Commonwealth legislation

AD/BEECH 400/4 - Fuselage Rivets

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Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This directive requires owners/operators of specified Beechcraft 400A (RK‑1–RK‑41) and 400T (TT‑3–TT‑20) aeroplanes to carry out the work in Beechcraft Mandatory Service Bulletin 2482 within 100 hours’ time in service after 9 December 1993. It was issued to address reports that rivets may have been omitted near the upper edge of the emergency exit door; affected operators bear the inspection/repair cost and downtime.

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AD/BEECH 400/4 - Fuselage Rivets

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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 Beechcraft 400 Series Aeroplanes

AD/BEECH 400/4 Fuselage Rivets 13/93

Applicability: Model 400A with serial numbers RK-1 through RK-41. Model 400T with serial numbers TT-3 through TT-20.

Requirement: Action in accordance with Beechcraft Mandatory Service Bulletin 2482.

Note: FAA AD 93-16-12 Amdt 39-8670 refers.

Compliance: Within 100 hours’ time in service after 9 December 1993.

Background: The FAA received reports that during manufacture, rivets may have been inadvertently omitted from the area adjacent to the upper edge of the emergency exit door.

Source text

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