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and 27-30).
X* X X
9. Examine the Pitot-static system water traps. X X X
10. Examine the stall-warning hose. Look specially for
contamination by water. (Refer to Section 34-20).
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 30
20 Sep 2007 05-20-00 Doc # 6.02.01
Rev. 5
% 11. Examine the rudder pedals. Look specially for
%
S Incorrect attachment and function.
% S Corrosion and damaged surface protection.
% S Damaged adjustment mechanism.
% S Improper function of adjustable mechanism.
% (Refer to Section 27-20).
X X X
%
12. Examine the rudder cables and pulleys. Look
specially for
S Incorrect attachment and function. (Refer to
Section 27-20).
S Rub marks.
S Defective safety plates.
S Worn out pulleys.
X X X
13. Examine the brake pipes/hoses and components.
Look specially for leakage.
X X X
14. Examine the brake fluid reservoirs on the
co-pilot's side. Make sure the fluid level is correct.
S The fluid level must be 12 mm to 25 mm (1/2
to 1 in.) below the top face of the reservoir
filler hole.
X X X
15. Examine the instruments. Make sure that:
S The markings are clear.
S The function is correct.
S Switches are correctly attached.
S The instrument lights operate correctly.
X X X
16. Examine the placards. Make sure that:
S They are not damaged.
S None are missing. (Refer to Chapter 11).
X X X
17. Remove the instrument panel cover. 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 31
20 Sep 2007
18. Examine the instrument panel. Make sure that:
S The wiring is correctly attached.
S The instruments are correctly attached.
S The hoses are correctly attached.
S The circuit breakers are correctly attached.
S The cooling fan is operative and correctly
attached.
X* X X
19. Examine the emergency battery system, if
installed:
S Measure the voltage of the emergency battery
on the EMERGENCY switch. Replace
emergency battery (all 28 cells) if the voltage
% is below 42 V (below 21 V for the TAE
% version).
% S Make sure that the seal on the EMERGENCY
switch is intact.
X X X
20. Lycoming version only: Replace the DPU battery
memory pack of the VM 1000 engine instrument
unit. (Refer to Section 77-40).
8
yrs.
21. TAE version only: Examine the ECU backup
battery:
S Check for leakage, damage, insecure
mounting, and loose connectors.
S Measure voltage (minimum: 12.5 volts).
X X X
22. TAE version only: Replace the ECU backup
battery.
2
yrs.
23. TAE version only: Replace the alternator
excitation battery.
1
yr.
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 32
20 Sep 2007 05-20-00 Doc # 6.02.01
Rev. 5
24. Examine the alternate static valve, if installed.
Make sure that:
S The valve is correctly attached.
S The valve is not blocked.
S The hoses are correctly attached.
X* X X
25. Examine the compass. Make sure that:
S The compass is correctly attached.
S The fluid level is correct.
X X
26. Examine the controls in the center console. Make
sure that for each control lever:
S There is full and free movement.
S There is no unusual play.
S The friction is correct.
S The mixture lock-out operates correctly
(Lycoming version only).
X X X
% 27. Inspect universal joints in fuel selector shaft
% (upper and lower) very carefully for:
% S excessive wear
% S uneven movement
% S pins not completely pressed in
% S loose pins
X
28. Examine the control cables in the center console:
S Remove the retaining screws for the center
console cover plate.
S Lift the center console cover plate and visually
examine the cables. Look specially for wear
and kinks in the cables.
S Lower the center console cover plate into the
correct position, install the retaining screws.
X X X
AIRCRAFT
DA 40 Series
AMM
Time Limits and
Maintenance Checks
　
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