PREPARED
CHECKED
APPROVED
PIPER AIRCRAFT CORP. DEVELOPMENT CENTER, YERO BEACH, FLA.
Weight and Balance Data Model PA 28 - 180
PAGE 1 Section 1
ACTUAL WEIGHT AND BALANCE
MODEL PA 28 - 180
SERIAL NUMBER 28 - 2520
CERTIFICATE NUMBER N8338W
DATE May 27, 1965
"h.>
Theron Nolan Bevis DMLR 6085
PREPARED
CHECKED
PIPER AIRCRAFT CORP. DEVROPMENT CENTER, YERO BEACH, FLA.
Weight and Balance Data Model PA 28 - 180
PAGE 2 Section 1
WEIGHT AND BALANCE
STANDARD EQUIPMENT LIST
MODEL PA 28 - 180
Check if Installed
x
ITEM WEIGHT
(LBS.)
ARM AFT DATUM
(INCHES)
MOMENT (POUND -INCHES)
Engine Accessories
285
1.8
26.1
41.8
7439
75
Engine - Lycoming Model 0 -360 -A3A
Fuel Pump, Electric Auxiliary, Bendix Model 478360
x
x Fuel Pump, Engine Driven, Lycoming Dwg. No. 73297, 74082 or 75148 1.6 41.3 66
Oil Cooler, Piper Dwg. 18622 2.6 18.1 47
x Filter, Fram Model CA -161 PL or
x
AC No. A48C or Purolator AFP -2
Alternator, 35 Amp., Chrysler
.9 20.1 18
No. 2098615 12.5 19.0 238
Propeller and Propeller Accessories
Propeller, Sensenich M76EMM 34.5 10.1 349
Propeller, Sensenich M76EMMS60 38.5 8.8 339
Spinner and Attachment Plates 2.0 8.0 16
APPROVED
PREPARED
CHECKED
PIPER AIRCRAFT CORP. DEVELOPMENT CENTER, YERO BEACH, fl.A.
Weight and Balance Data Model PA 28 - 180
APPROVED PAGE 3 Section 1
ITEM
WEIGHT (LBS.)
ARM AFT
DATUM (INCHES)
MOMENT (POUND -INCHES)
Landing Gear and Brakes
Two Main Wheel Assemblies 6.00 -6
(a) Cleveland Aircraft Products
32.0 109.6 3507
Wheel Assembly No. 40 -28 Brake Assembly No. 30 - 18
(b) Two Main 4 -Ply Rating Tires 6.00 -6 with Regular Tubes
Two Main Wheel Assemblies (a) Cleveland Aircraft Products
32.3 109.6 3540
Wheel Assembly No. 40 - 86 Brake Assembly No. 30 - 55
(b) Two Main 4 -Ply Rating Tires 6.00 -6 with Regular Tubes
One Nose Wheel 6.00 -6 14.0 34.3 480 (a) Cleveland Aircraft Products
Wheel Assembly No. 38501 (Less Brake Drum)
Check if Installed
(b) One Nose Wheel 4 -Ply Rating Tire 6.00 -6 with Regular Tubes
x Electrical Equipment
Stall Warning Device, Safe Flight
x Inst . Corp. No. C52207 -4 .2 80.2
Voltage Regulator, Chrysler No. 2098613 .5 57.8 x
Battery 12V., 25 A.H., Rebat Model S -25 21.5 160.9
16
29
3459
x
x
PREPARED
CHECKED
PIPER AIRCRAFT CORP. DEVELOPMENT CENTER, VERB BEACH FLA.
Weight and Balance Data Model PA 28 - 180
PAGE 4 Section 1
Check if ITEM
WEIGHT (LBS.)
ARM AFT DATUM
IINCHES)
MOMENT (POUND-INCHES)
Installed
x
Instruments
Compass - Airpath No. C2350 - L41 .9 66.6 60
Airspeed Indicator, PAC 63205 .6 67.7 41
Tachometer, AC 1548302 .8 67.7 54
Tachometer, Stewart Warner PAC 62177 .7 67.7 47
Altimeter, Aero Marine No. 552 1.4 66.8 94
Engine Cluster, PAC 63922 .8 68.8 55
Engine Cluster, PAC 63426 .8 68.8 55
x
Miscellaneous
Fwd. Seat Belts 1.0 86.9 87
x Aft Seat Beits .8 123.0 98
Flight Manual
TOTAL
AIRCRAFT EMPTY WEIGHT AS COMPUTED
(INCLUDES ITEMS CHECKED ON STANDARD EQUIPMENT LIST)
1260 84.5 107584
APPROVED
PREPARED
CHECKED
PIPER AIRCRAFT CORP. DEVELOPMENT CENTER, VERO BEACH, FLA.
Weight and Balance Data Model PA 28 - 180
APPROVED
PAGE 5 Section 1
OPTIONAL EQUIPMENT LIST
MODEL PA 28 - 180
Check if ITEM
WEIGHT (LBS.)
