Piper Aircraft Corporation Cherokee Arrow II Скачать руководство пользователя

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A. ELECTRIC PITCH TRIM INSTALLATION

LIMITATIONS

There are no limitations for this installation.

PROCEDURES

Preflight

( 1) Circuit breaker - Set

(2) Operate rocker switch - Trim fore and aft

(3) Manually override electric trim

(4) Check manual trim operation

ARROW

(5) If trim fails preflight, disengage electric trim by operating push button

trim switch on instrument panel until repaired. If trim does not

disengage have unit repaired before further flight.

lnflight

( 1) Activate rocker fore-aft trim

EMERGENCY OPERATION

In case of malfunction, disengage electric pitch trim by pushing pitch trim

switch on instrument panel to off position.

In an emergency, electric pitch trim may be overpowered using manual

pitch trim.

Jn cruise configuration, a malfunction can result in a 10

pitch change and

200 ft. altitude variation.

In approach configuration, a malfunction can result in a 5

pitch change

and 50 ft. altitude loss.

FAA APPROVED December 29, 1971

REPORT: VB-343 PAGE 3-16

MODEL: PA-28R-200

N16422 POH

Содержание Cherokee Arrow II

Страница 1: ...RAL SPECIFICATIONS 2 DESCRIPTION AIRPLANE AND SYSTEMS 3 FLIGHT MANUAL FAA APPROVED 4 EMERGENCY PROCEDURE 5 WEIGHT AND BALANCE 6 OPERATING INSTRUCTIONS 7 OPERATING TIPS 8 PERFORMANCE CHARTS 9 HANDLING...

Страница 2: ...GENERAL SPECIFICATIONS 1 1 Performance 1 1 Weights 1 1 Power Plant 1 2 Fuel and Oil 1 2 Baggage 1 2 1 2 Drme 1s1ons _ Landing Gear N16422 POH...

Страница 3: ...tude mi 780 Optimum Cruising Range 55 power optimum altitude mi 900 Stalling Speed flaps down gear down mph 64 Stalling Speed flaps and gear up mph 71 Landing Roll flaps down ft 780 Landing Roll Over...

Страница 4: ...ONS Wing Span ft Wing Area sq ft Wing Loading lbs per sq ft Length ft Height ft Power Loading lbs per hp LANDING GEAR Wheel Base ft Wheel Tread ft Tire Pressure psi Nose Main Tire Size Nose four ply r...

Страница 5: ...ARROW II 12 10 5 1 I63 __ __ ___ _ __J I I 1 32 2 5 GENERAL SPECIFICATIONS ISSUED November 15 1971 REVISED June 15 1972 l 1 3 N16422 POH...

Страница 6: ...S MANUFACTURER S MODEL PA 28R 200 MANUFACTURER S SERIAL 28R 7335145 REGISTRATION N 16422 FAA APPROVED BY c GLENN C STEPHEN PIPER AIRCRAFT CORPORATION D O A No SO 1 VERO BEACH FLORIDA DATE OF APPROVAL...

Страница 7: ...ight 2 H Baggage Capacity 2 I C G Range 2 J Maneuvers 3 K Placards 3 SECTION II Procedures A System Operations B Emergency Procedures SECTION ID Performance A Stalls SECTION IV 7 7 11 13 13 Supplement...

Страница 8: ...ARROW THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 343 PAGE 3 ii MODEL PA 28R 200 FAA APPROVED October 14 1971 N16422 POH...

Страница 9: ...Revised B 1 item g and B 2 item a 6 Title Added PAC Approval Form NOTE AIRCRAFf DELIVERED WITH MANUALS PRIOR TO THIS REVISION DO NOT REQUIRE THIS REVISION 7 3 1 Added figure to Oil Pressure Red Line...

Страница 10: ...ARROW THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 343 PAGE 3 iv MODEL PA 28R 200 FAA APPROVED October 14 1971 N16422 POH...

Страница 11: ...T MARKINGS Power Plant OIL TEMPERATURE Green Arc Normal Operating Range Red Line Maximum OIL PRESSURE Green Arc Normal Operating Range Yellow Arc Caution Range Red Line Minimum Red Line Maximum FUEL P...

Страница 12: ...S Positive Load Factor Maximum 3 8 G Negative Load Factor Maximum No inverted maneuvers approved MAXIMUM WEIGHT 2650 LBS BAGGAGE CAPACITY 200 LBS C G RANGE Weight Forward Limit Rearward Limit Pounds I...

