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Piper Arrow IV Turbo User Manual

Piper Arrow IV Turbo
752 pages
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AEROFICHE EXPLANATION AND REVISION STATUS
Maintenance manual information incorporated in this set of Aerofiche cards is arranged in accordance with
the general specifications of Aerofiche adopted by the General Aircraft Manufacturer’s Association. The
information compiled in this Aerofiche maintenance manual will be kept current by revisions distributed
periodically. These revisions supersede all previous revisions and are complete Aerofiche card replacements
and supersede Aerofiche cards of the same number in the set.
Identification of revised material:
Revised text and illustrations are indicated by a black vertical line along the left-hand margin of the frame,
opposite revised, and added material. Revision lines indicate only current revisions with changes and additions
to existing text and illustrations. Changes in capitalization, spelling, punctuation, indexing, the physical
location of the material or complete page additions are not identified by revision lines.
A reference and record of the material revised is included in each chapter’s Table of Contents/Effectivity.
The codes used in the effectivity columns of each chapter are defined as follows:
TABLE OF CONTENTS/EFFECTIVITY CODES
Original Issue: None
First Revision: Revision Identification, (1R Month-Year)
Second Revision: Revision Identification, (2R Month-Year)
All subsequent revisions will follow with consecutive revision numbers
such as 3R, 4R, etc., along with the appropriate month-year.
Added Subject: Revision Identification, (A Month-Year)
Introduction
Page - 4
Interim Revision: September 21, 1986
1A5
PIPER AIRCRAFT
PA-28RT-201 / 201T
MAINTENANCE MANUAL

Table of Contents

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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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