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4. Examine the vent and drain holes in the rear
fuselage. Make sure they are clear.
X X X
5. Examine the rear fuselage structure. Look for disbonding,
delamination and damage specially to
these components:
S The fuselage shells.
S Ring frames 1, 2 and 3.
X
% 6. If the Autopilot Static Source (OÄM 40-267) is
% installed:
% Check static source holes for blockage.
X X X
AIRCRAFT
DA 40 Series
AMM
Time Limits and
Maintenance Checks
Doc # 6.02.01
Rev. 5 05-20-00 Page 37
20 Sep 2007
F. Tail
100 hr items marked X* apply to US registered airplanes only Interval
Inspection Items 50 100 200 1000 Time Initials
1. Examine the complete surface of the aft part of
the fuselage, vertical stabilizer, and horizontal
stabilizer. Look specially for damage (dents,
cracks, holes and delamination).
Examine the paint coat.
X X X
2. Examine the lower fin. Look specially for:
S Damage to the bottom of the fin.
S Incorrect attachment.
X X X
3. Remove the rudder. Lubricate the hinge bushes.
(Refer to Section 55-40).
X X X
4. Examine the inside of the vertical stabilizer. X X
5. Examine the rudder mounting and control cable
connections.
X X X
6. Examine the rudder support bracket. X X X
7. Examine the bottom edge of the rudder. Look
specially for cracks and deformation.
X X X
8. Examine the rudder-stop reinforcement bars.
Look specially for cracks and corrosion.
X X X
9. Examine the trim mechanism. Look specially for:
S Incorrect attachment.
S Wear.
X X X
10. Examine the trim tab for damage. Look specially
for incorrect attachment and loose or missing lock
devices. (Refer to Section 55-20).
X X X
11. Adjust the friction of the trim mechanism. 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 38
20 Sep 2007 05-20-00 Doc # 6.02.01
Rev. 5
12. Examine the horizontal stabilizer:
S Remove the fairing for the horizontal
stabilizer.
S Examine the mounting brackets. Look
specially at the attachment bolts for corrosion.
(Refer to Section 55-10).
X* X X
13. Remove the tips from the horizontal stabilizer.
S Examine the interior of the horizontal
stabilizer. Look specially for dis-bonding,
delamination and damage to the shells, spars
and ribs.
S Install the horizontal stabilizer tips.
(Refer to Section 55-10).
X
14. Examine the elevator for damage. Look specially
for incorrect attachment and loose or missing lock
devices. (Refer to Section 55-20).
X X X
15. Examine the elevator hinges and control horn.
Look specially for too much play.
Play allowed:
S Axial ± 1.00 mm (± 0.04 in.).
S Radial ± 0.25 mm (± 0.01 in.).
X X X
16. Examine the elevator push-rod:
S Remove the elevator push-rod which goes
through the rear fuselage.
S Look specially for rub marks.
S Install the push-rod.
(Refer to Section 27-30).
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 39
20 Sep 2007
17. Examine the structure of the vertical stabilizer.
Look specially for dis-bonding, delamination and
damage to the shells, spars and ribs.
X
18. Install the fairing for the horizontal stabilizer.
(Refer to Section 55-10).
X* X X
19. Install the rudder. (Refer to Section 55-40). X X X
20. Examine the vent and drain holes in the horizontal
stabilizer and control surfaces. Make sure they
are clear.
X X X
AIRCRAFT
Time Limits and
Maintenance Checks
DA 40 Series
AMM
Page 40
20 Sep 2007 05-20-00 Doc # 6.02.01
Rev. 5
G. Wings
100 hr items marked X* apply to US registered airplanes only Interval
Inspection Items 50 100 200 1000 Time Initials
1. Examine the complete surface of the wings. Look
specially for damage (dents, cracks, holes and
delamination).
Examine the paint coat.
X X X
2. Examine the ailerons. Look specially for damage
(dents, cracks, holes and delamination).
X X X
3. Examine the aileron hinges and horn. Look
specially for too much play.
Play allowed:
S Axial ± 1.00 mm (± 0.04 in).
　
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