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Arrow PA-28R-201 Pilot's Operating Handbook And Faa Approved Airplane Flight Manual

Sn 2837001 and up
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REFERENCE ONLY
THIS ELECTRONIC VERSION
OF THE POH IS
NOT APPROVED TO
REPLACE ANY OPERATING
INFORMATION REQUIRED
BY THE REGULATIONS.
AirplAne
seriAl no.
pA-28r-201
report: vb-1365 fAA Approved by:
dAte of ApprovAl:
November 29, 1988
This handbook includes The maTerial required To be furnished To The
piloT by The federal aviaTion regulaTions and addiTional informaTion
provided by The manufacTurer and consTiTuTes The faa approved
airplane flighT manual. This handbook musT be carried in The airplane
aT all Times.
Arrow
pA-28r-201
AirplAne flight mAnuAl
AirplAne
regist. no.
d.h. trompler
d.o.A. no. so-1
piper AirCrAft CorporAtion
vero beACh, floridA
sn 2837001 And up
pilot's
operAting
hAndbook
And
fAA Approved

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Summary of Contents for Arrow PA-28R-201

  • Page 1 Arrow pA-28r-201 sn 2837001 And up REFERENCE ONLY pilot’s THIS ELECTRONIC VERSION operAting OF THE POH IS hAndbook NOT APPROVED TO REPLACE ANY OPERATING INFORMATION REQUIRED BY THE REGULATIONS. fAA Approved AirplAne flight mAnuAl AirplAne AirplAne seriAl no. regist. no.
  • Page 2 PIPER AIRCRAFT CORPORATION PA-28R-201, ARROW WARNING eXTreme care musT be eXercised To limiT The use of This handbook To applicable aircrafT. This hand- book revised as indicaTed beloW or subsequenTly revised is valid for use WiTh The airplane idenTified on The face of The TiTle page. subsequenT revisions s u p p l i e d b y p i p e r a i r c r a f T c o r p o r a T i o n m u s T b e properly inserTed.
  • Page 7 Corporation pa-28r-201, arroW pilot’s operating handbook log of revisions (cont) Revision FAA Approval Number and Revised Description of Revisions Signature Code Pages and Date Rev. 5 (Cont’d) 5-25b Added Page & Fig. 5-25b. 5-26 Revised Fig. 5-27. 5-26a Added Page &...
  • Page 8 Corporation pa-28r-201, arroW pilot’s operating handbook log of revisions (cont) Revision FAA Approval Number and Revised Description of Revisions Signature Code Pages and Date Rev. 7 8-1b Added page and moved info. (PR040607) from pages 8-1 and 8-2.
  • Page 59 SECTION 4 PIPER AIRCRAFT CORPORATION NORMAL PROCEDURES PA-28R-201, ARROW THIS PAGE INTENTIONALLY LEFT BLANK REPORT: VB-1365 ISSUED: SEPTEMBER 15, 1988 4-iv...

  • Page 68: Taxiing Checklist (4.17)

    PIPER AIRCRAFT CORPORATION SECTION 4 PA-28R-201, ARROW NORMAL PROCEDURES 4.5e Taxiing Checklist (4.17) TAXIING (4.17) Taxi Area..................CLEAR Parking Brake ................RELEASE Propeller ................... HIGH RPM Throttle ................APPLY SLOWLY Brakes ..................... CHECK Steering ..................CHECK 4.5f Ground Check Checklist (4.19) GROUND CHECK (4.19)

  • Page 69: Takeoff Checklist (4.23)

    SECTION 4 PIPER AIRCRAFT CORPORATION NORMAL PROCEDURES PA-28R-201, ARROW 4.5g Before Takeoff Checklist (4.21) (continued) BEFORE TAKEOFF (4.21) (continued) Fuel Selector ..............PROPER TANK Electric Fuel Pump ................. ON Engine Gauges ................CHECK Alternate Air ................CLOSED Seat Backs ..................ERECT Mixture ....................SET...

  • Page 70: Soft Field Technique (4.23B)

    PIPER AIRCRAFT CORPORATION SECTION 4 PA-28R-201, ARROW NORMAL PROCEDURES 4.5h Takeoff Checklist (4.23) (continued) SOFT FIELD TECHNIQUE (4.23b) Flaps ................25Þ (second notch) Accelerate to 50 to 60 KIAS depending on aircraft weight. Control Wheel ...........hack pressure to ROTATE to CLIMB ATTITUDE After breaking ground, accelerate to 55 to 65 KIAS depending on aircraft weight.

  • Page 71: Approach And Landing Checklist (4.29)

    SECTION 4 PIPER AIRCRAFT CORPORATION NORMAL PROCEDURES PA-28R-201, ARROW 4.5k Approach And Landing Checklist (4.29) APPROACH AND LANDING (4.29) Fuel Selector ..............PROPER TANK Seat Backs ..................ERECT Belts/Harness.................FASTEN Electric Fuel Pump ................. ON Mixture ....................SET Propeller ................ FULL INCREASE Emergency Gear Extension Lever ........

