Piper Arrow IV Turbo User Manual

AIRWORTHINESS LIMITATIONS.
GENERAL.
The airworthiness limitations is FAA approved and specifies inspections and maintenance required under
Part 91.163 of the Federal Aviation Regulations.
The following limitations related to fatigue life of the airplane and its components have been established
with respect to the PA-28RT-201/201T airplane:
1. The safe life of the airframe structure will be released when the information becomes available.
2. The safe life limit of the propeller blades is unlimited.
—NOTE—
Refer to the LIMITATIONS in the Pilot’s Operating Handbook
and FAA Approved Airplane Flight Manual for a detailed
delineation of the flight limitations of the airplane. The
mandatory replacement time and/or inspection intervals of life
limited parts are contained in Chapter 5 of this manual.
—END—
4-00-01
Page 4-01
December 1, 1978
1A20
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