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Piper Arrow IV Turbo User Manual

Piper Arrow IV Turbo
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CHAPTER 24 - ELECTRICAL POWER
TABLE OF CONTENTS/EFFECTIVITY
CHAPTER
SECTION GRID
SUBJECT SUBJECT NO. EFFECTIVITY
24-00-00 GENERAL 1H20 8-82
24-01-00 Description and Operation 1H20 2-79
24-02-00 Troubleshooting 1H20
24-30-00 D.C. GENERATOR 1I6
24-31-00 Description of Alternator System 1I6 8-82
24-31-01 Checking Alternator System 1I7 A 8-82
24-31-02 Service Precautions 1I8 A 8-82
24-31-03 Overhaul of Alternator 1I8 A 8-82
24-32-00 Alternator System (CHRYSLER) 1I9
24-32-01 Bench Testing Alternator 1I9
24-32-02 Rotor Field Coil Current Draw 1I9 8-82
24-32-03 Testing Alternator Internal Field Circuit 1I9 8-82
24-32-04 Inspection 1I11
24-32-05 Testing of Rectifier Assemblies 1I11 A 8-82
24-32-06 Testing of Positive Rectifiers Using C-3829 Tester 1I11 8-82
24-32-07 Testing of Negative Rectifiers Using C-3829 Tester 1I13 8-82
24-32-08 Testing of Rectifier Assemblies Using Test Lamp 1I13 A 8-82
24-32-09 Removal of Rectifier and Heat Sink Assembly 1I15 A 8-82
24-32-10 Testing of Stator 1I15 8-82
24-32-11 Removal of Pulley and Bearing 1I15 8-82
24-32-12 Testing of Rotor 1I17 A 8-82
24-32-13 Slip Rings 1I17 A 8-82
24-32-14 Assembly of Alternator 1I17 2R 7-83
24-33-00 Alternator System (PRESTOLITE) 1I22
24-33-01 Alternator Nomenclature 1I22
24-33-02 Alternator Service Precautions 1I22
24-33-03 Description of Alternator 1I23
24-33-04 Overhaul of Alternator 1J1
24-33-05 Disassembly of Alternator 1J1
24-33-06 Inspection and Testing of Components 1J1
24-33-07 Assembly of Alternator 1J3
24-33-08 Testing of Alternator 1J5
24-33-09 Alternator Service Test Specification 1J5
24-33-10 Checking Alternator Belt Tension (PA-28R1-201) 1J7
24 - Cont./Effec.
Page - 1
Revised: July 13, 1983
1H18
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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