TIRE SPEED T


3.38 727-200/JT8D-15 JUN 26, 2012



JUN 26, 2012 727-200/JT8D-15 3.39

15° FLAPS LAS VEGAS INTL, NEV


40 186.0F 186.0F 184.5F 173.6F 177.9 40 104

38 187.1F 187.1F 185.6F 174.6F 180.4 38 100

36 188.1F 188.1F 186.6F 175.7F 182.9 36 97

34 189.2F 189.2F 187.7F 176.7F 187.2 34 93

32 190.2F 190.2F 188.7F 177.7F 187.2 32 90

30 191.2F 191.2F 189.8F 178.7F 187.2 30 86

28 192.3F 192.3F 190.8F 179.7F 187.2 28 82

26 193.3F 193.3F 191.8F 180.7F 187.2 26 79

24 194.4F 194.4F 192.9F 181.8F 187.2 24 75

22 195.4F 195.4F 193.9F 182.8F 187.2 22 72

20 196.5F 196.5F 195.0F 183.8F 187.2 20 68

18 197.5F 197.5F 196.0F 184.8F 187.2 18 64

16 198.6F 198.6F 197.1F 185.8F 187.2 16 61

14 199.6F 199.6F 198.1F 186.8F 187.2 14 57

12 200.7F 200.7F 199.2F 187.9F 187.2 12 54

10 201.7F 201.7F 200.2F 188.9F 187.2 10 50

8 202.8F 202.8F 201.2F 189.9F 187.2 8 46

6 203.8F 203.8F 202.3F 190.9F 187.2 6 43

4 204.9F 204.9F 203.3F 191.9F 187.2 4 39

2 205.9F 205.9F 204.4F 192.9F 187.2 2 36

0 207.0F 207.0F 205.4F 194.0F 187.2 0 32

-2 208.0F 208.0F 206.5F 195.0F 187.2 -2 28

-4 209.1F 209.1F 207.5F 196.0F 187.2 -4 25

-6 210.1F 210.1F 208.6F 197.0F 187.2 -6 21

-8 211.2F 211.2F 209.6F 198.0F 187.2 -8 18

-10 212.2F 212.2F 210.6F 199.0F 187.2 -10 14

-12 213.2F 213.2F 211.7F 200.0F 187.2 -12 10

-14 214.3F 214.3F 212.7F 201.1F 187.2 -14 7

-16 215.3F 215.3F 213.8F 202.1F 187.2 -16 3

-18 216.4F 216.4F 214.8F 203.1F 187.2 -18 0

-20 217.4F 217.4F 215.9F 204.1F 187.2 -20 -4

-22 218.5F 218.5F 216.9F 205.1F 187.2 -22 -8

-24 219.5F 219.5F 218.0F 206.1F 187.2 -24 -11

-26 220.6F 220.6F 219.0F 207.2F 187.2 -26 -15

-28 221.6F 221.6F 220.0F 208.2F 187.2 -28 -18

-30 222.7F 222.7F 221.1F 209.2F 187.2 -30 -22

-32 223.7F 223.7F 222.1F 210.2F 187.2 -32 -26

-34 224.8F 224.8F 223.2F 211.2F 187.2 -34 -29

-36 225.8F 225.8F 224.2F 212.2F 187.2 -36 -33

-38 226.9F 226.9F 225.3F 213.3F 187.2 -38 -36

-40 227.9F 227.9F 226.3F 214.3F 187.2 -40 -40

LENGTH (FT) 10185 10185 9395 9395 LIMITATIONS SLOPE (%) 0.00 0.00 -1.10 +1.10 RUNWAY LENGTH F LIMITATION OBSTACLE * HEAD ADD 295 295 295 275 BRAKE ENERGY BE TAIL SUB 1040 1040 1050 1110 TIRE SPEED T


3.40 727-200/JT8D-15 JUN 26, 2012

15° FLAPS LAS VEGAS INTL, NEV


40 194.7F 186.3F 205.2F 203.5F 177.9 40 104

38 195.7F 187.4F 206.2F 204.5F 180.4 38 100

36 196.8F 188.4F 207.2F 205.5F 182.9 36 97

34 197.8F 189.5F 208.1F 206.6F 187.2 34 93

32 198.9F 190.5F 209.1F 207.6F 187.2 32 90

30 200.0F 191.5F 210.1F 208.7F 187.2 30 86

28 201.0F 192.6F 211.1F 209.7F 187.2 28 82

26 202.1F 193.6F 212.0F 210.8F 187.2 26 79

24 203.1F 194.7F 213.0F 211.8F 187.2 24 75

22 204.2F 195.7F 214.0F 212.8F 187.2 22 72

20 205.3F 196.8F 214.9F 213.9F 187.2 20 68

18 206.3F 197.8F 215.9F 214.9F 187.2 18 64

16 207.4F 198.9F 216.9F 216.0F 187.2 16 61

14 208.4F 199.9F 217.9F 217.0F 187.2 14 57

12 209.5F 201.0F 218.8F 218.0F 187.2 12 54

10 210.6F 202.0F 219.8F 219.1F 187.2 10 50

8 211.6F 203.1F 220.8F 220.1F 187.2 8 46

6 212.7F 204.1F 221.8F 221.2F 187.2 6 43

4 213.7F 205.2F 222.7F 222.2F 187.2 4 39

2 214.8F 206.2F 223.7F 223.3F 187.2 2 36

0 215.9F 207.3F 224.7F 224.3F 187.2 0 32

-2 216.9F 208.3F 225.6F 225.3F 187.2 -2 28

-4 218.0F 209.4F 226.6F 226.4F 187.2 -4 25

-6 219.0F 210.4F 227.6F 227.4F 187.2 -6 21

-8 220.1F 211.5F 228.6F 228.5F 187.2 -8 18

-10 221.1F 212.5F 229.5F 229.5F 187.2 -10 14

-12 222.2F 213.6F 230.5F 230.5F 187.2 -12 10

-14 223.3F 214.6F 231.5F 231.6F 187.2 -14 7

-16 224.3F 215.7F 232.5F 232.6F 187.2 -16 3

-18 225.4F 216.7F 233.4F 233.7F 187.2 -18 0

-20 226.4F 217.8F 234.4F 234.7F 187.2 -20 -4

-22 227.5F 218.8F 235.4F 235.8F 187.2 -22 -8

-24 228.6F 219.9F 236.3F 236.8F 187.2 -24 -11

-26 229.6F 220.9F 237.3F 237.8F 187.2 -26 -15

-28 230.7F 221.9F 238.3F 238.9F 187.2 -28 -18

-30 231.7F 223.0F 239.3F 239.9F 187.2 -30 -22

-32 232.8F 224.0F 240.2F 241.0F 187.2 -32 -26

-34 233.9F 225.1F 241.2F 242.0F 187.2 -34 -29

-36 234.9F 226.1F 242.2F 243.0F 187.2 -36 -33

-38 236.0F 227.2F 243.2F 244.1F 187.2 -38 -36

-40 237.0F 228.2F 244.1F 245.1F 187.2 -40 -40



JUN 26, 2012 727-200/JT8D-15 3.41

15° FLAPS LONG BEACH INTL, CALIF


40 174.9F 170.7F 186.5 40 104

38 176.7F 172.5F 188.1 38 100

36 178.6F 174.3F 189.7 36 97

34 180.5F 176.1F 191.3 34 93

32 182.4F 178.0F 193.0 32 90

30 184.3F 179.8F 194.6 30 86

28 186.1F 181.6F 196.2 28 82

26 188.0F 183.5F 197.8 26 79

24 189.9F 185.3F 199.5 24 75

22 191.8F 187.1F 201.1 22 72

20 193.7F 189.0F 202.7 20 68

18 195.6F 190.8F 204.4 18 64

16 197.2F 192.5F 205.7 16 61

14 198.1F 193.4F 205.7 14 57

12 199.0F 194.2F 205.7 12 54

10 199.9F 195.1F 205.7 10 50

8 200.8F 196.0F 205.7 8 46

6 201.7F 196.9F 205.7 6 43

4 202.5F 197.8F 205.7 4 39

2 203.4F 198.6F 205.7 2 36

0 204.3F 199.5F 205.7 0 32

-2 205.2F 200.4F 205.7 -2 28

-4 206.1F 201.3F 205.7 -4 25

-6 206.9F 202.2F 205.7 -6 21

-8 207.8F 203.1F 205.7 -8 18

-10 208.7F 203.9F 205.7 -10 14

-12 209.6F 204.8F 205.7 -12 10

-14 210.5F 205.7F 205.7 -14 7

-16 211.4F 206.6F 205.7 -16 3

-18 212.2F 207.5F 205.7 -18 0

-20 213.1F 208.3F 205.7 -20 -4

-22 214.0F 209.2F 205.7 -22 -8

-24 214.9F 210.1F 205.7 -24 -11

-26 215.8F 211.0F 205.7 -26 -15

-28 216.6F 211.9F 205.7 -28 -18

-30 217.5F 212.8F 205.7 -30 -22

-32 218.4F 213.6F 205.7 -32 -26

-34 219.3F 214.5F 205.7 -34 -29

-36 220.2F 215.4F 205.7 -36 -33

-38 221.1F 216.3F 205.7 -38 -36

-40 221.9F 217.2F 205.7 -40 -40

LENGTH (FT) 10000 10000 LIMITATIONS SLOPE (%) -0.40 +0.40 RUNWAY LENGTH F LIMITATION OBSTACLE * HEAD ADD 380 385 BRAKE ENERGY BE TAIL SUB 1090 1100 TIRE SPEED T


3.42 727-200/JT8D-15 JUN 26, 2012



JUN 26, 2012 727-200/JT8D-15 3.43

15° FLAPS LOS ANGELES INTL, CALIF


40 200.1F 200.1F 188.1F 189.1F 190.3 40 104

38 200.9F 200.9F 188.9F 189.9F 192.8 38 100

36 201.7F 201.7F 189.7F 190.7F 195.4 36 97

34 202.5F 202.5F 190.5F 191.5F 196.4 34 93

32 203.4F 203.4F 191.3F 192.3F 196.4 32 90

30 204.2F 204.2F 192.0F 193.1F 196.4 30 86

28 205.0F 205.0F 192.8F 193.9F 196.4 28 82

26 205.8F 205.8F 193.6F 194.6F 196.4 26 79

24 206.6F 206.6F 194.4F 195.4F 196.4 24 75

22 207.4F 207.4F 195.2F 196.2F 196.4 22 72

20 208.2F 208.2F 196.0F 197.0F 196.4 20 68

18 209.0F 209.0F 196.7F 197.8F 196.4 18 64

16 209.8F 209.8F 197.5F 198.6F 196.4 16 61

14 210.6F 210.6F 198.3F 199.3F 196.4 14 57

12 211.4F 211.4F 199.1F 200.1F 196.4 12 54

10 212.2F 212.2F 199.9F 200.9F 196.4 10 50

8 213.0F 213.0F 200.6F 201.7F 196.4 8 46

6 213.8F 213.8F 201.4F 202.5F 196.4 6 43

4 214.6F 214.6F 202.2F 203.3F 196.4 4 39

2 215.4F 215.4F 203.0F 204.1F 196.4 2 36

0 216.2F 216.2F 203.8F 204.8F 196.4 0 32

-2 217.0F 217.0F 204.6F 205.6F 196.4 -2 28

-4 217.8F 217.8F 205.3F 206.4F 196.4 -4 25

-6 218.6F 218.6F 206.1F 207.2F 196.4 -6 21

-8 219.4F 219.4F 206.9F 208.0F 196.4 -8 18

-10 220.2F 220.2F 207.7F 208.8F 196.4 -10 14

-12 221.0F 221.0F 208.5F 209.5F 196.4 -12 10

-14 221.9F 221.9F 209.2F 210.3F 196.4 -14 7

-16 222.7F 222.7F 210.0F 211.1F 196.4 -16 3

-18 223.5F 223.5F 210.8F 211.9F 196.4 -18 0

-20 224.3F 224.3F 211.6F 212.7F 196.4 -20 -4

-22 225.1F 225.1F 212.4F 213.5F 196.4 -22 -8

-24 225.9F 225.9F 213.2F 214.3F 196.4 -24 -11

-26 226.7F 226.7F 213.9F 215.0F 196.4 -26 -15

-28 227.5F 227.5F 214.7F 215.8F 196.4 -28 -18

-30 228.3F 228.3F 215.5F 216.6F 196.4 -30 -22

-32 229.1F 229.1F 216.3F 217.4F 196.4 -32 -26

-34 229.9F 229.9F 217.1F 218.2F 196.4 -34 -29

-36 230.7F 230.7F 217.9F 219.0F 196.4 -36 -33

-38 231.5F 231.5F 218.6F 219.7F 196.4 -38 -36

-40 232.3F 232.3F 219.4F 220.5F 196.4 -40 -40

LENGTH (FT) 10285 10285 8925 8925 LIMITATIONS SLOPE (%) 0.00 0.00 +0.10 -0.10 RUNWAY LENGTH F LIMITATION OBSTACLE * HEAD ADD 300 300 290 290 BRAKE ENERGY BE TAIL SUB 1060 1060 1150 1150 TIRE SPEED T


