Piper Arrow IV Turbo User Manual

CHAPTER 74-IGNITION (cont.)
TABLE OF CONTENTS/EFFECTIVITY
CHAPTER
SECTION GRID
SUBJECT SUBJECT NO. EFFECTIVITY
74-00-00 GENERAL (PA-28RT-201) (cont.)
74-20-00 DISTRIBUTION 3E15
74-21-00 Inspection of Harness 3E15
74-21-01 Removal of Harness 3E15
74-21-02 Maintenance of Harness 3E18
74-21-03 Installation of Harness 3E20
74-22-00 SPARK PLUGS 3E22 A 8-82
74-22-01 Removal of Spark Plugs 3E22
74-22-02 Inspection and Cleaning of Spark Plug 3E23
74-22-03 Installation of Spark Plugs 3E24
74-30-00 SWITCHING 3F1 A 7-81
74-30-01 Removal of Ignition Switch 3F1 A 7-81
74-30-02 Installation of Ignition Switch 3F1 A 7-81
74-Cont./Effec.
Page-2
Revised: August 17, 1982
3D9
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