Commonwealth legislation

AD/JETSTREAM/66 - Wing - Main Spar Fuel Fitting Attachment Holes

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Commonwealth

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legislative instrument

Plain English Summary

2/10 complexity

This AD requires owners/operators of Jetstream 3200 aircraft up to constructor’s number 950 to modify the fuel tank drainage hole at wing station 64.8 on both wings per BAe Service Bulletin 57‑JM 8175 Rev 1. The modification must be done before 6,000 landings or 15 March 1995 (whichever is later) to address observed wing spar web cracking; the compliance obligation (and cost) rests with the owner/operator.

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AD/JETSTREAM/66 - Wing - Main Spar Fuel Fitting Attachment Holes

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

View image in the official source British Aerospace BAe 3100 (Jetstream) Series Aeroplanes

AD/JETSTREAM/66 Wing - Main Spar Fuel Fitting Attachment Holes

Applicability: Jetstream 3200 Series aircraft up to and including constructor’s number 950.

10/94

Requirement: Modify the fuel tank drainage hole at wing station 64.8 on the left and right hand sides in accordance with British Aerospace SB 57-JM 8175 revision 1.

Compliance: Prior to 6000 landings or before 15 March 1995 whichever is the later.

Background: Cracking of the wing main spar webs has been found at this location on the Jetstream 3200 series wing test specimen.

Source text

Sourced from the Federal Register of Legislation (legislation.gov.au), CC BY 4.0.