3.44 727-200/JT8D-15 JUN 26, 2012

15° FLAPS LOS ANGELES INTL, CALIF

ELEVATION 126 OAT ZERO WIND RUNWAY LIMIT (1000 LBS) 2nd OAT OAT °C SEGMENT °C °F 07L 25R 07R 25L LIMIT

40 211.7F 210.2F 206.5F 204.7F 190.3 40 104

38 212.5F 211.0F 207.3F 205.5F 192.8 38 100

36 213.4F 211.8F 208.1F 206.3F 195.4 36 97

34 214.2F 212.6F 208.9F 207.1F 196.4 34 93

32 215.0F 213.4F 209.7F 207.9F 196.4 32 90

30 215.8F 214.3F 210.5F 208.7F 196.4 30 86

28 216.6F 215.1F 211.3F 209.5F 196.4 28 82

26 217.4F 215.9F 212.1F 210.3F 196.4 26 79

24 218.2F 216.7F 213.0F 211.1F 196.4 24 75

22 219.0F 217.5F 213.8F 211.9F 196.4 22 72

20 219.8F 218.3F 214.6F 212.8F 196.4 20 68

18 220.7F 219.1F 215.4F 213.6F 196.4 18 64

16 221.5F 219.9F 216.2F 214.4F 196.4 16 61

14 222.3F 220.8F 217.0F 215.2F 196.4 14 57

12 223.1F 221.6F 217.8F 216.0F 196.4 12 54

10 223.9F 222.4F 218.6F 216.8F 196.4 10 50

8 224.7F 223.2F 219.4F 217.6F 196.4 8 46

6 225.5F 224.0F 220.3F 218.4F 196.4 6 43

4 226.3F 224.8F 221.1F 219.2F 196.4 4 39

2 227.2F 225.6F 221.9F 220.0F 196.4 2 36

0 228.0F 226.4F 222.7F 220.8F 196.4 0 32

-2 228.8F 227.3F 223.5F 221.7F 196.4 -2 28

-4 229.6F 228.1F 224.3F 222.5F 196.4 -4 25

-6 230.4F 228.9F 225.1F 223.3F 196.4 -6 21

-8 231.2F 229.7F 225.9F 224.1F 196.4 -8 18

-10 232.0F 230.5F 226.7F 224.9F 196.4 -10 14

-12 232.8F 231.3F 227.6F 225.7F 196.4 -12 10

-14 233.6F 232.1F 228.4F 226.5F 196.4 -14 7

-16 234.5F 232.9F 229.2F 227.3F 196.4 -16 3

-18 235.3F 233.8F 230.0F 228.1F 196.4 -18 0

-20 236.1F 234.6F 230.8F 228.9F 196.4 -20 -4

-22 236.9F 235.4F 231.6F 229.8F 196.4 -22 -8

-24 237.7F 236.2F 232.4F 230.6F 196.4 -24 -11

-26 238.5F 237.0F 233.2F 231.4F 196.4 -26 -15

-28 239.3F 237.8F 234.0F 232.2F 196.4 -28 -18

-30 240.1F 238.6F 234.9F 233.0F 196.4 -30 -22

-32 240.9F 239.4F 235.7F 233.8F 196.4 -32 -26

-34 241.8F 240.3F 236.5F 234.6F 196.4 -34 -29

-36 242.6F 241.1F 237.3F 235.4F 196.4 -36 -33

-38 243.4F 241.9F 238.1F 236.2F 196.4 -38 -36

-40 244.2F 242.7F 238.9F 237.0F 196.4 -40 -40



JUN 26, 2012 727-200/JT8D-15 3.45

15° FLAPS LOS CABOS, MEXICO


40 169.6F 169.6F 184.6 40 104

38 171.4F 171.4F 186.2 38 100

36 173.2F 173.2F 187.8 36 97

34 175.1F 175.1F 189.4 34 93

32 176.9F 176.9F 191.0 32 90

30 178.8F 178.8F 192.6 30 86

28 180.6F 180.6F 194.3 28 82

26 182.4F 182.4F 195.9 26 79

24 184.3F 184.3F 197.5 24 75

22 186.1F 186.1F 199.1 22 72

20 188.0F 188.0F 200.7 20 68

18 189.8F 189.8F 202.4 18 64

16 191.7F 191.7F 204.0 16 61

14 193.6F 193.6F 205.6 14 57

12 194.5F 194.5F 205.8 12 54

10 195.4F 195.4F 205.8 10 50

8 196.3F 196.3F 205.8 8 46

6 197.2F 197.2F 205.8 6 43

4 198.1F 198.1F 205.8 4 39

2 199.0F 199.0F 205.8 2 36

0 199.8F 199.8F 205.8 0 32

-2 200.7F 200.7F 205.8 -2 28

-4 201.6F 201.6F 205.8 -4 25

-6 202.5F 202.5F 205.8 -6 21

-8 203.4F 203.4F 205.8 -8 18

-10 204.2F 204.2F 205.8 -10 14

-12 205.1F 205.1F 205.8 -12 10

-14 206.0F 206.0F 205.8 -14 7

-16 206.9F 206.9F 205.8 -16 3

-18 207.8F 207.8F 205.8 -18 0

-20 208.7F 208.7F 205.8 -20 -4

-22 209.5F 209.5F 205.8 -22 -8

-24 210.4F 210.4F 205.8 -24 -11

-26 211.3F 211.3F 205.8 -26 -15

-28 212.2F 212.2F 205.8 -28 -18

-30 213.1F 213.1F 205.8 -30 -22

-32 213.9F 213.9F 205.8 -32 -26

-34 214.8F 214.8F 205.8 -34 -29

-36 215.7F 215.7F 205.8 -36 -33

-38 216.6F 216.6F 205.8 -38 -36

-40 217.5F 217.5F 205.8 -40 -40



3.46 727-200/JT8D-15 JUN 26, 2012



JUN 26, 2012 727-200/JT8D-15 3.47

15° FLAPS MEDFORD INTL, OREG


40 177.0F 182.0F 182.8 40 104

38 177.9F 182.9F 185.4 38 100

36 178.8F 183.8F 187.9 36 97

34 179.7F 184.7F 190.9 34 93

32 180.6F 185.7F 190.9 32 90

30 181.5F 186.6F 190.9 30 86

28 182.4F 187.5F 190.9 28 82

26 183.4F 188.5F 190.9 26 79

24 184.3F 189.4F 190.9 24 75

22 185.2F 190.3F 190.9 22 72

20 186.1F 191.2F 190.9 20 68

18 187.0F 192.2F 190.9 18 64

16 187.9F 193.1F 190.9 16 61

14 188.9F 194.0F 190.9 14 57

12 189.8F 195.0F 190.9 12 54

10 190.7F 195.9F 190.9 10 50

8 191.6F 196.8F 190.9 8 46

6 192.5F 197.8F 190.9 6 43

4 193.4F 198.7F 190.9 4 39

2 194.4F 199.6F 190.9 2 36

0 195.3F 200.5F 190.9 0 32

-2 196.2F 201.5F 190.9 -2 28

-4 197.1F 202.4F 190.9 -4 25

-6 198.0F 203.3F 190.9 -6 21

-8 198.9F 204.3F 190.9 -8 18

-10 199.9F 205.2F 190.9 -10 14

-12 200.8F 206.1F 190.9 -12 10

-14 201.7F 207.0F 190.9 -14 7

-16 202.6F 208.0F 190.9 -16 3

-18 203.5F 208.9F 190.9 -18 0

-20 204.4F 209.8F 190.9 -20 -4

-22 205.3F 210.8F 190.9 -22 -8

-24 206.3F 211.7F 190.9 -24 -11

-26 207.2F 212.6F 190.9 -26 -15

-28 208.1F 213.5F 190.9 -28 -18

-30 209.0F 214.5F 190.9 -30 -22

-32 209.9F 215.4F 190.9 -32 -26

-34 210.8F 216.3F 190.9 -34 -29

-36 211.8F 217.3F 190.9 -36 -33

-38 212.7F 218.2F 190.9 -38 -36

-40 213.6F 219.1F 190.9 -40 -40



3.48 727-200/JT8D-15 JUN 26, 2012



JUN 26, 2012 727-200/JT8D-15 3.49

15° FLAPS MONTEREY INTL, CALIF

ELEVATION 257 OAT ZERO WIND RUNWAY LIMIT (1000 LBS) 2nd OAT OAT °C SEGMENT °C °F 10R 28L LIMIT

40 167.2F 179.9F 189.5 40 104

38 168.0F 180.6F 192 38 100

36 168.7F 181.4F 194.6 36 97

34 169.4F 182.2F 195.8 34 93

32 170.2F 183.0F 195.8 32 90

30 170.9F 183.8F 195.8 30 86

28 171.7F 184.5F 195.8 28 82

26 172.4F 185.3F 195.8 26 79

24 173.2F 186.1F 195.8 24 75

22 173.9F 186.9F 195.8 22 72

20 174.7F 187.7F 195.8 20 68

18 175.4F 188.5F 195.8 18 64

16 176.2F 189.2F 195.8 16 61

14 176.9F 190.0F 195.8 14 57

12 177.7F 190.8F 195.8 12 54

10 178.4F 191.6F 195.8 10 50

8 179.2F 192.4F 195.8 8 46

6 179.9F 193.1F 195.8 6 43

4 180.7F 193.9F 195.8 4 39

2 181.4F 194.7F 195.8 2 36

0 182.1F 195.5F 195.8 0 32

-2 182.9F 196.3F 195.8 -2 28

-4 183.6F 197.0F 195.8 -4 25

-6 184.4F 197.8F 195.8 -6 21

-8 185.1F 198.6F 195.8 -8 18

-10 185.9F 199.4F 195.8 -10 14

-12 186.6F 200.2F 195.8 -12 10

-14 187.4F 200.9F 195.8 -14 7

-16 188.1F 201.7F 195.8 -16 3

-18 188.9F 202.5F 195.8 -18 0

-20 189.6F 203.3F 195.8 -20 -4

-22 190.4F 204.1F 195.8 -22 -8

-24 191.1F 204.8F 195.8 -24 -11

-26 191.9F 205.6F 195.8 -26 -15

-28 192.6F 206.4F 195.8 -28 -18

-30 193.3F 207.2F 195.8 -30 -22

-32 194.1F 208.0F 195.8 -32 -26

-34 194.8F 208.7F 195.8 -34 -29

-36 195.6F 209.5F 195.8 -36 -33

-38 196.3F 210.3F 195.8 -38 -36

-40 197.1F 211.1F 195.8 -40 -40



3.50 727-200/JT8D-15 JUN 26, 2012



JUN 26, 2012 727-200/JT8D-15 3.51

15° FLAPS OAKLAND INTL, CALIF


40 198.7F 198.7F 191.0 40 104

38 199.5F 199.5F 193.5 38 100

36 200.3F 200.3F 196.1 36 97

34 201.1F 201.1F 197.0 34 93

32 201.9F 201.9F 197.0 32 90

30 202.7F 202.7F 197.0 30 86

28 203.5F 203.5F 197.0 28 82

26 204.2F 204.2F 197.0 26 79

24 205.0F 205.0F 197.0 24 75

22 205.8F 205.8F 197.0 22 72

20 206.6F 206.6F 197.0 20 68

18 207.4F 207.4F 197.0 18 64

16 208.2F 208.2F 197.0 16 61

14 209.0F 209.0F 197.0 14 57

12 209.8F 209.8F 197.0 12 54

10 210.5F 210.5F 197.0 10 50

8 211.3F 211.3F 197.0 8 46

6 212.1F 212.1F 197.0 6 43

4 212.9F 212.9F 197.0 4 39

2 213.7F 213.7F 197.0 2 36

0 214.5F 214.5F 197.0 0 32

-2 215.3F 215.3F 197.0 -2 28

-4 216.1F 216.1F 197.0 -4 25

-6 216.8F 216.8F 197.0 -6 21

-8 217.6F 217.6F 197.0 -8 18

-10 218.4F 218.4F 197.0 -10 14

-12 219.2F 219.2F 197.0 -12 10

-14 220.0F 220.0F 197.0 -14 7

-16 220.8F 220.8F 197.0 -16 3

-18 221.6F 221.6F 197.0 -18 0

-20 222.3F 222.3F 197.0 -20 -4

-22 223.1F 223.1F 197.0 -22 -8

-24 223.9F 223.9F 197.0 -24 -11

-26 224.7F 224.7F 197.0 -26 -15

-28 225.5F 225.5F 197.0 -28 -18

-30 226.3F 226.3F 197.0 -30 -22

-32 227.1F 227.1F 197.0 -32 -26

-34 227.9F 227.9F 197.0 -34 -29

-36 228.6F 228.6F 197.0 -36 -33

-38 229.4F 229.4F 197.0 -38 -36

-40 230.2F 230.2F 197.0 -40 -40



3.52 727-200/JT8D-15 JUN 26, 2012



JUN 26, 2012 727-200/JT8D-15 3.53

15° FLAPS ONTARIO INTL, CALIF


40 169.2F 168.2F 183.5F 182.4F 181.2 40 104

38 171.1F 170.0F 185.6F 184.5F 182.8 38 100

36 173.0F 171.9F 187.7F 186.6F 184.4 36 97

34 174.9F 173.8F 189.8F 188.7F 186.0 34 93

32 176.7F 175.6F 191.9F 190.8F 187.5 32 90

30 178.6F 177.5F 194.0F 192.9F 189.1 30 86

28 180.5F 179.4F 196.1F 195.0F 190.7 28 82

26 182.4F 181.2F 198.3F 197.1F 192.3 26 79

24 184.3F 183.1F 200.4F 199.2F 193.9 24 75

22 186.2F 185.0F 202.5F 201.3F 195.5 22 72

20 188.1F 186.9F 204.6F 203.4F 197.2 20 68

18 190.0F 188.8F 206.8F 205.5F 198.8 18 64

16 191.8F 190.6F 208.9F 207.6F 200.4 16 61

14 193.7F 192.5F 211.0F 209.7F 202.0 14 57

12 195.6F 194.4F 213.2F 211.8F 203.6 12 54

10 197.5F 196.3F 215.3F 214.0F 205.3 10 50

8 198.9F 197.7F 216.8F 215.4F 206.0 8 46

6 199.8F 198.5F 217.7F 216.3F 206.0 6 43

4 200.7F 199.4F 218.5F 217.2F 206.0 4 39

2 201.6F 200.3F 219.4F 218.1F 206.0 2 36

0 202.4F 201.2F 220.3F 218.9F 206.0 0 32

-2 203.3F 202.1F 221.2F 219.8F 206.0 -2 28

-4 204.2F 202.9F 222.1F 220.7F 206.0 -4 25

-6 205.1F 203.8F 222.9F 221.6F 206.0 -6 21

-8 206.0F 204.7F 223.8F 222.5F 206.0 -8 18

-10 206.8F 205.6F 224.7F 223.4F 206.0 -10 14

-12 207.7F 206.5F 225.6F 224.2F 206.0 -12 10

-14 208.6F 207.4F 226.5F 225.1F 206.0 -14 7

-16 209.5F 208.2F 227.4F 226.0F 206.0 -16 3

-18 210.4F 209.1F 228.2F 226.9F 206.0 -18 0

-20 211.3F 210.0F 229.1F 227.8F 206.0 -20 -4

-22 212.1F 210.9F 230.0F 228.6F 206.0 -22 -8

-24 213.0F 211.8F 230.9F 229.5F 206.0 -24 -11

-26 213.9F 212.6F 231.8F 230.4F 206.0 -26 -15

-28 214.8F 213.5F 232.6F 231.3F 206.0 -28 -18

-30 215.7F 214.4F 233.5F 232.2F 206.0 -30 -22

-32 216.5F 215.3F 234.4F 233.1F 206.0 -32 -26

-34 217.4F 216.2F 235.3F 233.9F 206.0 -34 -29

-36 218.3F 217.1F 236.2F 234.8F 206.0 -36 -33

-38 219.2F 217.9F 237.1F 235.7F 206.0 -38 -36

-40 220.1F 218.8F 237.9F 236.6F 206.0 -40 -40



3.54 727-200/JT8D-15 JUN 26, 2012



JUN 26, 2012 727-200/JT8D-15 3.55

15° FLAPS ORANGE COUNTY, CALIF

ELEVATION 56 OAT ZERO WIND RUNWAY LIMIT (1000 LBS) 2nd OAT OAT °C SEGMENT °C °F 01L 19R LIMIT

40 129.2F 127.2F 186.5 40 104

38 130.8F 128.8F 188.2 38 100

36 132.4F 130.5F 189.8 36 97

34 134.0F 132.1F 191.4 34 93

32 135.7F 133.7F 193.0 32 90

30 137.3F 135.4F 194.6 30 86

28 138.9F 137.0F 196.2 28 82

26 140.6F 138.6F 197.9 26 79

24 142.2F 140.3F 199.5 24 75

22 143.9F 141.9F 201.1 22 72

20 145.5F 143.5F 202.8 20 68

18 147.1F 145.2F 204.4 18 64

16 148.6F 146.7F 205.7 16 61

14 149.5F 147.5F 205.7 14 57

12 150.4F 148.4F 205.7 12 54

10 151.3F 149.3F 205.7 10 50

8 152.1F 150.2F 205.7 8 46

6 153.0F 151.1F 205.7 6 43

4 153.9F 151.9F 205.7 4 39

2 154.8F 152.8F 205.7 2 36

0 155.7F 153.7F 205.7 0 32

-2 156.5F 154.6F 205.7 -2 28

-4 157.4F 155.5F 205.7 -4 25

-6 158.3F 156.4F 205.7 -6 21

-8 159.2F 157.2F 205.7 -8 18

-10 160.1F 158.1F 205.7 -10 14

-12 161.0F 159.0F 205.7 -12 10

-14 161.8F 159.9F 205.7 -14 7

-16 162.7F 160.8F 205.7 -16 3

-18 163.6F 161.6F 205.7 -18 0

-20 164.5F 162.5F 205.7 -20 -4

-22 165.4F 163.4F 205.7 -22 -8

-24 166.2F 164.3F 205.7 -24 -11

-26 167.1F 165.2F 205.7 -26 -15

-28 168.0F 166.1F 205.7 -28 -18

-30 168.9F 166.9F 205.7 -30 -22

