Federal Register of Legislation
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY SCHEDULE OF AIRWORTHINESS DIRECTIVES
Mitsubishi MU-2 Series Aeroplanes
AD/MU-2/37 Flap Flexible Shaft Sealing and Torque Check 12/85
Applicability: All models MU-2B/-10/-15/-20/-25/-26 with S/Nos. 008 to 347 except S/Nos. 313 and 321. All models MU-2B-30/-35/- 36 with S/Nos.501 to 696 except S/Nos. 652 and 661.
Requirement: Action in accordance with Mitsubishi SB No. 198.
Note: JCAB AD No. TCD-2451-85 refers.
Compliance: At the next scheduled inspection for Maintenance Release issue after 31 December 1985.
Background: The manufacturer reports failures of the flexible drive shaft attributable to ingress of moisture.
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