Page 1 N16422 POH TABLE OF CONTENTS GENERAL SPECIFICATIONS DESCRIPTION-AIRPLANE AND SYSTEMS FLIGHT MANUAL FAA APPROVED EMERGENCY PROCEDURE WEIGHT AND BALANCE OPERATING INSTRUCTIONS OPERATING TIPS PERFORMANCE CHARTS HANDLING AND SERVICING...
Page 2 N16422 POH GENERAL SPECIFICATIONS r m ance ..• • · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · Perf : 1-1 Weight...
Page 3 N16422 POH ARROW II SPECIFICATIONS PERFORMANCE Performance figures are for airplanes equipped for cross-country transportation and flown at gross weight under standard conditions at sea level or stated altitude. Any changes in equipment may result in changes in performance. ° Take-off Run (maximum effort, 25 flap) (ft) °...
Page 4 ARROW.II N16422 POH FUEL AND OIL Usable Fuel Capacity (U. S. gal) Oil Capacity (qts) Fuel, Aviation Grade (min octane) 100/130 BAGG AGE Maximum Baggage (lbs) Baggage Space (cu ft) Baggage Door Size (in) DIMENSIONS 32.2 Wing Span (ft) Wing Area (sq ft) Wing Loading (lbs per sq ft) 15.6 Length (ft)
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Page 7: Table Of Contents
D. Air Conditioner Installation ......19 FAA APPROVED 1 4, 1971 REPORT: VB-343 PAGE 3-i REVISED: February 10, 1972 MODEL: PA-28R-200 October...
Page 8 N16422 POH ARROW THIS PAGE INTENTIONALLY LEFT BLANK REPORT: VB-343 PAGE 3-ii FAA APPROVED October 14, 1971 MODEL: PA-28R-200...
Page 9: Log Of Revisions
Added figure to Oil Pressure Red Line !Jee. 5, I 975 (Minimum) Limitation. �EV�-- Ward Evans 3-11 April 10, 1979 Revised item B. 1. f ., JJ-,J\ •:.O.�- Ward Evans FAA APPROVED October 14, 1971 REPORT: VB-343 PAGE 3-iii MODEL: PA-28R-200 REVISED: APRIL 10, 1979...
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Page 11: Limitations
N16422 POH...
Page 12: Airspeed Limitations And Instrument Markings (Calibrated Airspeed)
It is the responsibility of the airplane owner and the pilot to insure that the airplane is properly loaded. See "Weight and Balance Section" for proper loading instructions. PORT: VB-343 PAGE 3-2 DEL: PA-28R-200 FAA APPROVED October 14, 1971 REVISED: January 21, 1972...
Page 13: Maneuvers
N16422 POH ARROW MANEUVERS All acrobatic maneuvers including prohibited. spins PLACARDS In full view of the pilot: "THIS AIRCRAFT APPROVED FOR NIGHT IFR NON-I -::ING FLIGHT WHEN EQUIPPED IN ACCORDANCE WITH FAR 91 OR FAR 135." "THIS AIRCRAFT MUST BE OPERATED AS A NORMAL CATEGORY AIRPLANE IN COMPLIANCE WITH THE OPERATING LIMITATIONS STATED IN THE FORM OF...
Page 14 ARROW N16422 POH Adjacent to upper door latch: "ENGAGE LATCH BEFORE FLIGHT' On the inside of the baggage compartment door: "BAGGAGE MAXIMUM 200 LBS. SEE WEIGHT AND BALANCE DATA FO BAGGAGE LAODINGS BETWEEN 150 LBS AND 200 LBS." Near emergency gear lever: "EMERGENCY DOWN"...
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Page 16 ARROW N16422 POH THIS PAGE INTENTIONALLY LEFT BLANK REPORT: VB-343 PAGE� MODEL: PA-28R-200 ,FAA APPROVED October 14, 1971...
Page 17: A. System Opera Tio Ns
N16422 POH AR RO W SECTION II PR(,)CEDURES A. SYSTEM OPERA TIO NS • • · . · ; · The: stall-warning system is inoperative with the master swhch off. The electric fuel pump must be on ,for both landing and takeoff. Some aircraft are equipped with an airspeed - power sensing system (back-up gear extender) which extends the landing gear under low airspeed - power conditions•...
