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List of Illustrations A18 1R0202
List of Charts A23 1R0202
Introduction - Cont./Effec. Page 1 Revised: February 28, 2002
THE NEW PIPER AIRCRAFT, INC.
PA-44-180
AIRPLANE MAINTENANCE MANUAL

THIS PAGE INTENTIONALLY BLANK


Introduction - Cont./Effec. Page 2 Revised: February 28, 2002
4A6
THE NEW PIPER AIRCRAFT, INC.
PA-44-180
AIRPLANE MAINTENANCE MANUAL

INTRODUCTION
INSTRUCTIONS FOR CONTINUED AIRWORTHINESS
The PIPER PA-44-180 Seminole Maintenance Manual constitutes the Instructions for Continued Airworthiness as required by Federal Aviation Regulations (FAR) Part 23, Appendix G. Chapter 4 contains the Airworthiness Limitations section (4-00-00) and Inspection Program is in Chapter 5 (5-20-00).
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: February 28, 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 and up  4496043 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.
 
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