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
Summary of Contents for DA 62
Page 2: ...DA 62 AFM Introduction Intentionally left blank Page 0 0a Rev 0 11 Jan 2019 Doc 11 01 05 E ...
Page 36: ...DA 62 AFM General 1 7 THREE VIEW DRAWING Doc No 11 01 05 E Rev 0 11 Jan 2019 Page 1 19 ...
Page 363: ...Performance DA 62 AFM Intentionally left blank Page 5 92 Rev 0 11 Jan 2019 Doc No 11 01 05 E ...
Page 438: ...Airplane Description DA 62 AFM Page 7 46 Rev 0 11 Jan 2019 Doc No 11 01 05 E ...
Page 496: ...Handling Care Maintenance DA 62 AFM Page 8 10 Rev 0 11 Jan 2019 Doc No 11 01 05 E 1 4 5 2 3 ...