program-manual-appendix14c-b210.pdf

7/27/2019 program-manual-appendix14c-b210.pdf

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KING AIR B210

FOR TRAINING PURPOSES ONLY

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KING AIR B210AIRCRAFT FLIGHT MANUAL


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TABLE OF CONTENTS1.0 GENERAL .................................................................................................................... 4

1.1 Introduction ............................................................................................................... 4

1.2 Safety Instructions .................................................................................................... 52.0 LIMITATIONS ............................................................................................................. 7

2.1 Airspeeds: ................................................................................................................. 7

2.2 Maximum weights: ................................................................................................... 8

2.3 Powerplant: ............................................................................................................... 9

2.4 Power settings: ........................................................................................................ 10

2.5 Propellers: ............................................................................................................... 11

2.6 Fuel: ........................................................................................................................ 11

2.7 Engine oil: ............................................................................................................... 11

2.8 Hydraulic fluid: ....................................................................................................... 11

2.9 Pressurization: ......................................................................................................... 12

2.10 Electrical: .............................................................................................................. 122.11 Generator Limitations: .......................................................................................... 12

2.12 Starter Limitations: ............................................................................................... 12

2.13 Ice Protection: ....................................................................................................... 12

3.0 NORMAL PROCEDURES ........................................................................................ 13

3.1 Captains Before Start Flow: .................................................................................. 13

3.2 First Officers Before Start Flow: ........................................................................... 18

3.3 Normal Checklist with flows ............................................................................... 20

3.4 Normal Checklist .................................................................................................... 23

4.0 EMERGENCY PROCEDURES ................................................................................. 27

4.1 Engine: .................................................................................................................... 27

4.2 Electrical: ................................................................................................................ 30

4.3 Pressurization and Fuel: .......................................................................................... 31

4.4 Landing Gear and Trim:.......................................................................................... 33

5.0 PERFORMANCE ....................................................................................................... 34

5.1 Takeoff Weight Flaps-0% ....................................................................................... 34

5.2 Takeoff Weight-Flaps 40% ..................................................................................... 35

5.3 Takeoff Flight Path ................................................................................................. 36

5.4 Takeoff Distance-Flaps 0% ..................................................................................... 37

5.5 Accelerate-stop-Flaps 0% ....................................................................................... 38

5.6 Accelerate-go-Flaps 0% .......................................................................................... 39

5.7 Net Gradient of Climb-Flaps 0% ............................................................................ 40

5.8 Takeoff Distance-Flaps 40% ................................................................................... 41

5.9 Accelerate-stop-Flaps 40% ..................................................................................... 42

5.10 Accelerate-go-Flaps 40% ...................................................................................... 43

5.11 Net Gradient of Climb-Flaps 40% ........................................................................ 44

5.12 Climb-Two Engines-Flaps 0% .............................................................................. 45

5.13 Climb-Two Engines-Flaps 40% ............................................................................ 46

5.14 Time, Fuel, and Distance to Climb ....................................................................... 47

5.15 Climb-One Engine Inoperative ............................................................................. 48


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5.16 Service Ceiling-One Engine Inoperative .............................................................. 49

5.17 Recommended Cruise Power-ISA -10C ............................................................. 50

5.18 Recommended Cruise Power-ISA ........................................................................ 51

5.19 Recommended Cruise Power-ISA+10C .............................................................. 52

5.20 Recommended Cruise Speeds ............................................................................... 53

5.21 Recommended Cruise Power ................................................................................ 545.22 Fuel Flow at Recommended Cruise Power ........................................................... 55

5.23 Maximum Range Power ....................................................................................... 56

5.24 Time, Fuel, and Distance to Descend ................................................................... 57

5.25 Landing Distance Without Propeller Reversing-Flaps 100% ............................... 58

5.26 Landing Distance Without Propeller Reversing-Flaps 0% ................................... 59

5.27 Landing Distance With Propeller Reversing-Flaps 100% .................................... 60

5.28 Landing Distance With Propeller Reversing-Flaps 0% ........................................ 61

6.0 FLIGHT PROFILES ................................................................................................... 62

