CHAPTER 07
PAGE 3
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RA - FLUGZEUGBAU GmbH
SERVICE MANUAL EXTRA 200
PAGE DATE: 1. July 1996
07-10-00 JACKING
07-10-01 Balance Weight
Prior to the removal of the horizontal and/or vertical
stabilizer(s) or prior to shoring the aircraft as described in
Chapter 07-20-00 it is necessary to weight the tail to
prevent aircraft from tilting onto the nose. In this case
follow the steps described below (refer to Figure 1):
1 Put a weight (1) of min. 30 kg under the tail.
2 Remove the RH tail side skin and the tail cone access
panel per Chapter 51.
3 Connect the weight with the now accessible steel tube
(3) by means of a strap (2). Prevent damage of paint and
control cables.
Balance Weight
Figure 1
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