Federal Register of Legislation
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY SCHEDULE OF AIRWORTHINESS DIRECTIVES
Pilatus Britten-Norman BN-2 Series Aeroplanes
AD/BN-2/19 Engine Mounting Bracket Jo-Bolts - Inspection NK
and Modification
Applicability: All models which have exceeded 1000 hours total time in service not incorporating Modification NB/M/455.
Requirement: 1. Inspect the engine mounting frames for loose jo-bolts in accordance with Britten Norman SB BN-2/SB.44.
2. If on inspection it is found possible to move or partially rotate Jo-Bolts in both brackets on any one engine mounting, Modification NB/M/455 must be carried out before further flight.
Compliance: Within 100 hours time in service after 31 March 1971 and there- after as detailed in SB No. BN-2/SB.44.
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