Diamond DA 62 - Page 172

DA 62 AFM
Normal Operating
Procedures
6. Fuselage, right side:
a) Fuselage skin . . . . . . . . . . . . . . . . . . . . . . . . visual inspection
b) Rear window + window . . . . . . . . . . . . . . . . . visual inspection
c) RH Pilot door . . . . . . . . . . . . . . . . . . . . . . . . . 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 5 cm/2.0 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) Tank air outlet on lower surface . . . . . . . . . . visual inspection
c) Tank drain/tank air inlet . . . . . . . . . . . . . . . . . drain off to check for water and
sediment (drain until no water
comes out)/visual inspection
CONTINUED
Doc. No. 11.01.05-E Rev. 0 11-Jan-2019 Page 4A - 15