-32 169.8F 167.8F 205.7 -32 -26

-34 170.7F 168.7F 205.7 -34 -29

-36 171.5F 169.6F 205.7 -36 -33

-38 172.4F 170.5F 205.7 -38 -36

-40 173.3F 171.3F 205.7 -40 -40



3.56 727-200/JT8D-15 JUN 26, 2012



JUN 26, 2012 727-200/JT8D-15 3.57

15° FLAPS PHOENIX INTL, ARIZ

ELEVATION 1135 OAT ZERO WIND RUNWAY LIMIT (1000 LBS) 2nd OAT OAT °C SEGMENT °C °F 07R 25L 07L 25R 08 26 LIMIT

40 169.7F 171.7F 192.5F 194.4F 200.2F 200.2F 184.1 40 104

38 170.6F 172.6F 193.4F 195.3F 201.2F 201.2F 186.6 38 100

36 171.5F 173.4F 194.3F 196.3F 202.1F 202.1F 189.1 36 97

34 172.4F 174.3F 195.3F 197.2F 203.1F 203.1F 191.8 34 93

32 173.2F 175.2F 196.2F 198.1F 204.0F 204.0F 191.8 32 90

30 174.1F 176.0F 197.1F 199.1F 204.9F 204.9F 191.8 30 86

28 175.0F 176.9F 198.0F 200.0F 205.9F 205.9F 191.8 28 82

26 175.8F 177.8F 199.0F 200.9F 206.8F 206.8F 191.8 26 79

24 176.7F 178.7F 199.9F 201.8F 207.7F 207.7F 191.8 24 75

22 177.6F 179.5F 200.8F 202.8F 208.7F 208.7F 191.8 22 72

20 178.4F 180.4F 201.7F 203.7F 209.6F 209.6F 191.8 20 68

18 179.3F 181.3F 202.7F 204.6F 210.5F 210.5F 191.8 18 64

16 180.2F 182.2F 203.6F 205.6F 211.5F 211.5F 191.8 16 61

14 181.0F 183.0F 204.5F 206.5F 212.4F 212.4F 191.8 14 57

12 181.9F 183.9F 205.4F 207.4F 213.3F 213.3F 191.8 12 54

10 182.8F 184.8F 206.4F 208.3F 214.3F 214.3F 191.8 10 50

8 183.6F 185.7F 207.3F 209.3F 215.2F 215.2F 191.8 8 46

6 184.5F 186.5F 208.2F 210.2F 216.1F 216.1F 191.8 6 43

4 185.4F 187.4F 209.1F 211.1F 217.1F 217.1F 191.8 4 39

2 186.2F 188.3F 210.1F 212.1F 218.0F 218.0F 191.8 2 36

0 187.1F 189.2F 211.0F 213.0F 219.0F 219.0F 191.8 0 32

-2 188.0F 190.0F 211.9F 213.9F 219.9F 219.9F 191.8 -2 28

-4 188.9F 190.9F 212.8F 214.8F 220.8F 220.8F 191.8 -4 25

-6 189.7F 191.8F 213.8F 215.8F 221.8F 221.8F 191.8 -6 21

-8 190.6F 192.7F 214.7F 216.7F 222.7F 222.7F 191.8 -8 18

-10 191.5F 193.5F 215.6F 217.6F 223.6F 223.6F 191.8 -10 14

-12 192.3F 194.4F 216.5F 218.6F 224.6F 224.6F 191.8 -12 10

-14 193.2F 195.3F 217.5F 219.5F 225.5F 225.5F 191.8 -14 7

-16 194.1F 196.2F 218.4F 220.4F 226.4F 226.4F 191.8 -16 3

-18 194.9F 197.0F 219.3F 221.3F 227.4F 227.4F 191.8 -18 0

-20 195.8F 197.9F 220.2F 222.3F 228.3F 228.3F 191.8 -20 -4

-22 196.7F 198.8F 221.2F 223.2F 229.2F 229.2F 191.8 -22 -8

-24 197.5F 199.6F 222.1F 224.1F 230.2F 230.2F 191.8 -24 -11

-26 198.4F 200.5F 223.0F 225.1F 231.1F 231.1F 191.8 -26 -15

-28 199.3F 201.4F 223.9F 226.0F 232.0F 232.0F 191.8 -28 -18

-30 200.1F 202.3F 224.9F 226.9F 233.0F 233.0F 191.8 -30 -22

-32 201.0F 203.1F 225.8F 227.8F 233.9F 233.9F 191.8 -32 -26

-34 201.9F 204.0F 226.7F 228.8F 234.8F 234.8F 191.8 -34 -29

-36 202.7F 204.9F 227.7F 229.7F 235.8F 235.8F 191.8 -36 -33

-38 203.6F 205.8F 228.6F 230.6F 236.7F 236.7F 191.8 -38 -36

-40 204.5F 206.6F 229.5F 231.6F 237.7F 237.7F 191.8 -40 -40

LENGTH (FT) 7800 7800 10300 10300 11490 11490 LIMITATIONS SLOPE (%) +0.20 -0.20 +0.20 -0.20 0.00 0.00 RUNWAY LENGTH F LIMITATION OBSTACLE * HEAD ADD 230 240 295 295 270 270 BRAKE ENERGY BE TAIL SUB 1150 1160 1060 1060 940 940 TIRE SPEED T


3.58 727-200/JT8D-15 JUN 26, 2012



JUN 26, 2012 727-200/JT8D-15 3.59

15° FLAPS PORTLAND INTL, OREG

ELEVATION 30 OAT ZERO WIND RUNWAY LIMIT (1000 LBS) 2nd OAT OAT °C SEGMENT °C °F 03 21 10R 28L 10L 28R LIMIT

40 167.8F 168.7F 205.7F 205.7F 179.9F 179.9F 190.8 40 104

38 168.5F 169.4F 206.5F 206.5F 180.6F 180.6F 193.4 38 100

36 169.2F 170.2F 207.3F 207.3F 181.4F 181.4F 196.0 36 97

34 170.0F 170.9F 208.1F 208.1F 182.1F 182.1F 196.9 34 93

32 170.7F 171.6F 208.9F 208.9F 182.9F 182.9F 196.9 32 90

30 171.4F 172.3F 209.7F 209.7F 183.6F 183.6F 196.9 30 86

28 172.1F 173.0F 210.5F 210.5F 184.4F 184.4F 196.9 28 82

26 172.8F 173.8F 211.3F 211.3F 185.2F 185.2F 196.9 26 79

24 173.6F 174.5F 212.1F 212.1F 185.9F 185.9F 196.9 24 75

22 174.3F 175.2F 212.9F 212.9F 186.7F 186.7F 196.9 22 72

20 175.0F 175.9F 213.7F 213.7F 187.4F 187.4F 196.9 20 68

18 175.7F 176.7F 214.5F 214.5F 188.2F 188.2F 196.9 18 64

16 176.4F 177.4F 215.3F 215.3F 188.9F 188.9F 196.9 16 61

14 177.2F 178.1F 216.1F 216.1F 189.7F 189.7F 196.9 14 57

12 177.9F 178.8F 216.9F 216.9F 190.4F 190.4F 196.9 12 54

10 178.6F 179.5F 217.7F 217.7F 191.2F 191.2F 196.9 10 50

8 179.3F 180.3F 218.5F 218.5F 191.9F 191.9F 196.9 8 46

6 180.0F 181.0F 219.3F 219.3F 192.7F 192.7F 196.9 6 43

4 180.7F 181.7F 220.1F 220.1F 193.4F 193.4F 196.9 4 39

2 181.5F 182.4F 220.9F 220.9F 194.2F 194.2F 196.9 2 36

0 182.2F 183.2F 221.7F 221.7F 194.9F 194.9F 196.9 0 32

-2 182.9F 183.9F 222.5F 222.5F 195.7F 195.7F 196.9 -2 28

-4 183.6F 184.6F 223.2F 223.2F 196.4F 196.4F 196.9 -4 25

-6 184.3F 185.3F 224.0F 224.0F 197.2F 197.2F 196.9 -6 21

-8 185.1F 186.0F 224.8F 224.8F 197.9F 197.9F 196.9 -8 18

-10 185.8F 186.8F 225.6F 225.6F 198.7F 198.7F 196.9 -10 14

-12 186.5F 187.5F 226.4F 226.4F 199.4F 199.4F 196.9 -12 10

-14 187.2F 188.2F 227.2F 227.2F 200.2F 200.2F 196.9 -14 7

-16 187.9F 188.9F 228.0F 228.0F 200.9F 200.9F 196.9 -16 3

-18 188.7F 189.7F 228.8F 228.8F 201.7F 201.7F 196.9 -18 0

-20 189.4F 190.4F 229.6F 229.6F 202.4F 202.4F 196.9 -20 -4

-22 190.1F 191.1F 230.4F 230.4F 203.2F 203.2F 196.9 -22 -8

-24 190.8F 191.8F 231.2F 231.2F 203.9F 203.9F 196.9 -24 -11

-26 191.5F 192.5F 232.0F 232.0F 204.7F 204.7F 196.9 -26 -15

-28 192.3F 193.3F 232.8F 232.8F 205.4F 205.4F 196.9 -28 -18

-30 193.0F 194.0F 233.6F 233.6F 206.2F 206.2F 196.9 -30 -22

-32 193.7F 194.7F 234.4F 234.4F 206.9F 206.9F 196.9 -32 -26

-34 194.4F 195.4F 235.2F 235.2F 207.7F 207.7F 196.9 -34 -29

-36 195.1F 196.2F 236.0F 236.0F 208.4F 208.4F 196.9 -36 -33

-38 195.9F 196.9F 236.8F 236.8F 209.2F 209.2F 196.9 -38 -36

-40 196.6F 197.6F 237.6F 237.6F 209.9F 209.9F 196.9 -40 -40

LENGTH (FT) 7000 7000 11000 11000 8000 8000 LIMITATIONS SLOPE (%) +0.10 -0.10 0.00 0.00 0.00 0.00 RUNWAY LENGTH F LIMITATION OBSTACLE * HEAD ADD 180 185 280 280 250 250 BRAKE ENERGY BE TAIL SUB 1180 1180 990 990 1180 1180 TIRE SPEED T


3.60 727-200/JT8D-15 JUN 26, 2012



JUN 26, 2012 727-200/JT8D-15 3.61

15° FLAPS RENO INTL, NEV


40 131.9F 130.5F 176.3F 176.3F 162.0F 161.0F 163.9 40 104

38 133.1F 131.6F 177.7F 177.7F 163.3F 162.3F 166.3 38 100

36 134.2F 132.8F 179.0F 179.0F 164.6F 163.6F 168.8 36 97

34 135.4F 133.9F 180.3F 180.3F 165.9F 164.9F 176.9 34 93

32 136.5F 135.1F 181.7F 181.7F 167.2F 166.2F 176.9 32 90

30 137.7F 136.2F 183.0F 183.0F 168.5F 167.5F 176.9 30 86

28 138.8F 137.3F 184.3F 184.3F 169.8F 168.8F 176.9 28 82

26 140.0F 138.5F 185.7F 185.7F 171.1F 170.1F 176.9 26 79

24 141.1F 139.6F 187.0F 187.0F 172.4F 171.4F 176.9 24 75

22 142.3F 140.8F 188.3F 188.3F 173.6F 172.7F 176.9 22 72

20 143.5F 141.9F 189.7F 189.7F 174.9F 174.0F 176.9 20 68

18 144.6F 143.1F 191.0F 191.0F 176.2F 175.3F 176.9 18 64

16 145.8F 144.2F 192.4F 192.4F 177.5F 176.5F 176.9 16 61

14 146.9F 145.4F 193.7F 193.7F 178.8F 177.8F 176.9 14 57

12 148.1F 146.5F 195.0F 195.0F 180.1F 179.1F 176.9 12 54

10 149.2F 147.7F 196.4F 196.4F 181.4F 180.4F 176.9 10 50

8 150.4F 148.8F 197.7F 197.7F 182.7F 181.7F 176.9 8 46

6 151.5F 150.0F 199.0F 199.0F 184.0F 183.0F 176.9 6 43

4 152.7F 151.1F 200.4F 200.4F 185.3F 184.3F 176.9 4 39

2 153.8F 152.3F 201.7F 201.7F 186.6F 185.6F 176.9 2 36

0 155.0F 153.4F 203.0F 203.0F 187.9F 186.9F 176.9 0 32

-2 156.2F 154.5F 204.4F 204.4F 189.2F 188.2F 176.9 -2 28

-4 157.3F 155.7F 205.7F 205.7F 190.5F 189.5F 176.9 -4 25

-6 158.5F 156.8F 207.0F 207.0F 191.8F 190.8F 176.9 -6 21

-8 159.6F 158.0F 208.4F 208.4F 193.1F 192.0F 176.9 -8 18

-10 160.8F 159.1F 209.7F 209.7F 194.4F 193.3F 176.9 -10 14

-12 161.9F 160.3F 211.0F 211.0F 195.7F 194.6F 176.9 -12 10

-14 163.1F 161.4F 212.4F 212.4F 197.0F 195.9F 176.9 -14 7

-16 164.2F 162.6F 213.7F 213.7F 198.3F 197.2F 176.9 -16 3

-18 165.4F 163.7F 215.0F 215.0F 199.5F 198.5F 176.9 -18 0

-20 166.5F 164.9F 216.4F 216.4F 200.8F 199.8F 176.9 -20 -4

-22 167.7F 166.0F 217.7F 217.7F 202.1F 201.1F 176.9 -22 -8

-24 168.8F 167.2F 219.1F 219.1F 203.4F 202.4F 176.9 -24 -11

-26 170.0F 168.3F 220.4F 220.4F 204.7F 203.7F 176.9 -26 -15

-28 171.2F 169.5F 221.7F 221.7F 206.0F 205.0F 176.9 -28 -18

-30 172.3F 170.6F 223.1F 223.1F 207.3F 206.2F 176.9 -30 -22

-32 173.5F 171.7F 224.4F 224.4F 208.6F 207.5F 176.9 -32 -26

-34 174.6F 172.9F 225.7F 225.7F 209.9F 208.8F 176.9 -34 -29

-36 175.8F 174.0F 227.1F 227.1F 211.2F 210.1F 176.9 -36 -33

-38 176.9F 175.2F 228.4F 228.4F 212.5F 211.4F 176.9 -38 -36

-40 178.1F 176.3F 229.7F 229.7F 213.8F 212.7F 176.9 -40 -40

LENGTH (FT) 6100 6100 11000 11000 9000 9000 LIMITATIONS SLOPE (%) -0.20 +0.20 0.00 0.00 -0.10 +0.10 RUNWAY LENGTH F LIMITATION OBSTACLE * HEAD ADD 90 75 280 280 270 270 BRAKE ENERGY BE TAIL SUB 1030 1030 940 940 1050 1050 TIRE SPEED T


3.62 727-200/JT8D-15 JUN 26, 2012



JUN 26, 2012 727-200/JT8D-15 3.63

15° FLAPS SACRAMENTO INTL, CALIF


40 186.2F 186.2F 186.6F 185.6F 190.9 40 104

38 186.9F 186.9F 187.4F 186.4F 193.4 38 100

36 187.7F 187.7F 188.2F 187.2F 196.0 36 97

34 188.5F 188.5F 188.9F 187.9F 196.9 34 93

32 189.2F 189.2F 189.7F 188.7F 196.9 32 90

30 190.0F 190.0F 190.5F 189.4F 196.9 30 86

28 190.8F 190.8F 191.2F 190.2F 196.9 28 82

26 191.5F 191.5F 192.0F 191.0F 196.9 26 79

24 192.3F 192.3F 192.8F 191.7F 196.9 24 75

22 193.0F 193.0F 193.5F 192.5F 196.9 22 72

20 193.8F 193.8F 194.3F 193.3F 196.9 20 68

18 194.6F 194.6F 195.1F 194.0F 196.9 18 64

16 195.3F 195.3F 195.8F 194.8F 196.9 16 61

14 196.1F 196.1F 196.6F 195.6F 196.9 14 57

12 196.9F 196.9F 197.4F 196.3F 196.9 12 54

10 197.6F 197.6F 198.1F 197.1F 196.9 10 50

8 198.4F 198.4F 198.9F 197.8F 196.9 8 46

6 199.2F 199.2F 199.7F 198.6F 196.9 6 43

4 199.9F 199.9F 200.4F 199.4F 196.9 4 39

2 200.7F 200.7F 201.2F 200.1F 196.9 2 36

0 201.5F 201.5F 202.0F 200.9F 196.9 0 32

-2 202.2F 202.2F 202.7F 201.7F 196.9 -2 28

-4 203.0F 203.0F 203.5F 202.4F 196.9 -4 25

-6 203.8F 203.8F 204.3F 203.2F 196.9 -6 21

-8 204.5F 204.5F 205.0F 204.0F 196.9 -8 18

-10 205.3F 205.3F 205.8F 204.7F 196.9 -10 14

-12 206.0F 206.0F 206.6F 205.5F 196.9 -12 10

-14 206.8F 206.8F 207.3F 206.2F 196.9 -14 7

-16 207.6F 207.6F 208.1F 207.0F 196.9 -16 3

-18 208.3F 208.3F 208.9F 207.8F 196.9 -18 0

-20 209.1F 209.1F 209.6F 208.5F 196.9 -20 -4

-22 209.9F 209.9F 210.4F 209.3F 196.9 -22 -8

-24 210.6F 210.6F 211.2F 210.1F 196.9 -24 -11

-26 211.4F 211.4F 211.9F 210.8F 196.9 -26 -15

-28 212.2F 212.2F 212.7F 211.6F 196.9 -28 -18

-30 212.9F 212.9F 213.5F 212.4F 196.9 -30 -22

-32 213.7F 213.7F 214.2F 213.1F 196.9 -32 -26

-34 214.5F 214.5F 215.0F 213.9F 196.9 -34 -29

-36 215.2F 215.2F 215.7F 214.6F 196.9 -36 -33

-38 216.0F 216.0F 216.5F 215.4F 196.9 -38 -36

-40 216.8F 216.8F 217.3F 216.2F 196.9 -40 -40

LENGTH (FT) 8600 8600 8600 8600 LIMITATIONS SLOPE (%) 0.00 0.00 -0.10 +0.10 RUNWAY LENGTH F LIMITATION OBSTACLE * HEAD ADD 275 275 285 280 BRAKE ENERGY BE TAIL SUB 1170 1170 1160 1170 TIRE SPEED T