Page 18 N16422 POH · ;� Takeoff considerations: After takeoff on aircraft equipped with the back':,I P geaf e 9er, if the gear selector � � switch is placed in the gear up position before reaching the ai n1 p��d at which the system ' :t!O longer commands gear d'own, •...
Page 19 N16422 POH ARROW THIS PAGE INTENTIONALLY LEFT BLANK APP�O�J}.-_ Op ,toper 14, 1971 REPORT: VB-343 PAGE 3-9 MODEL: PA-28R-200...
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Page 21: Emergency Procedures
N16422 POH B. EMERGENCY PROCEDURES • =:· rg_f j\ �f la ding g nsio� ips r1,1ctio(1s: · •·J" •• • ,, , .• . • A��'�t1l!;5fi. t� following c.h cks prior to i iatfon •of the eme , r: g cy extension proc rd tir...
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Page 23: Performance
N16422 POH ARROW SECTION PERFORMANCE STALLS The following performance figures were obtained during 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 2650 pounds. Loss of altitude during stalls varied from 100 to 300 feet, depending on configuration and power.
Page 24 N16422 POH ARROW THIS PAGE INTENTIONALLY LEFT BLANK REPORT: VB-343 PAGE 3-14 FAA APPROVED October 14, 1971 MODEL: PA-28R-200...
Page 25: Supplements
IF THE EQUIPMENT WHI C H T HE SUBJECT OF SUPPLEMENT IS INSTALLED. Electric Pitch Trim Installation AutoControl III Installation AutoFlite II Installation Air Conditioner Installation FAA APPROVED December 29, 1971 REPORT: VB-343 PAGE 3-15 MODEL: PA-28R-200 REVISED: February 10, 1972...
Page 26: Electric Pitch Trim Installation
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...
Page 27: Autocontrol Iii Installation
( 4 ) An autopilot runaway, with a 1 second delay in the initiation of recovery, during an approach operation, coupled or uncoupled, could ° result in a 15 bank and a 40 foot altitude loss. PERFORMANCE The airplane performance remains unchanged. REPORT: VB-343 PAGE 3-17 FAA APPROVED December 29, 1971 MODEL: PA-28R-200...
Page 28: Autoflite Ii Installation
(4) An autopilot runaway, with a 1 second delay in the initiation of recovery, during an approach operation, coupled or uncoupled, could ° result in a 15 bank and a 40 foot altitude loss. PERFORMANCE The airplane performance remains unchanged. FAA APPROVED December 29, 1971 REPORT: VB-343 PAGE 3-18 MODEL: PA-28R-200...
Page 29: Air Conditioner Installation
100 fpm can be expected at all altitudes. Warning - The air conditioner must be off to insure normal takeoff performance. REPORT: VB-343 PAGE 3-19 FAA APPROVED February 10, 1972 MODEL: PA-28R-200...
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Page 31 ARROW II N16422 POH DESCRIPTION AIRPLANE AND SYSTEMS THE AIRPLANE The Cherokee Arrow II is a single-engine, retractable landing gear, aU metal aircraft. Increased fuselage length has enhanced the comfort in the rear seats. A large cabin door allows composed entry and exit of the spacious interior. Four individual seats aUow individual comfort for extended cross-country flights.
Page 32 ARROW II N16422 POH ENGINE AND PROPELLER It is furnished fuel injected engine RPM. The Cherokee Arrow 11 incorporates a Lycoming 10-360-C l C four-cylinder, direct drive, horizontally opposed rated at 200 horsepower at 2700 with a starter, 60 ampere 12-volt alternator, shielded ignition, vacuum pump drive, fuel pump, propeller governor and a dry automotive type induction air filter.
Page 33 N16422 POH 105MPH = 191 KT 85MPH = 74 KT (113 KT) (130 KT)
Page 34 ARROW II N16422 POH Throttle Quadrant OVERRIDE LATCH Console AIRPLANE AND SYSTEMS REVISED: August 30, 1973...
