Piper Arrow IV Turbo User Manual

GAMA SYSTEM/CHAPTER INDEX GUIDE (cont)
SYST SUB-SYST AEROFICHE
CHAP SECTION TITLE GRID INO.
39 ELECTRICAL/ELECTRONIC PANELS AND
MULTI-PURPOSE PARTS 2I2
51 STRUCTURES 2I6
52 DOORS 2J1
55 STABILIZERS 2J10
56 WINDOWS 2J19
57 WINGS 2J24
61 PROPELLER 3A18
70 STANDARD PRACTICES - ENGINE 3B9
71 POWER PLANT 3B12
73 ENGINE FUEL AND CONTROL 3C12
74 IGNITION 3D7
77 ENGINE INDICATING 3F16
78 EXHAUST 3G1
79 OIL SYSTEM 3G6
80 STARTING 3G10
81 TURBINES 3H1
91 CHARTS AND WIRING DIAGRAMS 3H7
95 SPECIAL PURPOSE EQUIPMENT 3K1
Introduction
Page - 7
Interim Revision: February 27, 1995
3A8
PIPER AIRCRAFT
PA-28RT-201 / 201T
MAINTENANCE MANUAL

Piper Arrow IV Turbo Specifications

General

Manufacturer	Piper Aircraft
Model	Arrow IV Turbo
Horsepower	200 hp
Seating Capacity	4
Landing Gear	Retractable tricycle
Range	773 nautical miles
Service Ceiling	20, 000 ft
Fuel Capacity	72 gallons
Propeller	2-blade constant speed
Max Takeoff Weight	2, 900 lb (1, 315 kg)
Stall Speed (Flaps Down)	55 knots
Rate of Climb	1, 000 ft/min