Piper Arrow IV Turbo User Manual

CHAPTER 34 - NAVIGATION AND PITOT/STATIC
TABLE OF CONTENTS/EFFECTIVITY
CHAPTER
SECTION GRID
SUBJECT SUBJECT NO. EFFECTIVITY
34-00-00 GENERAL 2G9
34-00-01 Description and Operation 2G9
34-00-02 Removal and Replacement of Face Mounted
Instruments 2G9
34-00-03 Removal and Replacement of Cluster Mounted
Instruments 2G11
34-00-04 Gyro Fitting Installation Procedure (Edo-Aire) 2G11 11-79
34-10-00 FLIGHT 2G12 11-79
34-10-01 Rate of Climb Indicator 2G12 11-79
34-10-02 Sensitive Altimeter 2G13 11-79
34-10-03 Airspeed Indicator 2G15
34-10-04 Gyro Horizon 2G16
34-10-05 Directional Gyro 2G17
34-10-06 Magnetic Compass 2G18
34-10-07 Adjustment of Compass 2G18
34-10-08 Turn and Bank Indicator 2G20
34 - Cont./Effec.
Page - 1
Revised: August 17, 1982
2G8
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