Commonwealth legislation

AD/BAe 146/70 - Skin Inspection at Frame 29 between Stringers 12 and 13

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

This AD, effective 16 July 1998, mandates the inspection in BAe Mandatory Service Bulletin 53-144 (as classified by the UK CAA) of the skin at frame 29 between stringers 12 and 13 on specified BAe 146 Series 100/200 and certain Series 300 aircraft after fatigue cracking was found. Operators must carry out and pay for the inspections and any repairs, increasing maintenance workload and potential aircraft downtime.

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AD/BAe 146/70 - Skin Inspection at Frame 29 between Stringers 12 and 13

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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 146 Series Aeroplanes

AD/BAe 146/70 Skin Inspection at Frame 29 between Stringers 12 and 13

8/98

Applicability: All BAe 146 Series 100 and 200 aircraft, and Series 300 aircraft with constructors numbers listed in effectivity of SB 53-144.

Requirement: Inspect in accordance with British Aerospace Mandatory Service Bulletin 53-144, classified mandatory by UK CAA.

Compliance: As specified in the Requirement document.

This airworthiness directive becomes effective on 16 July 1998.

Background: Fatigue cracking of the skin in the vicinity of frame 29 between stingers 12 and 13 has been found on two aircraft during routine inspection.

Source text

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