36.
Remove access panels in baggage compartment floor and inspect wing attach fittings for corrosion, general condition, and security.
— Note —
Printed copies of the 100 Hour / Annual Inspection Report (Piper P/N 230-1963) can be obtained through an authorized Piper Parts and Service Distributor.
Page 5-24 Revised: February 28, 2002
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THE NEW PIPER AIRCRAFT, INC.
PA-44-180
AIRPLANE MAINTENANCE MANUAL
SPECIAL INSPECTIONS.
— WARNING —
FAILURE TO CONSULT APPLICABLE VENDOR PUBLICATION(S), WHEN SERVICING OR INSPECTING VENDOR EQUIPMENT INSTALLED IN PIPER AIRCRAFT, MAY RENDER THE AIRCRAFT UNAIRWORTHY. (SEE INTRODUCTION - SUPPLEMENTARY PUBLICATIONS.)
The following inspections are required in addition to those listed in scheduled maintenance. These inspections are required at intervals based on the specific operation being conducted or the environment being operated in.
Unless otherwise indicated, these inspections are to be repeated at each occurance of the specified interval. Note that the items listed herein are guidelines based on past operating experience. Each operator should closely monitor his own unique operating conditions/environment and react accordingly to keep his aircraft airworthy.
A. OPERATION IN HIGH DUST OR INDUSTRIAL POLLUTION ENVIRONMENT
— CAUTION —
DISCONNECT LINES FROM PITOT/STATIC SYTEM BEFORE CONDUCTING THIS INSPECTION.
Item Inspection Inspection Interval
. Engine Air Filter. Clean and inspect. Daily.
. Cabin Environmental Instrument Air Filters. and Inspect and replace if necessary. 100 Hours.
. Pitot/Static system. Check for obstruction. Reverse 100 Hours or
flow to lines. as required.
. Landing Gear Clean, inspect and lubricate. (Refer to 100 Hours.
Down Lock Assemblie s. Lubrication Chart, 12-20-00.)
. Landing Gear Oleos. Clean. Before each flight.
Inspect. 100 Hours.
. Landing Gear Wheel Bearings. Clean, inspect and repack. 50 Hours.
. Windows. Inspect for cracks, erosion, crazing, Daily.
visibility, and cleanliness.
. Structure drain holes. Clean with pipe cleaner. Before each flight.
Page 5-25 Revised: February 28, 2002
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THE NEW PIPER AIRCRAFT, INC.
PA-44-180
AIRPLANE MAINTENANCE MANUAL
B. OPERATION IN HIGH SALT OR HIGH HUMIDITY ENVIRONMENT
Item Inspection Inspection Interval
.
Fuselage, Empennage Remove floor panels and exterior 200 Hours. and Wings. access plates; inspect for corrosion.
.
Landing Gear. Inspect for corrosion and lubrication; 200 Hours.
— WARNING —
ENSURE BOTH MAGNETO SWITCHES ARE OFF (GROUNDED), BEFORE TURNING PROPELLER. ENGINE MAY START IF BOTH SWITCHES ARE NOT OFF. USE EXTREME CAUTION WHEN ROTATING PROPELLER BY HAND; PROPELLER MAY KICK BACK.
.
Engines with more than Each five days, pull prop through five Each 5 days
50 hours total time. complete revolutions. and Each 30 days, fly aircraft for 30 minutes each 30 days. or, ground run until oil temperature is in the green arc. Avoid excessive ground run.
.
Engines with less than Each day, pull prop through five Daily
50 hours total time. complete revolutions. and Each 30 days, fly aircraft for 30 minutes each 30 days. or, ground run until oil temperature is in the green arc. Avoid excessive ground run.
.
Instruments and Wiring. Inspect for proper seal of cases and 100 Hours. corrosion.
.
Interior. Inspect upholstery, seat belts, seats and 100 Hours. rugs for corrosion and integrity.
Note: Do not use metallic tie downs (i.e. - chains, cables, etc.) in high salt or high humidity environments.
C. OPERATION IN EXTREME COLD
Item Inspection Inspection Interval
. Hydraulic, Pneumatic and Environmental. Check all fittings and attachments for security and leaks. First 100 Hour, then as required.
5-30-00 Page 5-26 Revised: February 28, 2002
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THE NEW PIPER AIRCRAFT, INC.
PA-44-180
AIRPLANE MAINTENANCE MANUAL
D. OPERATION FROM SOFT OR UNUSUAL TERRAIN
Item Inspection Inspection Interval
.
Landing Gear.
.
Wheels.
.
Tires.
.
Wheel Wells.
.
Brakes.
.
Flaps, Lower Fuselage and Wing.
Inspect for cracks, attachment, 100 Hours.
damage, cleanliness and lubrication.
Inspect for cracks, damage, chipped 100 Hours. 中國航空網 www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：西門諾爾飛機維護手冊 simenole PA-44-180 AMM 1(19)
