Sourced from the Federal Register of Legislation (legislation.gov.au), CC BY 4.0.
Terminating Action Terminating Action
Terminating Action
Compliance with this Directive terminates the actions required by paragraph (a) of FAA AD 91-22-02, amendment 39-8062.
Note 2: FAA AD 94-17-03, amendment 39-8998.refers.
Compliance: For Requirement 1: Prior to the issue of a Certificate of Airworthiness.
For Requirement 2: Within 3,000 flight hours after accomplishment of Requirement 1, or within 1,000 flight hours after the effective date of this Directive, whichever occurs later.
For Requirement 3: At intervals not exceeding 3,000 flight hours. This Airworthiness Directive becomes effective on 8 August 2002.
Boeing 767 Series Aeroplanes Boeing 767 Series Aeroplanes
Boeing 767 Series Aeroplanes
AD/B767/174 (continued)
Background: This Directive requires inspections, adjustments, functional checks, the installation of a modification and repetitive operational checks of the thrust reverser gearbox locks and the airmotor. These actions are intended to enhance the level of safety inherent in the original type design of the thrust reverser system to prevent possible discrepancies that exist in the current thrust reverser control system, that could result in an inadvertent deployment of a thrust reverser during flight.
Eugene Paul Holzapfel
Delegate of the Civil Aviation Safety Authority 28 June 2002
The above AD is notified in the Commonwealth of Australia Gazette on 17 July 2002.