3.64 727-200/JT8D-15 JUN 26, 2012



JUN 26, 2012 727-200/JT8D-15 3.65

15° FLAPS SAN DIEGO INTL, CALIF


40 193.7F 193.7F 190.9 40 104

38 194.5F 194.5F 193.5 38 100

36 195.3F 195.3F 196.1 36 97

34 196.1F 196.1F 196.9 34 93

32 196.8F 196.8F 196.9 32 90

30 197.6F 197.6F 196.9 30 86

28 198.4F 198.4F 196.9 28 82

26 199.2F 199.2F 196.9 26 79

24 200.0F 200.0F 196.9 24 75

22 200.7F 200.7F 196.9 22 72

20 201.5F 201.5F 196.9 20 68

18 202.3F 202.3F 196.9 18 64

16 203.1F 203.1F 196.9 16 61

14 203.8F 203.8F 196.9 14 57

12 204.6F 204.6F 196.9 12 54

10 205.4F 205.4F 196.9 10 50

8 206.2F 206.2F 196.9 8 46

6 207.0F 207.0F 196.9 6 43

4 207.7F 207.7F 196.9 4 39

2 208.5F 208.5F 196.9 2 36

0 209.3F 209.3F 196.9 0 32

-2 210.1F 210.1F 196.9 -2 28

-4 210.9F 210.9F 196.9 -4 25

-6 211.6F 211.6F 196.9 -6 21

-8 212.4F 212.4F 196.9 -8 18

-10 213.2F 213.2F 196.9 -10 14

-12 214.0F 214.0F 196.9 -12 10

-14 214.8F 214.8F 196.9 -14 7

-16 215.5F 215.5F 196.9 -16 3

-18 216.3F 216.3F 196.9 -18 0

-20 217.1F 217.1F 196.9 -20 -4

-22 217.9F 217.9F 196.9 -22 -8

-24 218.7F 218.7F 196.9 -24 -11

-26 219.4F 219.4F 196.9 -26 -15

-28 220.2F 220.2F 196.9 -28 -18

-30 221.0F 221.0F 196.9 -30 -22

-32 221.8F 221.8F 196.9 -32 -26

-34 222.5F 222.5F 196.9 -34 -29

-36 223.3F 223.3F 196.9 -36 -33

-38 224.1F 224.1F 196.9 -38 -36

-40 224.9F 224.9F 196.9 -40 -40



3.66 727-200/JT8D-15 JUN 26, 2012



JUN 26, 2012 727-200/JT8D-15 3.67

15° FLAPS SAN FRANCISCO INTL, CALIF


40 186.7F 186.7F 174.4F 174.4F 191.0 40 104

38 187.5F 187.5F 175.1F 175.1F 193.5 38 100

36 188.3F 188.3F 175.8F 175.8F 196.1 36 97

34 189.0F 189.0F 176.6F 176.6F 196.9 34 93

32 189.8F 189.8F 177.3F 177.3F 196.9 32 90

30 190.5F 190.5F 178.1F 178.1F 196.9 30 86

28 191.3F 191.3F 178.8F 178.8F 196.9 28 82

26 192.1F 192.1F 179.5F 179.5F 196.9 26 79

24 192.8F 192.8F 180.3F 180.3F 196.9 24 75

22 193.6F 193.6F 181.0F 181.0F 196.9 22 72

20 194.4F 194.4F 181.7F 181.7F 196.9 20 68

18 195.1F 195.1F 182.5F 182.5F 196.9 18 64

16 195.9F 195.9F 183.2F 183.2F 196.9 16 61

14 196.7F 196.7F 183.9F 183.9F 196.9 14 57

12 197.4F 197.4F 184.7F 184.7F 196.9 12 54

10 198.2F 198.2F 185.4F 185.4F 196.9 10 50

8 199.0F 199.0F 186.1F 186.1F 196.9 8 46

6 199.7F 199.7F 186.9F 186.9F 196.9 6 43

4 200.5F 200.5F 187.6F 187.6F 196.9 4 39

2 201.2F 201.2F 188.3F 188.3F 196.9 2 36

0 202.0F 202.0F 189.1F 189.1F 196.9 0 32

-2 202.8F 202.8F 189.8F 189.8F 196.9 -2 28

-4 203.5F 203.5F 190.5F 190.5F 196.9 -4 25

-6 204.3F 204.3F 191.3F 191.3F 196.9 -6 21

-8 205.1F 205.1F 192.0F 192.0F 196.9 -8 18

-10 205.8F 205.8F 192.7F 192.7F 196.9 -10 14

-12 206.6F 206.6F 193.5F 193.5F 196.9 -12 10

-14 207.4F 207.4F 194.2F 194.2F 196.9 -14 7

-16 208.1F 208.1F 195.0F 195.0F 196.9 -16 3

-18 208.9F 208.9F 195.7F 195.7F 196.9 -18 0

-20 209.7F 209.7F 196.4F 196.4F 196.9 -20 -4

-22 210.4F 210.4F 197.2F 197.2F 196.9 -22 -8

-24 211.2F 211.2F 197.9F 197.9F 196.9 -24 -11

-26 211.9F 211.9F 198.6F 198.6F 196.9 -26 -15

-28 212.7F 212.7F 199.4F 199.4F 196.9 -28 -18

-30 213.5F 213.5F 200.1F 200.1F 196.9 -30 -22

-32 214.2F 214.2F 200.8F 200.8F 196.9 -32 -26

-34 215.0F 215.0F 201.6F 201.6F 196.9 -34 -29

-36 215.8F 215.8F 202.3F 202.3F 196.9 -36 -33

-38 216.5F 216.5F 203.0F 203.0F 196.9 -38 -36

-40 217.3F 217.3F 203.8F 203.8F 196.9 -40 -40

LENGTH (FT) 9650 9650 7500 7500 LIMITATIONS SLOPE (%) 0.00 0.00 0.00 0.00 RUNWAY LENGTH F LIMITATION OBSTACLE * HEAD ADD 280 280 220 220 BRAKE ENERGY BE TAIL SUB 1160 1160 1190 1190 TIRE SPEED T


3.68 727-200/JT8D-15 JUN 26, 2012

15° FLAPS SAN FRANCISCO INTL, CALIF

ELEVATION 13 OAT ZERO WIND RUNWAY LIMIT (1000 LBS) 2nd OAT OAT °C SEGMENT °C °F 10L 28R 10R 28L LIMIT

40 210.3F 211.1F 202.6F 203.6F 191.0 40 104

38 211.1F 211.9F 203.4F 204.4F 193.5 38 100

36 211.9F 212.7F 204.2F 205.2F 196.1 36 97

34 212.7F 213.5F 205.0F 206.0F 196.9 34 93

32 213.5F 214.3F 205.8F 206.8F 196.9 32 90

30 214.3F 215.1F 206.6F 207.6F 196.9 30 86

28 215.1F 215.9F 207.4F 208.4F 196.9 28 82

26 215.9F 216.7F 208.2F 209.2F 196.9 26 79

24 216.7F 217.5F 209.0F 210.0F 196.9 24 75

22 217.5F 218.3F 209.8F 210.7F 196.9 22 72

20 218.3F 219.1F 210.6F 211.5F 196.9 20 68

18 219.1F 219.9F 211.4F 212.3F 196.9 18 64

16 219.9F 220.7F 212.2F 213.1F 196.9 16 61

14 220.7F 221.5F 213.0F 213.9F 196.9 14 57

12 221.5F 222.3F 213.7F 214.7F 196.9 12 54

10 222.3F 223.1F 214.5F 215.5F 196.9 10 50

8 223.1F 223.9F 215.3F 216.3F 196.9 8 46

6 223.9F 224.7F 216.1F 217.1F 196.9 6 43

4 224.7F 225.5F 216.9F 217.9F 196.9 4 39

2 225.5F 226.3F 217.7F 218.7F 196.9 2 36

0 226.3F 227.1F 218.5F 219.5F 196.9 0 32

-2 227.1F 227.9F 219.3F 220.3F 196.9 -2 28

-4 227.9F 228.7F 220.1F 221.1F 196.9 -4 25

-6 228.7F 229.5F 220.9F 221.9F 196.9 -6 21

-8 229.5F 230.3F 221.7F 222.7F 196.9 -8 18

-10 230.3F 231.1F 222.5F 223.4F 196.9 -10 14

-12 231.1F 231.9F 223.3F 224.2F 196.9 -12 10

-14 231.9F 232.7F 224.1F 225.0F 196.9 -14 7

-16 232.7F 233.4F 224.8F 225.8F 196.9 -16 3

-18 233.4F 234.2F 225.6F 226.6F 196.9 -18 0

-20 234.2F 235.0F 226.4F 227.4F 196.9 -20 -4

-22 235.0F 235.8F 227.2F 228.2F 196.9 -22 -8

-24 235.8F 236.6F 228.0F 229.0F 196.9 -24 -11

-26 236.6F 237.4F 228.8F 229.8F 196.9 -26 -15

-28 237.4F 238.2F 229.6F 230.6F 196.9 -28 -18

-30 238.2F 239.0F 230.4F 231.4F 196.9 -30 -22

-32 239.0F 239.8F 231.2F 232.2F 196.9 -32 -26

-34 239.8F 240.6F 232.0F 233.0F 196.9 -34 -29

-36 240.6F 241.4F 232.8F 233.8F 196.9 -36 -33

-38 241.4F 242.2F 233.6F 234.6F 196.9 -38 -36

-40 242.2F 243.0F 234.4F 235.4F 196.9 -40 -40

LENGTH (FT) 11870 11870 10600 10600 LIMITATIONS SLOPE (%) +0.10 -0.10 +0.10 -0.10 RUNWAY LENGTH F LIMITATION OBSTACLE * HEAD ADD 245 235 295 300 BRAKE ENERGY BE TAIL SUB 950 1030 1040 1000 TIRE SPEED T


