% WARNING: WHEN YOU COMPLETE AN INSPECTION, MAKE SURE THAT YOU
% REMOVE ALL LOOSE ITEMS/TOOLS FROM THAT AREA. LOOSE
% ITEMS/TOOLS CAN PREVENT FULL MOVEMENT OF THE AIRPLANE
% CONTROLS. THIS CAN CAUSE DEATH OR INJURY TO PERSONS.
% CAUTION: YOU MUST ATTACH BLANKS/CAPS TO HOLES/PIPES WHEN YOU % REMOVE COMPONENTS. IF YOU DO NOT DO THIS, UNWANTED % DEBRIS CAN ENTER THE HOLES/PIPES. THIS CAN CAUSE % BLOCKAGE TO THE AIRPLANE SYSTEMS.
Doc # 6.02.01 Page 49
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Maintenance Checks
AMM
% 5 Hour Engine Check (TAE) % 1. General
% This check must only be done on new TAE 125 Diesel engines after 5 hours of operation.
% Enter the applicable data in the blocks below:
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Registration : ____________________ Date : _________________
Airplane S/N : ____________________ Airplane Operating Hours : _________________
Engine S/N : ____________________ Engine Operating Hours : _________________
% % 2. Checklist for the 5 Hour Engine Check
% % % Do the inspection items given in the following table. Refer to the TAE 125-01 Operation and Maintenance Manual OM-02-01, latest effective issue.
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Inspection Items Initials
1. 2. 3. 4. Check oil system for leakage. Refer to Section 79-01. Check engine fuel system for leakage. Refer to Section 73-01. Check engine cooling system for leakage. Refer to Section 75-01. Read the engine event log. Record events. Refer to Section 72-01.
Events/Remarks: ______________ ______________ Place Date ______________ Authorized
Page 50 Doc # 6.02.01 09 Jan 2003 Rev. 4
05-20-00
AMM
Maintenance Checks
% 2000 Hour Structural Check DA 40 % 1. General
% Enter the applicable data in the blocks below: %
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Registration : ____________________ Date : _________________
Airplane S/N : ____________________ Airplane Operating Hours : _________________
% % % 2. Checklist for 2000 Hour Structural Check
% % % Do the 1000 hour inspection, supplemented by the structural inspection items given in the following table.
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Inspection Items Initials
Note: Do inspection items 1 and 2 while the wing tips, wings, and fuel tanks are removed.
1. Inspect the inner wing skin through all access holes with mirror and flashlight. Check for damage, cracks, delamination and disbonding from the sandwich foam. Refer to Section 57-10.
2. Inspect the interior structure of the wing through all access holes with mirror and flashlight. Check for damage, cracks, delamination and disbonding from the wing skin. Look specially at these components: S Front spar. S Rear spar. S Rear web. S Root rib (front, middle & rear). S End rib. S All interior ribs & stiffeners. Refer to Section 57-10.
Doc # 6.02.01 Page 51
Rev. 4 09 Jan 2003
05-20-00
Maintenance Checks
AMM
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DA 40 Series
Inspection Items Initials 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：钻石40飞机维护手册 DA 40 SERIES AMM 1(55)
