Diamond DA 62 - Page 175

Normal Operating
Procedures
DA 62 AFM
10. Front fuselage and nose landing gear:
a) Left and right front baggage door . . . . . . . . . . visual inspection, closed and locked
b) Nose landing gear strut . . . . . . . . . . . . . . . . . visual inspection, sufficient height
(typical visible length of bare piston:
at least 10 cm/3.9 in)
c) Down & uplock switches . . . . . . . . . . . . . . . . visual inspection
d) Wear, tread depth of tire . . . . . . . . . . . . . . . . check
e) Slip marks . . . . . . . . . . . . . . . . . . . . . . . . . . . visual inspection
f) Gear door and linkage . . . . . . . . . . . . . . . . . . visual inspection
g) If OÄM 62-009 is installed:
Nose cone surface . . . . . . . . . . . . . . . . . . . . visual inspection
h) If OÄM 62-009 is installed:
Nose cone attachment screws . . . . . . . . . . . visual inspection
i) If OÄM 62-009 is installed:
Nose cone lightning protection strips . . . . . . . visual inspection
j) Chocks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . remove
k) OAT sensor . . . . . . . . . . . . . . . . . . . . . . . . . . check
l) EPU connector. . . . . . . . . . . . . . . . . . . . . . . . check
m) Tow bar . . . . . . . . . . . . . . . . . . . . . . . . . . . . . remove
END OF CHECKLIST
Page 4A - 18 Rev. 0 11-Jan-2019 Doc. No. 11.01.05-E