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Service Difficulty Advisory

AV 1999-03
15 July 1999

Bell 206 Series

Cracked Frame

An SDR submitter reported cracking under the nutplates on the passenger seat bulkhead frame P/N 206-033-107-049. The cause was due to AN525 washer-head screws having been replaced by AN3 bolts and AN970 washers. The extra length of the unauthorized substitution meant that the bolt indented the frame, initiating the fatigue cracking.

If left uncorrected, the integrity of the frame is compromised and the damage spreads to surrounding structures. Cracks were also reported on the inner skin and these could migrate up to the frame.

This cracking can only be found after removal of the interior. Therefore, Transport Canada strongly recommends an immediate inspection for the proper use of AN525 washer-head screws. If an AN3 bolt is found instead, the removal of the interior and close inspection of the frame for cracking is required.

The following Bell Illustrated Parts Breakdowns refer:

  • BHT-206A/B-Series-IPB, Fig. 53-16, items 28, 39, 40; Fig. 53-17, item 38; and Fig. 53-20, items 39 and 40.
  • BHT-206L-Series-IPB, Fig. 53-25, items 21, 22, 27, 28; Fig, 53-28, items 19, 44; Fig. 53-26, items 33, 34.
Arrows pointing to cracks under the nutplates on the passenger seat bulkhead

For further information contact a Transport Canada Centre, or call Mr. Bogdan Gajewski, Continuing Airworthiness, Ottawa, telephone (613) 952-4450, facsimile (613) 996-9178 or e-mail gajewsb@tc.gc.ca.

For Director, National Aircraft Certification

B. Goyaniuk
Chief, Continuing Airworthiness

 

Date modified:
2012-02-03