Federal Register of Legislation
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY SCHEDULE OF AIRWORTHINESS DIRECTIVES
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.
2. 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.
We try to embed the page this law was scraped from. If the site blocks framing, you still get the link and a local excerpt.
Last checked with source on —
Checking whether the official page can be embedded…
Plain-English simplify of this law: a short summary, key points, and both sides of the argument. Generated on first view via Replicate, then cached. Vote on what helps your study.
No study brief is cached for this law yet. Sign up to generate a plain-English brief.
Sign up to generate