Страница 13: ...Seat Backs Erect Fuel on Proper Tank Seat Back Erect Fasten Belts Harness TAKEOFF CHECK LIST Mixture Set Propeller Set Fasten Belts Harness LANDING CHECK LIST Electric Fuel Pump On Mixture Rich Prope...

Страница 14: ...view of the pilot when AutoFlite is installed FOR HEADING CHANGES PRESS DISENGAGE SWITCH ON CONTROL WHEEL CHANGE HEADING RELEASE DISENGAGE SWITCH On the instrument panel in full view of the pilot when...

Страница 15: ...e air conditioner controls when the air conditioner is installed WARNING AIR CONDITIONER MUST BE OFF TO INSURE NORMAL TAKEOFF CLIMB PERFORMANCE FAA APPROVED October 14 1971 REVISED February 10 1972 RE...

Страница 16: ...ARROW THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 343 PAGE MODEL PA 28R 200 FAA APPROVED October 14 1971 N16422 POH...

Страница 17: ...r i iiQ g Hgbt on the r instrument paneJ a rtd the hom operate imultan o sJy w cn _ r 1 In flight when the throttle is 1r educ ed to wher c the manifold pressure is approximately 14 inches of mercury...

Страница 18: ...be selected and latched before takeoff and the e i will th o retract as soon as the gear selector switch is placed in the up pdsition In this case care should be taken not to retract the gear prematu...

Страница 19: ...ARROW THIS PAGE INTENTIONALLY LEFT BLANK FAA APP O J _Op toper 14 1971 REPORT VB 343 PAGE 3 9 MODEL PA 28R 200 N16422 POH...

Страница 20: ...ARROW THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 343 PAGE 3 10 MODEL PA 28R 200 FAA APPROVED October 14 1971 N16422 POH...

Страница 21: ...backup gear extender raise emergency gear lever to Override Engaged position h If gear has still failed to lock down _ move emergency gear lever to Emergency Down position i If gear has still failed...

Страница 22: ...ARROW THIS PAGE INTENTIONALLY LEFT BLANK IJ EPORT VB 343 PAGE 3 12 MODtL PA lSR 200 FAA AP PROVED October 14 1971 N16422 POH...

Страница 23: ...erformance is given for 2650 pounds Loss of altitude during stalls varied from 100 to 300 feet depending on configuration and power Stalling speeds in mph power off versus angle of bank Calibrated air...

Страница 24: ...ARROW THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 343 PAGE 3 14 MODEL PA 28R 200 FAA APPROVED October 14 1971 N16422 POH...

Страница 25: ...IF THE EQUIPMENT WHICH IS THE SUBJECT OF THE SUPPLEMENT IS INSTALLED A Electric Pitch Trim Installation B AutoControl III Installation C AutoFlite II Installation D Air Conditioner Installation ARROW...

Страница 26: ...sengage have unit repaired before further flight b lnflight 1 Activate rocker fore aft trim 3 EMERGENCY OPERATION a In case of malfunction disengage electric pitch trim by pushing pitch trim switch on...

Страница 27: ...OFF 2 The AutoControl III can be overpowered at either control wheel 3 An autopilot runaway with a 3 second delay in the initiation of recovery while operating in a climb cruise or descending flight c...

Страница 28: ...OFF 2 Unit may be overpowered manually at either control wheel ARROW 3 An autopilot runaway with a 3 second delay in the initiation of recovery while operating in a climb cruise or descending flight...

Страница 29: ...er door is in the up position d If the AIR COND DOOR OPEN light does not respond as specified above an air conditioner system or indicator bulb malfunction is indicated and further investigation shoul...

Страница 30: ...anding Gear 2 3 Flight Controls 2 8 Fuel System 2 9 Electrical System 2 11 Vacuum System 2 14 Instrument Panel 2 1S Pitot Static System 2 1S Heating Ventilating and Defrosting System 2 18 Cabin Featur...

Страница 31: ...raft are a large cabin door and a large baggage compartment door Maintenance has been reduced to a minimum with advanced fuselage design The wing is of conventional design incorporating a laminar flow...

Страница 32: ...system incorporates a Bendix RSA SADI type fuel injector The injector is based on the principle of differential pressure which balances air pressure against fuel pressure The regulated fuel pressure...

Страница 33: ...ated mast is turned on whenever the PITOT HEAT is turned on WARNING Avoid ejecting objects out of the pilot storm window which could possibly enter or obstruct the holes in the mast The emergency gear...

Страница 34: ...ARROW II OVERRIDE LATCH 2 4 Throttle Quadrant Console AIRPLANE AND SYSTEMS REVISED August 30 1973 N16422 POH...

