Commonwealth legislation

AD/EMB-110/52 - Rear Door Operating Mechanism

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This directive requires owners/operators of Embraer EMB-110 aircraft serials 110001–110085 to carry out the inspection/repair detailed in Embraer Service Bulletin 110-52-0044 within 300 flight hours or at the next B2 inspection (whichever is first) after 14 August 1997. It targets a reported rivet-shear failure on rear door hardware that could allow a door to open in flight; operators must fund and schedule the mandated work.

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AD/EMB-110/52 - Rear Door Operating Mechanism

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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 Embraer EMB-110 (Bandeirante) Series Aeroplanes

AD/EMB-110/52 Rear Door Operating Mechanism 9/97

Applicability: Model EMB-110 with serial numbers 110001 through 110085. Requirement: Action in accordance with Embraer Service Bulletin 110-52-0044.

Note: CTA AD 97-05-01 Amdt 39-773 refers.

Compliance: Within 300 hours time in service or at the next B2 level inspection, whichever occurs first; after 14 August 1997.

Background: The CTA received reports of sheared rivets that attach the opening/closing mechanism to the locking rod’s arm of the rear doors of several aircraft. This failure could result in an in-flight door opening, and possible loss of the door.

Source text

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