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To operate the extinguisher, remove it from the quick-release bracket, hold it upright in either hand by the handgrip, with the spray nozzle pointing forward. Slide the (red) safety catch down with the thumb or remove the safety pin; direct the nozzle towards the base of the fire source, squeeze the lever with the palm of the hand. When you squeeze the lever, an indicator disc is ejected from the rear of the operating head of the extinguisher, and extinguishant is released from the nozzle in a wide, flat pattern. Maximum extinguishing effect is obtained if the fire-fighter keeps moving in towards the base of the fire source as it is extinguished. Releasing the lever closes a secondary seal inside the operating head. This interrupts the flow of extinguishant, thus retaining part of the charge, for dealing with a flash-back or re-ignition should they occur, without waste or leakage. Ejection of the indicator disc provides visual indication of partial or total discharge. A partly or totally discharged charge assembly should be replaced immediately after use.
26-20-00 Page 26-5 Revised: February 28, 2002
30 DAY INSPECTION
The extinguisher shall be inspected monthly, unless otherwise specified. The nozzle shall be examined to ascertain that it is unobstructed. The tamper tag or tamper indicator shall be intact. The extinguisher shall be pressurized as indicated and weight shall be within tolerances specified on the label.
— Note —
Ambient temperature has a direct relationship to the pressure displayed on the gauge. The pressure gauge has temperature extremes noted on the scale. The effects of the temperature may be eliminated by allowing the unit to remain at room temperature (70°F) for several hours, then reading the gauge.
26-20-00 Page 26-6 Revised: February 28, 2002
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AIRPLANE MAINTENANCE MANUAL
CARD 2 OF 4

PA-44-180

(SN 4496001 AND UP)

 

 

THE NEW PIPER AIRCRAFT, INC.

PART NUMBER 761-892 REVISED: DECEMBER 6, 2002

THE NEW PIPER AIRCRAFT, INC.
PA-44-180
AIRPLANE MAINTENANCE MANUAL

Published by
Technical Publications

. The New Piper Aircraft, Inc.
2926 Piper Drive
Vero Beach, Florida  32960
U.S.A.

Member General Aviation Manufacturers Association
THE NEW PIPER AIRCRAFT, INC.
PA-44-180
AIRPLANE MAINTENANCE MANUAL

AEROFICHE REVISION STATUS
Revisions to this Maintenance Manual (P/N 761-892) issued April 1, 1997 are as follows:
Revision Publication Date Aerofiche Card Effectivity

ORG970401 April 1, 1997 1, 2, 3, and 4 PR020228 February 28, 2002 1, 3, and 4 PR021206* December 6, 2002 2
* PARTIAL REVISION OF MAINTENANCE MANUAL 761-892
Revisions appear only in Aerofiche Card 2. Accordingly, discard your existing Aerofiche Card2 and replace it with this one dated 12/06/02.
Consult the Customer Service Information Aerofiche (P/N 1753-755) for current revision dates for this manual.
Aerofiche Effectivity Page 1 Revised: December 6, 2002
THE NEW PIPER AIRCRAFT, INC.
PA-44-180
AIRPLANE MAINTENANCE MANUAL

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Aerofiche Effectivity Page 2 Revised: December 6, 2002
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THE NEW PIPER AIRCRAFT, INC.
PA-44-180
AIRPLANE MAINTENANCE MANUAL

INTRODUCTION 
TABLE OF CONTENTS / EFFECTIVITY 
CHAPTER SECTION  SUBJECT  GRID NO.  EFFECTIVITY 

Introduction A7 2R1202 Instructions for Continued Airworthiness A7 A1202 General A7 A1202 Effectivity A8 A1202 Serial Number Explanation A8 Assignment of Subject Material A8 A1202 Pagination A8 A1202 Aerofiche Effectivity A9 2R1202 Identifying Revised Material A9 2R1202 Indexing A9 A1202 Warnings, Cautions, and Notes A10 2R1202 Supplementary Publications A10 A1202 PIPER Publications A10 2R1202 Vendor Publications A10 2R1202 Chapter/Section Index Guide A13 2R1202
List of Illustrations A18 2R1202
List of Charts A23 2R1202
Introduction - Cont./Effec. Page 1 Revised: December 6, 2002
THE NEW PIPER AIRCRAFT, INC.
PA-44-180
AIRPLANE MAINTENANCE MANUAL

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Introduction - Cont./Effec. Page 2 Revised: December 6, 2002
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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).
　
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