Страница 35: ...TE 21 aurn o E E PUMP OfrN 011 t IIOM PRESSURE HEAD ON FUSE QE SIDE STATIC MAmTAIN UP NOTE 11 1 RAM A o1 t rxtl _ AUT OIIAtlOIW II OWN SENSIIII iNOTE f1 0Rlf1CE ion 1 A 1 iAFT EQUIPPED WITH BACKUP BEA...

Страница 36: ...a hydraulic shimmy dampener to reduce nose wheel shimmy The oleo strots are of the air oil type with normal extension being 2 7 5 inches for the nose gear and 2 0 inches for the main gear under norma...

Страница 37: ...AIRPLANE AND SYSTEMS ISSUED Novemoer 15 1971 Main Wheel Assembly ARROWil BRAKE HOUSING 2 7 N16422 POH...

Страница 38: ...gives nose right trim and counterclockwise rotation gives nose left trim Ailerons are provided with differential deflection This feature reduces adverse yaw in turning maneuvers and thus reducing the...

Страница 39: ...nd RIGHT TANK The arrow on the handle of the selector points to the tank which is supplying fuel to the engine The valve also incorporates a safety latch which prevents inadvertently selecting the OFF...

Страница 40: ...ANK FUEL FLOW GAUGE FUEL PRESSURE GAUGE ff VENT FUEL QUANTITY GAUGE J fI ______ FU L LEn TANK SELECTOR ASCOUTOR ELECTRIC FUEL PUMP DRAIN ENGINE DRIVEN FUEL PUMP VENT Fuel Schematic SERVO REGULATOR AIR...

Страница 41: ...llision and landing lights are controlled by rock r switches on the switcb panel WARNING I J I 1 4 nti cotli 1 sion lig t 0 1 1P ngt be oper a ing when 0yin _ g throu h clouds fog_ or haze ince t ref...

Страница 42: ...987 i I J I I I _4 l f l i I Tl Ulam lUT lWffCI NOTES l s t I I I c r i 1 U AIR CRAFT EQUIPPED i i P S SEE NO E l J SIIIAT SIRCI WITH BACKu p GEAR EXTENDER I Ufl l IU I SUITII SIJ 01 ll llll l ll t n...

Страница 43: ...AIRPLANE AND SYSTEMS J I ISSUED November 15 1971 REVISED June 1S 1972 ARROW II Circuit Breaker Panel 2 13 N16422 POH...

Страница 44: ...cuum pump is a dry type pump which eliminates the need for an air oil separator and its plumbing A shear drive protects the pump from damage If the drive shears the gyros will become inoperative The v...

Страница 45: ...rottle and propeller controls The circuit breakers are protected by a cover door The climatic controls when the air conditioning system is installed are located in the right instrument panel above the...

Страница 46: ...IRSPEED INDICA TQR 117 TRANSCEIVERS 29 I I PITCH CONTROL 1 6 DIRECTION1L GYAQ 18 ADF 30 MAGNETO STAfTER SWITCH 7 ATTITUDE GYRO 1 i19 DME 1 3 1 FUEL GAUGES 8 GEAR UP WARNING LIGHT 20 SUCTION GAUGE 32 M...

Страница 47: ...AIRPLANE AND SYSTEMS ISSUED November 1s 1971 Static System ARROW IT 2 17 _ I N16422 POH...

Страница 48: ...s are placed too close to heat duct outlets or surface Defrosting is accomplished by heat outlets located on the right and left side of the cowl cover Heated air is ducted directly to defroster shut o...

Страница 49: ...I Heat Defrost and Ventilating System AIRPLANE AND SYSTEMS ISSUED November 1S 1971 REVISED June IS 1972 ARROWil I 2 19 I N16422 POH...

Страница 50: ...the shoulder adjacent to the window and attached to the lap belt in the general area of the occupant s inboard hip A check of the inertia reel mechanism can be made by pulling sharply on the strap and...

Страница 51: ...and gentle pitching may also precede the stall Stall speeds vs Angle of Bank for a gross weight of 2650 pounds are shown on a graph in the Performance Chart section During preflight the stall warning...

Страница 52: ...ARROW II 2 22 THIS PAGE INTENTIONALLY LEFT BLANK AIRPLANE AND SYSTEMS ISSUED November 15 1971 N16422 POH...

Страница 53: ...control center panel The temperature control regulates the desired temperature of the cabin Turn the control clockwise for increased cooling counterclockwise for decreased cooling Located inboard of t...

Страница 54: ...System SKETCH A Overhead Duct 2 24 EVAPORATOR INLET FILTER AIRPLANE AND SYSTEMS ISSUEO February 4 1972 O HEAD DUCT SKETCHA v 1 I _ SEE SKETCH C C OMP RESSOR CLIMATE cc r SEE SKETTROL PANEL 1 CHS J i...

