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% (2) Elevator end rib, next to the rear spar, next to lower shell, RH
% (3) Mid rib in front of rear spar, next to lower shell, LH
% (4) Mid rib in front of rear spar, next to lower shell, RH
% (5) Mid rib rear of front spar, next to lower shell, LH
% (6) Mid rib rear of front spar, next to lower shell, RH
% (7) Mid rib in front of front spar, next to lower shell, LH
% (8) Mid rib in front of front spar, next to lower shell, RH
% (9) Left rib, rear of front spar, next to lower shell
% (10) Right rib, rear of front spar, next to lower shell
% (11) Left rib, in front of front spar, next to lower shell
% (12) Right rib, in front of front spar, next to lower shell
% (13) Lower shell, to the left of mid inspection hole
% (14) Lower shell, to the right of mid inspection hole
AIRCRAFT
Time Limits and
Maintenance Checks
DA 40 Series
AMM
% Drain hole location Initials
Page 56
20 Sep 2007 05-20-00 Doc # 6.02.01
Rev. 5
% (15) Lower shell, to the left of front inspection hole
% (16) Lower shell, to the right of front inspection hole
% (d) Elevator
% Drain hole location Initials
% (1) Lower shell, in front of trailing edge bonding, LH
% (2) Lower shell, in front of trailing edge bonding, RH
% (3) Lower shell, leading edge section, LH
% (4) Lower shell, leading edge section, RH
% (e) Wings
% Drain hole location Initials
% (1) Front root rib, in front of front spar, next to lower shell
% (2) Rear root rib, aft of rear spar, next to lower shell
% (3) First inner fuel tank rib, next to front spar bonding and lower shell
% (4) First inner fuel tank rib, next to rear spar bonding and lower shell
% (5) Second inner fuel tank rib, next to front spar bonding and lower shell
% (6) Second inner fuel tank rib, next to rear spar bonding and lower shell
% (7) First outer fuel tank rib, next to front spar bonding and lower shell
% (8) First outer fuel tank rib, next to rear spar bonding and lower shell
% (9) Second outer fuel tank rib, next to front spar bonding and lower shell
% (10) Second outer fuel tank rib, next to rear spar bonding and lower shell
% (11) Rear web, next to mass balance recess
% (12) Lower shell, next to end rib in front of front spar
AIRCRAFT
DA 40 Series
AMM
Time Limits and
Maintenance Checks
Doc # 6.02.01
Rev. 5 05-20-00 Page 57
20 Sep 2007
% (f) Flap
% Drain hole location Initials
% (1) Root rib, next to trailing edge bonding
% (g) Aileron
% Drain hole location Initials
% (1) Root rib, next to trailing edge bonding
% (2) Lower shell, mass balance aft of heavy metal
% (3) Lower shell, mass balance in front of hingeline
% (h) Cowling
% Drain hole location Initials
% (1) Cowling bulkhead, on lowest spot, LH
% (2) Cowling bulkhead, on lowest spot, RH
AIRCRAFT
Time Limits and
Maintenance Checks
DA 40 Series
AMM
Page 58
20 Sep 2007 05-20-00 Doc # 6.02.01
Rev. 5
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:
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.
Inspection Items Initials
1. Check oil system including hoses for leakage. Refer to Section 79-01.
2. Check engine fuel system including hoses and pipes for leakage. Refer to
Section 73-01.
3. Check engine cooling system including hoses for leakage. Refer to Section
% 75-01.
%
% 4. Replace coolant. Refer to Section 75-01.
% 5. Visually inspect the air filter. Refer to Section 71-61.
6. Visually inspect the FADEC sensors. Look specially for loose connectors and
% abrasion on the harness. Refer to Section 76-01.
%
% 7. Visually inspect the exhaust system. Refer to Section 78-01.
% 8. Visually inspect the flat belt. Refer to Section 75-01.
9. Perform an engine test run in accordance with Paragraph 7.B, Engine
% Ground Test Record - TAE Version.
%
AIRCRAFT
DA 40 Series
AMM
Time Limits and
Maintenance Checks
Inspection Items Initials
Doc # 6.02.01
Rev. 5 05-20-00 Page 59
20 Sep 2007
%
10. Read the engine event log. Record events. E-mail Real Time Log Files and
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钻石40系列AMM 1(44)
