AD/B747/230 Amdt 1 - Thrust Reverser Checks
Terminating ActionTerminating Action
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Terminating Action
Accomplishment of Requirement 1 and 2, or installation of an additional locking system during production in accordance with production equivalent PRR 81000- 39, is terminating action for the inspections and tests required by Requirement 3 of AD/B747/277.
Note: FAA AD 2000-02-22 Amendment 39-11540 refers.
Compliance: For Requirement 1: Within 36 months time in service from 13 July 2000 (the effective date of original issue of this Directive).
For Requirement 2: Prior to or concurrent with Requirement 1 compliance.
For Requirement 3: Within 3,000 flight hours after accomplishment of Requirement 1 or within 1,000 flight hours from 13 July 2000 (the effective date of original issue of this Directive), whichever occurred later.
For Requirement 4: Prior to further flight. For Requirement 5: Prior to further flight.
For Requirement 6: At intervals not exceeding 3,000 flight hours time in service. This Amendment becomes effective on 5 September 2002.