Piper Arrow IV Turbo User Manual

CHAPTER 57 - WINGS
TABLE OF CONTENTS/EFFECTIVITY
CHAPTER
SECTION GRID
SUBJECT SUBJECT NO. EFFECTIVITY
57-00-00 GENERAL 2K2
57-00-01 Description 2K2
57-20-00 AUXILIARY STRUCTURE 2K2
57-20-01 Removal of Wing Tip 2K2
57-20-02 Installation of Wing Tip 2K2
57-20-03 Repair of Wing Tip 2K2
57-40-00 ATTACH FITTINGS 2K6
57-40-01 Removal of Wing 2K6 2-79
57-40-02 Installation of Wing 2K7 2R 8-80
57-50-00 FLIGHT SURFACES 2K10
57-50-01 Removal of Aileron 2K10
57-50-02 Installation of Aileron 2K10
57-50-03 Checking Aileron Free Play 2K11
57-50-04 Balancing Aileron 2K11
57-50-05 Removal of Wing Flap 2K12
57-50-06 Installation of Wing Flap 2K12
57 - Cont./Effec.
Page - 1
Revised: August 18, 1980
2K1
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