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Page 36 N16422 POH ARROW II !I ,. •---------------------------------------- · --- Two micro-switches in the throttle quadrant activate a warning horn and a red "Warning Gear Up" light under the following conditions: Gear up and power reduced below approximately 14 inches of manifold pressure. On aircraft equipped with the backup gear extender.
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Page 39 ARROW II N16422 POH FUEL SYSTEM The fuel system was designed with simplicity in mind. It incorporates two fuel tanks, one in each wing containing twenty-five (25) U.S. gallons, giving a total of 48 usable gallons. The tanks are attached to the leading edge of the wing with screws and are an integral part of the wing structure.
Page 40 N16422 POH ARROW II FUEL QUANTIT Y FUEL QUANTITY FUEL PRESSURE GAUGE GAUGE GAUGE � ' ff " I.,__ ___ _ LEn TANK RIGHT TANK FU�L SELECTOR DRAIN DRAIN &ASCOUTOR FUEL FLOW GAUGE VENT ELECTRIC FUEL PUMP VENT ENGINE DRIVEN FUEL PUMP VENT SERVO REGULATOR Fuel Schematic...
Page 41 N16422 POH ARROW ELECTRICAL SYSTEM The electrical system is very simple and functional. All switches are grouped in a s�itch panel above the power quadrant. On the lower right side of the inStr'ument panel is the circuit breaker panel. with each breaker clearly marked to show what circuit•it protects. A- l so. circuit provisions arc made to handle a complete complement of communication and navigational equipment.
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Page 43 N16422 POH ARROW II Circuit Breaker Panel AIRPLANE AND SYSTEMS • 2-13 ISSUED: November 15, 1971 REVISED: June 1S, 1972...
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Page 45 N16422 POH ARROW 11 INSTJUMENT PANEL The instrument panel is designed to be functional and professional, acco mmodating complete instruments and avionics equipment for VFR and IFR flights. A wi de r ange of optional instruments and avionics pennits an equipment selection uniquely suited to individual needs.
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Page 47 ARROW IT N16422 POH ·' Static System AIRPLANE AND SYSTEMS ISSUED: November ·1s, 1971 2-17...
Page 48 N16422 POH ARROW II HEATING, VENTILATING AND DEFROSTING SYSTEM The heating system is designed to provide maximum comfort for the occupants dur winter and cool weather flights. The system includes a heat shroud, heat ducts, defroster outlets, heat and defroster controls. An opening in the front of the lower cowl admits ram air to the heater shroud and then the air is ducted to the heater shut-offs on the right and left side of the firewall.
Page 49 ARROWil N16422 POH ---- Heat, Defrost and Ventilating System AIRPLANE AND SYSTEMS ISSUED: November 1 S, 1971 2-19 REVISED: June IS, 1972...
Page 50 ARROW II N16422 POH CABIN FEATURES The interior has been designed for passenger comfort and safety. All seat backs have three positions: normal, intermediate and recline. The adjustment lever is located at the base of the seat back on the outboard side of the seat. The front seats adjust fore and aft for case of entry and occupant comfort.
Page 51 N16422 POH ARROW II BAGG A GE AREA A large baggage area, located behind the rear seats, is accessible either from the cabin or through a large outside baggage door on the right side of the aircraft. Maximum capacity is 200 lbs.
Page 52 ARROW II N16422 POH THIS PAGE INTENTIONALLY LEFT BLANK AIRPLANE AND SYSTEMS ISSUED: November 15, 1971 2-22...
Page 53 ARROWU N16422 POH AIR CONDITIONING* The air conditioning system is a recirculating air system. The major items include; evaporator, condenser, compressor, blower, switches and temperature controls. The evaporator is located behind the left rear side of the baggage compartment. This cools the air that is used for air conditioning.
Page 54 N16422 POH ARROWil EVAPORATOR & INLET FILTER Air Conditioning System SKETCH A. Overhead Duct ISSUEO:,·February 4, AIRPLANE AND SYSTEMS 1972. 2-2 4...
Page 55 N16422 POH ARR0Wll SKETCH 8. Oimate Control Panel CONDENSER SKETCH C. Condenser AIRPLANE AND SYSTEMS ISSU E D: February 4, 1972 2-25 REVISED: June 15, 1972...
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Page 57 N16422 POH EMERGENCY PROCEDURE Introduction ..........Engine Fire During Start ........
