Piper Arrow IV Turbo User Manual

LIST OF ILLUSTRATIONS (cont)
FIGURE NO. SUBJECT GRID NO.
29-10. End Gland Locking Device 2C24
29-11. Main Gear Actuating Cylinder 2D1
32-1. Main Gear Oleo Strut Assembly 2D16
32-2. Main Gear Installation 2D17
32-3. Main Gear Service Tolerances 2D19
32-3a. Aligning Main Gear 2E3
32-4. Nose Gear Oleo Strut Assembly 2E7
32-5. Nose Gear Installation 2E9
32-5a. Nose Gear Service Tolerances 2E10
32-6. Nose Gear Adjustment (PA-28RT-201) 2E16
32-7. Nose Gear Adjustment (PA-28RT-201T) 2E17
32-8. Clamping Rudder Pedals in Neutral Position 2E19
32-9. Rudder Pedals at Neutral Angle 2E19
32-10. Nose Gear Door Retraction Mechanism(PA-28RT-201) 2E20
32-11. Nose Gear Door Retraction Mechanism (PA-28RT-201T) 2E21
32-12. Nose Wheel Assembly 2E24
32-13. Main Wheel Assembly 2F1
32-14. Wheel Brake Assembly (30-55) 2F2
32-15. Removal of Anchor Bolt 2F4
32-16. Installation of Anchor Bolt 2F5
32-17. Brake System Installation 2F7
32-18. Brake Master Cylinder (Hand Parking Brake) 2F8
32-19. Toe Brake Installation 2F9
32-20. Brake Cylinder (17000) (Toe Brake) 2F10
32-21. Brake Cylinder (10-30) (Toe Brake) 2F11
32-22. Adjustment of Nose Gear Down Limit Switch 2F15
32-23. Adjustment of Main Gear Down Limit Switch 2F15
32-24. Throttle Warning Switches 2F17
33-1. Annunciator Panel 2G1
33-2. Strobe Light Connections 2G4
34-1. Pitot-Static System Installation 2G10
35-1. Fixed Oxygen System 2G24
35-2. Portable Oxygen System 2H1
35-3. Test Apparatus for Testing Oxygen System 2H4
35-4. Oxygen Tubing Installations 2H5
35-5. Installation of Swagelok Fittings 2H8
51-1. Skin Materials and Thickness 2I9
51-1a. Baggage Compartment Inspection Holes Cutout Details 2I12
51-2. Surfaces Scratches, Abrasions or Ground-in-Dirt 2I16
51-3. Deep Scratches, Shallow Nicks and Small Holes 2I17
51-4. Mixing of Epoxy Patching Compound 2I17
51-5. Welding Repair Method 2I19
51-6. Repairing of Cracks 2I19
51-7. Various Repairs 2I20
51-8. Repair of Stress Lines 2I22
51-9. Repair of Impacted Damage 2I22
52-1. Installation of Door Snubber 2J7
Introduction
Page - 11
Interim Revision: February 27, 1995
1A12
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