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RA - FLUGZEUGBAU GmbH
SERVICE MANUAL EXTRA 200
CHAPTER 57
PAGE 6
PAGE DATE: 1. July 1996
57-05-00 MAINTENANCE PRACTICES
57-05-01 Wing
Removal
Reverse procedure of installation omitting step 19.
Installation
1 Remove the canopy per Chapter 53, the engine cowl-
ings and the main fuselage cover per Chapter 51.
2 Remove the right front canopy hinge.
3 Loosen the breather line clamps located at the engine
side of the firewall and in the main spar area, push the
front part of the breather line some centimeters to the
front until it is disconnected from the connecting hose
(10, Figure 3) and remove the breather line (5) by pull-
ing it to the rear.
4 Remove the fuel selector valve control rod per Chap-
ter 28.
5 Remove the prop. vernier control handle and tie-wraps
fastening the cable in the cockpit area and lay vernier
control and cable forward over the engine.
6 Fix throttle lever and control sticks in rearmost posi-
tion.
C A U T I O N Ensure that areas in which the wing shall be slided are
clear of obstructions.
C A U T I O N Prevent cables and pitot/static lines from damage. Keep
them at the rear of the main spar and outside of the
upper longerons.
C A U T I O N Pay attention to the front canopy hinge and the throttle,
when sliding down the wing. These parts and the wing
could be damaged.
PAGE DATE: 15. December 1999
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