Page 58: Introduction
ARROWn N16422 POH EMERGENCY PROCEDURES INTRODUCTION This section contains procedures that are recommended if an emergency condition should occur during ground operation, take-off, or in-flight. These procedures are suggested as lhe best c ourse of action for coping with the particular condition described, but are not a substitute for sound judgment and common sense.
Page 59: Engine Power Loss During Take-Off
ARROW II N16422 POH ENGINE POWER LOSS DURING TAKE-OFF The proper action to be taken if loss of power occurs during take-off will depend on circumstances. If sufficient runway remains for a normal landing, leave the gear down and land straight ahead.
Page 60: Engine Power Loss In Flight
N16422 POH ARROW 11 ENGINE POWER LOSS IN FLIGHT Complete engine power loss is usually caused by fuel flow interruption, and power will be least 110 MPH IAS, gear and flaps up and if altitude permits proceed as follows: restored shortly after fuel flow is restored. power loss occurs at low altitude, the first step is to prepare for an emergency landing (See POWER OFF LANDING).
Page 61: Gear Down Landing
ARROW II N16422 POH CAUTION ,.,.. This will increase your rate of descent, so be sure you have adequate altitude. Excess altitude may be lost by widening your pattern, using flaps or slipping, or a combination of these. Whether to attempt a landing with gear up or down depends on many factors. If the field down position will better protect the occupants of the aircraft.
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Page 63 N16422 POH ARROW II NOTE Refer to page 3-1 I for differences when emergency extension procedure is performed for training purposes. SPl�S . . . ; -'• Intentional spins are prohibited in this aircraft. If a spin is inadvert. e ntly entered, immediately THROTTLE - IDLE •...
Page 64: Fire
ARROWD N16422 POH FIRE The presence of fire is noted through smoke, smell, and heat in the cabin. It is essential that the source of the fire be promptly identified through instrument readings, character of the smoke, or other indications, since the action to be taken differs somewhat in each case. Source of Fire - Check Electrical Fire (Smoke in Cabin): Master Switch - Off...
Page 65: Alternator Failure
ARROWD N16422 POH change power settings unnecessarily, as this may hasten complete power loss. Depending on the circumstances, it may be advisable to make an off airport landing while power is still available, particularly if other indications of actual oil pressure loss, such as sudden increase in temperatures, or oil smoke, are apparent, and an airport is not close.
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Page 67 ..M. Miscellaneous (O p tional E q uipment) ....ISSUED: October 14, 1971 REPORT: VB-334 PAGE 5-i MODEL: PA-28R-200...
Page 68 N16422 POH ARROW THIS PAGE INTENTIONALLY LEFT BLANK REPORT: VB-334 PAGE 5-ii ISSUED: October 14, 1971 MODEL: PA-28R-200...
Page 69 Narco Comm I 0A and Comm 11 A. Jan. 15, 1973 5-26 Changed from Narco Comm l O and Comm 11 1/tZ�Y. 5-28 Add: King KX-175, KN-73, KN-77 and KNl-520 Installations. VISED: January 15, 1973 MODEL: PA-28R-200 ISSUED: October 14, 1971 REPORT: VB-334 PAGE S-iii...
Page 70 Vacuum Regulator. � April 10, 1979 Revised Weight and Balance info. Added Caution; relocated para. 2. b. to pg. 5-4. Added para. 2.b. from page 5-3. �� REPORT: VB-334 PAGES-iv ISSUED: October 14, 1971 MODEL: PA-28R-200 REVISED: APRIL 10, 1979...
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Page 72 ARROW N16422 POH THlS PAGE INTENTIONALLY LEFT BLANK ISSUED: October 14, 1971 REPORT: VB-334 PAGE 5-2 MODEL: PA-28R-200...
Page 73 WEIGHT AND BALANCE DATA WEIGHING PROCEDURE At the time of delivery, Piper Aircraft Corporation provides each airplane with the licensed empty weight and center of gravity location. This data is on Page l , Section I of this Flight Manual.
