钻石40飞机维护手册 DA 40 SERIES AMM 1(49)

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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 

Page 30 Doc # 6.02.01 09 Jan 2003 Rev. 4
05-20-00
AMM
Maintenance Checks

%

DA 40 Series

100 hr items marked X* apply to US registered airplanes only  Interval 
Inspection Items  50  100  200  1000  Time  Initials 
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 baggage compartment. 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 

05-20-00
Maintenance Checks
AMM

E. Rear Fuselage
%

DA 40 Series

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 
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 dis-bonding, delamination and damage specially to these components: S The fuselage shells. S Ring frames 1, 2 and 3.  X 

Page 32 Doc # 6.02.01 09 Jan 2003 Rev. 4
05-20-00
AMM
Maintenance Checks

F. Tail
%

DA 40 Series

100 hr items marked X* apply to US registered airplanes only  Interval 
Inspection Items  50  100  200  1000  Time  Initials 
　
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