  • Page 78: Normal Start - Hot Engine (4.5C)

    PIPER AIRCRAFT CORPORATION SECTION 4 PA-28R-201, ARROW NORMAL PROCEDURES 4.13 ENGINE START (4.5c) (continued) 4.13b Normal Start - Hot Engine (4.5c) Open the throttle approximately l/2 inch. Turn ON the alternator and battery master switches, and the electric fuel pump. The mixture control lever should be in idle cut-off.

  • Page 79: Warm-Up (4.5D)

    SECTION 4 PIPER AIRCRAFT CORPORATION NORMAL PROCEDURES PA-28R-201, ARROW 4.13 ENGINE START (4.5c) (continued) 4.13d Engine Start With External Power Source (4.5c) (continued) NOTE For all normal operations using the PEP jumper cables, the battery master and alternator switches should be OFF.

  • Page 80: Ground Check

    PIPER AIRCRAFT CORPORATION SECTION 4 PA-28R-201, ARROW NORMAL PROCEDURES 4.17 TAXIING (4.5e) (continued) Release the parking brake and apply power slowly to start the taxi roll. Taxi a few feet forward and apply the brakes to determine their effectiveness. Taxi with the propeller set in low pitch, high rpm setting. While taxiing, make slight turns to ascertain the effectiveness of the steering.

  • Page 81: Before Takeoff (4.5G)

    TAKEOFF (4.5h) 4.23a Normal Technique (4.5h) The normal takeoff technique is conventional for the Arrow. Flaps should be up and the trim should be set slightly aft of neutral, with the exact setting determined by the loading of the airplane. Allow the airplane to accelerate to 65 to 75 KIAS, depending on the weight of the aircraft, and ease back on the control wheel to rotate to climb attitude.

  • Page 84: Approach And Landing (4.5K)

    PIPER AIRCRAFT CORPORATION SECTION 4 PA-28R-201, ARROW NORMAL PROCEDURES 4.29 APPROACH AND LANDING (4.5k) Check to ensure the fuel selector is on the proper (fullest) tank and that the seat backs are erect. The seat belts and shoulder harness should be fastened and the inertia reel checked.

  • Page 85: Mooring (4.5N)

    Mild airframe buffeting and gentle pitching may also precede the stall. The gross weight stalling speed of the Arrow with power off and full flaps is 55 KIAS. With the flaps up this speed is increased 5 KTS. Loss of altitude during stalls can be as great as 400 feet, depending on configuration and power.

  • Page 86: Turbulent Air Opera Non

    PIPER AIRCRAFT CORPORATION SECTION 4 PA-28R-201, ARROW NORMAL PROCEDURES 4.37 TURBULENT AIR OPERATION In keeping with good operating practice used in all aircraft, it is recommended that when turbulent air is encountered or expected, the airspeed be reduced to maneuvering speed to reduce the structural loads caused by gusts and to allow for inadvertent speed build-ups which may occur as a result of the turbulence or of distractions caused by the conditions.

  • Page 87: Weight And Balance

    SECTION 4 PIPER AIRCRAFT CORPORATION NORMAL PROCEDURES PA-28R-201, ARROW 4.41 WEIGHT AND BALANCE It is the responsibility of the owner and pilot to determine that the airplane remains within the allowable weight vs. center of gravity envelope while in flight.
  • Page 159 PIPER AIRCRAFT CORPORATION SECTION 7 PA-28R-201, ARROW DESCR/OPERATION ENGINE CONTROLS (continued) CONTROL QUADRANT AND CONSOLE Figure 7-1 ISSUED: SEPTEMBER 15, 1988 REPORT: VB-1365...

  • Page 160: Landing Gear

    Figure 7-3 7.11 LANDING GEAR The Arrow is equipped with a retractable tricycle landing gear, which is hydraulically actuated by an electrically powered reversible pump. The pump is controlled by a selector switch on the instrument panel to the left of the control quadrant (Figure 7-3).

  • Page 171: Electrical System

    PIPER AIRCRAFT CORPORATION SECTION 7 PA-28R-201, ARROW DESCR/OPERATION 7.17 ELECTRICAL SYSTEM (continued) Secondary power is provided by a 12-volt, 35-ampere-hour battery. The ammeter as installed does not show battery discharge; rather it shows the electrical load placed on the system. With all the electrical...

  • Page 172: Pitot-Static System

    SECTION 7 PIPER AIRCRAFT CORPORATION DESCR/OPERATION PA-28R-201, ARROW 7.19 VACUUM SYSTEM (continued) A vacuum regulator is provided in the system to protect the gyros. The valve is set so the normal vacuum reads 4.8 to 5.2 inches of mercury, a setting which provides sufficient vacuum to operate all the gyros at their rated rpm.

  • Page 190: General

    PIPER AIRCRAFT CORPORATION SECTION 8 PA-28R-201, ARROW HAND/SERV/MAINT 8.1 GENERAL (CONTINUED) Every owner should stay in close contact with an authorized Piper Service Center or Piper’s Customer Service Department to obtain the latest informa- tion pertaining to their airplane, and to avail themselves of Piper Aircraft’s support systems.

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