AD/BEECH 55/26 - Electrical Cable Loom
1AD/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
Image unavailable in extracted text 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.