AIRCRAFT
DA 42 NG AMM
Wings
Doc # 7.02.15
Rev. 4
57-10-00
Page 213
15 Mar 2018
B. Install the A or B-Bolt
Detail Steps/Work Items
Key Items/References
(1)
Examine the A or B-bolt. Look specially for:
S
Corrosion.
S
Scratches on the bearing surfaces.
S
Deformation.
S
Damage to the threads.
No corrosion permitted.
Maximum depth 0.1 mm (0.004 in).
No deformation permitted.
No damage permitted.
(2)
Examine the A or B-bolt bush. Look specially
for:
S
Looseness between the A or B-bolt bush
and the root rib.
S
Damage to the root rib where the bush
attaches.
S
Damage to the bush.
(3)
Install the A or B-bolt:
S
Install the bolt in the bush.
S
Hold the flats on the flange of the bolt with a
wrench.
S
Install the washer and self-locking nut.
Refer to Figure 3.
Access for the A-bolt through the hole in
the front root rib.
Access for the B-bolt through the access
panel in the bottom shell.
Torque: 32 Nm (23.6 lbf.ft.).
(4)
Install the wing.
Refer to Paragraph 2.
Summary of Contents for DA 42 NG
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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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