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Piper Arrow IV Turbo User Manual

Piper Arrow IV Turbo
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CHAPTER 80 - STARTING
TABLE OF CONTENTS/EFFECTIVITY
CHAPTER
SECTION GRID
SUBJECT SUBJECT NO. EFFECTIVITY
80-00-00 GENERAL 3G12
80-00-01 Description and Operation 3G12
80-00-02 Troubleshooting 3G12
80-10-00 CRANKING 3G15
80-10-01 Maintenance of Starting System 3G15 7-81
80-10-02 Overhaul of Starting Motor 3G16
80-10-03 Removal of Starting Motor 3G16
80-10-04 Disassembly of Starting Motor 3G16
80-10-05 Brushes 3G18
80-10-06 Armature 3G18
80-10-07 Field Coils 3G18
80-10-08 Brush Holders 3G18
80-10-09 Gear and Pinion H ousing 3G18
80-10-10 Bendix Drive 3G18
80-10-11 Assembly of Starting Motor 3G19
80-10-12 Bench Test 3G20
80-10-13 Starting Motor Control Circuit 3G20
80-10-14 Starting Motor Service Test Specifications 3G21
80-10-15 Starting Through External Power Receptacle with
Airplane’s Battery Nearly Depleted 3G21
80 - Cont./Effec.
Page - 1
Revised: February 23, 1979
3G11
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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