Piper Aircraft Corporation Cherokee PA-28-180 Airplane Flight Manual Download Page 5 | Manualshive

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Summary of Contents for Cherokee PA-28-180

Page 1: ...f Engineering Manufacturing Branch Southern Region Atlanta Georgia DATE August 3 1962 FAA APPROVED C e u 7 Gene Dearing Aerospace Engineer For Retype Only DATE August 12 1964 VH CHJ THIS AFM HAS BEEN...

Page 2: ...lacard No 5 Supervisor 7 8 64 Added to Placard No 3 BAGGAGE MAX 200 LBS z csupervisor 8 5 64 SEE WEIGHT AND BALANCE SO EMD0 43 DATA FOR BAGGAGE LOADINGS BETWEEN 150 LBS AND 200 LBS l 1 Added Sensenich...

Page 3: ...III Approved Date Added Page 6 I 7 l c_ Henry C Falier 7 15 66 Supervisor Limitations Section Add or 0 360 A4A C G Range Placard No 1 and Placard No 3 revised to include utility category operations SO...

Page 4: ...Placard No 4 and No 7 to read In full view of the pilot Added Aircraft Serial Numbers 1571 and 1573 to Engine and Propeller Limitations Added Propeller Designations Allocated Piper Report No VB 163 to...

Page 5: ...thru 5600 Changed applicable Serial Nos from 1 thru 5600 to S71 thru 56 00 Added Forward Ir1termediate and Forward Gross Weight Points Deleted Forward Intermediate and Forward Gross Weight Points Cha...

Page 6: ...ic RPM at maximum permissible throttle setting Not over 2450 not under 2275 No additional tolerance permitted Oil temperature GREEN arc normal operating range 1200F to 45 F YELLOW arc caution range 60...

Page 7: ...al Category Forward Limit Weight Pounds In Aft of Datum 2400 2200 1975 1650 2 Utility Category 92 l 89 2 85 9 84 0 Weight Forward Limit Pounds In Aft of Datum 1950 85 8 1650 84 0 Rearward Limit In Aft...

Page 8: ...H BEFORE FLIGHT On the inside of the baggage compartment door MAXIMUM BAGGAGE 125 LBS S N 671 to 1760A MAXIMUM BAGGAGE MAY BE INCREASED TO 200 LBS IN ACCORD ANCE WITH PIPER SERVICE SPARES LEITER NO 24...

Page 9: ...The following information is noteworthy a The stall characteristics of the PA 28 180 are normal with the nose pitching down moderately following the stall occasionally with a moderate roll which can b...

Page 10: ...e of autoflite malfunction a In case of malfunction PRESS disconnect switch on pilot s control wheel b Rocker switch on instrument panel ORF c Unit may be overpowered manually d In cruise configuratio...

Page 11: ...FAA Type tests and may be realized under conditions indicated with the airplane and engine in good condition and with average piloting technique All performance is given for 2400 potmds Loss of altitu...

Page 12: ...NUAL SUPPLEMENT IS APPLICABLE TO AIRCRAFT WITH SERIAL NUMBERS 28 671 TO 28 3072 I0 CLUSIVE WHEN PIPER PART NO 65280 00 TUBE LANDING GEAR STRUT PISTON IS INSTALLED SERIAL NUMBERS 28 3073 TO 28 5859 MAY...

Page 13: ...ane Flignt Manual i Supplement I CHICKIO OEHlOPiHXT CUTER nan SUCH FLA Iodel PA 2 8 1 80 I MPltOVSI PU REPORT V13 261 i i t_IPER MODEL PA 28 180 zg c I I REVISION I AGE APPROVED DATE NO I I I I I I I...

Page 14: ...performance data not contained in this document consult the manual proper 1 Limitations Section Maximum Weight C G Range 2 Procedures 3 Performance FAA APPROVED 9 14 70 REVISED The following limitatio...

Page 15: ...I Ul AilCD FAAA roved9 14 70 PI PER O HlOPM U AIRCRAFT CUTEI YEU REPORT VB 261 C0RP IUCH FlA C G RANGE AND WEIGHT INCHES AFT OF DATU t 1 Airplane Flight 1anual Supplement tv1odel PA 28 l80 PUE 2 or 2...

Page 16: ...of Datum In lbs Actual Standard Empty Weight Computed Optional Equipment Unusable Fuel 3 Pints _2 2 103 0 227 Licensed Empty Weight Total of Above Items Standard Empty Weight includes paint hydraulic...

Page 17: ...If the point falls within the C G envelope the loading meets the weight and balance requirements SAMPLE LOADING PROBLEM Normal Categorl Weight Arm Aft Datum Moment lbs Inches In Lbs Licensed Empty We...

Page 18: ...CHECKED APPROVED 5 10 PIPER AIRCRAFT CORP DEVELOPMENT Cf TER VERO BEACH _ FLA r REPORT VB 165 LOADING GRAPH 15 20 25 30 35 40 MOMENT 1000 POUND INCHES 45 Weight Balance Data Model PA 28 180 PAGE 3 Sec...