Page 74 Left Main Wheel (L ) Airplane Empty Weight, as Weighed (T) EMPTY WEIGHT CENTER OF GRAVITY The following geometry applies to the PA-28R-200 airplane when airplane is level (See Item 2). ----C. G. ARM---, M Level Points (Fuselage Left Side) ---- 7 8 .
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Page 76 N16422 POH ARROW THIS PAGE INTENTIONALLY LEFT BLANK REPORT: VB-334 PAGE 5-6 MODEL: P A-28R-200 ISSUED: October 14. 1971...
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Page 78 IT IS THE RESPONSIBILITY OF THE PILOT AND AIRCRAFT OWNER TO INSURE THAT THE AIRPLANE TS LOADED PROPERLY. *Check Aft C.G. between 150 lbs and 200 lbs. 'fooRT, VB-334 PAGE 5-ll ISSUED: October 14, 1971 ODEL: PA-28R-200...
Page 79 � �-- '<"' --< � c,'> q'I> 'b<:.' 1._--- fl,,_ I- ... 'I.'- , ..'" � �e ',,I �./(>r:i,C/,� I,;' ',,I , ., � r,,,,, ;"': MOMENT/1000 (POUND - INCHES) ISSUED: October 14, 1971 REPORT: VB-334 PAGE MODEL: PA-28R-200...
Page 80 N16422 POH ARROW IT IS THE RESPONSIBILITY OF THE OWNER AND PILOT TO ASCERTAIN THAT THE AIRPLANE ALWAYS REMAINS WITHIN THE ALLOWABLE WEIGHT VS. CENTER OF GRAVITY ENVELOPE WHILE IN FLIGHT. C. G. RANGE AND WEIGHT 2800 �.,, 2600 •' 2400 2200 2 000...
Page 81 ARROW N16422 POH EQUIPMENT LIST The following is a list of equipment which may be installed in the PA-28R-200. ftems marked with.an "X" are items installed when the airplane was delivered by the manufacturer. Cert. Weight Arm Aft Item Lbs.
Page 82 Alternator 1 2V 60 Amp TC 2A13 12.5 Chrysler 2642997 Starter - 12V Prestolite Model MZ-4206 TC lEI0 10.5 18.0 Lycoming 76211 39.7 TC 2 A l3 2 .6 Oil Cooler, PAC 67848 REPORT: VB-334 PAGE 5-12 ISSUED: October 14, 1971 MODEL: PA-28R-200...
Page 83 109.8 3777 34.4 6.00-6 with Regular Tubes One Nose Wheel Assembly 40-77 Wheel Assembly (Cleveland) (less brake drum) One 4 Ply Rating Tire 15.S TC 2A 13 5.00-5 Regular Tube REPORT: VB-334 PAGE 5-13 MODEL: PA-28R-200 ISSUED: October 14, 1971...
Page 84 Overvoltage Relay 55.4 Wico Electric No. X-16799B TC 2A13 Starter Relay 47.0 Piper Dwg. 99130-2 TC 2Al3 Landing Gear Motor Contactor Cole-Hersee �24059 (2) .8 lbs. each 162.0 TC 2AI3 REPORT: VB-334 PAGE 5-14 , ISSUED: October 14, 1971 MODEL: PA-28R-200...
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Page 87 Pump Assembly - Piper 159.0 1431 TC 2Al3 67500-2 Switch, Pressure Consolidated 116.7 TC 2Al3 Controls �211 C243-3 Valve - Free Fall Piper 675 2 2-2 114.0 TC 2Al3 ...--, ISSUED: 14, 1971 REPORT: VB-334 PAGE 5-17 MODEL: PA-28R-200 October...
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Page 89 N16422 POH ARROW THIS PAGE INTENTIONALLY LEFT BLANK ISSUED: ISSUED: October 14, 1971 REPORT: VB-334 PAGE S-19 MODEL: PA-28R-200...
Page 90 Oil System (Optional Equipment) Vacuum Pump Airborne M anufacturing Co. Model 200CC 29.6 TC 2AI3 Oil Filter with Adapter AC 0F5578770 (3.3 lbs. each) 33.1 (Lycoming �75528) TC 2A13 ---- REPORT: VB-334 PAGE 5-20 ISSUED: October 14, 1971 MODEL: PA-28R-200...
