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an approved procedures manual. Contact Diamond Aircraft if damages are determined which
cannot be repaired in accordance with an approved procedures manual.
Interval (Flight Hours)
Inspection Items 50 100 200 1000 6000 Initials.
1. Remove the seat shells.
(Refer to Chapter 25-10).
x x x x
2. Visually examine the seats and seat
attachments. Look especially for cracks,
delamination and damage around the
fastener holes.
x
3. Visually examine the cockpit floor. Look
especially for cracks or delamination around
the aft rudder pedal bracket, boarding step,
and the throttle quadrant opening.
x
4. Examine the safety belts for general
condition and security of the metal fitting in
the surrounding composite.
Make sure the lock mechanism operates
correctly.
− Insert the connector into the buckle and
pull on the connector. Make sure the
ratchet holds the connector. The
connector must fall freely from buckle
when held in a vertical position and when
you open the cover to the release
position.
x x x x
5. Examine the cable ties and electrical
connectors. Pull lightly to make sure they
are not loose
x 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 x
7. Examine the control stick stops. x x x x
8. Examine the pitot-static system water traps. x x x x
9. Examine the stall warning hose. Look
especially for contamination by water.
(Refer to Chapter 34-20).
x x x x
10. Examine the flap-actuator indicator and
position switches. Look especially for
correct attachment and operation.
x x x x
Time Limits and
Maintenance Checks
DA20-C1 AMM
Page 20
30 Apr 2008 05-20-00 Doc # DA201-C1
Rev. 13
Interval (Flight Hours)
Inspection Items 50 100 200 1000 6000 Initials.
11. Examine the flap-actuator stops and support.
Look especially for correct attachment.
Examine for security of the bracket on the
laminate and cracks in the surrounding
laminate.
x x x x
12. Examine the locking-device for the wing
main-bolt. Look especially for:
− Correct operation.
− Condition.
x x x x
13. Examine the mounting for the landing gear.
Look especially for correct attachment and
lock devices.
x x x x
14. Visually examine the MLG and A-bolt
attachment brackets. Look especially for:
- Cracks in, or corrosion of the bracket.
- Disbond from the laminate.
- Delamination in the surrounding
laminate.
x
15. Examine the rudder pedals. Look especially
for correct attachment and function.
(Refer to Chapter 27-20)
x x x x
16. Examine the rudder cables and pulleys.
Look especially for correct attachment and
function, and for wear, damage and
corrosion.
(Refer to Chapter 27-20)
x x x x
17. Examine the areas where the rudder cable
pulley-brackets attach to the fuselage. Look
especially for security of the pulley brackets
on the laminate and cracks in the
surrounding laminate.
x
18. Examine the brake pipes/hoses and
components. Look especially for leakage.
x x x x
19. Drain and replace the brake fluid in the
brake reservoirs.
(Refer to Chapter 32-40)
x
20. Examine the brake reservoirs on the
co-pilots side. Make sure the fluid level is
correct.
The fluid level must be 12mm to 25mm
(1/2 to 1 in) below the top face of the
reservoir filler hole.
x x x x
DA20-C1 AMM
Time Limits and
Maintenance Checks
Doc # DA201-C1
Rev. 13 05-20-00 Page 21
30 Apr 2008
Interval (Flight Hours)
Inspection Items 50 100 200 1000 6000 Initials.
21. Examine the instruments. Make sure that:
− The markings are clear.
− The function is correct.
− Switches are correctly attached.
x x x x
22. Examine the interior placards. Make sure
that they are not damaged and that none
are missing.
Replace any that are damaged or missing.
(Refer to Chapter 11-30).
x* x x x
23. Remove the instrument panel cover. x x x x
24. Remove the instrument panel.
(Refer to Chapter 31-10).
x
25. Remove the cover box for access to the fuel
shut-off valve.
(Refer to Chapter 28-20).
x
26. Examine the two fuel hoses that run from the
drain trap block, along the floor of the cockpit
to the fuel shut-off valve, as follows:
NOTE: You must bleed the engine fuel
system after any work which allows
air into the airplane fuel supply
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