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GENERAL
This publication is prepared in accordance with the General Aviation Manufacturers Association (GAMA) Specification No. 2, with respect to the arrangement and content of the System/Chapters within the designated Chapter/Section-numbering system.
— WARNING— USE ONLY GENUINE PIPER AIRCRAFT PARTS OR PIPER AIRCRAFT APPROVED PARTS OBTAINED FROM PIPER APPROVED SOURCES, IN
CONNECTION WITH THE MAINTENANCE AND REPAIR OF PIPER AIRPLANES.
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-44-180 Parts Catalog P/N 761-891, and FAR 43 for proper utilization.
Genuine PIPER parts are produced and inspected under rigorous procedures to insure airworthiness and suitability for use in PIPER airplane applications. Parts purchased from sources other than PIPER, even though identical in appearance, may not have had the required tests and inspections performed, may be different in fabrication techniques and materials, and may be dangerous when installed in an airplane.
Additionally, reworked or salvaged parts or those parts obtained from non-PIPER approved sources, may have service histories which are unknown or cannot be authenticated, may have been subjected to unacceptable stresses or temperatures or may have other hidden damage not discernible through routine visual or nondestructive testing. This may render the part, component or structural assembly, even though originally manufactured by PIPER, unsuitable and unsafe for airplane use.
THE NEW PIPER AIRCRAFT, INC. expressly disclaims any responsibility for malfunctions, failures, damage or injury caused by use of non-PIPER approved parts.
— Note — THE NEW PIPER AIRCRAFT, INC. expressly reserves the right to supersede, cancel and/or declare obsolete any part, part numbers, kits or publication that may be referenced in this manual without prior notice.
Be sure to supply the correct serial number information in any correspondence or communication concerning your airplane.
Introduction Page 3 Revised: December 6, 2002
THE NEW PIPER AIRCRAFT, INC.
PA-44-180
AIRPLANE MAINTENANCE MANUAL

EFFECTIVITY
This maintenance manual is effective for PA-44-180 Seminole airplanes serial numbers 4496001 and up. This encompasses the following model years:
Model Year  Serial Numbers
1995 4496001 thru 4496005
1996 4496006 thru 4496013
1997
4496014 thru 4496023; less 4496020
1999 4496024 thru 4496030; and 4496020
2000 4496031 thru 4496042
2001 4496043 thru 4496108
2002 4496109 thru 4496168
2003 4496169 and up

SERIAL NUMBER EXPLANATION
Example:
44 96 001

MODEL SEQUENCE NUMBER TYPE CERTIFICATE DESIGNATION
MODEL CODE 96 = PA-44-180 SEMINOLE
ASSIGNMENT OF SUBJECT MATERIAL
This publication is divided into industry standard, three element, numeric subject groupings as follows:
A.  System/Chapter - The various groups are broken down into major systems such as Environmental Systems, Electrical Power, Landing Gear, etc. They are assigned a number, which becomes the first element of the standardized numbering system. Thus, the element “28” of the number 28-40-01 refers to the chapter “Fuel”. Everything concerning the fuel system will be covered in this chapter.
B.  Sub-System/Section - The major systems/chapters of an airplane are broken down into subsystems. These sub-systems are identified by the second element of the standard numbering system. The element “40” of the number 28-40-01 concerns itself with the indicating section of the fuel system.
C.  Unit/Subject - The individual units within a sub-system/section may be identified by the third element of the standard numbering system. The element “01” of the number 28-40-01 is a subject designator. This element is assigned at the option of the manufacturer and is normally zeroed out by PIPER.
Refer to Chapter/Section Index Guide, for a complete breakdown and list. The material is arranged in ascending numerical sequence.
PAGINATION
The Chapter - Section (i.e. - 28-40-00) numbering system (explained above) forms the primary page numbering system for this manual. Within each Chapter, pages are numbered consecutively beginning with Page 1 (i.e. - Page 28-1). Additionally, the aerofiche grid numbering system (explained below) may also be used to indicate location within the manual.
Introduction Page 4 Revised: December 6, 2002
THE NEW PIPER AIRCRAFT, INC.
PA-44-180
AIRPLANE MAINTENANCE MANUAL

AEROFICHE EFFECTIVITY
A.  The General Aviation Manufacturers Association (GAMA) have developed specifications for microfiche reproduction of aircraft publications. The information compiled in this Aerofiche Maintenance Manual will be kept current by revisions distributed periodically. These revisions will supersede all previous revisions and will be complete Aerofiche card replacements and shall supersede Aerofiche cards of the same number in the set. The “Aerofiche Effectivity” page at the front of this manual lists the current revision for each card in this set.
　
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