Piper Arrow IV Turbo User Manual

GAMA SYSTEM/CHAPTER INDEX GUIDE
SYST SUB-SYST AEROFICHE
CHAP SECTION TITLE GRID NO.
4 AIRWORTHINESS LIMITATIONS 1A18
5 TIME LIMITS/MAINT CHECKS 1A22
6 DIMENSIONS AND AREAS 1B16
7 LIFTING AND SHORING 1C5
8 LEVELING AND WEIGHING 1C9
9 TOWING AND TAXIING 1C14
10 PARKING AND MOORING 1C18
11 REQUIRED PLACARDS 1C22
12 SERVICING 1D5
20 STANDARD PRACT - AIRFRAME 1E14
21 ENVIRONMENTAL SYSTEM 1E21
22 AUTOFLIGHT 1H1
23 COMMUNICATIONS 1H8
24 ELECTRICAL POWER 1H17
27 FLIGHT CONTROLS 1J17
28 FUEL 2A18
29 HYDRAULIC POWER 2B17
32 LANDING GEAR 2D4
33 LIGHTS 2F19
34 NAVIGATION & PITOT/STATIC 2G7
35 OXYGEN SYSTEM 2G21
37 VACUUM SYSTEM 2H17
Introduction
Page - 6
Revised: July 13, 1983
3A7
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