Страница 55: ...CONDENSER AIRPLANE AND SYSTEMS ISSUED February 4 1972 REVISED June 15 1972 SKETCH 8 Oimate Control Panel SKETCH C Condenser ARR0Wll 2 25 N16422 POH...

Страница 56: ...hich disengages the compressor and retracts the scoop This is done to obtain maximum power and maximum rate of climb The fan continues to operate and the air will remain cool for approximately one min...

Страница 57: ...r Loss In Flight Power Off Landing I Gear Down Landing Gear Up Landing Propeller Overspeed Emergency Landing Gear Extension Spins Open Door Fire Loss of Oil Pressure Loss of Fuel Pressure High Oil Tem...

Страница 58: ...ures such as power off landings are a part of nonnal pilot training Although these emergencies are discussed here this infonnation is not intended to replace such training but only to provide a source...

Страница 59: ...TCH TO ANOTHER TANK CONTAINING FUEL c ELECTRIC FUEL PUMP CHECK ON d MIXTURE CHECK RICH e ALTERNATE AlR ON f EMERGENCY GEAR LEVER AS REQUIRED NOTE The landing gear will extend automatically when engine...

Страница 60: ...restore power If power loss is due to water fuel pressure indications will be normal NOTE If engine failure was caused by fuel exhaustion power will not be restored after tanks are switched until emp...

Страница 61: ...ake six to eight seconds to be down and locked If a gear up landing is desired it will be necessary to latch the override lever in the up position before airspeed drops to 115 mph to prevent landing g...

Страница 62: ...UCE AIRSPEED l i 1 l 5 i HROITLE AS REQUIRED TO REMAIN BELOW i 700 R P M _ I _ EMERGENCY LANDING GEAR EXTENSION ll _ I Accomplish the following checks prior to initiation of the emergency e xtension p...

Страница 63: ...J l gear will extend in this flight condition but will retract du ing recovery and has no adverse affect on the spin characteristics OPEN P O 1 3 1 t The ca bin door on the Cherokee Arrow II is latch...

Страница 64: ...m engine with starter This is an attempt to pull the fire into the engine b If engine has already started and is running continue operating to try pulling the fire into the engine c In either case sta...

Страница 65: ...ed A steady rapid rise in oil temperature is a sign of trouble Land at the nearest airport and let a mechanic investigate the problem Watch the oil pressure gauge for an accompanying loss of pressure...

Страница 66: ...WEIGHT AND BALANCE FOR CHEROKEE ARROW MODEL PA 28R 2OO ISSUED August 2 1972 REPORT VB 334 MODEL PA 28R 200 N16422 POH...

Страница 67: ...and Oil Systems 12 C Landing Gear and Brakes I 3 D Electrical Equipment 14 E Instruments 15 F Hydraulic Equipment 17 G Miscellaneous 18 H Engine and Engine Accessories Fuel and Oil System Optional Equ...

Страница 68: ...ARROW THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 334 PAGE 5 ii MODEL PA 28R 200 ISSUED October 14 1971 N16422 POH...

Страница 69: ...on Loop Antenna Add Tru Speed Indicator Correct Instrument Specification Numbers Change from Tum and Bank Piper 99005 to Tum and Slip Indicator Piper PS50030 2 or 3 Delete Tum Coordinators Add Page Ad...

Страница 70: ...l Form Oct 18 1974 NOTE AIRCRAFT DELIVERED WITH MANUALS PRIOR TO THIS REVISION DO NOT REQUIRE THIS REVISION Added Applicable Ser Nos Dec 5 1975 Revised Item Weight and Moment of _ tl 4 Vacuum Regulato...

Страница 71: ...ntended Before the aircraft is delivered the Arrow is weighed and a basic weight and C G location computed Basic weight consists of the empty weight of the aircraft plus the unusable fuel and full oil...

Страница 72: ...ARROW THlS PAGE INTENTIONALLY LEFT BLANK REPORT VB 334 PAGE 5 2 MODEL PA 28R 200 ISSUED October 14 1971 N16422 POH...

Страница 73: ...ne on each tank until all undrainable fuel is used and engine stops CAUTION Whenever the fuel system is completely drained and fuel is re plenished it will be necessary to run the engine for a minimum...

Страница 74: ...se 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 applies to the PA 28R 200 airplane when airplane is level S...

Страница 75: ...d parallel to the airplane centerline to each side of the nose wheel axle Then average the measurements d The empty weight center of gravity as weighed including optional equipment and undrainable oil...

