Federal Register of Legislation
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY SCHEDULE OF AIRWORTHINESS DIRECTIVES
SIAI Marchetti S205 and S208 Series Aeroplanes
AD/SM-205/34 Amdt 1
Wing Rear Spar - Inspection 3/84
Applicability: All models S205-18/F, S205-20F; S205-18/R, S205-20/R, S205-22/R, S208, S208A.
Requirement: SIAI-Marchetti S.B. No. 205B57.
Compliance: Unless already accomplished, before further flight and thereafter at intervals not exceeding 50 hours time in service.
Background: a. The manufacturer has received reports of cracking in the wing rear spar at the locations described above.
b. This Directive has been amended to reflect the revised Aircraft Applicability and Requirement Document reissue.
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