6.1 Precision Approach ................................................................................................. 62

6.2 Non-precision Approach ......................................................................................... 63


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1.0 GENERAL

1.1 Introduction

This document is the Selkirk College approved operating manual for

the King Air B210. It is meant to complement, and should be used in

conjunction with the Selair SOPs. The information contained in this

document closely resembles that of a Super King Air B200, but some

significant system differences warranted the creation of a manual specific to

the Alsim flight training device. It contains relevant information regarding

operating limitations, systems, performance, normal and abnormal

procedures. This manual is designed to emulate the AFM of an actual

aircraft, however, in the interest of effective training some additional

information has been included.

If a conflict is found between this document and any other Selkirk College

reference materials please bring it to the attention of the Chief Flight

Instructor.


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1.2 Safety Instructions


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2.0 LIMITATIONS

2.1 Airspeeds:

Vmca 86KIAS- air minimum control speedVsse 104KIAS- intentional one engine inoperative speed

Va 181KIAS- maneuvering speed (12,500 lbs)

Vb 170KIAS- turbulent air penetration speedVmo 259KIAS- maximum operating limit speed

Vle 181KIAS- maximum landing gear extended speed

Vlo 181KIAS- extension- maximum landing gear operating speed163KIAS- retraction- maximum landing gear operating speed

Vfe 200KIAS- approach position 40%- maximum flaps extended speed

157KIAS- full down position 100%- maximum flaps extended speed

Vs 99KIAS- stall speed flaps up (12,500Lbs)

Vso 75KIAS- stall speed flaps 100% (12,500lbs)Vx 100KIAS- two-engine best angle of climb

Vxse 115KIAS- one-engine inoperative best angle of climbVy 126KIAS- two-engine best rate of climb

Vyse 121KIAS- one-engine inoperative best rate of climb

Min. flap retraction speed- 100KIAS

Max. range glide speed- 135KIAS

Min. reverse speed- 60KIASMax. demonstrated crosswind- 25kts (not limiting)

Cruise climb:Sea level to 10,000ft- 160KIAS10,000 to 20,000ft- 140KIAS

20,000 to 25,000ft- 130KIAS25,000 to 35,000ft- 120KIAS

Holding speeds:Two engine- 140KIAS, flaps approach.

One engine- 140KIAS, flaps up.

Approach speeds and configurations:

Initially- flaps approach,140KIAS.IF inbound, upon commencing descent- gear down,140 KIAS.Precision approach:

2 NM from FAF- flaps down, Vref + 20.

Landing assured- Vref + gust factor.

Non-precision approach:2 NM from FAF- Vref + 20, flaps remain at approach.

Landing assured- flaps down,Vref + gust factor.


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Approach speeds and configurations one engine inoperative:

As above with the exception of: 2NM from FAF- Vref + 25.

Airspeed Indicator Markings:

2.2 Maximum weights:

Zero fuel- 10,400lbs

Ramp- 12,590lbsTakeoff- 12,500lbs

Landing- 12,500lbs

Aft Baggage Compartment- 410lbs


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2.3 Powerplant:

Two Pratt & Whitney PT6A-42

Reverse flow, free turbine.

850 SHP- shaft horsepower per engine.


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400 to 2230 ft-lbs 2230 ft-lbs

2.4 Power settings:

Take-off- 2000rpm, 2230ft/lbs torque, 800C ITTClimb- 1900rpm, 2230ft/lbs torque, 750 C ITT

Cruise- 1700rpm, 2230ft/lbs torque, 725 C ITT

Low Idle- 56% N1

High Idle- 70% N1


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Note: For continued operation with oil pressure between 60 and 85 PSI limit torque to

1100ft/lbs. Values below 60 PSI are unsafe and require engine shutdown or immediatelanding using minimum power required.