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Page 93 AutoFlite II 122.2 STC SAi l 57SW Roll Servo #1C363-l -183R STC SAi 157SW 93.4 Cable Panel Unit 11 52D75-3 or -4 59.4 STC SAJ I 57SW ISSUED: October 14, 1971 REPORT: VB-334 PAGE S-23 REVISED: December 29, 1971 MODEL: PA-28R-200...
Page 94 ARROW N16422 POH THIS PAGE INTENTIONALLY LEFT BLANK REPORT: VB-334 PAGE 5-24 MODEL: PA-28R-200 ISSUED: October 14, 1971...
Page 95 TC 2A13 Servo Indicator 551 A 160.8 TC 2Al3 Loop Antenna 232 1E Sense Antenna and Cable Cable, Interconnecting 108.0 TC 2Al3 150 .0 TC 2Al3 ISSUED: October 14, 1971 REPORT: VB-334 PAGE S-2S REVISED: November 14, 1972 MODEL: PA-28R-200...
Page 96 61.3 TC 2A13 Loop Antenna 161.5 TC 2Al3 Loop Cable 105.5 TC 2Al3 Audio Ampl ifier 51.0 TC 2Al3 Sense Antenna and Cable 147.5 TC 2Al3 REPORT: VB-334 PAGE 5-26 ISSUED: October 14, 1971 MODEL: PA-28R-200 REVISED: January 15, 1973...
Page 97 TC 2Al3 .3 3 235.4 Shelf & Access Hole King KT76/78 Transponder 1 80 TC 2Al3 3. 1 58. 1 Panel Unit TC 2Al3 Antenna & Cable REPORT: VB-334 PAGE S-27 ISSUED: October 14, 1971 REVISED: November 14, 1972 MODEL: PA-28R-200...
Page 98 Ki n g KX-17 5 VHF Tr nscei v er (2nd) 56.6 TC 2A13 King KN- 7 7 VOR/LOC Conv. 183.6 TC2AJ3 King X:NI- 5 20 VOR/I LS Indicator 60.5 TC 2Al3 REPORT: VB-334' PAGE S-28 �UED: October 14.1971 MODEL: PA-28R-200 REVISED: Jmmry IS. 1973...
Page 99 Exh aust Gas Temperature Gauge TC 2A13 55.4 Piper 99026 T ru- Speed lndica tor Piper 67433-2 or -3 or (same as Standard Equipment) PS50049-4 ISSU E D� October 14, 1971 REPORT: VB-334 PAGE 5-29 REVISED: December 5, 1975 MODEL: PA-28R-200...
Page 100 N16422 POH ARROW TIDS PAGE INTENTIONALLY LEFT BLANK REPORT: VB-334 PAGE S-30 -l�UED: October 14, 1971 MODEL: PA-28R-200...
Page 101 Alternate Static Source Zinc Chromate Finish 158.0 TC 2Al3 7235 TC 2A13 Air Conditioner Instl. 68.9 105.0 Calibrated Alternate Static Source Placard Required: TOT AL OPTIONAL EQUIPMENT ISSUED: October 14, 1971 REVISED: February 10, 1972 REPORT: VB-334 PAGE S-31 MODEL: PA-28R-200...
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Page 103 N16422 POH CUMBERLAND AVIONICS, LLC Revised Weight & Balance 210 TUNE AIRPORT DRIVE NASHVILLE TN 37209 FAA REPAIR STATION X24R306X A/C PA28R-200 5/N: 28R7335145 Call sign: N16422 Old empty wgt: 1603.7 Taken from W&B Old empyt wgt cg: 82.65 Dated: 10/15/14 Old useful load: 1046.3 Old moment:...
Page 104 N16422 POH OPERATING INSTRUCTIONS Starting Engine ......... . . 6-2 Starting Engine When Cold .
Page 105 ARROWll N16422 POH OPERA TING INSTRUCTIONS PREFLIGHT The airplane should be given a thorough visual inspection prior to each flight. Parti c ular attention should be given to the following items: Master switch and ignition OFF; landing gear switch DOWN; remove seat belt securing control wheel or wheel control _ lock.
