Federal Register of Legislation
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY SCHEDULE OF AIRWORTHINESS DIRECTIVES
McDonnell Douglas (Hughes) and Kawasaki 369 Series Helicopters
AD/HU 369/89 Main Blade Root End 8/96 DM
Applicability: Model 369, 369A, 369D, 369E, 369F, 369FF, 369H, 369HE, 369HM, 369HS, and 500N helicopters.
Requirement: Inspect in accordance with Part I and Part II of McDonnell Douglas Helicopter Systems Service Information Notice HN-239, DN-188,EN-81, FN-67, or NN-008, as applicable.
Note: FAA AD 96-10-09 Amdt 39-9615 refers.
Compliance: For Part I: Unless the initial inspection has already been accomplished, within 10 hours time in service after 17 June 1996.
For Part II: Within 100 hours time in service after 17 June 1996, thereafter at intervals not to exceed 100 hours time in service.
Background: The FAA received a report of one accident in which a blade separated from the helicopter, as well as eight other reports of cracked blades. The actions specified in this Directive are intended to prevent failure of a blade and subsequent loss of control of the helicopter.
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