Piper Arrow IV Turbo User Manual

LIST OF ILLUSTRATIONS (cont)
FIGURE NO. SUBJECT GRID NO.
21-17. Condenser Air Scoop Installation 1G14
21-18. Expansion Valve 1G15
21-19. Components Installation 1G17
21-20. Adjustment of Air Conditioning Throttle Switch
(PA-28RT-201) 1G17
21-21. Air Conditioning Wiring Schematic 1G19
23-1. ELT Portable Folding Antenna (Narco) 1H12
23-2. ELT Using Fixed Aircraft Antenna (Narco) 1H12
23-3. ELT Schematics 1H16
24-1. Lamp-Bank Load 1I8
24-2. Exploded View of Alternator (Chrysler) 1I10
24-3. Checking Field Coil Current Draw 1I10
24-4. Testing Field Circuit 1I10
24-5. Testing Positive Rectifiers With C-3829 Tester 1I12
24-6. Testing Negative Rectifiers With C-3829 Tester 1I12
24-7. Rectifier End Shield and Stator Assembly 1I12
24-8. Testing Positive Rectifiers With Test Lamp 1I14
24-9. Testing Negative Rectifiers With Test Lamp 1I14
24-10. Rectifier and Heatsink Assembly Removal 1I14
24-11. Rectifier End Shield Assembly 1I14
24-12. Testing Stator 1I16
24-13. Removal of Pulley 1I16
24-14. Removal of Bearing 1I16
24-15. Removal of Rectifier End Shield Bearing 1I16
24-16. Testing Rotor for Ground 1I17
24-17. Testing Rotor for Opens or Shorts 1I17
24-18. Installation of Grease Retainer 1I18
24-19. Installation of Rectifier End Shield Bearing 1I18
24-20. Installation of Drive End Shield Bearing 1I18
24-21. Installation of Pulley 1I18
24-22. Installation of Insulators 1I20
24-23. Installation of Positive Rectifier Assembly 1I20
24-24. Installation of Capacitor 1I20
24-25. Installation of Battery Output Insulator 1I20
24-26. Installation of Negative Rectifier Assembly 1I21
24-27. Installation of Stator 1I21
24-28. Exploded View of Alternator (Prestolite) 1I23
24-29. Removal of Slip Ring End Bearing 1I24
24-30. Removal of Rectifier 1I24
24-31. Removal of Drive End Head 1J2
24-32. Removal of End Head Bearing 1J2
24-33. Testing Rotor for Ground 1J2
24-34. Testing Rotor for Shorts 1J2
LIST OF ILLUSTRATIONS (cont)
Introduction
Page - 9
Revised: July 13, 1983
3A10
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