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Extra 200 - Main Landing Gear Maintenance

Extra 200
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CHAPTER 32
PAGE 4
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RA - FLUGZEUGBAU GmbH
SERVICE MANUAL EXTRA 200
PAGE DATE: 1. July 1996
32-11-00 MAINTENANCE PRACTICES
32-11-01 Main Landing Gear
Removal/Installation
Refer to Figure 2
1 Remove the engine cowling, the landing gear cuffs and
the bottom covering sheet as per chapter 51-00-01.
2 Shore the aircraft as per Chapter 07-20-00
3 Drain brake system.
4 Unfasten the ventilation tubings and brake lines, and
disconnect the brake lines from the brake assembly.
5 Remove the four landing gear attachment stop nuts
(LN9348-8) (1) and the DIN 125 M8 washers.
6 Remove the bottom halves of the mounting clamps (2),
the anti abrasion strips (3) and the landing gear (4).
7 Install in reverse sequence of removal using new stop
nuts. For correct position of landing gear the mandrel,
which is located at the bottom of the fuselage, is to put
into the respective sleeve at the top of the landing gear
spring. Replenish brake fluid.
32-11-02 Top Half of the Mounting Clamp
Removal/Installation
Refer to Figure 2
1 Remove the main landing gear as per Chapter 32-11-
01.
2 Remove the LN9348-10 stop nuts, the DIN125 M10
washers and the LN9037-10054 bolts (5).
3 Remove the top half of the mounting clamp (6).
4 Reverse procedure for installation.
PAGE DATE: 1. June 1996

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