Commonwealth legislation

AD/BELL 205/48 - Fuselage Main Beams Splice - Modification

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This directive mandates modification of the fuselage main beam splice on specified Bell 205A-1 helicopters (listed serial numbers) to replace/correct aluminium rivets installed at manufacture with the proper rivets, using Bell Technical Bulletin No. 205-79-34 or FAA AD 80-03-07. Owners/operators must perform and pay for the work before 3 April 1980 to restore compliance and address the manufacturing error that affects airworthiness.

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AD/BELL 205/48 - Fuselage Main Beams Splice - Modification

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

Bell Helicopter Textron 205 Series Helicopters

AD/BELL 205/48 Fuselage Main Beams Splice - Modification 4/80

Applicability: All model 205A-1 with S/Nos. 30001 to 30287 and 30289 to 30296. Documents: 1. Bell Technical Bulletin No. 205-79-34; or

FAA AD 80-03-07 Amdt. 39-3681.

Compliance: Unless already accomplished, before 3 April 1980.

Background: At manufacture aluminium rivets were installed in the subject splice instead of Monel rivets.

Source text

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