Страница 76: ...ARROW THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 334 PAGE 5 6 MODEL PA 28R 200 ISSUED October 14 1971 N16422 POH...

Страница 77: ...es p s Weight X Lbs 1513 0 48 8 10 0 j71 8 ARROW C G Arm Inches Aft Moment of Datum In Lbs 83 5 126310 106 9 5219 103 0 1030 84 3 132559 LOAD NORMAL CATEGORY OPERATION eig t Licensed Empty Weight Usef...

Страница 78: ...Lbs Inches In Lbs I 1 I SOI I Licensed Empty Weight k A Atr J PYi32 559 t Oil 8 quarts 15 24 5 368 Pilot and Front Passenger 340 80 5 27370 Passengers Aft Rear Seat 340 118 1 40154 Fuel 50 Gal Maximum...

Страница 79: ...971 15 LOADING GRAPH J I I I 20 J J I 1 fl S 0 0 I I b I b 1 _ j fl _ I 03 it c e I q I I I I I I J I e r i C I 11 I 25 30 35 40 ARROW 45 50 MOMENT 1000 POUND INCHES REPORT VB 334 PAGE 5 9 MODEL PA 28...

Страница 80: ...BLE WEIGHT VS CENTER OF GRAVITY ENVELOPE WHILE IN FLIGHT C G RANGE AND WEIGHT 2800 2600 V 2400 z 2200 2000 1800 1600 1400 80 82 84 86 88 90 92 94 INCHES AFT OF DATUM MOMENT DUE TO RETRACTING LANDING G...

Страница 81: ...Item A Propellers and Propeller Accessories X Propeller Hartzell Model HC C2YK 1 7666A 2 or HC C2YK 1 F F7666A 2 X Spinner and Attachment Plate Installation PAC Dwg 99374 X Hydraulic Governor Hartzell...

Страница 82: ...Engine Driven Lycoming75247 X Alternator12V 60 Amp Chrysler 2642997 X Starter 12V Prestolite Model MZ 4206 Lycoming 76211 Oil Cooler PAC67848 REPORT VB 334 PAGE 5 12 MODEL PA 28R 200 Weight Ann Aft Ce...

Страница 83: ...Main 4 Ply Rating Tires 6 00 6 with Regular Tubes One Nose Wheel Assembly 40 77 Wheel Assembly Cleveland X less brake drum One 4 Ply Rating Tire 5 00 5 Regular Tube ISSUED October 14 1971 Weight Lbs...

Страница 84: ...co Electric No X 16300B X Overvoltage Relay Wico Electric No X 16799B X Starter Relay Piper Dwg 99130 2 X Landing Gear Motor Contactor Cole Hersee 24059 2 8 lbs each REPORT VB 334 PAGE 5 14 MODEL PA 2...

Страница 85: ...2 3 4 or 5 c Manifold Pressure and Fuel Flow Piper PS50031 6 Airspeed Indicator Piper PS 50049 5 ISSUED October 14 1971 REVISED July 10 1972 Weight Lbs 9 6 7 8 8 1 0 1 7 6 ARROW Ann Aft Cert Datum Mom...

Страница 86: ...ARROW TffiS PAGE INTENTIONALLY LEFr BLANK REPORT VB 334 PAGE S 16 MODEL PA 28R 200 ISSUED October 14 1971 N16422 POH...

Страница 87: ...mp Assembly Piper 67500 2 X Switch Pressure Consolidated Controls 211C243 3 X Valve Free Fall Piper 67522 2 X ISSUED October 14 1971 Weight Lbs 9 1 8 9 0 2 3 ARROW AnnAft Cert Datum Moment Basis 45 0...

Страница 88: ...Seat Piper Dwg 76171 l Individual Rear Seats 2 X Piper Dwg 99730 0 and I 13 5 lbs each X Flight Manual and Logs X Tow Bar Piper Dwg 67336 0 REPORT VB 334 PAGE 5 18 MODEL PA 28R 200 Weight L bs 1 5 1 4...

Страница 89: ...ARROW THIS PAGE INTENTIONALLY LEFT BLANK ISSUED ISSUED October 14 1971 REPORT VB 334 PAGE S 19 MODEL PA 28R 200 N16422 POH...

Страница 90: ...ent Vacuum Pump X Airborne Manufacturing Co Model 200CC X Oil Filter with Adapter AC 0F5578770 3 3 lbs each Lycoming 75528 REPORT VB 334 PAGE 5 20 MODEL PA 28R 200 Weight Lbs 5 0 3 3 Arm Aft Cert Datu...