2.5 Propellers:

Three blade, variable pitch, constant speed.Engine oil boosted to 400PSI controls blade pitch.

Limit torque to 1800ft lbs for sustained operation at 2080rpm.

Sustained operation above 2080rpm is not approved.

2.6 Fuel:

Max. useable- 544 US Gallons (3645 lbs)

Min. fuel for takeoff- 265lbs/side

Max. imbalance 1000lbs.

One fuel pump may be inoperative for takeoff. (Crossfeed of fuel will not be available

from the side of the inoperative boost pump.)

Operation with the fuel pressure annunciator illuminated is limited to 10 hours beforeoverhaul or replacement of the engine-driven fuel pump.

Recommended Grades- Jet A, Jet A-1, Jet B, JP-4, JP-5

Note: Avgas is an approved fuel for emergency situations, but the following limitations

apply.

- 150 hours between engine overhauls.- FL200 or below if either fuel pump is inoperative.- Crossfeed capability is required for climbs above FL200.

2.7 Engine oil:

Capacity- 14 quartsMax. consumption- 1QT/10hrs.

Min. level- 4 QTS low on dipstickMax. level- Full on dipstick

Type- Exxon Turbo Oil 2380

2.8 Hydraulic fluid:

Brakes, landing gear, struts.

Type- MIL-H-5606


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2.9 Pressurization:

Max. operating altitude- 25,000 ft

Max. operating altitude yaw damp inoperative- 17,000 ft

Max. cabin differential- 5.2 PSI

2.10 Electr ical:

Two 28VDC, 250 Amp starter generators.

One 24VDC, 34 Amp/Hour Nickel Cadmium battery.

External power (GPU) 24-30VDC, 400 Amps continuous, 1100 Amps surge.

Two 28VDC, 115/26VAC inverters.

Note: A minimum battery voltage of 20V is required before connecting to external power

or attempting a battery start.

2.11 Generator Limi tations:

S.L. to FL250- 100% Load

Ground Ops- 85% Load

2.12 Starter Limitations:

40 seconds on, 60 seconds off

40 seconds on, 60 seconds off

40 seconds on, 30 minutes off

2.13 Ice Protection:

Do not operate deice boots below -40 C

Do not operate prop heat when props not turning.Engine anti-ice on for all ground operations.

Engine anti-ice on during flight in visible moisture below 5 C

Brake deice is not approved for takeoff.


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3.0 NORMAL PROCEDURES

3.1 Captains Before Start Flow:

1. Parkingbrakeon2. Confirmgeardown3. Confirmexternalpowerconnected4. Batteryon5. Avionicsmasteron


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Complete flow checks: Start with overhead panel


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After overhead flow move to main panel and flow as follows:

Notes:

Standard HSI model is to be used. If it is not already selected use EHSI mode toset it.

Determine 400 agl and set on red (#2) altitude bug. IMPORTANT - if thedeparture has a special restriction calling for initial climb to an altitude greater

than 400 agl set that instead.

Get the V1 and V2 speeds from the checklist and set them on the bugs as shownabove

Leave Speed selector on position 3 (orange) to be updated in climb. Post the TOLD card


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Next move to the center pedestal:

Set elevator trim slightlynose up refer to graphic

on center panel when

setting.

Power levers to idle Props full forward Condition levers off Rudder trim to zero Confirm Autopilot is off Set autopilot to PF


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Notes:

Certain anomalies with the simulator on start can be forestalled by releasingparking brake and resetting before starting.

On the back of the pedestal set roll trim to zero

Turn on the fuel valves.Once the above flow checks have been completed use the Before Start checklist to double

check the most important items.Your co-pilot will be obtaining the ATIS and setting up the radios, GPS flight plan, etc.

When you have received a radio setup briefing from the First Officer complete your

departure briefing, confirm no questions and announce Before start checklist complete

1. Avionics Master-Off2. Rotating beacon-On

Complete start procedure per start procedure simulation and ALSIM SOPs.

