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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 33
20 Sep 2007
29. Examine the trim control in the center console.
Make sure that:
S There is full and free movement.
S There is no unusual play.
X X X
30. If the autopilot system is installed, then examine
the trim servo assembly. Look specially for:
S Wear and corrosion.
S Insecure attachment of servo.
S Damaged, deformed, or worn out cardan shaft
and chain gears.
(Refer to Section 22-10).
X X X
31. Examine the front cockpit structure. Look for disbonding,
delamination and damage, specially to
these components:
S The fuselage shells.
S The firewall.
S The floor.
S The control bulkhead.
S The fuel pipe channels.
S The front main bulkhead.
S The rear main bulkhead.
S The inner faces of the front and rear closing
ribs.
S The front and rear seat crash elements.
X
AIRCRAFT
Time Limits and
Maintenance Checks
DA 40 Series
AMM
Page 34
20 Sep 2007 05-20-00 Doc # 6.02.01
Rev. 5
D. Center Fuselage, Internal
100 hr items marked X* apply to US registered airplanes only Interval
Inspection Items 50 100 200 1000 Time Initials
1. Examine the fire extinguisher. Make sure that:
S The fire extinguisher will release from the
mounting bracket.
S The fire extinguisher contents are full.
X X X
2. Examine the baggage net. Make sure the spring
clips operate correctly.
X X X
3. Examine the ELT. (Refer to Section 25-60). X X X
4. Do an inspection of the ELT system. (Refer to
Section 25-60).
1 yr.
5. If the autopilot system is installed, then examine
the pitch servo assembly. Look specially for:
S Wear and corrosion.
S Insecure attachment of servo.
S Defective bridle cable assembly.
S Loose bridle cables or clamps on the elevator
push-rod.
(Refer to Section 22-10).
X X X
6. Examine the cable ties and electrical connectors.
Pull lightly to make sure they are not loose.
X* X X
7. Examine the push rod guides for the elevator
push-rod. Look specially for incorrect attachment
and interference.
X* X X
8. Examine the flap control mechanism on the aft
main bulkhead. Look specially for:
S Damage and corrosion.
S Incorrect attachment and loose or missing
lock devices.
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 35
20 Sep 2007
9. Examine the flap-actuator indicator and position
switches. Look specially for incorrect attachment
and operation.
X* X X
10. Examine the aileron control system on the aft
main bulkhead. Look specially for:
S Damage and corrosion.
S Incorrect attachment and loose or missing
lock devices.
X* X X
11. If the autopilot system is installed, then examine
the roll servo assembly. Look specially for:
S Wear and corrosion.
S Insecure attachment of servo.
S Defective bridle cable assembly.
S Loose bridle cables or clamps on the aileron
push-rod.
(Refer to Section 22-10).
X X X
12. If the KCS 55A compass system is installed, then
% examine the directional gyro below the passenger
% seats. Make sure that it is attached correctly.
X* X X
13. Do a cable tension test of the rudder control
cable. (Refer to Section 27-20).
X* X X
14. Examine the center fuselage structure. Look for
dis-bonding, delamination and damage, specially
to these components:
S The fuselage shells.
S The baggage compartment frame.
X
AIRCRAFT
Time Limits and
Maintenance Checks
DA 40 Series
AMM
Page 36
20 Sep 2007 05-20-00 Doc # 6.02.01
Rev. 5
E. Rear Fuselage
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 rear
fuselage. Look specially for damage (dents,
cracks, holes and delamination).
Examine the paint coat.
X X X
2. Examine the push rod guides for the elevator
push-rod. Look specially for:
S Incorrect attachment.
S Interference.
X* X X
3. Examine the rudder-control cables and
turnbuckles. Look specially for:
S Corrosion and wear.
S Incorrect lock devices.
X* X X
　
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