Page 19: ...Section 1 C G RANGE AND WEIGHT i i f _ _ r fJ 3 H 4 l 1 1 1 t 1 r t H t t f f l l H t H t 7 r l t i t t j l w i l l 1 I I I I ttt P J f H J tr f j 1q t t t j j 1 t1 t J J_ t t t H i J j t i tjt ttl j...

Page 20: ...ve dirt grease moisture foreign items such as rags and tools from the airplane before weighing c Defuel airplane Then open all fuel drains until all remaining fuel is drained Operate engine on each ta...

Page 21: ...Net Scale Position and Symbol Reading Tare Weight Nose Wheel N Right Main Wheel R Left Main Wheel L Airplane Empty Weight as Weighed T 4 EMPTY WEIGHT CENTER OF GRAVITY a The following geometry applie...

Page 22: ...heel centerline c Obtain measurement B by measuring the distance from the main wheel center iine horizontally and parallel to the airplane centerline to each side of the nose wheel axle Then average t...

Page 23: ...PUPAUD PIPER A t R C aAFT CORP Weight and Balance Data c caD DEYELOPIEIT Cfll 1 YEIO BEACH FLA Model PA 28 180 APNOVID PUE Title REPORT VB 165 EQUIPMENT LIST MODEL PA 28 180 SERIAL NOS 4378 THRU 5859...

Page 24: ...2 Added Narco Mark 16 fustallations CJ i _ 7 U If Added Adjustable Front Seat fustal lations and Overhead Vent System Added Strobe Light Whelen Engineering Company q t C _ I o c Removed Piper Drawing...

Page 25: ...and Balance Data Model PA 28 180 PACI iii DESCRIPTION APPROVED DATE Deleted Flight Manual Supplement q tt t _ Added Serial Nos 4378 thru 5859 Deleted Page 4a _Delet d Individual Rear Seats Adqed Stro...

Page 26: ...wg Harrison C 8526250 2 6 Filter Fram Model CA 161 PL or AC No A48C or Purolator AFP 2 Alternator 35 Amp Chrysler No 2098615 Alternator 60 Amp Chrysler No 2642210 or 2642997 Starter Lycoming 74092 Del...

Page 27: ...ake Assembly No 30 55 b Two Main 4 Ply Rating Tires 6 00 6 with Regular Tubes One Nose Wheel 6 00 6 12 5 a Cleveland Aircraft Products Wheel Assembly No 38501 Less Brake Drum Weight and Balance Data M...

Page 28: ...rspeed Indicator Piper Drawing 63205 2 6 66 8 40 Tachometer Piper Drawing 62177 3 7 66 2 46 Altimeter Piper Drawing 67467 1 0 65 9 66 Engine Cluster Piper Drawing 65852 2 8 67 4 54 Engine Cluster Pipe...

Page 29: ...acon Grimes 40 0101 7 12 or Grimes 40 0101 15 12 Landing Light G E Model 4509 Navigation Light Rear 1 Grimes Model 2064 White Navigation Lights 2 Grimes Model A1285 Red and Green Batterfu 12V 35 A H R...

Page 30: ...3 2 7 External Power Cable PAC 62355 2 4 6 Piper Pitch Trim 4 0 Heated Pitot Head 4 Strobe Light Whelen Engineering Co 2 7 Instruments Sucti n Gauge Piper Drawing 67481 5 Suction Gauge U S Gauge AW182...

Page 31: ...2 4 3 1 1 8 2 2 2 4 Weight and Balance Data Model PA 28 180 PAGE 13 Section 1 ARM AFT DATUM INCHES 64 9 65 9 64 7 64 0 64 9 64 4 82 6 67 4 MOMENT POUND INCHES 143 66 155 198 117 142 17 27 Tru Speed In...

Page 32: ...6 Garwin Attitude Gyro Mitchell 52D66 AIM Directional Gyro Mitchell 52D54P Garwin Directional Gyro Mitchell 52D54P AIM Omni Coupler AutoFlite Roll Servo Mitchell 1D363 183R Gyro Amplifier Mitchell 1C3...

Page 33: ...7 1 4 VHF Antenna Transmitting VHF 1 3 VHF Antenna Transmitting VHF 2 3 Cable VHF 1 4 Cable VHF 2 5 Low Frequency Antenna 5 Loop Antenna PRC 3 3 Omni Tracker 1D482 5 Narco Mark 12A or Narco Mark 12B T...

Page 34: ...6 Omni Convertor 1 8 64 4 116 Narco VOA 5 Omni Convertor 3 1 64 4 200 Narco VOA 4 Omni Convertor 3 0 64 4 193 Narco VOA 4 Omni Convertor 3 0 64 4 193 Narco ADF 31A Piper Drawing 67456 Panel Unit 4 8...

Page 35: ...470 Narco VDI 4 DME Receiver 8 5 61 7 524 Antenna 3 113 9 34 Cable Antenna 4 100 0 40 UGR 2 Glide Slope Receiver 2 4 173 8 417 Cable 2 1 128 0 269 Antenna 4 92 4 37 Cable Antenna 5 145 0 73 Transmitt...

Page 36: ...With Brackets Adjustable Front Seat Left Adjustabl Front Seat Right Overhead Vent System Alternate Static Source Calibrated Alternate Static Source Placard Required Yes__No__ TOTAL OPTIONAL EQUIPMENT...

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