3. External power- Disconnect

4. Generators-On

Once the PF is satisfied the generators are online and operating within limits s/he will call

After start checklist


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1. ATIS / weather update2. Obtain IFR clearance3. Load required GPS flight plan insert required departure procedure4. Tune radios for departure (or ground test if required.)5. Set DME switch

Once the above is done complete a flow check of the panel. The Captain will have posted

a TOLD card from which you can obtain the required speeds to set.


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Notes:

Get the ATIS right away. If the weather is below landing minima check theweather at the departure alternate.

Load the required GPS flight plan Insert any required departure procedures Set red altitude bug to 400 agl unless a special altitude restriction is called for on

the departure procedure.

Set the white speed bug to V1 and the orange bug to V2. Obtain these speeds fromthe TOLD card posted by the Captain.

Give the Captain a radio setup briefing.

3.3 Normal Checklist with flows

Students must learn all the checklist flows. This reference may be helpful to you in

keeping them straight.

CHECKLIST NOTES

AFTER START

1. Generators ................................................................. ON

2. Voltage & Loadmeters ............................... CHECKED

3. Avionics Master ...................................................... ON

4. Radios .................................................................. SET5. Instrument Panel ............ CHECKED LEFT & RIGHT

6. Lights .................................................................... SET

7. Cabin Master ........................................................... ON

Yellow copilot flowsGray captain flows

BEFORE TAKEOFF1. Brakes ........................................................ CHECKED

2. Instruments ................................................. CHECKED

3. Altimeters .................. ____SET & CROSSCHECKED4. Trim..........................................................THREE SET

5. Flaps ..................................................................... SET

6. Fuel & Engine Instruments ........................ CHECKED7. Departure Briefing .................................. COMPLETE

8. Engine Anti-ice ..................................................... OFF

9. Ice Protection .......................................................... ON10. Annunciators ...................................... CONSIDERED

_________________________________________________________

11. Transponder .................................................. ALT____

Flaps to approach

Pitot heat on


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12. Taxi, Recognition & Landing Lights ...................... ON

AFTER TAKEOFF (CHECKS)

1. Landing Gear .......................................................... UP

2. Flaps ........................................................................ UP3. Taxi Light.............................................................. OFF

4. Climb Power ......................................................... SET5. Pressurization ............................................. CHECKED

6. Engine Instruments .................................... CHECKED

7. Yaw Damper ........................................................... ON

10,000 (CHECKS)

1. Landing & Recognition Lights ............................. OFF

2. Windshield Heat..................................................... ON

3. Pressurization ............................................. CHECKED4. Speedbugs/Rad Alt................................................ SET

Windshield heat on low

Zero all altimeter and

speed bugs with theexception of the orange

speed bugs.

Set radar alt to 2000 AGL.

CRUISE (CHECKS)

1. Cruise Power ......................................................... SET


4. Fuel Quantity ............................................. CHECKED5. Switches & Circuit Breakers ...................... CHECKED

6. Cabin Lights .......................................................... SET

Can turn of seatbelt lightif desired.

PNF should check alllights including nav,

landing, etc.

DESCENT

1. Approach Briefing .................................. COMPLETE2. Pressurization ........................................................ SET

3. Altimeters .................. ____SET & CROSSCHECKED

4. TOLD card ................................................SELECTED5. Cabin Lights .......................................................... SET

GNSS

6. Approach ...................................................... LOADED

7. Waypoints .................................................. VERIFIED8. RAIM ..................................................... AVAILABLE

Cabin pressure to 500

AAE.

Seat belt light goes on-

also check all other lights

APPROACH

1. Landing & Recognition Lights ............................... ON

2. Pressurization ............................................. CHECKED

3. Altimeters .................. ____SET & CROSSCHECKED4. Engine Anti-ice ....................................................... ON

GNSS

5. Approach Mode ................................................ TERM6. Approach ................................................ ACTIVATED

Performed at 10,000 feet.


