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S Minimum thickness 3.0 mm (0.12 in).
X X X
15. Examine the brake disks. Look specially for wear.
S Minimum thickness 7.4 mm (0.29 in).
X* X X
16. Remove the access panels for the main landing
gear legs. (Refer to Section 52-40).
X* X X
17. Examine the mounting for the landing gear. Look
specially for
S Incorrect attachment.
S Loose or missing lock devices.
X* X X
18. Examine the main landing gear. Look specially for
cracks and deformation.
X* X X
AIRCRAFT
DA 40 Series
AMM
Time Limits and
Maintenance Checks
100 hr items marked X* apply to US registered airplanes only Interval
Inspection Items 50 100 200 1000 Time Initials
Doc # 6.02.01
Rev. 5 05-20-00 Page 27
20 Sep 2007
19. Do a test for toe-in and camber. (Refer to Section
32-10).
X
20. Examine the wing main bolts. Look specially for
incorrect locking.
X* X X
21. Examine these components on LH and RH sides
for dis-bonding, delamination and damage:
S The center section top and bottom shells.
S The outer faces of the front and rear main
bulkheads. Look specially in the area of the
bushes for the main pins.
S The front, middle and rear outer ribs.
S The main landing gear rib.
S The front and rear closing ribs.
S The rear web.
X
22. Examine the inner faces of the front and rear main
bulkheads with the wings removed. Look specially
in the area of the bushes for the main bolts. (See
also Zone G).
X
23. Install the access panels for the main landing gear
legs. (Refer to Section 52-40).
X* X X
24. Install the wheel fairings. X* X X
25. Remove the access panel for the nose landing
gear leg. (Refer to Section 52-40).
X* X X
26. Examine the nose-wheel assembly. Look
specially for incorrect attachment, cracks and
deformation.
X* X X
27. Examine the nose-gear journal-bearings in the
bottom of the fuselage. Look specially for play.
X* X X
28. Examine the journals in the elastomeric spring.
Look specially for play.
X X X
29. Examine the spherical bearing at the top of the
elastomeric spring. Look specially for play.
X X X
AIRCRAFT
Time Limits and
Maintenance Checks
DA 40 Series
AMM
100 hr items marked X* apply to US registered airplanes only Interval
Inspection Items 50 100 200 1000 Time Initials
Page 28
20 Sep 2007 05-20-00 Doc # 6.02.01
Rev. 5
30. Examine the elastomeric spring. Look specially for
S Looseness. Tighten if necessary.
S Damage. Replace elastomer donuts if
necessary.
X X X
31. Examine the nose-wheel fork. Do a test for play
and caster friction (refer to Section 32-20).
S The friction force should be 3 - 5 daN (6.75 -
11.25 lb) at the axle.
X X
32. Examine the gascolator:
S Remove and clean the fuel filter bowl.
S Install the filter bowl. (Refer to Section 28-20
for the Lycoming version or Section 28-21 for
the TAE version).
S Do a check for fuel leakage.
X X X
33. Examine the fuel pump electrical cables. Look
specially for rub marks.
X X X
34. Examine the top hat profile. Look specially for disbonding,
delamination and damage.
X
35. Install the access panel for the nose landing gear
leg. (Refer to Section 52-40).
X* X X
AIRCRAFT
DA 40 Series
AMM
Time Limits and
Maintenance Checks
Doc # 6.02.01
Rev. 5 05-20-00 Page 29
20 Sep 2007
C. Cockpit
100 hr items marked X* apply to US registered airplanes only Interval
Inspection Items 50 100 200 1000 Time Initials
% 1. Remove the front seats and the access panels in
% rear seat (if installed). (Refer to Section 25-10).
X* X X
% 2. Remove the rear seat shells.
% (Refer to Section 25-10)
X
3. Examine the seats for damage. X* X X
4. Examine the safety belts. Make sure the lock
mechanism operates correctly.
S Insert the tongue into the buckle.
S Pull on the strap. Make sure the ratchet holds
the tongue in the buckle.
S Operate the release button. The tongue must
pull freely from buckle.
X X X
5. Examine the cable ties and electrical connectors.
Pull lightly to make sure they are not loose.
X* X X
6. Examine the control sticks. Make sure that the
control stick attachments are not loose and do not
catch.
X X X
7. Examine the control stick stops. X X X
8. Examine the aileron and elevator control system.
Look specially for incorrect attachment and loose
or missing lock devices. (Refer to Sections 27-10
　
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