Piper Arrow IV Turbo User Manual

CHAPTER 22 - AUTOFLIGHT
TABLE OF CONTENTS/EFFECTIVITY
CHAPTER
SECTION GRID
SUBJECT SUBJECT NO. EFFECTIVITY
22-00-00 GENERAL 1H3 A 8-82
22-10-00 NON-PIPER A.F.C.S. EQUIPMENT CONTACTS 1H3 A 8-82
22-10-01 PIPER A.F.C.S. EQUIPMENT 1H4 A 8-82
22 - Cont./Effec.
Page - 1
Revised: August 17, 1982
1H2
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