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RA - FLUGZEUGBAU GmbH
SERVICE MANUAL EXTRA 200
CHAPTER 57
PAGE 7
PAGE DATE: 1. July 1996
W A R N I N G Beware not to get jammed between wing and fuselage.
7 Slide wing down into fuselage attachment brackets (3).
8 Preinstall LN 9037-08042 auxiliary spar attachment
bolts (1) from front to rear. Use two DIN 125-M8 wash-
ers at each side and LN 9348-08 nuts. Fasten only fin-
ger tight.
9 Install upper longeron cutout bridges (7) using at each
side 3x DIN912 M8 x 180, 3x DIN125 M8 washers
and 3x LN9348-08 stop nuts at the top and 1x DIN912
M10 x 230 bolt, DIN125 M10 washer and LN9348-10
stop nut at the bottom (6). Check cutout bridges for
RH and LH marking. Install the bolts from front (fire-
wall) to rear (aircraft tail). Torque stop nuts for fasten-
ing.
10 Install the shear connectors (8). Use two DIN 912
M12x220 bolts and safety wire.
I M P O R T A N T If there is clearance between the main spar and the at-
tachment brackets (1, Figure 2), use shims (3) like shown
below which are to be slided in the front gaps (2).
Shims Installation
Figure 2
11 Slide in shims if necessary and install the main spar
tubular bolts (4, Figure 3) from front to rear.
MAINTENANCE PRACTICES
Wing
PAGE DATE: 15. December 1999
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