Страница 91: ...ry Power Receptacle Piper 65647 2 7 178 5 482 TC 2Al3 External Power Cable Piper 62355 2 4 6 142 8 657 TC 2A13 Cabin Speaker Quincy Spkr Co 8B l 5052 or Oaktron Ind GEV 1937 8 99 0 79 TC 2A13 _ L Cabi...

Страница 92: ...lights Light Fin Tip A408 Cable Fin Light A4 l7 l 300 Lights Wing Tip 2 0 15 lbs each No A429 Cable Wing Lights A417 1 298 A417 l 252 Electric Trim System REPORT VB 334 PAGE S 22 MODEL PA 28R 200 Weig...

Страница 93: ...ble Panel Unit 1152D75 3 or 4 ISSUED October 14 1971 REVISED December 29 1971 Weight Lbs 2 5 1 2 7 2 3 3 2 9 2 5 7 2 4 ARROW Arm Aft Cert Datum Moment Basis 122 2 306 STC SAl 406SW 60 1 72 STC SA1406S...

Страница 94: ...ARROW THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 334 PAGE 5 24 MODEL PA 28R 200 ISSUED October 14 1971 N16422 POH...

Страница 95: ...a 3 192 8 58 TC2A13 Cable n2 VHF Comm Antenna 5 147 5 60 TC2Al3 Anti Static Kit It 1 VHF Comm Antenna 1 0 160 8 16 1 TC2A13 Cable II1 VHF Comm Antenna 4 103 4 4 1 TC2Al3 112 VHF Comm Antenna 1 0 195 8...

Страница 96: ...le REPORT VB 334 PAGE 5 26 MODEL PA 28R 200 Weight Lbs 3 9 3 6 7 1 1 9 2 8 3 4 5 6 7 5 15 0 2 5 3 3 5 0 5 9 5 9 5 0 1 6 5 0 2 5 2 3 4 4 3 1 2 1 3 1 8 8 4 Arm Aft Cert Datum Moment Basis 57 4 224 TC 2A...

Страница 97: ...6 78 Transponder Panel Unit Antenna Cable ISSUED October 14 1971 REVISED November 14 1972 Weight Lbs 1 1 3 3 2 4 1 8 4 5 6 8 2 3 2 3 I 3 1 7 1 8 1 1 1 7 2 33 3 1 ARROW ArmAft Cert Datum Moment Basis 1...

Страница 98: ...I 520 VOR ILS I ndicator King KX 175 VHF Tra nscei ver 2nd King KN 77 VOR LOCConv King X NI 520 VOR ILS Indicator REPORT VB 334 PAGE S 28 MODEL PA 28R 200 Weight Lb s 2 0 5 7 4 3 3 0 2 8 5 4 7 5 5 9 4...

Страница 99: ...lock Piper99478 Turn and Slip Indicator Piper PS50030 2 or 3 Exhaust Gas Temperature Gauge Piper99026 Tru Speed lndicator Piper67433 2 or 3 or PS50049 4 ISSUED October 14 1971 REVISED December 5 1975...

Страница 100: ...ARROW TIDS PAGE INTENTIONALLY LEFT BLANK REPORT VB 334 PAGE S 30 MODEL PA 28R 200 l UED October 14 1971 N16422 POH...

Страница 101: ...s Rear 2 99255 3 1 0 lbs each 2 0 Overhead Vent System Piper 1 2 Alternate Static Source 4 Zinc Chromate Finish 5 0 Air Conditioner Instl 68 9 Calibrated Alternate Static Source Placard Required Yes N...

Страница 102: ...OW EXTERIOR FINISH Base Color ______ Trim Color ______ Accent Color ______ REPORT VB 334 PAGE S 32 MODEL PA 28R 200 Registration No Color ______ Type Finish _________ __ ISSUED October 14 1971 N16422...

Страница 103: ...5 N 28R7335145 Call sign N16422 Old empty wgt 1603 7 Old empyt wgt cg 82 65 Old useful load 1046 3 Old moment 132 550 02 IRCRAFT WAS WEIGHED 10 15 14 Revised Weight Balance Page 1 Taken from W B Dated...

Страница 104: ...tarting Engine When Flooded 6 3 Warm Up and Ground Check 6 3 Take Off 6 4 O imb 6 5 Stalls 6 5 Cruising 6 5 Approach and Landing 6 6 Stopping Engine 6 7 Moorings 6 7 Weight and Balance 6 7 Air Conditi...

Страница 105: ...r wheel control_lock 1 2 3 a Check for external damage and operational interference of control surfaces or hinges b Insure that wings and control surfaces are free of snow ice or frost a Visually chec...