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BEFORE LANDING

1. Landing Gear .............................. DOWN & LOCKED2. Flaps ....................................................... APPROACH

3. Brakes ........................................................ CHECKEDGNSS

4. Approach Mode .................................................... APR_______________________________________________________

5. Flaps ................................................................ DOWN

To the line performed at

gear extension.

No flow items

Below the line performedat Flaps down.

PF calls flaps down,below the line no need

to say below 157 on NPA.

AFTER LANDING (CHECKS)

1. Landing Lights ...................................................... OFF

2. Recognition Lights ................................................ OFF3. Transponder ............................................... STANDBY

4. Ice Protection ........................................................ OFF5. Propellers .......................................FULL FORWARD

6. Trim......................................................... THREE SET

7. Flaps ........................................................................ UP

8. Speed bugs/Rad Alt............................................ ZERO

Completed upon reaching

a safe taxi speed.

Once the aircraft has reached its parking spot the Captain will complete the followingshutdown procedure by memory prior to running the shutdown checks.

1. Avionics Master-Off2. ITT-Stable (approx. 500C)3. Condition Levers- Cut-off

4. Propellers-Feather

5. External Power Connect


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3.4 Normal Checklist

BEFORE START (CHECKS)1. Parking Brake.......................................................... ON

2. Battery Master ......................................................... ON

3. Inverter .................................................................... ON4. Voltmeter ................................................... CHECKED

5. Oxygen .......................................................... CLOSED

6. Pressurization ........................................................ SET

7. Power Levers ...................................................... IDLE8. Propellers .......................................FULL FORWARD

9. Condition Levers .......................................... CUT-OFF

10. Trim..........................................................THREE SET11. Circuit Breakers ......................................... CHECKED

12. Fuel Selectors ........................................................ SET

13. Fuel Quantity ............................................. CHECKED14. Fuel Totaliser ................................................... RESET

15. Cabin Master ......................................................... OFF

16. Cabin Mode ....................................................... AUTO

17. Engine Anti-ice ....................................................... ON18. Annunciators .............................................. CHECKED

19. Controls ............................................................... FREE

20. TOLD card ................................................SELECTED21. Altimeters .................. ____SET & CROSSCHECKED

22. Departure Briefing .................................. COMPLETE

AFTER START1. Generators ............................................................... ON

2. Voltage & Loadmeters ............................... CHECKED3. Avionics Master ...................................................... ON

4. Radios .................................................................. SET

5. Instrument Panel ............ CHECKED LEFT & RIGHT

6. Lights .................................................................... SET7. Cabin Master ........................................................... ON


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BEFORE TAKEOFF1. Brakes ........................................................ CHECKED2. Instruments ................................................. CHECKED


4. Trim..........................................................THREE SET5. Flaps ..................................................................... SET

6. Fuel & Engine Instruments ........................ CHECKED

7. Departure Briefing .................................. COMPLETE

8. Engine Anti-ice ..................................................... OFF9. Ice Protection .......................................................... ON

10. Annunciators ...................................... CONSIDERED_________________________________________________________

11. Transponder .................................................. ALT____

12. Taxi, Recognition & Landing Lights ...................... ON

AFTER TAKEOFF (CHECKS)

1. Landing Gear .......................................................... UP2. Flaps ........................................................................ UP

3. Taxi Lights ............................................................ OFF

4. Climb Power ......................................................... SET5. Pressurization ............................................. CHECKED


7. Yaw Damper ........................................................... ON

10,000 (CHECKS)

1. Landing & Recognition Lights ............................. OFF2. Windshield Heat..................................................... ON3. Pressurization ............................................. CHECKED

4. Speedbugs/Rad Alt................................................ SET

CRUISE (CHECKS)

1. Cruise Power ......................................................... SET


4. Fuel Quantity ............................................. CHECKED5. Switches & Circuit Breakers ...................... CHECKED

