Fuel - Piper Arrow IV Turbo Maintenance Manual

INTRODUCTION.
This PIPER AIRCRAFT Maintenance Manual is prepared in accordance with the GAMA (General
Aviation Manufacturers Association) format. This maintenance manual is divided into various Groups which
enable a broad separation of contents (Chapters) within each group.
The various Chapters are broken down into major systems such as Electrical Power, Flight Controls, Fuel,
Landing Gear, etc. The System/Chapters are arranged more or less alphabetically rather than by precedence or
importance. All System/Chapters are assigned a number, which becomes the first element of a standardized
numbering system. Thus the element "32" of the number series 32-00-00 refers to the System/Chapter on
"Landing Gear." All information pertaining to the landing gear will be covered in this System/ Chapter.
The major System/Chapters are then broken down into Sub-System/Sections. These sections are identified
by the second element of the standardized numbering system. The number "40" of the basic number series 32-
40-00 is for the "Wheels and Brakes" portion of the landing gear.
The individual units within a Sub-System/ Section may be identified by a third element of the standardized
numbering system, such as 32-40-01. This number could be assigned by the manufacturer to fit the coverage
requirements of the publication.
Example:
CHAPTER/SYSTEM
LANDING GEAR
This manual does not contain hardware callouts for installation. Hardware callouts are only indicated
where a special application is required. To confirm the correct hardware used, refer to the PA-28RT-201/201T
Parts Catalog P/N 761 693, and FAR 43 for proper utilization.
PIPER AIRCRAFT
PA-28RT-201 / 201T
MAINTENANCE MANUAL
32-40-01
2A2
SUB-SYSTEMS
WHEELS AND BRAKES
INDIVIDUAL UNITS
NOSE WHEEL REMOVAL
December 1, 1978
Introduction
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