Commonwealth legislation

AD/BEECH 200/5 - Generator Leads

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Commonwealth

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legislative instrument

Plain English Summary

2/10 complexity

This directive requires owners/operators of specific Beechcraft Model 200 aeroplanes (listed by serial number) to visually inspect generator output leads for chafing/discolouration and to re‑route the leads using Beechcraft Service Instruction No. 0768‑358 with Kit No. 101‑3011‑1S. Inspections and the mandated modification must be done within tight service‑hour deadlines; costs, parts and downtime are borne by the aircraft owners. The rule cites FAA AD 75‑25‑01.

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AD/BEECH 200/5 - Generator Leads

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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 200 (Super King Air) Series Aeroplanes

AD/BEECH 200/5 Generator Leads 1/76

Applicability: Model 200 S/Nos BB-2, BB-6 thru BB-76 and BB-78 thru BB-80.

Requirement: 1. Visually inspect the generator output leads for chafing or discolouration in the area of the air conditioner compressor pulley housing and oil line coupling nut.

Modify the generator lead routing in accordance with Beechcraft SI No 0768-358, Kit No 101-3011-1S.

Note: FAA AD 75-25-01 refers.

Compliance: Inspect within 25 hours time in service after 8 December 1975. Modify within 100 hours time in service after 8 December 1975.

Source text

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