Federal Register of Legislation
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY SCHEDULE OF AIRWORTHINESS DIRECTIVES
Boeing 737 Series Aeroplanes
AD/B737/72 Side of Body Floor Panel Inserts 12/92
Applicability: Model 737-400 and 737-500 series, as listed in Boeing ASB 737-53A1152, Revision 1.
Requirement: Inspect the side-of-body floor panels forward of Body Station 887 to determine if the panels were manufactured by Hexcel and the date of their manufacture; in accordance with the Accomplishment Instructions of Boeing ASB 737-53A1152 Revision 1.
(a) If the floor panels were not manufactured by Hexcel, or if the floor panels were manufactured by Hexcel on or after 7 January 1991; no further action is necessary.
(b) If the floor panels were manufactured by Hexcel before 7 January 1991, prior to further flight, either replace the floor panels or repair all one-piece inserts in the panels, in accordance with Boeing ASB 737-53A1152 Revision 1.
Note: FAA AD 92-16-01 Amdt 39-8310 refers.
Compliance: Prior to 8 September 1994.
Background: The FAA has received reports of disbonded one-piece inserts being found in certain side-of-body floor panels. The actions specified in this Directive are intended to prevent floor panels from breaking away from floor structure during a 9g forward load event.
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