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Piper Arrow IV Turbo User Manual

Piper Arrow IV Turbo
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CHAPTER 27 - FLIGHT CONTROLS
TABLE OF CONTENTS/EFFECTIVITY
CHAPTER
SECTION GRID
SUBJECT SUBJECT NO. EFFECTIVITY
27-00-00 GENERAL 1J20
27-00-01 Description and Operation 1J20 2R 7-83
27-00-02 Troubleshooting 1J20 1R 2-79
27-00-03 Standard Procedures 1K4
27-05-00 CONTROL COLUMN ASSEMBLY 1K4
27-05-01 Removal of Control Column Assembly 1K4 1R 2-79
27-05-02 Installation of Control Column Assembly 1K6 1R 2-79
27-10-00 AILERON CONTROLS 1K7
27-10-01 Removal of Aileron Control Cables 1K7
27-10-02 Installation of Aileron Control Cables 1K9
27-10-03 Removal of Aileron Bellcrank Assembly 1K10 1R 2-79
27-10-04 Installation of Aileron Bellcrank Assembly 1K10
27-10-05 Rigging and Adjustment of Aileron Controls 1K11 2R 8-84
27-20-00 RUDDER CONTROLS 1K14
27-20-01 Removal of Rudder and Steering Pedal Assembly 1K14
27-20-02 Installation of Rudder and Steering Pedal Assembly 1K16 2R 8-82
27-20-03 Removal of Rudder Control Cables 1K19 1R 2-79
27-20-04 Installation of Rudder Control Cables 1K19 1R 2-79
27-20-05 Rigging and Adjustment of Rudder Controls 1K20 2R 8-84
27-25-00 RUDDER TRIM CONTROLS 1K20
27-25-01 Removal of Rudder Trim Controls 1K20
27-25-02 Installation of Rudder Trim Controls 1K21 1R 2-79
27-25-03 Rigging and Adjustment of Rudder Trim Controls 1K21
27-30-00 STABILATOR CONTROLS 1K21
27-30-01 Removal of Stabilator Control Cables 1K21 1R 2-79
27-30-02 Installation of Stabilator Control Cables 1K23 1R 2-79
27-30-03 Rigging and Adjustment of Stabilator Controls 1L2 2R 8-84
27- Cont./Effec.
Page - 1
Revised: August 8, 1984
1J18
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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