Страница 106: ...red papers are in order and in the airplane STARTING ENGINE After completetion of the preflight inspection 1 Set parking brakes ON 2 Set the propeller control in full INCREASE RPM control forward 3 Se...

Страница 107: ...NOT ATTEMPT FLIGHT IF THERE IS NO INDJCATION OF ALTERNATOR OUTPUT When the engine is firing evenly advance the throttle to 800 RPM If oil pressure is not indicated within 30 seconds stop the engine an...

Страница 108: ...ight instruments checked and set as required 5 Master Switch ON 6 Alternate air closed 7 Prop set 8 Mixture set 9 Seat backs erect 10 Fasten belts harness 11 Empty seats seat belts snugly fastened 12...

Страница 109: ...his will produce better forward speed and increase visibility over the nose during the climb with little sacrifice in rate of climb Air f rt1 tif PfifJ 9 Y e t JllQJ f t r all pbstacics haYe bee n cle...

Страница 110: ...sl ould be used alfemately from eaqh t 1 k Jt is recQm m_epd _g_ t l on tat k _be uied fq r one hour_after tak t f then the oth t b e u o r ifl it t n m ta 1Jre ffrst ta nk for one hour ia eh ffit Wn...

Страница 111: ...lied to the control wheel putting most of the airplane weight on the main wheels without lifting the nose wheel In high wind conditions although it may be desirable to approach at higher than normal s...

Страница 112: ...ARROW II 6 8 THIS PAGE INTENTIONALLY LEFT BLANK OPERATING INSTRUCTIONS ISSUED November 15 1971 N16422 POH...

Страница 113: ...THJS PAGE INTENTIONALLY LEFT BLANK OPERATING INSTRUCTIONS ISSUED February 4 1972 ARROW 11 6 9 N16422 POH...

Страница 114: ...ARROWD 6 10 Tms PAGE INTENTIONALLY LEFT BLANK OPERATING INSTRUCTIONS ISSUED February 4 1972 N16422 POH...

Страница 115: ...the Air Cond Door Open light does not respond as specified above an air conditioner system or indicator bulb malfunction is indicated and further investigation should be conducted prior to fljght The...

Страница 116: ...laced if the transmitter has been used in an emergency situation or if the accumulated test time exceeds one hour The replacement date is marked on the transmitter label The unit has a three position...

Страница 117: ...starting the engine check that all radio switches light switches and the pitot heat switch are in the off position so as not to create an overloaded condition when the starter is engaged 10 A hlgh fu...

Страница 118: ...der pedals or operating the toe brakes 15 The shape of the wing fuel tanks is such that in certain maneuvers the fuel may move away from the tank outlet If the outlet is uncovered the fuel flow will b...

Страница 119: ...Density Altitude 8 2 Rate of Oimb vs Densi ty Altitude 8 3 True Airspeed vs Density Altitude 8 4 Range vs Density Altitude 8 5 Stalling Speed vs Angle of Banlc 8 6 Glide Distance vs Altitude 8 7 Landi...

Страница 120: ...STING TEMPERATURE AND PRESSURE ALTITUDE CONDITIONS FOR USE WITH PERFORMANCE CHARTS l STD l TEMP it i l l l i__ i _ i i _ Y _ rr 1 v __ L J I __ t I l v __ 20 0 20 40 60 80 100 TEMPERATURE F J PERFORMA...

Страница 121: ...I I I I I S f _ Q_ Q ti ti s Q Q j 25 FLAPS co _co c ic t I 0 FLAPS I I I I i I I I I I REF SHORT FIELD OBSTACLE CLEARANCE PROCEDURE IN I SECTION Ill I I 1 1000 2000 3000 4000 5000 TAKE OFF DISTANCE...

Страница 122: ...JlP GEAR AND FLAPS RETRACTED GROSS WT 2650 LBS MIXTURE LEAN PER LYCOMING INSTRUCTION 200 1 400 600 800 1000 RATE OF CLIMB 1n MIN I NOTE SEE SECTION 6 FOR EFFECTS OF AIR COHOITIOHIHG INSTALLATION OH RA...

Страница 123: ...MIXTURE LEAN PER LYCOMING INSTRUCTION JI I I j le 1 g I o I I I I A 1 I i I I 1 _ I 1 1 I I 130 I I 140 150 1 0 170 180 TRUE AIRSPEED MPH MOTE SEE SECTION 6 FOR EFFECTS OF AIR CONDITIONING INSTALLATI...

Страница 124: ...1 r t t r l I I C 8000 I I r I 6000 I I I r l l 1 l I I I II I 4000 t i 1 H I I I NO RESERVE 45 MIN RES I I I I 2000 t t t t 1 I I I I j I I 0 ____ _____ ____ _ __ __ __ ___ ____ _ __ _L __L______J__...