6. Cabin Lights .......................................................... SET


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DESCENT

1. Approach Briefing .................................. COMPLETE2. Pressurization ........................................................ SET


4. TOLD card ................................................SELECTED5. Cabin Lights .......................................................... SET

GNSS

6. Approach ...................................................... LOADED

7. Waypoints .................................................. VERIFIED8. RAIM ..................................................... AVAILABLE

APPROACH

1. Landing & Recognition Lights ............................... ON

2. Pressurization ............................................. CHECKED3. Altimeters .................. ____SET & CROSSCHECKED

4. Engine Anti-ice ....................................................... ONGNSS

5. Approach Mode ................................................ TERM6. Approach ................................................ ACTIVATED

BEFORE LANDING

1. Landing Gear .............................. DOWN & LOCKED

2. Flaps ....................................................... APPROACH3. Brakes ........................................................ CHECKED

GNSS

4. Approach Mode .................................................... APR_______________________________________________________

5. Flaps ................................................................ DOWN


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AFTER LANDING (CHECKS)

1. Landing Lights ...................................................... OFF2. Recognition Lights ................................................ OFF

3. Transponder ............................................... STANDBY

4. Ice Protection ........................................................ OFF5. Propellers .......................................FULL FORWARD

6. Trim......................................................... THREE SET

7. Flaps ........................................................................ UP

8. Speed bugs/Rad Alt............................................ ZERO

SHUTDOWN (CHECKS)

1. Parking Brake........................................................ SET

2. Avionics Master .................................................... OFF

3. ITT ........................................................ STABILIZED4. Condition Levers ........................................ CUT - OFF

5. Propellers .............................................. FEATHERED

6. Inverter .................................................................. OFF7. Cabin Mode ........................................................... OFF

8. Cabin Master ......................................................... OFF

9. Rotating Beacon .................................................... OFF10. Overhead Panel Switches ..................................... OFF

11. Voltmeter .................................................. CHECKED

12. Fuel Quantity ............................................ CHECKED

13. Generators ............................................................ OFF14. Battery Master ...................................................... OFF

BEFORE START CHECKS- completed silently by the left seat pilot.AFTER START CHECKLIST- challenge response.

BEFORE TAKEOFF CHECKLIST TO THE LINE- completed during taxi as

challenge response.BELOW THE LINE-completed when cleared to position as challenge response.

AFTER TAKEOFF CHECKS- completed through 400 silently by the PNF.

10,000 FEET CHECKS- completed silently by the PNF.

CRUISE CHECKS- completed silently by the PNF.DESCENT CHECKLIST- completed prior to descent as challenge response.

APPROACH CHECKLIST- completed through 10,000 feet as challenge response.

BEFORE LANDING CHECKLIST TO THE LINE- completed at gear extension as

challenge response.BELOW THE LINE- completed at full flap extension as challenge response.

AFTER LANDING CHECKS- completed at safe taxi speed silently by the PNF.SHUTDOWN CHECKS- completed silently by left seat pilot.


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ENGINE FAILURE AFTER V11. Power - MAXIMUM ALLOWABLE

2. Airspeed MAINTAIN V2

3. Landing Gear UP (positive rate)

4.

Propeller - FEATHER5. Airspeed V2

6. Flaps UP (Vyse)

(Secure Inoperative Engine)

a. Condition Lever - CUT OFFb. Propeller - FEATHERc. Fuel Selector Valve CLOSEDd. Fire Extinguisher IF REQUIREDe. Fuel Pump - OFFf.

Generator OFFg. Prop Sync - OFFh. Electrical Load - MONITOR

EMERGENCY ENGINE SHUTDOWN(ENGINE FAILURE/FIRE, LOW OIL PRESSURE)

Affected Engine:

1. Condition Lever - CUT OFF

2. Propeller - FEATHER

3. Fuel Selector Valve - CLOSED

4.

