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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.
55-1. Stabilator Installation 2J13
55-2. Stabilator Balance Configuration 2J14
55-3. Vertical Fin Installation 2J15
55-4. Rudder Installation 2J17
55-5. Rudder Balancing 2J18
56-1. Windshield Installation (Typical) 2J22
56-2. Side Window Installation, Single Pane (Typical) 2J23
57-1. Wing Installation 2K3
57-2. Aileron and Flap Installation 2K8
57-3. Aileron Balance Configuration 2K11
61-1. Propeller Installation (Hartzell) 3A21
61-2. Propeller Blade Minor Repair 3A23
61-3. Propeller Governor 3A24
61-4. Propeller Controls 3B2
61-5. Propeller Installation (Hartzell) 3B4
61-6. Propeller Blade Minor Repair 3B5
61-7. Propeller Governor 3B7
71-1. Engine Installation (PA-28RT-201T) 3B21
71-2. Engine Cowling Installation (PA-28RT-201T) 3B24
71-3. Engine Installation (PA-28RT-201) 3C7
71-4. Engine Cowling Installation (PA-28RT-201) 3C11
73-1. Schematic Diagram of Fuel Injection System 3C15
73-2. Fuel Injector Nozzle Assembly 3C17
73-3. Engine Controls 3C17
73-4. Idle Speed and Mixture Adjustment Points 3C19
73-5. Sectional View of Altitude Compensating Fuel Pump Assembly 3C19
73-6. Exhaust Bypass Screw 3C21
73-7. Fuel Injector 3D1
73-8. Schematic Diagram of RSA Fuel Injector System 3D2
73-9. Fuel-Air Bleed Nozzle 3D4
73-10. Adjustments of Engine Controls 3D4
74-1. Magneto Assembly 3D12
74-2. Contact Spring Inspection 3D13
74-3. Contact Points 3D14
74-4. Impulse Coupling 3D15
74-5. Flyweight Clearance of Impulse Coupling 3D15
74-6. Rotor Holding Tool Installed 3D15
74-7. Timing Kit Installed 3D15
74-8. Cast-In Timing Marks 3D17
74-9. Fabricated Pointer 3D17
74-10. Engine Timing Marks 3D17
74-11. Removing Spring From Lead Assembly 3D20
Introduction
Page-12
Interim Revision: February 27, 1995
1A13
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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