Страница 125: ...OA 00 0 10 i 20 GROSS WEIGHT 2650 POWER OFF V 3 I Co I __ o __ 30 40 50 60 70 ANGLE OF BANK DEGREES PERFORMANCE CHARTS ISSUED overnber 1S 1971 I 7 I I I I f f I f I I i I I I I I I I 4 I f I I f I _ l...

Страница 126: ...t t i 2 i l l l I Uv iC f I I l r i i t t I I j I a 10 0 f _ I _ t 1 r _ J h lt i _J 1 r _ f r l J i r C 1 f 1 I fr f 1 a w 1 f y f i I w 0 CXl w a I 8000 6000 4000 2000 0 r I j I 0 t I J I I 6 I I i...

Страница 127: ..._ J _ L lrof f Ji ltW I I i 1 1 t t p OO a trw ll i t1 it 1 _ t FLAPS 40 POWER OFFP A VED LEVE ti RY UNWAY N OWIND MAX IMUM 8R A KI N 6 SHORT F IE m i OfT f G ROS SW E IG HT2650LBS i _ e i 1 fl 1 I 1...

Страница 128: ...25 1 22 2 24 7 3 000 4 000 45 21 9 19 5 24 8 22 0 24 4 4 000 5 000 41 21 7 19 3 FT 21 7 FT 5 000 6 000 38 21 4 19 1 21 5 6 000 7 000 34 21 2 18 9 21 3 7 000 8 000 31 21 0 18 7 21 0 8 000 9 000 27 FT...

Страница 129: ...by a qualified pilot or other responsible person Engine starting and shut down procedures should be covered as well as taxi techniques When it is ascertained that the propeller back blast and taxi ar...

Страница 130: ...ld be moored to insure its immovability protection and security under varying weather conditions The following procedure should be used for proper mooring of the airplane a Head the airplane into the...

Страница 131: ...ess solvent has evaporated or otherwise been removed d Remove the protective covers from the magnetos e Lubricate controls bearing surfaces etc in accordance with the Lubrication Chart CLEANING LAND I...

Страница 132: ...h clean water b Wash with mild soap and wann water c r an aircraft plastic cleaner Use a soft cloth or sponge using a straight rubbing motion Do not rub surface harshly c Remove oil and grease with a...

Страница 133: ...aced The usable life of the filter should be restricted to one year or 500 hours whichever comes first JNSTALLATION OF INDUCTION AIR FILTER a After cleaning or replacing filter install filter in rever...

Страница 134: ...ing gear or other service two hydraulic jacks and a tail stand should be used At least 250 pounds of ballast should be placed on the base of the tail stand before the airplane is jacked up The hydraul...

Страница 135: ...50 hours of operation The following grades are required for temperatures Temperatures above 60 F Temperatures between 30 F and 90 F Temperatures between O F and 70 F Temperatures below 10 F FUEL SYSTE...

Страница 136: ...installation and the relationship of tire tube and wheel should be maintained upon reinstallation In the installation of new components it may be necessary to rebalance the wheels with the tires mount...

Страница 137: ...WINTERIZATION For winter operation a winterization kit is installed on the inlet opening of the oil cooler plenum chamber This kit should be installed whenever the ambient temperature is 50 F or less...

Страница 138: ...ARROW II 9 10 THIS PAGE INTENTIONALLY LEFT BLANK a I l j I HANDLING AND SERVICING ISSUED November 15 1971 u J N16422 POH...

Страница 139: ...s and optional equipment which were not available originally and which may be of interest to the awner If an owner is not having h is aircraft serviced by an Authorized Piper Service Center he should...

Страница 140: ...rates and which is not used in air carrier service The following is a list of the maintenance which the pilot may perform 9 12 I Repair or change tires and tubes 2 Service landing gear wheel bearings...

Страница 141: ...signed by an Inspection Authorized JA mcc hanic or a General Aviation Disfrict Office GADO representative This inspection is requi_red whether the aircraft is operated commercially or for pleasure A...

Страница 142: ...IL t FII M l OMASE Ji ON AAFTE WITHIACICuPt EXlENqal G PAll R O l IIIGU JIIRICAHT i H AERO tlJMIPLAT E FISKE fROS t i l _ 1 ffE FINING CO S C TIONS FLUOffOCMIIO LEASE MS 12 1 i AGENT ORY lUMICANT I 1...

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Piper Aircraft Corporation Cherokee Arrow II, Руководство по эксплуатации

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