A quick
inspection reveals that he can not turn the engine over, it has
locked up. He removes the engine, and takes it to his local Rotax
ultralight aircraft engine repair station.
Upon
disassembly it is found that the gear box ring halves (30) have
shattered, the angular retaining ring (29) has been damaged and
the groove on the prop shaft that the ring halves fit into has
been damaged.
Further inspection reveals that the spring washers
(25), are worn badly on the edges and at the center. The service
center decides to reassemble the gear box to check for gear box
preload. To get the proper preload a number of shims had to be
added. For diagnosing proper preload see below.*
The improper preload was allowing the springs to compress and
decompress. This was putting a "hammering" action on the retaining
ring and ring halves, pounding the halves against the prop shaft
groove, until they failed. Suggestions:
If you are flying on a Rotax A or B gear box it is suggested that
at 150 hours and at engine rebuild 300 hours the gear box be
inspected and the proper preload on the spring washers be set.
Ring half 827 860 (1 set) |
Angular ring 827 840 (1) |
Disk Springs (12) 939 020 |
Shims
944 474 .01 |
944 472-0.5 |
944 470-0.2 |
944 473-1 |
944 471-0.3 |
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