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Piper Arrow IV Turbo User Manual

Piper Arrow IV Turbo
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LIST OF ILLUSTRATIONS (cont)
FIGURE NO. SUBJECT GRID NO.
24-35. Installation of Drive End Head 1J4
24-36. Installation of Rectifier 1J4
24-37. Terminal Assembly (Prestolite) 1J4
24-38. Slip Ring End Bearing Assembly 1J6
24-39. Testing Alternator 1J6
24-40. Brush Installation 1J7
24-41. Internal Wiring Diagram 1J7
27-1. Rod End Installation Method 1K3
27-2. Control Column Assembly 1K5
27-3. Aileron Controls (Typical) 1K8
27-4. Aileron Rigging 1K12
27-5. Bellcrank Rigging Tool 1K12
27-6. Aileron Rigging Tool 1K13
27-7. Rudder and Steering Pedal Assembly 1K15
27-8. Rudder Controls 1K17
27-9. Rudder Rigging Tool 1K18
27-10. Clamping Rudder Pedals 1K18
27-11. Rudder Rigging 1K18
27-12. Rudder and Stabilator Travel Adjustments 1K22
27-13. Rudder Trim Control 1K22
27-14. Stabilator Controls 1K24
27-15. Stabilator and Stabilator Trim Travel Adjustments 1L1
27-16. Stabilator Rigging Tool 1L1
27-17. Methods of Securing Trim Cables 1L4
27-18. Stabilator Trim Control 1L5
27-19. Flap Controls 1L9
27-20. Flap Step Adjustment 1L11
27-21. Flap Rigging Tool 1L11
27-22. Flap Rigging 1L14
28-1. Fuel System Diagram (PA-28RT-201) 2A24
28-2. Fuel System Diagram (PA-28RT-201T) 2B1
28-3. Engine Primer System Placards (PA-28RT-201T) 2B2
28-4. Locking Fuel Cap Assembly 2B4
28-5. Fuel Filter Bowl and Screen 2B5
28-6. Auxiliary Fuel Pump Variable Resistor 2B7
28-7. Tolerances; Union Nut and Tubing Nut 2B12
28-8. Fuel Gauge 2B14
29-1. Schematic Diagram of Hydraulic System 2B20
29-2. Schematic Diagram of Hydraulic System 2B21
29-3. Hydraulic System Installation 2B22
29-4. Hydraulic System Installation 2B23
29-5. Hydraulic Pump/Reservoir, Exploded View 2C12
29-6. Test and Adjustment of Hydraulic Pump 2C13
29-7. Checking Aligning Brackets of Gear Back-Up Extender
Actuator 2C17
29-8. Gear Back-Up Extender Actuator 2C18
29-9. Nose Gear Actuating Cylinder 2C22
Introduction
Page - 10
Revised: August 8, 1984
1A11
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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