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RA - FLUGZEUGBAU GmbH
SERVICE MANUAL EXTRA 200
CHAPTER 55
PAGE 8
PAGE DATE: 1. July 1996
55-21-00 MAINTENANCE PRACTICES
55-21-01 Horizontal Stabilizer
Removal
Remove elevator and rudder per Chapter 27-31-01, remove
the vertical stabilizer per Chapter 55-21-02 and then re-
verse procedure of installation.
Installation
C A U T I O N Make shure that the trim bowden cable will not be dam-
aged when installing the horizontal stabilizer.
1 Slide the horizontal stabilizer with its front spar
(1, Figure 3) into the attach brackets (4) on fuselage.
The rear spar (2) is situated behind the rear attachment
bracket (5). (Trim tab is on the right side.)
2 Slide in LN 9037-10054 front spar attachment bolts
(8) with an additional DIN 125 M10 washer under bolt
head from the front to the rear. These bolts are also
used for the vertical stabilizer attachment. So do not
apply stop nuts before the vertical stabilizer is fitted to
the fuselage.
3 Slide in the rear spar attachment bolts (7) from front to
rear. Use LN 9037-10042 bolts in connection with LN
9348-10 stop nuts and DIN 125 M10 washers. Torque
nuts for fastening.
4 Fasten the ground bonding lead (3) by means of the
DIN 933 M5x12 bolt (6), the DIN 125 M5 washers
and the LN 9348-05 stop nuts.
5 Follow the procedure of Vertical Stabilizer Installation
(refer to Chapter 55-21-02).
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