Commonwealth legislation

AD/BEECH 55/26 - Electrical Cable Loom

RepealedCTH

This Act has been repealed and is no longer in force. It is retained for historical reference.

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

1/10 complexity

This Airworthiness Directive requires owners/operators of Beechcraft Model E55 and Model 58 aeroplanes to inspect the electrical wiring behind the lower left circuit breaker panel for adequate clearance, chafing where the cable passes the stand-off pillar clip, and correct insulation of the clip, and to increase the stand-off spacer length if clearance is insufficient. The inspection must be completed within 15 flight hours after 21 October 1971 to prevent insulation wear, shorts, or in‑flight fires.

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AD/BEECH 55/26 - Electrical Cable Loom

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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 55, 58 and 95-55 (Baron) Series Aeroplanes

AD/BEECH 55/26 Electrical Cable Loom 11/71

Applicability: Model E55 and Model 58.

Requirement: Inspect electrical cables behind lower left hand circuit breaker panel adjacent to the control pedestal to ascertain that there is adequate clearance between the cable loom and any panels or screws connecting leads to the rear of the circuit breakers. Also inspect loom for chafing where it passes through the stand-off pillar clip and check that this clip is still well insulated.

Note: It may be necessary to increase the length of the stand-off pillar to ensure that the loom will have adequate clearance.

Compliance: Within 15 hours’ time in service after 21 October 1971.

Source text

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