钻石40飞机维护手册 DA 40 SERIES AMM 1(46)

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10.  Examine the tires. Look specially for cuts and wear. Measure the tire pressure. (Refer to Section 12-10).  X  X  X 
11.  Examine the rims of the main and the nose wheels. Look specially for cracks.  X*  X  X 
12.  Examine the wheel bearings. Look specially for play, corrosion and irregular operation.  X*  X  X 
13.  Remove the main and nose wheels. S Clean and lubricate the bearings (Refer to Section 12-20). Install the main and nose wheels (Refer to Section 32-40).  X*  X  X 
14.  Examine the brake lining. Look specially for wear. S Minimum thickness 3.0 mm (0.12 in).  X  X  X 
15.  Examine the brake disks. Look specially for wear. S Minimum thickness 3.8 mm (0.15 in).  X*  X  X 
16.  Remove the access panels for the main landing gear legs. (Refer to Section 52-40).  X*  X  X 
17.  Examine the mounting for the landing gear. Look specially for S Incorrect attachment. S Loose or missing lock devices.  X*  X  X 
18.  Examine the main landing gear. Look specially for cracks and deformation.  X*  X  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 
19.  Do a test for toe-in and camber. (Refer to Section 32-10).  X 
20.  Examine the wing main bolts. Look specially for incorrect locking.  X*  X  X 
21.  Examine these components on LH and RH sides for dis-bonding, delamination and damage: S The center section top and bottom shells. S The outer faces of the front and rear main bulkheads. Look specially in the area of the bushes for the main pins. S The front, middle and rear outer ribs. S The main landing gear rib. S The front and rear closing ribs. S The rear web.  X 
22.  Examine the inner faces of the front and rear main bulkheads with the wings removed. Look specially in the area of the bushes for the main bolts. (See also Zone G).  X 
23.  Install the access panels for the main landing gear legs. (Refer to Section 52-40).  X*  X  X 
24.  Install the wheel fairings.  X*  X  X 
25.  Remove the access panel for the nose landing gear leg. (Refer to Section 52-40).  X*  X  X 
26.  Examine the nose-wheel assembly. Look specially for incorrect attachment, cracks and deformation.  X*  X  X 
27.  Examine the nose-gear journal-bearings in the bottom of the fuselage. Look specially for play.  X*  X  X 
28.  Examine the journals in the elastomeric spring. Look specially for play.  X  X  X 
29.  Examine the spherical bearing at the top of the elastomeric spring. Look specially for play.  X  X  X 
30.  Examine the elastomeric spring. Look specially for S Looseness. Tighten if necessary. S Damage. Replace elastomer donuts if necessary.  X  X  X 

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 
31.  Examine the nose-wheel fork. Do a test for play and caster friction (refer to Section 32-20). S The friction force should be 3 - 5 daN (6.75 -11.25 lb) at the axle.  X  X 
32.  Examine the gascolator: S Remove and clean the fuel filter bowl. S Install the filter bowl. (Refer to Section 28-20 for the Lycoming version or Section 28-21 for the TAE version). S Do a check for fuel leakage.  X  X  X 
　
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