JUN 26, 2012 727-200/JT8D-15 3.69

15° FLAPS SEATTLE TACOMA, WASH


40 194.4F 187.3F 210.4F 204.8F 188.4 40 104

38 195.2F 188.1F 211.3F 205.6F 190.9 38 100

36 196.1F 188.9F 212.1F 206.5F 193.5 36 97

34 196.9F 189.7F 213.0F 207.3F 195.0 34 93

32 197.7F 190.6F 213.8F 208.2F 195.0 32 90

30 198.6F 191.4F 214.7F 209.0F 195.0 30 86

28 199.4F 192.2F 215.5F 209.9F 195.0 28 82

26 200.2F 193.0F 216.4F 210.7F 195.0 26 79

24 201.1F 193.8F 217.2F 211.6F 195.0 24 75

22 201.9F 194.7F 218.1F 212.4F 195.0 22 72

20 202.7F 195.5F 218.9F 213.3F 195.0 20 68

18 203.6F 196.3F 219.8F 214.1F 195.0 18 64

16 204.4F 197.1F 220.6F 215.0F 195.0 16 61

14 205.2F 197.9F 221.5F 215.8F 195.0 14 57

12 206.1F 198.8F 222.3F 216.7F 195.0 12 54

10 206.9F 199.6F 223.2F 217.5F 195.0 10 50

8 207.8F 200.4F 224.0F 218.4F 195.0 8 46

6 208.6F 201.2F 224.9F 219.2F 195.0 6 43

4 209.4F 202.1F 225.7F 220.1F 195.0 4 39

2 210.3F 202.9F 226.6F 220.9F 195.0 2 36

0 211.1F 203.7F 227.4F 221.8F 195.0 0 32

-2 211.9F 204.5F 228.3F 222.6F 195.0 -2 28

-4 212.8F 205.3F 229.1F 223.5F 195.0 -4 25

-6 213.6F 206.2F 230.0F 224.3F 195.0 -6 21

-8 214.4F 207.0F 230.8F 225.2F 195.0 -8 18

-10 215.3F 207.8F 231.6F 226.0F 195.0 -10 14

-12 216.1F 208.6F 232.5F 226.9F 195.0 -12 10

-14 216.9F 209.4F 233.3F 227.7F 195.0 -14 7

-16 217.8F 210.3F 234.2F 228.6F 195.0 -16 3

-18 218.6F 211.1F 235.0F 229.4F 195.0 -18 0

-20 219.4F 211.9F 235.9F 230.3F 195.0 -20 -4

-22 220.3F 212.7F 236.7F 231.1F 195.0 -22 -8

-24 221.1F 213.5F 237.6F 232.0F 195.0 -24 -11

-26 222.0F 214.4F 238.4F 232.8F 195.0 -26 -15

-28 222.8F 215.2F 239.3F 233.7F 195.0 -28 -18

-30 223.6F 216.0F 240.1F 234.5F 195.0 -30 -22

-32 224.5F 216.8F 241.0F 235.4F 195.0 -32 -26

-34 225.3F 217.7F 241.8F 236.2F 195.0 -34 -29

-36 226.1F 218.5F 242.7F 237.1F 195.0 -36 -33

-38 227.0F 219.3F 243.5F 237.9F 195.0 -38 -36

-40 227.8F 220.1F 244.4F 238.8F 195.0 -40 -40



3.70 727-200/JT8D-15 JUN 26, 2012



JUN 26, 2012 727-200/JT8D-15 3.71

15° FLAPS SPOKANE INTL, WASH


40 177.4F 171.5F 167.6F 166.6F 176.4 40 104

38 178.5F 172.6F 168.6F 167.7F 178.9 38 100

36 179.6F 173.6F 169.6F 168.7F 181.4 36 97

34 180.6F 174.7F 170.7F 169.7F 186.2 34 93

32 181.7F 175.7F 171.7F 170.7F 186.2 32 90

30 182.7F 176.8F 172.7F 171.8F 186.2 30 86

28 183.8F 177.8F 173.8F 172.8F 186.2 28 82

26 184.9F 178.8F 174.8F 173.8F 186.2 26 79

24 185.9F 179.9F 175.8F 174.8F 186.2 24 75

22 187.0F 180.9F 176.9F 175.9F 186.2 22 72

20 188.0F 182.0F 177.9F 176.9F 186.2 20 68

18 189.1F 183.0F 178.9F 177.9F 186.2 18 64

16 190.2F 184.0F 179.9F 178.9F 186.2 16 61

14 191.2F 185.1F 181.0F 180.0F 186.2 14 57

12 192.3F 186.1F 182.0F 181.0F 186.2 12 54

10 193.3F 187.2F 183.0F 182.0F 186.2 10 50

8 194.4F 188.2F 184.1F 183.0F 186.2 8 46

6 195.5F 189.3F 185.1F 184.1F 186.2 6 43

4 196.5F 190.3F 186.1F 185.1F 186.2 4 39

2 197.6F 191.3F 187.1F 186.1F 186.2 2 36

0 198.6F 192.4F 188.2F 187.1F 186.2 0 32

-2 199.7F 193.4F 189.2F 188.2F 186.2 -2 28

-4 200.8F 194.5F 190.2F 189.2F 186.2 -4 25

-6 201.8F 195.5F 191.3F 190.2F 186.2 -6 21

-8 202.9F 196.5F 192.3F 191.2F 186.2 -8 18

-10 203.9F 197.6F 193.3F 192.3F 186.2 -10 14

-12 205.0F 198.6F 194.3F 193.3F 186.2 -12 10

-14 206.0F 199.7F 195.4F 194.3F 186.2 -14 7

-16 207.1F 200.7F 196.4F 195.4F 186.2 -16 3

-18 208.2F 201.8F 197.4F 196.4F 186.2 -18 0

-20 209.2F 202.8F 198.5F 197.4F 186.2 -20 -4

-22 210.3F 203.8F 199.5F 198.4F 186.2 -22 -8

-24 211.3F 204.9F 200.5F 199.5F 186.2 -24 -11

-26 212.4F 205.9F 201.5F 200.5F 186.2 -26 -15

-28 213.5F 207.0F 202.6F 201.5F 186.2 -28 -18

-30 214.5F 208.0F 203.6F 202.5F 186.2 -30 -22

-32 215.6F 209.1F 204.6F 203.6F 186.2 -32 -26

-34 216.6F 210.1F 205.7F 204.6F 186.2 -34 -29

-36 217.7F 211.1F 206.7F 205.6F 186.2 -36 -33

-38 218.8F 212.2F 207.7F 206.6F 186.2 -38 -36

-40 219.8F 213.2F 208.8F 207.7F 186.2 -40 -40



3.72 727-200/JT8D-15 JUN 26, 2012



JUN 26, 2012 727-200/JT8D-15 3.73

15° FLAPS STOCKTON INTL, CALIF

ELEVATION 33 OAT ZERO WIND RUNWAY LIMIT (1000 LBS) 2nd OAT OAT °C SEGMENT °C °F 11L 29R LIMIT

40 202.8F 203.8F 190.8 40 104

38 203.6F 204.6F 193.4 38 100

36 204.4F 205.4F 196.0 36 97

34 205.2F 206.2F 196.8 34 93

32 206.0F 207.0F 196.8 32 90

30 206.8F 207.8F 196.8 30 86

28 207.6F 208.6F 196.8 28 82

26 208.4F 209.4F 196.8 26 79

24 209.2F 210.2F 196.8 24 75

22 210.0F 211.0F 196.8 22 72

20 210.8F 211.8F 196.8 20 68

18 211.6F 212.6F 196.8 18 64

16 212.4F 213.4F 196.8 16 61

14 213.2F 214.2F 196.8 14 57

12 214.0F 214.9F 196.8 12 54

10 214.8F 215.7F 196.8 10 50

8 215.6F 216.5F 196.8 8 46

6 216.4F 217.3F 196.8 6 43

4 217.2F 218.1F 196.8 4 39

2 218.0F 218.9F 196.8 2 36

0 218.8F 219.7F 196.8 0 32

-2 219.6F 220.5F 196.8 -2 28

-4 220.4F 221.3F 196.8 -4 25

-6 221.1F 222.1F 196.8 -6 21

-8 221.9F 222.9F 196.8 -8 18

-10 222.7F 223.7F 196.8 -10 14

-12 223.5F 224.5F 196.8 -12 10

-14 224.3F 225.3F 196.8 -14 7

-16 225.1F 226.1F 196.8 -16 3

-18 225.9F 226.9F 196.8 -18 0

-20 226.7F 227.7F 196.8 -20 -4

-22 227.5F 228.5F 196.8 -22 -8

-24 228.3F 229.3F 196.8 -24 -11

-26 229.1F 230.1F 196.8 -26 -15

-28 229.9F 230.9F 196.8 -28 -18

-30 230.7F 231.7F 196.8 -30 -22

-32 231.5F 232.5F 196.8 -32 -26

-34 232.3F 233.3F 196.8 -34 -29

-36 233.1F 234.1F 196.8 -36 -33

-38 233.9F 234.9F 196.8 -38 -36

-40 234.7F 235.7F 196.8 -40 -40



3.74 727-200/JT8D-15 JUN 26, 2012



JUN 26, 2012 727-200/JT8D-15 3.75

15° FLAPS SAN JOSE INTL, CALIF


40 204.5F 206.3F 204.5F 206.3F 190.7 40 104

38 205.3F 207.1F 205.3F 207.1F 193.2 38 100

36 206.1F 207.9F 206.1F 207.9F 195.8 36 97

34 206.9F 208.7F 206.9F 208.7F 196.7 34 93

32 207.7F 209.5F 207.7F 209.5F 196.7 32 90

30 208.5F 210.3F 208.5F 210.3F 196.7 30 86

28 209.3F 211.1F 209.3F 211.1F 196.7 28 82

26 210.1F 211.9F 210.1F 211.9F 196.7 26 79

24 210.9F 212.7F 210.9F 212.7F 196.7 24 75

22 211.7F 213.5F 211.7F 213.5F 196.7 22 72

20 212.5F 214.3F 212.5F 214.3F 196.7 20 68

18 213.3F 215.1F 213.3F 215.1F 196.7 18 64

16 214.1F 215.9F 214.1F 215.9F 196.7 16 61

14 214.9F 216.7F 214.9F 216.7F 196.7 14 57

12 215.7F 217.5F 215.7F 217.5F 196.7 12 54

10 216.5F 218.3F 216.5F 218.3F 196.7 10 50

8 217.3F 219.1F 217.3F 219.1F 196.7 8 46

6 218.1F 220.0F 218.1F 220.0F 196.7 6 43

4 218.9F 220.8F 218.9F 220.8F 196.7 4 39

2 219.7F 221.6F 219.7F 221.6F 196.7 2 36

0 220.5F 222.4F 220.5F 222.4F 196.7 0 32

-2 221.3F 223.2F 221.3F 223.2F 196.7 -2 28

-4 222.1F 224.0F 222.1F 224.0F 196.7 -4 25

-6 222.9F 224.8F 222.9F 224.8F 196.7 -6 21

-8 223.7F 225.6F 223.7F 225.6F 196.7 -8 18

-10 224.5F 226.4F 224.5F 226.4F 196.7 -10 14

-12 225.3F 227.2F 225.3F 227.2F 196.7 -12 10

-14 226.1F 228.0F 226.1F 228.0F 196.7 -14 7

-16 226.9F 228.8F 226.9F 228.8F 196.7 -16 3

-18 227.7F 229.6F 227.7F 229.6F 196.7 -18 0

-20 228.5F 230.4F 228.5F 230.4F 196.7 -20 -4

-22 229.3F 231.2F 229.3F 231.2F 196.7 -22 -8

-24 230.1F 232.0F 230.1F 232.0F 196.7 -24 -11

-26 230.9F 232.8F 230.9F 232.8F 196.7 -26 -15

-28 231.7F 233.6F 231.7F 233.6F 196.7 -28 -18

-30 232.5F 234.4F 232.5F 234.4F 196.7 -30 -22

-32 233.3F 235.2F 233.3F 235.2F 196.7 -32 -26

-34 234.1F 236.0F 234.1F 236.0F 196.7 -34 -29

-36 234.9F 236.8F 234.9F 236.8F 196.7 -36 -33

-38 235.7F 237.6F 235.7F 237.6F 196.7 -38 -36

-40 236.5F 238.4F 236.5F 238.4F 196.7 -40 -40

LENGTH (FT) 11000 11000 11000 11000 LIMITATIONS SLOPE (%) +0.20 -0.20 +0.20 -0.20 RUNWAY LENGTH F LIMITATION OBSTACLE * HEAD ADD 285 275 285 275 BRAKE ENERGY BE TAIL SUB 1010 980 1010 980 TIRE SPEED T


3.76 727-200/JT8D-15 JUN 26, 2012



JUN 26, 2012 727-200/JT8D-15 3.77

15° FLAPS TUCSON INTL, ARIZ


40 152.0F 152.9F 163.8F 170.6F 185.1F 190.5F 174.8 40 104

38 153.0F 153.9F 164.9F 171.7F 186.2F 191.7F 177.3 38 100

36 154.0F 154.9F 165.9F 172.7F 187.4F 192.8F 179.8 36 97

34 155.0F 155.9F 167.0F 173.8F 188.5F 193.9F 184.9 34 93

32 156.0F 156.9F 168.0F 174.9F 189.6F 195.0F 184.9 32 90

30 157.1F 157.9F 169.1F 176.0F 190.7F 196.1F 184.9 30 86

28 158.1F 158.9F 170.1F 177.0F 191.8F 197.3F 184.9 28 82

26 159.1F 160.0F 171.2F 178.1F 192.9F 198.4F 184.9 26 79

24 160.1F 161.0F 172.2F 179.2F 194.0F 199.5F 184.9 24 75

22 161.1F 162.0F 173.3F 180.3F 195.1F 200.6F 184.9 22 72

20 162.1F 163.0F 174.4F 181.3F 196.3F 201.7F 184.9 20 68

18 163.1F 164.0F 175.4F 182.4F 197.4F 202.9F 184.9 18 64

16 164.1F 165.0F 176.5F 183.5F 198.5F 204.0F 184.9 16 61

14 165.1F 166.0F 177.5F 184.6F 199.6F 205.1F 184.9 14 57

12 166.1F 167.0F 178.6F 185.6F 200.7F 206.2F 184.9 12 54

10 167.1F 168.0F 179.6F 186.7F 201.8F 207.3F 184.9 10 50

8 168.1F 169.1F 180.7F 187.8F 202.9F 208.5F 184.9 8 46

6 169.1F 170.1F 181.7F 188.9F 204.1F 209.6F 184.9 6 43

4 170.2F 171.1F 182.8F 189.9F 205.2F 210.7F 184.9 4 39

2 171.2F 172.1F 183.8F 191.0F 206.3F 211.8F 184.9 2 36

0 172.2F 173.1F 184.9F 192.1F 207.4F 212.9F 184.9 0 32

-2 173.2F 174.1F 185.9F 193.2F 208.5F 214.1F 184.9 -2 28

-4 174.2F 175.1F 187.0F 194.3F 209.6F 215.2F 184.9 -4 25

-6 175.2F 176.1F 188.0F 195.3F 210.7F 216.3F 184.9 -6 21

-8 176.2F 177.1F 189.1F 196.4F 211.8F 217.4F 184.9 -8 18

-10 177.2F 178.2F 190.1F 197.5F 213.0F 218.6F 184.9 -10 14

-12 178.2F 179.2F 191.2F 198.6F 214.1F 219.7F 184.9 -12 10

-14 179.2F 180.2F 192.2F 199.6F 215.2F 220.8F 184.9 -14 7

-16 180.2F 181.2F 193.3F 200.7F 216.3F 221.9F 184.9 -16 3

-18 181.2F 182.2F 194.4F 201.8F 217.4F 223.0F 184.9 -18 0

-20 182.2F 183.2F 195.4F 202.9F 218.5F 224.2F 184.9 -20 -4

-22 183.3F 184.2F 196.5F 203.9F 219.6F 225.3F 184.9 -22 -8

-24 184.3F 185.2F 197.5F 205.0F 220.8F 226.4F 184.9 -24 -11

-26 185.3F 186.2F 198.6F 206.1F 221.9F 227.5F 184.9 -26 -15

-28 186.3F 187.3F 199.6F 207.2F 223.0F 228.6F 184.9 -28 -18

-30 187.3F 188.3F 200.7F 208.2F 224.1F 229.8F 184.9 -30 -22

-32 188.3F 189.3F 201.7F 209.3F 225.2F 230.9F 184.9 -32 -26

-34 189.3F 190.3F 202.8F 210.4F 226.3F 232.0F 184.9 -34 -29

-36 190.3F 191.3F 203.8F 211.5F 227.4F 233.1F 184.9 -36 -33

-38 191.3F 192.3F 204.9F 212.5F 228.6F 234.2F 184.9 -38 -36

-40 192.3F 193.3F 205.9F 213.6F 229.7F 235.4F 184.9 -40 -40

LENGTH (FT) 7000 7000 8400 8400 11000 11000 LIMITATIONS SLOPE (%) +0.10 -0.10 +0.70 -0.70 +0.60 -0.60 RUNWAY LENGTH F LIMITATION OBSTACLE * HEAD ADD 170 175 240 270 290 270 BRAKE ENERGY BE TAIL SUB 1100 1120 1110 1100 1000 920 TIRE SPEED T


3.78 727-200/JT8D-15 JUN 26, 2012



JUN 26, 2012 727-200/JT8D-15 3.79

15° FLAPS YAKIMA AIR TERMINAL, WASH


40 162.2F 155.7F 174.8 40 104

38 163.2F 156.7F 177.3 38 100

36 164.3F 157.8F 179.8 36 97

34 165.3F 158.8F 184.9 34 93

32 166.3F 159.8F 184.9 32 90

30 167.4F 160.8F 184.9 30 86

28 168.4F 161.8F 184.9 28 82

26 169.5F 162.9F 184.9 26 79

24 170.5F 163.9F 184.9 24 75

22 171.6F 164.9F 184.9 22 72

20 172.6F 165.9F 184.9 20 68

18 173.7F 167.0F 184.9 18 64

16 174.7F 168.0F 184.9 16 61

14 175.8F 169.0F 184.9 14 57

12 176.8F 170.0F 184.9 12 54

10 177.9F 171.0F 184.9 10 50

8 178.9F 172.1F 184.9 8 46

6 180.0F 173.1F 184.9 6 43

4 181.0F 174.1F 184.9 4 39

2 182.0F 175.1F 184.9 2 36

0 183.1F 176.2F 184.9 0 32

-2 184.1F 177.2F 184.9 -2 28

-4 185.2F 178.2F 184.9 -4 25

-6 186.2F 179.2F 184.9 -6 21

-8 187.3F 180.3F 184.9 -8 18

-10 188.3F 181.3F 184.9 -10 14

-12 189.4F 182.3F 184.9 -12 10

-14 190.4F 183.3F 184.9 -14 7

-16 191.5F 184.3F 184.9 -16 3

-18 192.5F 185.4F 184.9 -18 0

-20 193.6F 186.4F 184.9 -20 -4

-22 194.6F 187.4F 184.9 -22 -8

-24 195.7F 188.4F 184.9 -24 -11

-26 196.7F 189.5F 184.9 -26 -15

-28 197.7F 190.5F 184.9 -28 -18

-30 198.8F 191.5F 184.9 -30 -22

-32 199.8F 192.5F 184.9 -32 -26

-34 200.9F 193.5F 184.9 -34 -29

-36 201.9F 194.6F 184.9 -36 -33

-38 203.0F 195.6F 184.9 -38 -36

-40 204.0F 196.6F 184.9 -40 -40



3.80 727-200/JT8D-15 JUN 26, 2012


Boeing 727-200 ENROUTE Performance Manual

JUN 26, 2012 727-200/JT8D-15 4.1

CHAPTER 4 - ENROUTE

4.1 CLIMB PERFORMANCE .............................................. 3 4.1.1 Maximum Climb EPR .......................................... 3 4.1.2 Economic Climb Speeds ...................................... 3 4.1.3 Distance, Time and Fuel .................................... 4

4.2 ALL ENGINE CRUISE .............................................. 5 4.2.1 Maximum Cruise EPR ......................................... 5 4.2.2 Cruise EPR and Specific Range .............................. 5 4.2.3 Turbulent Air Penetration .................................. 7

4.3 ENGINE OUT PERFORMANCE ......................................... 8 4.3.1 Maximum Continuous EPR ..................................... 8 4.3.2 One Engine Out.............................................. 9 4.3.3 Two Engine Out............................................. 10

4.4 HOLDING ....................................................... 11 4.5 DESCENT ....................................................... 12 4.6 ENGINE PARAMETER CHECK TABLES ................................. 13

ENROUTE Boeing 727-200 Performance Manual

4.2 727-200/JT8D-15 JUN 26, 2012



JUN 26, 2012 727-200/JT8D-15 4.3

4.1 CLIMB PERFORMANCE

4.1.1 Maximum Climb EPR

MAXIMUM CLIMB EPR Pressure TAT °C

Altitude ENG -40 -35 -30 -25 -20 -15 -10 -5 0 5 10 15 20 25 30 35 40 45 50

S.L. 1 & 3 2.07 2.07 2.07 2.07 2.07 2.07 2.07 2.07 2.07 2.03 1.97 1.93 1.88 1.84 1.79 1.75 1.72 1.68 1.64

2 2.09 2.09 2.09 2.09 2.09 2.09 2.09 2.09 2.09 2.05 2.00 1.95 1.90 1.86 1.82 1.78 1.74 1.70 1.67

1000 1 & 3 2.13 2.13 2.13 2.13 2.13 2.13 2.13 2.13 2.08 2.03 1.97 1.93 1.88 1.84 1.79 1.75 1.72 1.68 1.64

2 2.15 2.15 2.15 2.15 2.15 2.15 2.15 2.15 2.11 2.05 2.00 1.95 1.90 1.86 1.82 1.78 1.74 1.70 1.67

2000 1 & 3 2.19 2.19 2.19 2.19 2.19 2.19 2.18 2.13 2.08 2.03 1.97 1.93 1.88 1.84 1.79 1.75 1.72 1.68 1.64

2 2.21 2.21 2.21 2.21 2.21 2.21 2.20 2.16 2.11 2.05 2.00 1.95 1.90 1.86 1.82 1.78 1.74 1.70 1.67

3000 1 & 3 2.24 2.24 2.24 2.24 2.23 2.21 2.17 2.13 2.08 2.02 1.97 1.92 1.88 1.83 1.79 1.75 1.71 1.67 1.63

2 2.26 2.26 2.26 2.26 2.26 2.23 2.20 2.16 2.11 2.05 2.00 1.95 1.90 1.86 1.82 1.78 1.74 1.70 1.67

3900 to 1 & 3 2.29 2.28 2.27 2.25 2.23 2.20 2.17 2.13 2.08 2.02 1.97 1.92 1.87 1.83 1.79 1.75 1.71 1.67 1.63

5000 2 2.32 2.31 2.29 2.28 2.26 2.23 2.20 2.16 2.11 2.05 2.00 1.95 1.90 1.86 1.82 1.78 1.74 1.70 1.67

10000 1 & 3 2.28 2.27 2.26 2.24 2.22 2.20 2.16 2.12 2.07 2.01 1.96 1.91 1.86 1.82 1.78 1.74 1.70 1.66 1.62

2 2.32 2.31 2.29 2.28 2.26 2.23 2.20 2.16 2.11 2.05 2.00 1.95 1.90 1.86 1.82 1.78 1.74 1.70 1.67

20000 1 & 3 2.27 2.26 2.24 2.23 2.21 2.18 2.15 2.10 2.05 2.00 1.94 1.90 1.85 1.81 1.76 1.72 1.69 1.65 1.61

2 2.32 2.31 2.29 2.28 2.26 2.23 2.20 2.16 2.11 2.05 2.00 1.95 1.90 1.86 1.82 1.78 1.74 1.70 1.67

30000 1 & 3 2.25 2.24 2.23 2.21 2.19 2.17 2.13 2.09 2.04 1.98 1.93 1.88 1.83 1.79 1.75 1.71 1.67 1.63 1.59

2 2.32 2.31 2.29 2.28 2.26 2.23 2.20 2.16 2.11 2.05 2.00 1.95 1.90 1.86 1.82 1.78 1.74 1.70 1.67

40000 & 1 & 3 2.23 2.22 2.20 2.19 2.17 2.14 2.11 2.06 2.01 1.96 1.90 1.86 1.81 1.77 1.72 1.68 1.65 1.61 1.57

