AIRCRAFT
DA 42 NG AMM
Landing Gear
Detail Steps/Work Items
Key Items/References
Doc # 7.02.15
Rev. 4
32-20-00
Page 237
15 Mar 2018
(17)
The difference of the measurements in step 12
and step 16 must lie in between
0.1 mm (0.004 inch) and 0.9 mm (0.035 inch).
If the measurements do not meet the
requirement:
S
Adjust the pushrod of the nose landing gear
actuator.
S
Repeat steps 8 to 17.
Refer to Figure 8.
Maximum distance ‘Y’ (Min. screw-in
depth of rod end bearing): 34 mm
(1.34 in).
(19)
Tighten the nose landing gear actuator counter
nut and install the safety lock wire.
WARNING:
DUE TO THE HIGH FORCES INVOLVED, THE LANDING GEAR
RETRACTION SYSTEM CAN CAUSE SERIOUS INJURY TO
PERSONS. MAKE SURE THAT NO PERSON CAN BE HIT OR
CRUSHED WHEN OPERATING THE LANDING GEAR RETRACTION
SYSTEM.
(20)
Set the GEAR circuit breaker.
(21)
Set the ELECT. MASTER switch to ON.
(22)
Retract the landing gear:
S
Set the Landing Gear Switch to the UP
position and secure against inadvertent
operation.
(23)
Check the clearance between the nose landing
gear tire and the nose landing gear doors:
S
Close one NLG door by hand.
S
The clearance must be at least 20 mm
(0.8 in).
If the clearance does not meet the requirement:
Contact DAI.
Refer to Figure 7.
Summary of Contents for DA 42 NG
Page 933: ...AIRCRAFT DA 42 NG AMM Fuel Doc 7 02 15 Rev 4 28 TITLE Page 1 15 Mar 2018 CHAPTER 28 FUEL ...
Page 1459: ...AIRCRAFT DA 42 NG AMM Lights Doc 7 02 15 Rev 4 33 TITLE Page 1 15 Mar 2018 CHAPTER 33 LIGHTS ...
Page 1711: ...AIRCRAFT DA 42 NG AMM Doors Doc 7 02 15 Rev 4 52 TITLE Page 1 15 Mar 2018 CHAPTER 52 DOORS ...
Page 1853: ...AIRCRAFT DA 42 NG AMM Wings Doc 7 02 15 Rev 4 57 TITLE Page 1 15 Mar 2018 CHAPTER 57 WINGS ...
Page 2071: ...AIRCRAFT DA 42 NG AMM Engine Doc 7 02 15 Rev 4 72 TITLE Page 1 15 Mar 2018 CHAPTER 72 ENGINE ...
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