DA 42 NG AFM
Normal Operating
Procedures
Doc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4A - 15
6. Fuselage, right side:
a) Fuselage skin ........................ visual inspection
b) Rear window ......................... visual inspection
c) Canopy, right side ..................... visual inspection
d) Static source......................... check for blockage
7. Right Main Landing Gear:
a) Landing gear strut and lock ............. visual inspection, sufficient height
(typical visible length of bare
piston: at least 4 cm/1.6 in)
b) Down and uplock switches (2 pieces) ...... visual inspection
c) Wear, tread depth of tire ................ visual inspection
d) Tire, wheel, brake ..................... visual inspection
e) Brake line connection .................. check for leaks
f) Slip marks........................... visual inspection
g) Chocks ............................. remove
h) Landing gear door ..................... visual inspection
8. Right wing:
a) Entire wing surface .................... visual inspection
b) Vortex generators ..................... undamaged, 4 pieces, clean
c) Tank air outlet on lower surface .......... visual inspection
d) Tank drain/tank air inlet ................ drain off to check for water and
sediment (drain until no water
comes out)/visual inspection
CONTINUED
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