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/B737/98 Krueger Flap Actuator Support Fitting 13/96 Applicability: Model 737 -100 and -200 series aircraft, line positions 001 through 813. Requirement: Action in accordance with the technical requirements of FAA AD 96-17-04 Amdt 39-9712.
Compliance: As specified in the Requirement Document.
Note: Replacement of the support fitting with a steel fitting and modification of the actuator aft attachment in accordance with Boeing Service Bulletin 737-57-1129 Revision 1, as revised by Notices of Status Change 737-57-1129NSC1; 737-57- 1129NSC2; and 737-57-1129NSC3; constitutes terminating action for the repetitive inspections required by this Directive.
Background: The FAA received reports of cracking due to fatigue and stress corrosion of the support fittings of the Krueger flap actuator.
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