曝光臺 注意防騙 網(wǎng)曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

% Event Log Files to TAE. Refer to Section 72-01 and to the Operation &
% Maintenance Manual for the TAE 125-01 engine, Doc. No. OM-02-01.
%
11. Replace the gearbox oil filter. Refer to Section 72-01.
% Archive the used gearbox oil filter:
% S Store the filter in a clean container.
% S Label the container with airplane S/N, engine S/N, airplane registration,
% engine TSN, and date.
% S Keep the filter during the entire engine life to make it available to TAE
% upon request.
Events/Remarks:
______________ ______________ ______________
Place Date Authorized
AIRCRAFT
Time Limits and
Maintenance Checks
DA 40 Series
AMM
Page 60
20 Sep 2007 05-20-00 Doc # 6.02.01
Rev. 5
2000 Hour Structural Check DA 40
1. General
Enter the applicable data in the blocks below:
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.
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.
AIRCRAFT
DA 40 Series
AMM
Time Limits and
Maintenance Checks
Inspection Items Initials
Doc # 6.02.01
Rev. 5 05-20-00 Page 61
20 Sep 2007
Note: Do inspection items 3 through 10 while the rudder, the fairing for the horizontal
stabilizer, and the horizontal tail tips are removed.
3. Remove the horizontal stabilizer. Refer to Section 55-10.
4. Inspect the inner skin of the horizontal stabilizer through all access holes with
mirror and flashlight. Check for damage, cracks, and delamination. Refer to
Section 55-10.
5. Inspect the interior structure of the horizontal stabilizer through all access
holes with mirror and flashlight. Check for damage, cracks, delamination and
disbonding from the horizontal tail skin. Look specially at these components:
S Front spar.
S Rear spar.
S Trailing edge web.
S All interior ribs & stiffeners.
S Structure next to holes for mounting brackets.
Refer to Section 55-10.
6. Inspect the inner skin of the vertical stabilizer through all access holes with
mirror and flashlight. Check for damage, cracks, and delamination. Refer to
Section 53-10.
7. Inspect the interior structure of the vertical stabilizer through all access holes
with mirror and flashlight. Check for damage, cracks, delamination and
disbonding from the horizontal tail skin. Look specially at these components:
S Front web.
S Rear web.
S Lower rib (front & rear).
S Structure next to holes for horizontal tail mounting brackets.
Refer to Section 53-10.
8. Inspect the inner skin of the rear fuselage through all access holes with mirror
and flashlight. Check for damage, cracks, delamination and disbonding from
the sandwich foam. Refer to Section 53-10.
AIRCRAFT
Time Limits and
Maintenance Checks
DA 40 Series
AMM
Inspection Items Initials
Page 62
20 Sep 2007 05-20-00 Doc # 6.02.01
Rev. 5
9. Inspect the interior structure of rear fuselage through all access holes with
mirror and flashlight. Check for damage, cracks, delamination and disbonding
from the fuselage skin. Look specially at these components:
S Ring frames 1, 2, and 3.
Refer to Section 53-10.
10. Install the horizontal tail. Refer to Section 55-10.
11. Do a coin-tap test for delamination of the fuselage shell.
12. Do a coin-tap dest for delamination of the center section top and bottom
shells.
13. Complete the Findings Report (2 pages). Record the following:
S Defects found during the 2000 Hour Structural Check.
S Structural defects found during the associated 1000 hour inspection.
S All structural defects that were detected and repaired since new or since
the last 2000 Hour Structural Check.
14. Send a copy of the completed Findings Report (2 pages) to the manufacturer:
　
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