ABOVE 2 2.32 2.31 2.29 2.28 2.26 2.23 2.20 2.16 2.11 2.05 2.00 1.95 1.90 1.86 1.82 1.78 1.74 1.70 1.67

EPR BLEED CORRECTIONS ENG 1 & 3 ENG 2 S.L. OFF + .04 ON - .04

10000 FT OFF + .05 ON - .05 20000 FT OFF + .07 ON - .07 30000 FT OFF + .08 ON - .08

AIR CONDITIONING

AIR BLEED 40000 FT OFF + .11 ON - .10

ENGINE ANTI-ICE ON - .08 - .12 TWO ENG BLEEDS - .17 ENG AND WING

ANTI-ICE ONE ENG BLEED - .17 - .12

4.1.2 Economic Climb Speeds Economic climb speeds are presented as a function of gross weight.

Gross Speed Weight knots

lb IAS 120000 280 130000 285 140000 290 150000 295 160000 300 170000 305 180000 310 190000 315 200000 320 210000 325


4.4 727-200/JT8D-15 JUN 26, 2012

4.1.3 Distance, Time and Fuel Distance, time, and fuel for climb are shown for a 250/300/.78M climb speed schedule. Enter the table with top of climb flight level and read distance, time, and fuel required. Based on: 250 / 300 / M.78 Climb

FL Distance Time Fuel NM min lbs

90 33 7 2646 110 54 8 3086 130 63 9 3417 150 72 10 3858 170 89 12 4299 190 99 13 4519 210 110 14 4960 230 126 16 5512 250 141 18 5952 270 155 20 6393 290 169 22 6834 310 191 25 7496 330 227 30 8488 350 263 35 9149 370 238 32 7937 390 224 30 7385


JUN 26, 2012 727-200/JT8D-15 4.5

4.2 ALL ENGINE CRUISE

4.2.1 Maximum Cruise EPR

MAXIMUM CRUISE EPR TAT °C FL

ENG

-50 -45 -40 -35 -30 -25 -20 -15 -10 -5 0 5 10 15 20 25 30 35 40 45

50 2.24 2.23 2.22 2.21 2.20 2.18 2.15 2.13 2.09 2.04 1.99 1.93 1.87 1.80 1.75 1.70 1.65 1.61 1.57 1.53

100 2.24 2.23 2.22 2.20 2.19 2.18 2.16 2.13 2.09 2.04 1.99 1.93 1.86 1.80 1.74 1.69 1.65 1.60 1.56 1.52

200 2.23 2.22 2.21 2.19 2.18 2.17 2.14 2.12 2.08 2.03 1.98 1.92 1.85 1.79 1.73 1.68 1.64 1.59 1.55 1.51

300 2.22 2.21 2.00 2.18 2.17 2.16 2.13 2.10 2.07 2.02 1.97 1.91 1.84 1.78 1.72 1.67 1.63 1.58 1.54 1.50

400 2.19 2.18 2.17 2.16 2.15 2.13 2.11 2.08 2.04 2.00 1.94 1.89 1.82 1.76 1.70 1.65 1.60 1.56 1.52 1.48

420

1&3

2.19 2.18 2.17 2.16 2.14 2.13 2.11 2.08 2.04 1.99 1.94 1.88 1.82 1.75 1.69 1.64 1.60 1.56 1.52 1.48

50

420 2 2.25 2.24 2.23 2.22 2.21 2.19 2.17 2.14 2.10 2.06 2.01 1.95 1.89 1.82 1.76 1.72 1.67 1.63 1.59 1.55

EPR BLEED CORRECTIONS Flight Level

ENG 1 & 3 ENG 2

050 OFF + .03 ON - .03 100 OFF + .04 ON - .04 200 OFF + .05 ON - .05 300 OFF + .06 ON - .06 400 OFF + .08 ON - .07

Air Conditioning

Air Bleed

420 OFF + .08 ON - .07 Engine Anti-Ice ON - .08 - .11

TWO ENG BLEEDS - .16 ENG and Wing Anti-Ice ONE ENG BLEED - .16

-. 11

4.2.2 Cruise EPR and Specific Range The table presents the required EPR and the Specific Range (SR) as a function of gross weight and flight level. Fuel Flow (FF) can be calculated from the Specific Range (SR) by the following equation:

x1000SR

TASFF

To convert Nautical Miles (NM) into Nautical Air Miles (NAM) use the following equation, where GS is the Ground Speed:

GSTASNMNAM

TRUE AIRSPEED TABLE

M = 0.78 M = .80 OAT °C TAS KTS TAS KTS

-15 488 501 -20 484 496 -25 479 491 -30 474 486 -35 469 481 -40 464 476 -45 459 471 -50 454 466 -55 449 460 -60 444 455 -65 438 450 -70 433 444


4.6 727-200/JT8D-15 JUN 26, 2012

EPR required Specific Range NAM/1000lbs

CRUISE EPR required 250/350/M.78

Press STD STD STD Alt TAS IAS SAT TAT M

GROSS WEIGHT - 1000 LBS

-1000 KTS KTS °C °C 175 170 165 160 155 150 145 140 135 130 125 120 115 110 FT

2.09 2.04 1.99 1.95 1.91 1.88 39 447 241 -57 -31 .78

58.5 61.4 64.3 67.1 69.9 72.6 2.11 2.06 2.01 1.97 1.93 1.90 1.87 1.84 1.82

37 447 252 -57 -31 .78 52.4 54.9 57.3 59.6 61.9 64.2 66.4 68.6 70.7 2.11 2.06 2.02 1.98 1.95 1.91 1.89 1.86 1.83 1.81 1.79 1.77

35 450 264 -54 -27 .78 47.7 49.7 51.7 53.6 55.5 57.4 59.3 61.1 62.9 64.6 66.3 68.0

2.06 2.02 1.98 1.95 1.92 1.89 1.87 1.85 1.82 1.80 1.79 1.77 1.75 1.74 33 454 277 -50 -23 .78

45.5 47.1 48.7 50.3 51.9 53.4 54.9 56.4 57.9 59.3 60.7 62.1 63.4 64.8 1.95 1.92 1.90 1.87 1.85 1.83 1.81 1.79 1.78 1.76 1.75 1.73 1.72 1.71

31 458 289 -46 -18 .78 46.0 47.3 48.6 49.9 51.1 52.3 53.5 54.7 55.8 57.0 58.1 59.2 60.3 61.3 1.87 1.85 1.83 1.82 1.80 1.78 1.77 1.76 1.74 1.73 1.72 1.71 1.69 1.68

29 462 302 -42 -14 .78 45.6 46.6 47.6 48.6 49.6 50.6 51.5 52.5 53.4 54.3 55.2 56.1 56.9 57.8 1.82 1.80 1.79 1.77 1.76 1.75 1.74 1.72 1.71 1.70 1.69 1.68 1.67 1.66

27 466 315 -38 -9 .78 44.4 45.3 46.1 46.9 47.7 48.4 49.2 50.0 50.7 51.4 52.2 52.9 53.6 54.2 1.77 1.76 1.75 1.75 1.73 1.72 1.71 1.70 1.69 1.68 1.67 1.66 1.66 1.65

25 470 329 -35 -6 .78 42.9 43.6 44.2 44.9 45.4 46.1 46.7 47.3 47.9 48.5 49.1 49.7 50.2 50.8 1.74 1.73 1.72 1.71 1.70 1.69 1.69 1.68 1.67 1.66 1.66 1.65 1.64 1.63

23 474 342 -31 -2 .78 41.1 41.6 42.1 42.7 43.2 43.7 44.2 44.7 45.2 45.6 46.1 46.6 47.0 47.5 1.70 1.69 1.68 1.67 1.67 1.66 1.65 1.64 1.64 1.63 1.62 1.62 1.61 1.60

21 470 350 -27 1 .76 41.1 41.5 41.9 42.3 42.7 43.1 43.5 43.9 44.3 44.6 45.0 45.4 45.7 46.1 1.65 1.65 1.64 1.63 1.62 1.61 1.61 1.60 1.59 1.59 1.58 1.58 1.57 1.56

19 456 350 -23 2 .71 39.9 40.2 40.6 41.0 41.3 41.7 42.0 42.3 42.7 43.0 43.3 43.7 44.0 44.3 1.61 1.61 1.60 1.59 1.58 1.58 1.57 1.56 1.56 1.55 1.55 1.54 1.53 1.53

17 444 350 -19 7 .71 38.4 38.8 39.2 39.5 39.9 40.1 40.5 40.9 41.2 41.5 41.8 42.1 42.4 42.7 1.57 1.57 1.56 1.55 1.55 1.54 1.53 1.53 1.52 1.52 1.51 1.50 1.50 1.49

15 431 350 -15 9 .68 37.1 37.4 37.8 38.1 38.4 38.7 39.0 39.3 39.6 39.9 40.2 40.5 40.7 41.0 1.53 1.53 1.52 1.51 1.51 1.50 1.50 1.49 1.49 1.48 1.48 1.47 1.47 1.46

13 419 350 -11 12 .66 35.7 36.0 36.3 36.6 36.9 37.2 37.5 37.7 38.0 38.3 38.5 38.8 39.1 39.3 1.49 1.49 1.48 1.48 1.47 1.47 1.46 1.46 1.45 1.45 1.44 1.44 1.43 1.43

11 407 350 -7 15 .64 34.3 34.6 34.1 35.2 35.4 35.7 36.0 36.2 36.5 36.7 37.0 37.2 37.4 37.7 1.38 1.37 1.36 1.35 1.34 1.33 1.31 1.30 1.29 1.28 1.28 1.27 1.26 1.25

9 285 250 -3 7 .44 38.7 39.2 39.7 40.2 40.7 41.1 41.6 42.0 42.5 43.0 43.3 43.8 44.3 44.7 1.36 1.35 1.33 1.31 1.31 1.30 1.29 1.28 1.27 1.26 1.25 1.24 1.23 1.22

7 276 250 1 11 .43 36.8 37.2 37.7 38.1 38.6 39.0 39.5 39.9 40.3 40.7 41.2 41.6 42.0 42.4 1.33 1.32 1.31 1.30 1.29 1.28 1.27 1.26 1.25 1.24 1.23 1.22 1.21 1.20

5 268 250 5 14 .41 35.0 35.4 35.9 36.3 36.7 37.1 37.5 37.9 38.3 38.7 39.1 39.5 39.9 40.2 1.30 1.29 1.28 1.27 1.26 1.25 1.24 1.23 1.22 1.21 1.21 1.20 1.19 1.18

3 261 250 6 15 .40 33.4 33.8 34.2 34.5 34.9 35.3 35.7 36.1 36.4 36.8 37.2 37.5 37.9 38.2

Notes: - A/C bleed from pod engines "ON" - No bleed from center engine - Shaded area indicates optimum altitude


JUN 26, 2012 727-200/JT8D-15 4.7

4.2.3 Turbulent Air Penetration

Gross Weight – 1000 pounds 175 170 165 160 155 150 145 Target Speed

IAS/Mach Flight Level Nominal N1 % 390 93 92 350 95 93 91 88 88 86 85 310 88 88 86 84 84 82 81 270 84 85 82 81 81 80 79 200 80 83 78 77 77 76 75

280/.80

100 75 76 74 74 74 73 72


4.8 727-200/JT8D-15 JUN 26, 2012

4.3 ENGINE OUT PERFORMANCE

4.3.1 Maximum Continuous EPR

PRESS MAXIMUM CONTINUOUS EPR ALT TAT °C

FT ENG -40 -35 -30 -25 -20 -15 -10 -5 0 5 10 15 20 25 30 35 40 45 50

1 & 3 2.07 2.07 2.07 2.07 2.07 2.07 2.07 2.07 2.07 2.03 1.98 1.93 1.88 1.84 1.84 1.84 1.84 1.80 1.75 S.L.

2 2.09 2.09 2.09 2.09 2.09 2.09 2.09 2.09 2.09 2.05 2.00 1.95 1.91 1.87 1.86 1.86 1.86 1.83 1.78

1 & 3 2.13 2.13 2.13 2.13 2.13 2.13 2.13 2.13 2.09 2.03 1.98 1.93 1.88 1.84 1.84 1.84 1.84 1.80 1.75 1000

2 2.15 2.15 2.15 2.15 2.15 2.15 2.15 2.15 2.11 2.05 2.00 1.95 1.91 1.87 1.86 1.86 1.86 1.83 1.78

1 & 3 2.16 2.16 2.16 2.16 2.16 2.16 2.16 2.14 2.09 2.03 1.98 1.93 1.88 1.84 1.84 1.84 1.84 1.80 1.75 1499

2 2.17 2.17 2.17 2.17 2.17 2.17 2.17 2.16 2.11 2.05 2.00 1.95 1.91 1.87 1.86 1.86 1.86 1.83 1.78

1 & 3 2.16 2.16 2.16 2.16 2.16 2.16 2.16 2.16 2.16 2.16 2.14 2.10 2.05 2.01 1.96 1.91 1.86 1.80 1.75 1500

2 2.17 2.17 2.17 2.17 2.17 2.17 2.17 2.17 2.17 2.17 2.16 2.12 2.07 2.03 1.98 1.93 1.88 1.83 1.78

1 & 3 2.19 2.19 2.19 2.19 2.19 2.19 2.19 2.19 2.19 2.17 2.14 2.10 2.06 2.01 1.96 1.91 1.86 1.80 1.75 2000

2 2.20 2.20 2.20 2.20 2.20 2.20 2.20 2.20 2.20 2.19 2.16 2.12 2.07 2.03 1.98 1.93 1.88 1.83 1.78

1 & 3 2.24 2.24 2.24 2.24 2.24 2.24 2.24 2.23 2.20 2.17 2.13 2.09 2.05 2.00 1.95 1.90 1.85 1.80 1.75 3000

2 2.27 2.27 2.27 2.27 2.27 2.27 2.27 2.25 2.22 2.19 2.16 2.12 2.07 2.03 1.98 1.93 1.88 1.83 1.78

1 & 3 2.30 2.30 2.30 2.30 2.30 2.28 2.25 2.23 2.20 2.17 2.13 2.09 2.05 2.00 1.95 1.90 1.85 1.80 1.74 3900 TO

5000 2 2.32 2.32 2.32 2.32 2.32 2.30 2.28 2.25 2.22 2.19 2.16 2.12 2.07 2.03 1.98 1.93 1.88 1.83 1.78

1 & 3 2.29 2.29 2.29 2.29 2.29 2.27 2.25 2.22 2.19 2.16 2.12 2.08 2.04 1.99 1.94 1.89 1.84 1.79 1.74 10000

2 2.32 2.32 2.32 2.32 2.32 2.30 2.28 2.25 2.22 2.19 2.16 2.12 2.07 2.03 1.98 1.93 1.88 1.83 1.78

1 & 3 2.27 2.27 2.27 2.27 2.27 2.25 2.23 2.21 2.18 2.14 2.11 2.07 2.02 1.98 1.93 1.88 1.83 1.77 1.72 20000

2 2.32 2.32 2.32 2.32 2.32 2.30 2.28 2.25 2.22 2.19 2.16 2.12 2.07 2.03 1.98 1.93 1.88 1.83 1.78

1 & 3 2.26 2.26 2.26 2.26 2.26 2.24 2.22 2.19 2.16 2.13 2.09 2.05 2.01 1.96 1.91 1.86 1.81 1.76 1.71 30000

2 2.32 2.32 2.32 2.32 2.32 2.30 2.28 2.25 2.22 2.19 2.16 2.12 2.07 2.03 1.98 1.93 1.88 1.83 1.78

1 & 3 2.24 2.24 2.24 2.24 2.24 2.22 2.19 2.17 2.14 2.11 2.07 2.03 1.98 1.94 1.89 1.84 1.79 1.74 1.68 40000

2 2.32 2.32 2.32 2.32 2.32 2.30 2.28 2.25 2.22 2.19 2.16 2.12 2.07 2.03 1.98 1.93 1.88 1.83 1.78

1 & 3 2.23 2.23 2.23 2.23 2.23 2.21 2.19 2.16 2.13 2.10 2.06 2.02 1.98 1.93 1.88 1.83 1.78 1.73 1.68 42000

2 2.32 2.32 2.32 2.32 2.32 2.30 2.28 2.25 2.22 2.19 2.16 2.12 2.07 2.03 1.98 1.93 1.88 1.83 1.78

EPR BLEED CORRECTIONS ENG 1 &3 ENG 2

S.L. OFF + .04 ON - .04

10000 FT OFF + .05 ON - .05

20000 FT OFF + .07 ON - .07

30000 FT OFF + .08 ON - .08

40000 FT OFF + .10 ON - .09

AIR CONDITIONING AIR BLEED

42000 Ft OFF + .11 ON - .09

ENGINE ANTI-ICE ON - .08 - .12

TWO BLEEDS - .17 END AND WING ANTI-ICE

ONE BLEED - .17 - .12

MOD 'A' INLET - + .01


JUN 26, 2012 727-200/JT8D-15 4.9

4.3.2 One Engine Out The table shows maximum altitude that can be maintained at a given weight and air temperature, based on long range cruise speed and maximum continuous thrust. In some cases following engine failure, a descent to a lower altitude and reduction in airspeed may be necessary. In these circumstances, a driftdown procedure should be adopted in order to minimize the loss in specific range. The turbulent air penetration speed schedule is recommended. For driftdown following engine failure, set up maximum continuous thrust and establish a speed schedule of 280 KIAS or M = .80, whichever is lower.