Fire Extinguisher IF REQUIRED

(Secure Inoperative Engine)

a. Fuel Pump - OFFb. Generator OFFc. Prop Sync - OFFd. Electrical Load - MONITORe. Fuel Load MONITOR


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AIR STARTSTARTER ASSIST

1. Electrical Load MINIMUM REQUIRED2. Power Lever - IDLE3.

Condition Lever - CUT OFF4. Fuel Selector Valve OPEN

5. Fuel Pump - ON6. Ignition - ON7. Starter - ON8. Ignition Annunciator - CONFIRM ON9. Condition Lever - HIGH IDLE (10% N1)10.Starter - OFF (N1 50%)11.Ignition - OFF12.Propeller Lever - AS REQUIRED13.Power Lever - AS REQUIRED14.

Generator - ON15.Electrical Equipment - AS REQUIRED

AIR STARTWINDMILLING PROPELLER (NO STARTER ASSIST)

1. Electrical Load MINIMUM REQUIRED2. Power Lever - IDLE3. Propeller Lever - FULL FORWARD4. Condition Lever - CUT OFF5. Fuel Selector Valve OPEN6. Fuel Pump - ON7.

Generator (inoperative engine) - OFF8. Airspeed - 140 KNOTS MINIMUM

9. Altitude - BELOW FL20010.Ignition - ON11.Condition Lever HIGH IDLE (10% N1)12.Power - AS REQUIRED (after ITT has peaked)13.Ignition - OFF14.Generator - ON15.Electrical Equipment - AS REQUIRED


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GLIDE (BOTH ENGINES INOPERATIVE)

1. Landing Gear - UP

2. Flaps - UP3. Propellers - FEATHER

4. Airspeed - 135 KNOTS

5. Electrical Load - REDUCE

(Glide ratio is approx. 2nm/1000ft of altitude)

4.2 Electr ical:

INVERTER FAILURE(L or R INV PWR ANNUNCIATOR)

1. Select Switch Inverter - SELECT OTHER INVERTER

(If inverter power is not restored)2. Land as soon as practical.

GENERATOR FAILURE(L or R GEN INOP ANNUNCIATOR)

1. Generator Switch - OFF THEN ON

(If generator will not reset)

2. Generator Switch - OFF3. Operating Generator Load - MONITORDUAL GENERATOR FAILURE(L and R GEN INOP ANNUNCIATORS)

1. Generator Switches OFF THEN ON(If generator will not reset)

2. All Nonessential Equipment - OFF3. Land as soon as practical.

BATTERY OVERHEAT(BATT OVR TEMP ANNUNCIATOR)

1. Battery Master OFF

(If annunciator remains illuminated)

2. Land as soon as practical.


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ELECTRICAL SMOKE OR FIRE

1.

Oxygena. Crew Masks - DON

b. Oxygen Selector - OPEN

2. Cabin Mode - OFF3. Avionics Master Switch - OFF4. Nonessential Electrical Equipment - OFF

If fire or smoke ceases:1. Individually restore avionics and equipment previously turned off2. Isolate defective equipment

If fire or smoke persists:

1. Oxygena. Crew Masks DONb. Oxygen Selector - OPEN

2. Cabin Pressure Switch - DUMP3. Land as soon as possible

Note: Opening a storm window after depressurization will facilitate smoke and fume

removal.

4.3 Pressurization and Fuel:FUEL PUMP FAILURE(L or R FUEL PRESS ANNUNCIATOR)

1. Operative Fuel Pump - ON

2. FUEL PRESS Annunciator - OFFFUEL CROSSFEED

1. Fuel Selector (Inop. Engine) ON2. Crossfeed - ON3. Fuel Selector (Op engine) OFF

Before landing:

4. Fuel Selector (Op engine) ON5. Crossfeed OFF6. Fuel Selector (Inop engine) OFF


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PRESSURIZATION SYSTEM(RAPID DECOMPRESSION)

