Piper Arrow IV Turbo User Manual

CHAPTER 27 - FLIGHT CONTROLS (cont)
TABLE OF CONTENTS/EFFECTIVITY
CHAPTER
SECTION GRID
SUBJECT SUBJECT NO. EFFECTIVITY
27-35-00 STABILATOR TRIM CONTROLS 1L3
27-35-01 Removal of Stabilator Trim Assembly (Forward) 1L3 1R 2-79
27-35-02 Installation of Stabilator Trim Assembly (Forward) 1L4 1R 2-79
27-35-03 Removal of Stabilator Trim Assembly (Aft) 1L6 1R 2-79
27-35-04 Installation of Stabilator Trim Assembly (Aft) 1L7 1R 2-79
27-35-05 Rigging and Adjustment of Stabilator Trim 1L7 1R 2-79
27-50-00 FLAPS 1L8
27-50-01 Removal of Wing Flap Controls 1L8
27-50-02 Installation of Wing Flap Controls 1L10
27-50-03 Rigging and Adjustment of Wing Flaps 1L12 1R 8-84
27-90-00 STALL WARNING 1L13 A 7-83
27-91-00 Lift Detector 1L13 A 7-83
27-91-01 Removal of Lift Detector 1L13 A 7-83
27-91-02 Installation of Lift Dectector 1L13 A 7-83
27-91-03 Adjustment of Lift Detector 1L13 A 7-83
27- Cont./Effec.
Page - 2
Revised: August 8, 1984
1J19
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