Commonwealth legislation

AD/BEECH 400/6 - Escape Hatch Substructure Rivets

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This directive requires owners/operators of specified Beechcraft 400 and 400T serial-numbered aeroplanes to carry out the inspection/repair of the escape-hatch substructure per Beechcraft Mandatory Service Bulletin 2509, within 200 flight hours after 31 March 1994.

It delegates technical steps to the manufacturer’s MSB, concentrates cost and downtime on the listed operators, and mirrors a related FAA airworthiness finding.

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AD/BEECH 400/6 - Escape Hatch Substructure 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 400/6 Escape Hatch Substructure Rivets 4/94

Applicability: Model 400A aircraft with serial numbers RK-1 through RK-57, RK-59, RK-60, and RK-62 through RK-66.

Model 400T aircraft with serial numbers TT-02 through TT-30, and TT-32.

Requirement: Action in accordance with Beechcraft Mandatory Service Bulletin 2509.

Note: FAA AD 93-25-15 Amdt 39-8779 refers.

Compliance: Within 200 hours’ time in service after 31 March 1994.

Background: The FAA received reports that, during production, incorrect rivets may have been installed in the escape hatch substructure.

Source text

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