Diamond DA20-C1 Maintenance Manual page 129

DA20-C1 AMM
0
4.29
( )
330
3.77
0
290
Wing Assembly (LH)
0
0.72
0
(0.05 Nominal)
0.26
0
( )
20
55
SECTION B-B
Figure 203 - Installation of Spar bushing to a New Replacement Wing (Sweep and Dihedral Tolerances)
DA201-C1
Rev 17
(4400
(ALONG LEADING EGDE MOLD LINE)
(4400
(ALONG LEADING EGDE MOLD LINE)
Bushing,
Main Bolt Spar
Nut, Self-Locking
Spacer
57-10-00
)
)
(26)
C
A
B B
C
Filled Resin
Bushing,
Main Bolt Spar
Wing Assembly (RH)
Maintenance Practices
Wing Assembly (RH)
(4400)
(26)
WING ROOT
(REF.)
SECTION C-C
Spar Bridge, Fuselage
DETAIL A
Bolt, Main (Spar)
Assembly
Page 209
01 Nov 10