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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 

Doc # 6.02.01 Page 33
Rev. 4 09 Jan 2003

05-20-00
Maintenance Checks
AMM

%

DA 40 Series

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

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 
17. 18. 19. 20.  Examine the structure of the vertical stabilizer. Look specially for dis-bonding, delamination and damage to the shells, spars and ribs. Install the fairing for the horizontal stabilizer. (Refer to Section 55-10). Install the rudder. (Refer to Section 55-40). Examine the vent and drain holes in the horizontal stabilizer and control surfaces. Make sure they are clear.  X* X X  X X X  X X X X 

05-20-00
Maintenance Checks
AMM

G. Wings
%

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 wings. Look specially for damage (dents, cracks, holes and delamination). Examine the paint coat.  X  X  X 
　
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