ARM AFT DATUM
(INCHES)
MOMENT (POUND -INCHES)
Installed
x
Engine Accessories
Vacuum Pump, Airborne Mechanisms Model No. 10 - 113A1, 113A5 or 200cc 3.6 36.3 131
Electrical Equipment
Rotating Beacon, Grimes Model D7080 2.0 263.4 527
Landing Light, G. E. Model 4509 .5 18.1 9
Navigation Light (Rear) (1) Grimes
x Model 2064 (White) .1 280.9 28
Navigation Lights (2) Grimes Model A1285 Red and Green .4 106.6 43
Battery 12V, 33 A.H., Reading R -33 27.0 160.. 9 4344
Roll Servo Mitchell lx221E -CH - 1 2.8 60.6 170
Console Amplifier and Cables Mitchell lx214E 1.8 66.6 120
Cabin Light and Speaker 1.1 99.4 105
x Rotating Beacon, Whelan Model WRM L - 12 1.6 263.4 421
Auxiliary Power Receptacle PAC 62225 2.6 163.5 425
External Power Cable PAC 62355 -2 4.6 142.8 657
PREPARED
CHECKED
PIPER AIRCRAFT CORP. DEVELOPMENT CENTER, VERO BEACH, FLA.
Weight and Balance Data Model PA 28 - 180
PAGE 6 Section 1
Check if Installed
ITEM WEIGHT (LBS.)
ARM AFT MOMENT
DATUM (POUND
(INCHES) INCHES)
66.4 100
68.1 27
68.1 27
Standard Equipment Weight
Instruments
1.5
.4
.4
Same as
Turn and Bank, Pioneer A - 5
Suction Gauge, AN5771 - 11
Suction Gauge, U.S. Gauge AW1821AFO3
Altimeter, AN5760 - 2 (C12 or C13) x
Rate of Climb, Pioneer C -7 1.4 66.8 94
Directional Gyro, Vacuum 2.5 66.6 167
x Artificial Horizon, Vacuum
Air Temperature Gauge, Rochester
2.7 66.1 179
x
Manufacturing Co., No. 1592 -C2 .2 82.6 17
Clock, 8 Day .4 68.3 27
Directional Gyro, Vacuum (Auto Pilot) 4.3 66.6 286
Artificial Horizon, Vacuum (Auto Pilot) 4.5 66.1 298 x
Tru-Speed Indicator, PAC 62143 Same as Standard Equipment Weight
Piper Course Selector PAC 31058 3.0 66.6 200
APPROVED
PREPARED
CHECKED
PIPER AIRCRAFT CORP. DEVELOPMENT CENTER, YERO BEACH, RA.
Weight and Balance Data Model PA 28 - 180
APPROVED
Check if ITEM
WEIGHT (LBS.)
ARM AFT DATUM
(INCHES)
MOMENT (POUND INCHES)
Installed Radio
Piper Radio Compass PRC -3 4.5 64.4 290
Piper VHF Transceiver PTR - 1 5.0 64.8 324
Piper Omni Convertor 0 - 1 2.5 65.3 163
King KX 150A 9.1 62.8 572
x Omni Antenna 1.2 203.0 243
x Whip Antenna .7 131.0 92
Low Frequency Antenna .5 167.0 84
Loop Antenna (PRC -3) .3 54.5 16
x Narco Mark 12 VHF Transceiver 9.0 59.4 535
x Narco VOA -6 Omni Convertor
cl. <0
1.8
65.7
65.3
1,
118 5.1 ' '-i ,3 • 7 e
Narco VOA - 5 Omni Convertor 2.9 65.3 189
Narco ADF -30 9.9 107.9 1068
Narco Omnigator VTR - 2A 14.0 58.0 812 Installation (Less Ant.) Marker Antenna 1.2 64.8 78
Piper Radio Compass PRC -4 4.9 64.4 316
Loop Antenna (PRC -4) .4 112.6 45
Piper Omni Convertor OL - 1 2.8 65.3 183
Narco ADF -31 (Panel Unit) 4.8 64.4 309
Loop Antenna (ADF -31) 2.5 114.9 287
Loop Cable (ADF -31) 2.3 89.0 205
PAGE 7 Section 1
PREPARED
CHECKED
APFROVED
I
PIPER AIRCRAFT CORP. Weight and Balance Data
DEVELOPMENT CENTER, YERO BEACH, FLA. Model PA 28 - 180
PAGE 8 Section 1
t Sk :
k rder # TYPE RES T t RATION N83381.4
ARM AFT MOMENT WEIGHT DATUM (POUND - (LBS.) (INCHES) INCHES)
3.3 34.3 113
7.4 109.6 811
1.8 156.0 281
10.5 54.6 574
5.0 54.6 273
/ 3-g-14
ITEM Check if Installed Miscellaneous
x Nose Wheel Fairing
Main Wheel Fairing
Assist Step
Toe Brakes (Dual)
x Toe Brakes (Single)
Tra.spond er Pa,
Remote Unit 5
1Y Kx11 TanP 1
Power
Comm Antenn&
_TransPondiTAntgnna_
A i rQrArt_
0 _128.00
93E3.10
364. 80_
_448 . 50 _ a.