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Page 107: Starting Engine When Flooded
N16422 POH ARROW II • ST A RTIN G ENGINE WHEN FLOODED Open the throttle full. Tum the master switch ON. Tum the electric fuel pump OFF. Put mixture control in IDLE CUT-OFF. Engage the starter by rotating the magneto switch clockwise and pressing in. When the engine fires, advance the mixture control and retard the thr o ttle.
Page 108: Take-Off
ARROW II N16422 POH Check vacuum gauge. Indicator should read 5" Hg± .1" Hg at 2000 RPM. Check both the oil temperature and pressure. The temperature may be low for some time if the engine is being run f o r the first time of the day, but as long as the pressure is within limits the engine is ready f o r take-off.
Page 109: Stalls
N16422 POH (�I' I•·- - ' ,_.�·ARROW II Soft Field, No Obstacle: Proc ed as abov r gear r traction, continue climb at b st rat of climb spe d. 100 MPH. and slowly r tract th flaps. •If d sired on th aircraft equipped with th backup g...
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Page 111: Stopping Engine
ARROW TI N16422 POH The airplane should be trimmed to an approach speed of about 90 MPH with the flaps and gear extended. The flaps can be lowered at speeds up to 125 MPH and the gear can be extended at speeds up to 150 MPH if desired.
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Page 113 ARROW 11 N16422 POH THJS PAGE INTENTIONALLY LEFT BLANK OPERA TING INSTRUCTIONS ISSUED: February 4, 1972...
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Page 115: Air Conditioning
ARROWil N16422 POH OPTIONAL EQUIP AIR CONDITIONING To operate the air conditioning system either on the ground or in flight: Start the engine (ground operation). Turn the air conditioning "Master" switch to "ON." Turn "TEMP" control to desired temperature. Clockwise rotation increases cooling. Select desired "FAN"...
Page 116: Piper Automatic Locator
ARROW fl N16422 POH Although the cruise speed and range are only slightly affected by the air conditioner operation, these changes should be considere. d in preflight planning. To be conservative, the following figures assume that the compressor is operating continuously while the airplane is airborne.
Page 117 ARROWil N16422 POH OPERA TING TIPS The following Operating Tips are - o f particular value in the operation of the Cherokee Arrow IT. I. Learn to trim for take-off so that only a very Hght back pressure on the wheel is required to lift the airplane off the ground.
Page 118 ARRown N16422 POH If the vacuum gauge registers lower than 5" Hg + .1 0" Hg at 2000 RPM, the following items should be checked before flight: Common air filter, could be dirty or restricted. Vacuum lines, could be collapsed or broken. Vacuum pump, worn.
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Page 120 N16422 POH ARROW II £!\IL if�ifOJJ®� �@OOW�OO�O@OO ��£!\rtaif THIS CHART SHOULD BE USED TO DETERMINE DENSITY ALTITUDE FROM EXISTING TEMPERATURE AND PRESSURE ALTITUDE CONDITIONS FOR USE WITH PERFORMANCE CHARTS. 24000 ---- � l...---- 20000 ..--- STD. :\\\� � ----- l .. � ,:...
Page 121 ARROW II N16422 POH ii � ��ca@IFIF ®�$il�OO<C� W� ®��$�iIW �IL il�iilW®� PAVED LEVEL DRY RUNWAY GROSS WT . 2650 LBS. � • 7000 6000 5000 • 4000 ,_ ..S-!f/ ti: ti: '"""':! Q _ ,Q , s § °...
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Page 124 ARROWil N16422 POH · · !rd� 00 �00$01rl �IL 1r 01f M © � @� $ ID) _---I t-----+-- 48 GAL FUEL ECONOMY CRUISE GROSS WT. 2650 LBS . -+----+-----4 _-+--__ MIXTURE-LEAN PER LYCOMING INSTRULTION 18000 t---+----+--+---+ - --1----+ - +-�----1 75% POWER 10.15 GPH ,__ 65% POWER 9.16 GPH 14000 1---1----+---+----+- - �...
Page 125 N16422 POH ARROW II � $iI A\l[!J�((n $��[ID A\OO((nl� ©lF OOA\00� - GROSS WEIGHT · 2650 POWER OFF ·- ��/ � V '.\ 3/ - � � � I / � ..Co\� ..�� I � �� ..[__../ :\.'\�...
