AIRCRAFT
DA 40 Series AMM
Temporary Revision
NLG Inspection & Maintenance
100 hr items marked X* apply to US registered airplanes only
Inspection Items
100 200 1000 2000 Time Initials
37.
Install the nose wheel fork. Do a test for play and caster
friction (refer to Section 32-20).
The friction force should be 30 - 50 N (6.75 - 11.25
lb) at the axle.
X
X
X
X
38.
Install the main and nose wheels.
X
X
X
X
39.
Install the wheel fairings.
X
X
X
X
40.
Examine the gascolator:
Remove and clean the fuel filter bowl.
Clean inspect the filter.
Install the filter bowl. (Refer to Section 28-20 for the
Lycoming version or Section 28-21 for the TAE
version).
Do a check for fuel leakage.
X
X
X
X
41.
Examine the fuel pump electrical cables. Look specially
for rub marks.
X*
X
X
X
42.
Examine the top hat profile. Look specially for dis-
bonding, delamination and damage.
X
X
43.
Install the access panel for the nose landing gear leg.
(Refer to Section 52-40).
X*
X
X
X
44.
If canopy jettison system (OÄM 40-232) is installed:
Perform release test of canopy jettison system. (Refer
to Section 52-10).
X
X
2 yrs.
45.
If canopy jettison system (OÄM 40-232) is installed:
100h maintenance check of canopy jettison system.
(Refer to Section 52-10).
X
X
X
X
Doc # 6.02.01
AMM-TR-MÄM 40-1037
05-28-50
Page 8
13 Jul 2020