Altitude Capability One Engine Inop

Gross Weight Pressure Altitude - Feet

1000 lbs ISA-10°C ISA ISA+10°C ISA+20°C 200 21423 19995 16783 12158 190 22932 21684 18779 14551 180 24440 23374 20775 16943 170 25948 25063 22771 19336 160 27456 26753 24767 21729 150 28964 28443 26763 24122 140 30473 30132 28758 26514 130 31981 31822 30754 28907 120 33300 33512 32750 31300


4.10 727-200/JT8D-15 JUN 26, 2012

4.3.3 Two Engine Out After failure of the second engine, set maximum continuous limit EPR and allow the airplane to descent at the airspeed shown in the driftdown table. The airplane should level off at approximately the altitude and weight shown in the table. EPR must be checked frequently during the driftdown to ensure that the maximum continuous limit EPR is not exceeded. When the airplane has leveled off, constant altitude should be maintained. This will allow the airplane to slowly accelerate to the optimum range speed as weight reduces due to fuel burnoff. When the optimum range speed shown in the climbing cruise table is achieved, the airplane should follow a climbing cruise procedure, flying at the airspeed appropriate to the gross weight. The pressure altitudes achievable under these weight and speed conditions are shown in the table.

Climbing Cruise

Gross Optimum ISA Deviation °C Weight Range -10 0 10 20 LBS 1000 Speed KIAS Pressure Altitude - Feet 110 216 17553 16758 15468 13180 120 225 15249 14218 12497 9612 130 234 12944 11678 9526 6043 140 242 10640 9138 6555 2475 150 251 8336 6598 3584 160 260 6032 4058 170 269 3727 1518

Driftdown

Gross Weight LBS 1000 Driftdown Leveloff Press Alt - Feet

Start Approx Speed ISA Deviation °C Driftdown Level-Off KIAS -10 0 10 20

120 115 205 17539 16482 15014 12816 130 124 213 15634 14382 12510 9795 140 133 220 13728 12282 10006 6774 150 142 228 11823 10182 7502 3753 160 151 236 9918 8082 4998 732 170 160 244 8013 5981 2494 180 169 251 6108 3881 190 178 259 4203 1781


JUN 26, 2012 727-200/JT8D-15 4.11

4.4 HOLDING Target EPR and fuel flow per engine information is tabulated for holding with flaps up based on the minimum drag airspeed. Enter the table with weight and pressure altitude to read EPR and fuel flow per engine. All engines 2 airbleeds fuel flow based on ISA adjust fuel flow +1% per +5°C ISA deviation Minimum Drag Airspeed (200 KTS Lower Limit) Press Altitude Gross Weight - 1000 pounds

feet 160 150 140 130 120 110 ISA °C 40000 2200 2200 -57 2.02 2.00 35000 2530 2490 2300 2120 2120 -54 1.95 1.93 1.91 1.82 1.80 30000 2800 2510 2470 2280 2120 2120 -44 1.84 1.77 1.75 1.70 1.65 1.60 25000 2755 2558 2490 2240 2200 2200 -35 1.68 1.61 1.57 1.53 1.51 1.48 20000 2840 2670 2580 2270 2300 2300 -25 1.56 1.49 1.46 1.43 1.40 1.38 15000 2910 2780 2670 2310 2380 2380 -15 1.43 1.39 1.36 1.33 1.32 1.29 10000 3040 2850 2740 2460 2520 2520 -5 1.33 1.31 1.29 1.27 1.25 1.23 5000 3130 2960 2830 2510 2580 2580 5 1.27 1.24 1.22 1.21 1.20 1.19 1500 3200 3020 2010 2600 2670 2670 12 1.23 1.21 1.18 1.18 1.18 1.17

FF PER ENG – LB/HR EPR


4.12 727-200/JT8D-15 JUN 26, 2012

4.5 DESCENT Distance and time for descent are shown for a .78M/280 KIAS descent speed schedule. Enter the table with top of descent pressure altitude and read distance in nautical miles and time in minutes.

.78M / 280 knot descent Based on: - Idle power on all engines throughout descent down to initial approach configuration - Cruise Mach 0.78 to to crossover then 350 knots to 10000 feet - 250 knots or less below 10000 feet - Clean configuraton above 2000 feet - Add 120 pounds fuel burn for each minute of terminal area maneuvering Press. Distance Time Fuel Altitude NM min lbs feet 41000 133 23.6 1711 39000 127 22.8 1684 37000 121 22.1 1654 35000 115 21.3 1622 33000 109 20.6 1588 31000 104 19.9 1552 29000 98 19.2 1513 27000 93 18.6 1474 25000 88 18.0 1436 23000 83 17.4 1399 21000 78 16.7 1355 19000 72 16.0 1308 17000 66 15.2 1259 15000 60 14.4 1210 13000 54 13.7 1162 11000 49 12.9 1112 9000 36 10.6 1019 7000 30 9.4 974 5000 25 8.2 924 3000 18 6.5 848


JUN 26, 2012 727-200/JT8D-15 4.13

4.6 ENGINE PARAMETER CHECK TABLES

Engine Parameter Check

N1, N2, EGT versus EPR Pod Engines

TAT - °C -40 -30 -20 -10 0 10 20 30 40

EPR

N1 % 72.7 74.2 75.7 77.2 78.6 80.1 81.5 82.9 84.2 N2 % 77.2 78.8 80.4 82.0 83.5 85.0 86.5 88.0 89.4 1.55 EGT °C 308 333 358 383 407 432 457 482 507 N1 % 74.0 75.6 77.1 78.6 80.1 81.5 83.0 84.4 85.7 N2 % 77.8 79.5 81.1 82.7 84.2 85.8 87.3 88.7 90.2 1.60 EGT °C 308 333 358 383 408 433 458 483 508 N1 % 75.2 76.8 78.4 79.9 81.4 82.9 84.3 85.8 87.2 N2 % 78.4 80.1 81.7 83.3 84.9 86.5 88.0 89.5 90.9 1.65 EGT °C 309 334 359 384 409 434 459 484 508 N1 % 76.4 78.0 79.6 81.1 82.7 84.2 85.6 87.1 88.5 N2 % 79.1 80.8 82.4 84.0 85.6 87.1 88.7 90.2 91.6 1.70 EGT °C 309 334 359 384 409 434 459 484 509 N1 % 77.5 79.1 80.8 82.3 83.9 85.4 86.9 88.4 89.8 N2 % 79.7 81.4 83.1 84.7 86.3 87.8 89.4 90.9 92.4 1.75 EGT °C 310 335 360 385 410 435 460 485 510 N1 % 78.6 80.3 81.9 83.5 85.1 86.6 88.1 89.6 91.1 N2 % 80.3 82.0 83.7 85.4 87.0 88.5 90.1 91.6 93.1 1.80 EGT °C 310 335 360 385 410 435 460 485 510 N1 % 79.7 81.4 83.1 84.7 86.3 87.8 89.4 90.9 92.4 N2 % 81.0 82.7 84.4 86.0 87.7 89.2 90.8 92.3 93.9 1.85 EGT °C 311 336 361 386 411 436 461 486 511 N1 % 80.9 82.6 84.3 85.9 87.5 89.1 90.7 92.2 93.7 N2 % 81.6 83.4 85.1 86.7 88.4 90.0 91.5 93.1 94.6 1.90 EGT °C 311 336 361 386 412 437 462 487 512 N1 % 82.0 83.8 85.5 87.2 88.8 90.4 92.0 93.6 95.1 N2 % 82.3 84.1 85.8 87.5 89.1 90.7 92.3 93.9 95.4 1.95 EGT °C 312 337 362 387 412 437 462 487 512 N1 % 83.3 85.1 86.8 88.5 90.2 91.8 93.4 95.0 96.6 N2 % 83.0 84.8 86.5 88.2 89.9 91.5 93.1 94.7 96.2 2.00 EGT °C 312 337 362 388 413 438 463 488 513 N1 % 84.7 86.5 88.3 90.0 91.7 93.3 95.0 96.6 98.2 N2 % 83.7 85.5 87.3 89.0 90.6 92.3 93.9 95.5 97.1 2.05 EGT °C 313 338 363 388 413 438 463 489 514 N1 % 86.2 88.0 89.8 91.6 93.3 95.0 96.6 98.3 99.9 N2 % 84.5 86.3 88.1 89.8 91.5 93.1 94.8 96.4 97.9 2.10 EGT °C 313 338 363 389 414 439 464 489 514 N1 % 87.8 89.7 91.5 93.3 95.1 96.8 98.5 100.2 101.8 N2 % 85.3 87.1 88.9 90.6 92.3 94.0 95.6 97.3 98.9 2.15 EGT °C 314 339 364 389 414 439 465 490 515

Based on: - Straight and level flight - Only pod engines bleed, no bleed from center engine - Engines stabilized for five minutes


4.14 727-200/JT8D-15 JUN 26, 2012

Engine Parameter Check

N1, N2, EGT versus EPR Center Engine

TAT - °C

-40 -30 -20 -10 0 10 20 30 40 EPR

N1 % 73.1 74.6 76.2 77.6 79.1 80.5 82.0 83.3 84.7 N2 % 76.6 78.2 79.8 81.4 82.9 84.4 85.9 87.3 88.7 1.55 EGT °C 306 331 356 380 405 430 455 480 505 N1 % 74.2 75.7 77.3 78.8 80.3 81.7 83.2 84.6 85.9 N2 % 77.2 78.8 80.4 82.0 83.6 85.1 86.6 88.0 89.5 1.60 EGT °C 306 331 356 381 406 431 456 480 505 N1 % 75.2 76.8 78.3 79.9 81.4 82.9 84.3 85.7 87.1 N2 % 77.8 79.5 81.1 82.7 84.2 85.8 87.3 88.7 90.2 1.65 EGT °C 307 332 357 382 406 431 456 481 506 N1 % 76.2 77.8 79.4 80.9 82.5 84.0 85.4 86.9 88.3 N2 % 78.5 80.1 81.7 83.3 84.9 86.5 88.0 89.5 90.9 1.70 EGT °C 307 332 357 382 407 432 457 482 507 N1 % 77.2 78.8 80.4 82.0 83.5 85.0 86.5 88.0 89.4 N2 % 79.1 80.8 82.4 84.0 85.6 87.2 88.7 90.2 91.7 1.75 EGT °C 308 333 358 383 407 432 457 482 507 N1 % 78.2 79.8 81.5 83.1 84.6 86.1 87.7 89.1 90.6 N2 % 79.7 81.4 83.1 84.7 86.3 87.9 89.4 90.9 92.4 1.80 EGT °C 308 333 358 383 408 433 458 483 508 N1 % 79.2 80.9 82.5 84.2 85.7 87.3 88.8 90.3 91.8 N2 % 80.4 82.1 83.8 85.4 87.0 88.6 90.1 91.7 93.2 1.85 EGT °C 309 334 359 384 409 433 458 483 508 N1 % 80.3 82.0 83.7 85.3 86.9 88.5 90.0 91.6 93.1 N2 % 81.1 82.8 84.5 86.1 87.7 89.3 90.9 92.4 93.9 1.90 EGT °C 309 334 359 384 409 434 459 484 509 N1 % 81.5 83.2 84.9 86.6 88.2 89.8 91.4 92.9 94.4 N2 % 81.7 83.5 85.2 86.8 88.5 90.1 91.7 93.2 94.7 1.95 EGT °C 310 335 360 385 410 435 460 485 510 N1 % 82.7 84.5 86.2 87.9 89.6 91.2 92.8 94.4 95.9 N2 % 82.5 84.2 85.9 87.6 89.3 90.9 92.5 94.0 95.6 2.00 EGT °C 310 335 360 385 410 435 460 485 510 N1 % 84.1 85.9 87.7 89.4 91.1 92.7 94.3 95.9 97.5 N2 % 83.2 85.0 86.7 88.4 90.1 91.7 93.3 94.9 96.4 2.05 EGT °C 310 336 361 386 411 436 461 486 511 N1 % 85.7 87.5 89.3 91.0 92.7 94.4 96.1 97.7 99.3 N2 % 84.0 85.8 87.5 89.2 90.9 92.6 94.2 95.8 97.3 2.10 EGT °C 311 336 361 386 411 436 461 486 511 N1 % 87.4 89.2 91.0 92.8 94.6 96.3 98.0 99.6 101.2 N2 % 84.8 86.6 88.4 90.1 91.8 93.4 95.1 96.7 98.3 2.15 EGT °C 311 336 362 387 412 437 462 487 512

Based on: - Straight and level flight - Only pod engines bleed, no bleed from center engine - Engines stabilized for five minutes

Boeing 727-200 LANDING Performance Manual

JUN 26, 2012 727-200/JT8D-15 5.1

CHAPTER 5 - LANDING

5.1 LANDING PERFORMANCE ............................................ 3 5.1.1 Landing Field Length Limitation ............................ 3 5.1.2 Landing Climb Limitation ................................... 3

5.2 Landing Speeds ................................................. 9 5.3 Go-Around EPR .................................................. 9 5.4 PERFORMANCE LIMITED LANDING WEIGHT ............................ 10 5.4.1 Flaps 30................................................... 10 5.4.2 Flaps 40................................................... 13

LANDING Boeing 727-200 Performance Manual

5.2 727-200/JT8D-15 JUN 26, 2012



JUN 26, 2012 727-200/JT8D-15 5.3

5.1 LANDING PERFORMANCE Charts are provided for determining the maximum landing weight as limited by field length or climb requirements for flap positions 30 and 40. Maximum performance landing weight is the smaller of the field length limit weight and climb limit weight; do not exceed maximum structural landing weight. Normally the flap setting for landing is 30 degrees. A flap 30 landing is required when the airport elevation is above 2000 ft. The use of flap 40 is recommended when landing under adverse conditions such as:

Slippery Runway Runway Length 7000 ft or less Braking action reported less then good

5.1.1 Landing Field Length Limitation To determine the landing field length rquired enter the chart with gross weight and airport pressure altitude and read field length required. Charts are provided for DRY and WET runway conditions.

