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Piper Arrow IV Turbo User Manual

Piper Arrow IV Turbo
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GENERAL.
Due to the wide variety of A.F.C.S. (Automated Flight Control System) options, it is mandatory to follow
the service literature published by the individual manufacturer of the A.F.C.S. equipment installed in any
particular airplane. This includes mechanical service such as; adjusting bridle cable tension, servo removal and
installation, servo clutch adjustments, etc.
NON-PIPER A.F.C.S. EQUIPMENT CONTACTS.
Refer to the following list of AutoPilot/Flight Director manufacturers to obtain service direction, parts
support, and service literature:
Bendix Avionics Division
2100 N.W. 62nd. Street
Fort Lauderdale, Fla. 33310
(305) 776-4100/TWX 5109559884
Collins General Aviation Division
Rockwell International
Cedar Rapids, Iowa 52406
(319) 395-3625 Telex: 464-421
Edo Corporation - Avionics Division
Box 610
Municipal Airport
Mineral Wells, Texas 76067
(817) 325-2517 Telex: 76067
King Radio Corporation
400 North Rodgers Road
Olathe, Kansas 66061
(913) 782-0400 Telex: 4-2299-Kingrad
Sperry Flight Systems/Avionics Div.
8500 Balboa Blvrd.
P.O. Box 9028
VanNuys, CA. 91409
(213) 894-8111 Telex: 65- 1367
Global Navigation
2144 Michelson Drive
Irvine, CA. 92715
(714) 851-0119
22-10-00
Page 22-01
Revised: August 17, 1982
1H3
PIPER AIRCRAFT
PA-28RT-201 / 201T
MAINTENANCE MANUAL

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Piper Arrow IV Turbo Specifications

General IconGeneral
ManufacturerPiper Aircraft
ModelArrow IV Turbo
Horsepower200 hp
Seating Capacity4
Landing GearRetractable tricycle
Range773 nautical miles
Service Ceiling20, 000 ft
Fuel Capacity72 gallons
Propeller2-blade constant speed
Max Takeoff Weight2, 900 lb (1, 315 kg)
Stall Speed (Flaps Down)55 knots
Rate of Climb1, 000 ft/min

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