Federal Register of Legislation
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY SCHEDULE OF AIRWORTHINESS DIRECTIVES
Boeing 747 Series Aeroplanes
AD/B747/211 Upper Rudder Pedal Cover Doubler 11/99
Applicability: Model 747-400 series aircraft, as listed in Boeing Alert Service Bulletin 747- 27A2378.
Requirement: Conduct initial and repeat inspections in accordance with the technical requirements of FAA AD 99-16-08 Amdt 39-11243.
Compliance: As specified in the Requirement document for the initial and repetitive inspections, with a revised effective date of 4 November 1999.
This Airworthiness Directive becomes effective on 4 November 1999.
Background: The FAA received a report of a disbonded doubler on the upper rudder pedal cover that interfered with rudder pedal movement. This Directive requires initial and repetitive inspections of the doubler to determine whether it is securely bonded to the pedal cover; the Directive also provides for optional terminating action for the repetitive inspections.
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