Federal Register of Legislation
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY SCHEDULE OF AIRWORTHINESS DIRECTIVES
Piper PA-38 (Tomahawk) Series Aeroplanes
AD/PA-38/19 Aileron Balance Weight Rib - Inspection 11/81
Applicability: All models PA-38-112 with S/Nos. 38-78A0001 to 38-81A0051 and 38-81A0105. Document: Piper SB No. 723. Compliance: Within 25 hours time in service after 22 September 1981, and thereafter at intervals not exceeding 100 hours time in until modified by incorporation of Piper Kit P/N 764 140.
Background: The manufacturer has received reports of cracks developing in flange area of the aileron balance weight rib P/Nos. 77342-16 and -17.
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