1. Oxygen

a. Crew Masks - DON

b. Oxygen Selector - OPEN

2. Initiate Emergency Descent

EMERGENCY DESCENT

1. Power Levers - IDLE

2. Propellers - FULL FORWARD

3. Flaps - APPROACH

4. Landing Gear - EXTEND

5. Airspeed - 181 KNOTS MAXIMUM


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4.4 Landing Gear and Trim:

LANDING GEAR MANUAL EXTENSION

1. Airspeed - ESTABLISH 130 KNOTS2. Landing Gear Handle - DOWN3. Landing Gear Relay CB - PULL4. Emergency Gear Extension Switch - ACTUATE5. Confirm gear down and locked.

UNSCHEDULED ELECTRIC ELEVATOR TRIM

1. Airplane Attitude - MAINTAIN

2. Elevator Trim CB - PULL


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5.0 PERFORMANCE

5.1 Takeoff Weight Flaps-0%


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5.2 Takeoff Weight-Flaps 40%


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5.3 Takeoff Flight Path


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5.4 Takeoff Distance-Flaps 0%


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5.5 Accelerate-stop-Flaps 0%


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5.6 Accelerate-go-Flaps 0%


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5.7 Net Gradient of Climb-Flaps 0%


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5.8 Takeoff Distance-Flaps 40%


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5.9 Accelerate-stop-Flaps 40%


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5.10 Accelerate-go-Flaps 40%


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5.11 Net Gradient of Climb-Flaps 40%


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5.12 Climb-Two Engines-Flaps 0%


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5.13 Climb-Two Engines-Flaps 40%


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5.14 Time, Fuel, and Distance to Climb


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5.15 Climb-One Engine Inoperative


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5.16 Service Ceiling-One Engine Inoperative


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5.17 Recommended Cruise Power-ISA -10C


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5.18 Recommended Cruise Power-ISA


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5.19 Recommended Cruise Power-ISA+10C


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5.20 Recommended Cruise Speeds


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5.21 Recommended Cruise Power


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5.22 Fuel Flow at Recommended Cruise Power


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5.23 Maximum Range Power


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5.24 Time, Fuel, and Distance to Descend


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5.25 Landing Distance Without Propeller Reversing-Flaps 100%


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5.26 Landing Distance Without Propeller Reversing-Flaps 0%


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5.28 Landing Distance With Propeller Reversing-Flaps 0%


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6.0 FLIGHT PROFILES

6.1 Precision Approach

KING AIR B210 PRECISION APR

LANDING

1. Props Full Forward2. Beta or Reverse

3. Brakes as Required

4. Discontinue Reverse at 60

KIAS

THRESHOLD

1. Airspeed - Vref2. Power - Idle

MISSED APPROACH

1. Power Max2. Pitch - 8 Nose Up (FD-GA)

3. Flaps Up

4. Gear Up

IAF

FAF

1. GP check2. 5Ts - complete

FAF

GLIDE SLOPE INTERCEPT

1. Gear Down

2. Before Landing Checklist to the line

2NM FROM FAF

1. Flaps Down

2. Below the Line

3. Speed Vref+20

SE Vref+25

INITIAL

1. Descent and Approachchecklist complete

2. Flaps Approach

3. Speed 140 KIAS


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KING AIR B2106.2 Non-precis ion Approach

KING AIR B210 NON-PRECISION

APPROACH

INITIAL

1. Descent and Approach

checklist complete

2. Flaps Approach3. Speed 140 KIAS

IAF INBOUND STARTING

DESCENT

1. Gear Down

2. Before Landing Checklist to the lin

MISSED APPROACH

1. Power Max

2. Pitch - 8 Nose Up (FD-GA)

3. Flaps Up4. Gear Up

THRESHOLD

1. Airspeed - Vref

2. Power - Idle

LANDING

1. Props Full Forward

2NM FROM FAF

1. Speed Vref+20

SE Vref+25

FAF1. 5Ts - completeLANDING ASSURED

1. Flaps Down

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