Federal Register of Legislation
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY SCHEDULE OF AIRWORTHINESS DIRECTIVES
Bombardier (Canadair) CL-600 (Challenger) Series Aeroplanes
AD/CL-600/20 ADG Output Harness Chafing 8/91
DM
Applicability: All CL-600 aircraft as specified in the Requirement Documents.
Requirement: 1. Action in accordance with Part A of Canadair Service Bulletin A600-0612 or A601-0370 as applicable.
2. Action in accordance with Part B of Canadair Service Bulletin A600-0612 or A601-0370 as applicable.
Compliance: For Requirement 1. Within 25 hours time in service after 13 June1991. For Requirement 2. Within 600 hours time in service after 13 June 1991. Background: Three instances of the ADG electrical output harness being chafed through whilst in the stowed position have been reported. When deployed, the chafed wires short circuited to structure, and resulted in the ADG being unable to provide electrical power to the essential bus when required. Damage to the output harness and its supporting structure also resulted.
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