Page 126 N16422 POH ilROW II ._._ ,..- ., · ··· · �,�·� !'. < � DISTANCE l!�Gl]OE- ALTITuge- 2650 GROSS LBS..• !JI;•.· _ ; r , [91KTS] l �- - · • 1 • � rur- PROP WINDMILLING...
Page 127 N16422 POH . . . • t r- , r • ,.• ,. .,· /">� ':1· '>.-_' v1 <�·. : '. � "' 11 � .l• _..,r 7000 _1i-• ; ' � .. f· • .: .· , J � £:- •...
Page 128 N16422 POH ,-4 "'d �� .� g(".) Power Setting Table - Lycoming Model 10-360-C Series, 200 HP Engine ·g.�, Std. Alt Press. 110 HP - 55% Rated 130 HP - 65% Rated 150 HP - 75% Rated Press. �� Temp RPM AMO MAN.
Page 129 ARROWU N16422 POH HANDLI N G AND SERVICING This section contains infonnation on preventive maintenance. Refer to the appropriate Ser v ice Manual for .further maintenance procedures. Any complex repair or modification should be accomplished by a Piper Certified Service Center. GROUND HANDLING TOWING The airplane may be moved by using the nose wheel steering bar provided, or power...
Page 130 ARROWD N16422 POH PARKING When parking the airplane, insure that it is sufficiently protected against adverse weather conditions and presents no danger to other aircraft. When parking the airplane for any length of time or overnight, it is recommended that it be moored securely. To park the airplane, head it into the wind, possible.
Page 131 ARROW II N16422 POH CLEANING CLEANING ENGINE COMPARTMENT Before cleaning the engine compatment, place a strip of tape on the magneto vents to prevent solvent from entering these units. Place a large pan under the engine to catch waste. With the engine cowling removed, spray or brush the engine with solvent or a mixture of solvent and degreaser, as desired.
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Page 134 N16422 POH ARROW II LANDING GEAR SERVICE The main landing gear uses Oeveland Aircraft Products wheels and Oeveland single disc hydraulic brake assemblies. The main wheel tires are 6.00 x 6, four-ply rating, type with tubes. The nose wheel uses a Cleveland Aircraft Products 5.00 wheel with a 5.00 x 5, four-ply rating, type III tire with tube.
Page 135 N16422 POH ARROW II PROPELLER SERVICE The spinner and backing plate should be cleaned and inspected frequently for cracks. The propeller should be inspected before each flight for nicks, scratches and corrosion. If found, they should be taken care of as soon as possible by a rated mechanic, because nicks and scratches cause areas of increased stress which can cause serious damage or loss of a propeller tip.
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Page 137 ARROWil N16422 POH The external power receptacle, if installed, is located on the right side of the fuselage aft of the baggage compartment door. WINTERIZA TION Refer to the Arrow II Service Manual for battery servicing procedure. For winter operation a winterization kit is installed on the inlet opening of the oil cooler °...
Page 138 N16422 POH ARROW II THIS PAGE INTENTIONALLY LEFT BLANK • • �• I• • HANDLI N G AND SERVICING ISSUED: November 15, 1971 9-10...
Page 139 Piper dealer or A & P mechanic to see if he has the latest issued AD against his aircraft. Piper Aircraft Corporation takes a continuing interest in having the owner get the most efficient use from his aircraft and keeping it in the best mechanical condition. Consequently, Piper Aircraft from time to time issues Service Bulletins, Service Letters and Service Spares Letters relating to the aircraft.
Page 140 ARROWil N16422 POH The owner or pilot is required to ascertain ·that the following Aircraft Papers are in order .. , · and in the aircraft. To be displayed in the aircraft at all times: Aircraft Airworthiness Certificate Fonn FAA-13628. Aircraft Registration Certificate Fonn F AA-S00A.
Page 141 N16422 POH ,;,. (' ".:t ..i ,.,_,,. One h�red ,!low: ins�ctiQO.S...are _required by law if the aircra(t is�us� corfimercially. -Otherwise this inspection is.:! e ft,lQ the dis�re_tion.of tbe owner, This ins, p ectiol'\. is a complete check of the 3: ircr _ a f t �...
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