% 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
Rev. 4 09 Jan 2003

05-20-00
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 
　
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