96. 50
32.,0_0_ .41
111398
w71114T MOMENT
13P7,Q,
7 0
efu ad
Signature f
he9dore . Burri4
' ,-32453.qo
New rersft r:mT. New E.W,C.
stalia.t Superviso r
PREPARED
CHECKED
PIPER AIRCRAFT CORP. DEVELOPMENT CENTER, VERO BEACH, RA.
Weight and Balance Data Model PA 28 - 180
PAGE 9 Section 1 APPROVED
IT IS THE RESPONSIBILITY OF THE PILOT AND AIRCRAFT OWNER TO INSURE THAT THE AIRPLANE IS LOADED PROPERLY. THE EMPTY WEIGHT C. G. IS FOR THE AIRPLANE AS DELIVERED FROM THE FACTORY. REFER TO FORM FAA -337 WHEN ALTERATIONS HAVE BEEN MADE.
C. G. RANGE AND WEIGHT INSTRUCTIONS
. Add the weight of all items to be loaded to the licensed empty weight. Use the loading graph to determine the moment of all items to be carried in the airplane. Add the moment of all items to be loaded to the licensed empty weight moment. Divide the total empty weight moment by the total empty weight to determine the C . G. arm aft datum. By using the figures of item 1 and item 4, locate a point on the C. G. range and weight graph. If the point falls within the C. G. envelope, the loading meets all weight and balance requirements.
SAMPLE LOADING PROBLEM
WEIGHT (LBS.)
ARM AFT DATUM (INCHES)
MOMENT (POUND - INCHES)
LICENSED EMPTY WEIGHT
1307 13442..3
85.2 SS. 4
1113 98 I v-i gia.a.t.
OIL (2 GA L.) 15 31.7 476
PILOT & PASSENGER 340 85.5 29070
FUEL 5C gal. 300 95.0 28500
PASSENGERS (REAR SEAT) 340 118.1 40154
BAGGAGE 98 142.8 13994
TOTAL LOADED AIRPLANE 2400 223592
223592' = 93.2 INCHES (ARM AFT DATUM) 2400
LOCATE THIS POINT ( 93.2 ) ON THE C. G. RANGE AND WEIGHT GRAPH. SINCE THIS POINT FALLS WITHIN THE C. G. ENVELOPE THE LOADING MEETS ALL WEIGHT AND BALANCE REQUIREMENTS.
40 45 50 20 25 30 35
. PREPARED
CHECKED amsaocesms•I
Weight & Balance Data Model PA 28 -180
PAGE 10 Section 1 APPROVED
10 15
LOADING GRAPH
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MOMENT/1000 (POUND INCHES)
450
400
100
50
0
350
300
150
LO
AD
WE
IGH
T
250
200
PREPARED
CHECKED
APPROVED
PIPER AIRCRAFT CORP. DEVEIONEV CENTER, VERO BEACH , flA.
C.G. RANGE AND WEIGHT
Weight & Balance Data Model PA 28 -180
jPAGE 11 Section 1
2400
2200
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1400
1200
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86 88 90 92 94 96
INCHES AFT OF DATUM
KINGS AVIONICS, INC.
PHONE (913) 829-4606
151ST AND PFLUMM • OLATHE, KANSAS 66062
MINOR ALTERATION
WEIGHT & BALANCE AND INSTALLED EQUIPMENT DATA
Date Make & Model Registration Number Serial Number
7-7-85 PA-28-180 N-8338W 8-2520
Owner: Bill Miller
Item Weight Arm Moment
A/C Empty Wtg:
Installed:
KN- 64
/ ' Ll / t
4,, ,-.3
1342.3
2.6
85.6
65.3
114912.26
169.78
1344.9 115082.04
Gross Weight = 2400
Empty Weight = 1344.9
Useful Load = 1055.1
C. G. (Arm) . 85.57
Signature f Authorized Individual
, i....- ,-4t4-4!3 ■2_-)
KINGS AVIONICS, INC.
Repair #364-78
"SPECIALIZED AVIONICS SERVICE"
CHEROKEE PA28-180 N8338W WEIGHT AND BALANCE
WEIGHT X ARM = MOMENT (pounds) (inches) (in-lbs)
EMPTY WEIGHT 1321.4 85.60 113106.09
FRONT PAX 85.5
REAR PAX 118.1
OIL (8QTS) 15 31.7 475.5
FUEL 95.0
BAGGAGE 142.8
TOTAL
MOMENT/WEIGHT = ARM