5.1.2 Landing Climb Limitation Enter table with OAT and airport pressure altitude and read climb limited gross weight.


5.4 727-200/JT8D-15 JUN 26, 2012

4000

4200

4400

4600

4800

5000

5200

5400

5600

5800

6000

6200

6400

6600

100 110 120 130 140 150 160 170

Gross Weight 1000 lbs

Fiel

d Le

ngth

Req

uire

d ft

Flaps 30Landing Field Length Required

DRY Runway

Pressure Altitude feet

8000

7000

6000

5000

4000

3000

2000

1000

Sea Level


JUN 26, 2012 727-200/JT8D-15 5.5

4000

4200

4400

4600

4800

5000

5200

5400

5600

5800

6000

6200

6400

100 105 110 115 120 125 130 135 140 145 150


Fiel

d Le

ngth

Req

uire

d ft


DRY Runway


8000

7000

6000

5000

4000

3000

2000

1000

Sea Level


5.6 727-200/JT8D-15 JUN 26, 2012

4000

4200

4400

4600

4800

5000

5200

5400

5600

5800

6000

6200

6400

6600

6800

7000

7200

7400

7600

100 110 120 130 140 150 160 170


Fiel

Len

gth

Req

uire

d ft


WET Runway


8000

7000

6000

5000

4000

3000

2000

1000

Sea Level


JUN 26, 2012 727-200/JT8D-15 5.7

4400

4500

4600

4700

4800

4900

5000

5100

5200

5300

5400

5500

5600

5700

5800

5900

6000

6100

6200

6300

6400

6500

6600

6700

6800

6900

7000

7100

7200

100 105 110 115 120 125 130 135 140 145 150


Fiel

d Le

ngth

Req

uire

d ft


WET Runway


8000

7000

6000

5000

4000

3000

2000

1000

Sea Level


5.8 727-200/JT8D-15 JUN 26, 2012

Climb Limited Landing Weight Flaps 30

OAT AIRPORT ELEVATION (FEET) °F 0 1000 2000 3000 4000 5000 6000 7000 8000 Landing Climb Limited Weight pounds x 1000

50 160 160 160 160 160 160 160 160 160 55 160 160 160 160 160 160 160 160 160 60 160 160 160 160 160 160 160 160 160 65 160 160 160 160 160 160 160 160 160 70 160 160 160 160 160 160 160 160 160 75 160 160 160 160 160 160 160 160 160 80 160 160 160 160 160 160 160 160 160 85 160 160 160 160 160 160 160 160 160 90 160 160 160 160 160 160 160 160 158.6 95 160 160 160 160 160 160 160 160 155.5

100 160 160 160 160 160 160 160 157.9 151.9 105 160 160 160 160 160 160 159.7 153.7 147.9 110 160 160 160 160 160 160 154 149.1 143.5

Climb Limited Landing Weight Flaps 40

OAT AIRPORT ELEVATION (FEET) °F 0 1000 2000 3000 4000 5000 6000 7000 8000 Landing Climb Limited Weight pounds x 1000

50 142.5 142.5 142.5 142.5 142.5 142.5 142.5 142.5 142.5 55 142.5 142.5 142.5 142.5 142.5 142.5 142.5 142.5 142.5 60 142.5 142.5 142.5 142.5 142.5 142.5 142.5 142.5 142.5 65 142.5 142.5 142.5 142.5 142.5 142.5 142.5 142.5 142.5 70 142.5 142.5 142.5 142.5 142.5 142.5 142.5 142.5 142.5 75 142.5 142.5 142.5 142.5 142.5 142.5 142.5 142.5 142.5 80 142.5 142.5 142.5 142.5 142.5 142.5 142.5 142.5 142.5 85 142.5 142.5 142.5 142.5 142.5 142.5 142.5 142.5 141.6 90 142.5 142.5 142.5 142.5 142.5 142.5 142.5 142.5 139.3 95 142.5 142.5 142.5 142.5 142.5 142.5 142.5 141.7 136.6 100 142.5 142.5 142.5 142.5 142.5 142.5 142.5 133.5 133.5 105 142.5 142.5 142.5 142.5 142.5 142.5 140.2 134.9 129.9 110 142.5 142.5 142.5 142.5 142.5 141.3 136.1 130.9 126


JUN 26, 2012 727-200/JT8D-15 5.9

5.2 LANDING SPEEDS

Flaps 30 Flaps 40

Weight Vref Weight Vref lb kn lb kn

160000 137 145000 126 155000 135 140000 123 150000 132 135000 121 145000 130 130000 119 140000 128 125000 117 135000 126 120000 114 130000 123 115000 112 125000 121 110000 109 120000 118 105000 107 115000 116 100000 104 110000 113 105000 111

5.3 GO-AROUND EPR

GO AROUND EPR Pressure OAT °F -82 -10 0 10 18 27 38 47 55 69 73 83 91 100 110 119

Altitude °C -63 -23 -18 -13 -8 -3 3 8 13 18 23 28 33 38 43 48

TAT °C -60 -20 -15 -10 -5 0 5 10 15 20 25 30 35 40 45 50

-1000 1 & 3 2.02 2.02 2.02 2.02 2.02 2.02 2.02 2.02 2.02 2.02 2.02 2.02 2.02 1.99 1.94 1.89

2 2.04 2.04 2.04 2.04 2.04 2.04 2.04 2.04 2.04 2.04 2.04 2.04 2.04 2.01 1.97 1.91

Sea Level 1 & 3 2.07 2.07 2.07 2.07 2.07 2.07 2.07 2.07 2.07 2.07 2.07 2.07 2.04 1.99 1.94 1.89

2 2.09 2.09 2.09 2.09 2.09 2.09 2.09 2.09 2.09 2.09 2.09 2.09 2.06 2.01 1.97 1.91

1000 1 & 3 2.12 2.12 2.12 2.12 2.12 2.12 2.12 2.12 2.09 2.09 2.10 2.08 2.04 1.99 1.94 1.89

2 2.15 2.15 2.15 2.15 2.15 2.15 2.15 2.15 2.12 2.12 2.13 2.10 2.06 2.01 1.97 1.91

2000 1 & 3 2.18 2.18 2.18 2.18 2.18 2.18 2.17 2.13 2.12 2.12 2.10 2.08 2.04 1.99 1.94 1.89

2 2.20 2.20 2.20 2.20 2.20 2.20 2.19 2.16 2.15 2.15 2.13 2.10 2.06 2.01 1.97 1.91

3000 1 & 3 2.24 2.24 2.24 2.24 2.23 2.20 2.17 2.13 2.12 2.12 2.10 2.08 2.04 1.99 1.94 1.89

2 2.27 2.27 2.27 2.27 2.25 2.22 2.19 2.16 2.15 2.15 2.13 2.10 2.06 2.01 1.97 1.91

3900 & 1 & 3 2.30 2.30 2.28 2.26 2.23 2.20 2.17 2.13 2.12 2.12 2.10 2.08 2.04 1.99 1.94 1.89

ABOVE 2 2.32 2.32 2.30 2.28 2.25 2.22 2.19 2.16 2.15 2.15 2.13 2.10 2.06 2.01 1.97 1.91

EPR BLEED CORRECTIONS ENG 1 & 3 ENG 2 OFF ON A/C BLEEDS + .04 - .04

- - - .03 ENGINE ANTI-ICE ON - .03* - .06* - .09 - .03 TWO ENGINE

BLEEDS -. 12* - .06* - .10 - .03

ENGINE AND WING ANTI-ICE ONE ENGINE

BLEED - .13* - .06* MOD ‘A’ INSTALLED - - + .01

* USE IN SHADED AREA, COLDER THAN -18°C TAT REDUCE ENG 2 EPR BY .05 WITH 6TH STAGE BLEED ON (IF INSTALLED) FOR 10°C (50°F) OAT AND WARMER


5.10 727-200/JT8D-15 JUN 26, 2012

5.4 PERFORMANCE LIMITED LANDING WEIGHT

5.4.1 Flaps 30

30° FLAPS MAXIMUM LANDING WEIGHT

RUNWAY FIELD CLIMB STATION CODE NO COND LENGTH lbs x 1000 REMARKS

ALBUQUERQUE IKR 03 DRY 10000 154.5 154.5 ELEV 5355 21 DRY 10000 154.5 154.5

08 DRY 13793 154.5 154.5 26 DRY 13793 154.5 154.5 12 DRY 6000 30 DRY 6000

NOT AUTHORIZED FOR LANDING

17 DRY 10000 154.5 154.5 35 DRY 10000 154.5 154.5 BEND REDMONT RDM 04 DRY 7040 154.5 154.5

ELEV 3077 22 DRY 7040 154.5 154.5 10 DRY 7000 154.5 154.5

28 DRY 7000 154.5 154.5 BELLINGHAM BLI 16 DRY 6700

ELEV 170 34 DRY 6700 FLAPS 30 NOT AUTHORIZED

CONCORD JQF 02 DRY 7400 154.5 154.5 ELEV 705 20 DRY 7400 154.5 154.5

FRESNO FAT 11R DRY 7200 154.5 154.5 ELEV 336 29L DRY 7200 154.5 154.5

11L DRY 9200 154.5 154.5 29R DRY 9200 154.5 154.5 HOLLYWOOD-BURBANK BUR 08 DRY 5800

ELEV 778 26 DRY 5800 15 DRY 6890 33 DRY 6890

FLAPS 30 NOT AUTHORIZED

LAS VEGAS LAS 01R DRY 10185 154.5 154.5 ELEV 2141 19L DRY 10185 154.5 154.5

01L DRY 9395 154.5 154.5 19R DRY 9395 154.5 154.5 07R DRY 10936 154.5 154.5 25L DRY 10936 154.5 154.5 07L DRY 15135 154.5 154.5 25R DRY 15135 154.5 154.5 LONG BEACH LGB 12 DRY 10000 154.5 154.5

ELEV 60 30 DRY 10000 154.5 154.5 LOS ANGELES LAX 06R DRY 10285 154.5 154.5

ELEV 126 24L DRY 10285 154.5 154.5 06L DRY 8925 154.5 154.5 24R DRY 8925 154.5 154.5 07L DRY 12091 154.5 154.5 25R DRY 12091 154.5 154.5 07R DRY 11096 154.5 154.5 25L DRY 11096 154.5 154.5


JUN 26, 2012 727-200/JT8D-15 5.11


RUNWAY FIELD CLIMB STATION CODE

NO COND LENGTH lbs x 1000 REMARKS

LOS CABOS SJD 16 DRY 9843 154.5 154.5 ELEV 374 34 DRY 9843 154.5 154.5

MEDFORD MFR 14 DRY 8800 154.5 154.5 ELEV 1335 32 DRY 8800 154.5 154.5

MONTEREY MRY 10R DRY 7600 154.5 154.5 ELEV 257 28L DRY 7600 154.5 154.5

OAKLAND OAK 11 DRY 10000 154.5 154.5 ELEV 9 29 DRY 10000 154.5 154.5

ONTARIO ONT 08L DRY 12200 154.5 154.5 ELEV 944 26R DRY 12200 154.5 154.5

08R DRY 10200 154.5 154.5 26L DRY 10200 154.5 154.5

ORANGE COUNTY SNA 01L DRY 5700 ELEV 56 19R DRY 5700

FLAPS 30 NOT AUTHORIZED

PHOENIX PHX 07R DRY 7800 154.5 154.5 ELEV 1135 25L DRY 7800 154.5 154.5

07L DRY 10300 154.5 154.5 25R DRY 10300 154.5 154.5 08 DRY 11490 154.5 154.5 26 DRY 11490 154.5 154.5 PORTLAND PDX 03 DRY 7000 154.5 154.5

ELEV 30 21 DRY 7000 154.5 154.5 10L DRY 11000 154.5 154.5 28R DRY 11000 154.5 154.5 10R DRY 8000 154.5 154.5 28L DRY 8000 154.5 154.5 RENO RNO 07 DRY 6100 154.5 154.5

ELEV 4415 25 DRY 6100 154.5 154.5 16R DRY 11000 154.5 154.5 34L DRY 11000 154.5 154.5 16L DRY 9000 154.5 154.5 34R DRY 9000 154.5 154.5 SACRAMENTO SMF 16R DRY 8600 154.5 154.5

ELEV 27 34L DRY 8600 154.5 154.5 16L DRY 8600 154.5 154.5 34R DRY 8600 154.5 154.5 SAN DIEGO SAN 09 DRY 9400 154.5 154.5

ELEV 17 27 DRY 9400 154.5 154.5 SAN FRANCISCO SFO 01R DRY 9650 154.5 154.5



5.12 727-200/JT8D-15 JUN 26, 2012




SEATTLE TACOMA SEA 16R DRY 9426 154.5 154.5 ELEV 433 34L DRY 9426 154.5 154.5

16L DRY 11900 154.5 154.5 34R DRY 11900 154.5 154.5 SPOKANE GEG 03 DRY 9000 154.5 154.5

ELEV 2376 21 DRY 9000 154.5 154.5 07 DRY 8198 154.5 154.5 25 DRY 8198 154.5 154.5 STOCKTON SCK 11L DRY 10650 154.5 154.5

ELEV 33 29R DRY 10650 154.5 154.5 SAN JOSE SJC 12R DRY 11000 154.5 154.5

ELEV 62 30L DRY 11000 154.5 154.5 12L DRY 11000 154.5 154.5 30R DRY 11000 154.5 154.5 TUCSON TUS 03 DRY 7000 154.5 154.5

ELEV 2643 21 DRY 7000 154.5 154.5 11R DRY 8400 154.5 154.5 29L DRY 8400 154.5 154.5 11L DRY 11000 154.5 154.5 29R DRY 11000 154.5 154.5 YAKIMA YKM 09 DRY 7600 154.5 154.5

ELEV 1095 27 DRY 7600 154.5 154.5


JUN 26, 2012 727-200/JT8D-15 5.13

5.4.2 Flaps 40




ALBUQUERQUE IKR 03 DRY 10000 ELEV 5355 21 DRY 10000

08 DRY 13793 26 DRY 13793 12 DRY 6000 30 DRY 6000 17 DRY 10000 35 DRY 10000

NOT AUTHORIZED

BEND REDMONT RDM 04 DRY 7040 ELEV 3077 22 DRY 7040

10 DRY 7000 28 DRY 7000

NOT AUTHORIZED

BELLINGHAM BLI 16 DRY 6700 142.5 142.5 ELEV 170 34 DRY 6700 142.5 142.5

CONCORD JQF 02 DRY 7400 142.5 142.5 ELEV 705 20 DRY 7400 142.5 142.5

FRESNO FAT 11R DRY 7200 142.5 142.5 ELEV 336 29L DRY 7200 142.5 142.5

11L DRY 9200 142.5 142.5 29R DRY 9200 142.5 142.5 HOLLYWOOD-BURBANK BUR 08 DRY 5800 142.5 142.5

ELEV 778 26 DRY 5800 142.5 142.5 15 DRY 6890 142.5 142.5 33 DRY 6890 142.5 142.5 LAS VEGAS LAS 01R DRY 10185

ELEV 2141 19L DRY 10185 01L DRY 9395 19R DRY 9395 07R DRY 10936 25L DRY 10936 07L DRY 15135 25R DRY 15135

NOT AUTHORIZED

LONG BEACH LGB 12 DRY 10000 142.5 142.5 ELEV 60 30 DRY 10000 142.5 142.5

LOS ANGELES LAX 06R DRY 10285 142.5 142.5 ELEV 126 24L DRY 10285 142.5 142.5

06L DRY 8925 142.5 142.5 24R DRY 8925 142.5 142.5 07L DRY 12091 142.5 142.5 25R DRY 12091 142.5 142.5 07R DRY 11096 142.5 142.5 25L DRY 11096 142.5 142.5 LOS CABOS SJD 16 DRY 9843 142.5 142.5

ELEV 374 34 DRY 9843 142.5 142.5


5.14 727-200/JT8D-15 JUN 26, 2012




MEDFORD MFR 14 DRY 8800 142.5 142.5 ELEV 1335 32 DRY 8800 142.5 142.5

MONTEREY MRY 10R DRY 7600 142.5 142.5 ELEV 257 28L DRY 7600 142.5 142.5

OAKLAND OAK 11 DRY 10000 142.5 142.5 ELEV 9 29 DRY 10000 142.5 142.5

ONTARIO ONT 08L DRY 12200 142.5 142.5 ELEV 944 26R DRY 12200 142.5 142.5

08R DRY 10200 142.5 142.5 26L DRY 10200 142.5 142.5

ORANGE COUNTY SNA 01L DRY 5700 142.5 142.5 ELEV 56 19R DRY 5700 142.5 142.5

PHOENIX PHX 07R DRY 7800 142.5 142.5 ELEV 1135 25L DRY 7800 142.5 142.5

07L DRY 10300 142.5 142.5 25R DRY 10300 142.5 142.5 08 DRY 11490 142.5 142.5 26 DRY 11490 142.5 142.5 PORTLAND PDX 03 DRY 7000 142.5 142.5

ELEV 30 21 DRY 7000 142.5 142.5 10L DRY 11000 142.5 142.5 28R DRY 11000 142.5 142.5 10R DRY 8000 142.5 142.5 28L DRY 8000 142.5 142.5 RENO RNO 07 DRY 6100

ELEV 4415 25 DRY 6100 16R DRY 11000 34L DRY 11000 16L DRY 9000 34R DRY 9000

NOT AUTHORIZED

SACRAMENTO SMF 16R DRY 8600 142.5 142.5 ELEV 27 34L DRY 8600 142.5 142.5

16L DRY 8600 142.5 142.5 34R DRY 8600 142.5 142.5 SAN DIEGO SAN 09 DRY 9400 142.5 142.5

ELEV 17 27 DRY 9400 142.5 142.5 SAN FRANCISCO SFO 01R DRY 9650 142.5 142.5



JUN 26, 2012 727-200/JT8D-15 5.15




SEATTLE TACOMA SEA 16R DRY 9426 142.5 142.5 ELEV 433 34L DRY 9426 142.5 142.5

16L DRY 11900 142.5 142.5 34R DRY 11900 142.5 142.5 SPOKANE GEG 03 DRY 9000

ELEV 2376 21 DRY 9000 07 DRY 8198 25 DRY 8198

NOT AUTHORIZED

STOCKTON SCK 11L DRY 10650 142.5 142.5 ELEV 33 29R DRY 10650 142.5 142.5

SAN JOSE SJC 12R DRY 11000 142.5 142.5 ELEV 62 30L DRY 11000 142.5 142.5

12L DRY 11000 142.5 142.5 30R DRY 11000 142.5 142.5 TUCSON TUS 03 DRY 7000

ELEV 2643 21 DRY 7000 11R DRY 8400 29L DRY 8400 11L DRY 11000 29R DRY 11000

NOT AUTHORIZED

YAKIMA YKM 09 DRY 7600 142.5 142.5 ELEV 1095 27 DRY 7600 142.5 142.5


5.16 727-200/JT8D-15 JUN 26, 2012


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727 200 Performance Manual

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