AD/B747/25 - Wing Leading Edge Flap System - Modification
1AD/B747/25 - Wing Leading Edge Flap System - Modification
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text Boeing 747 Series Aeroplanes
AD/B747/25 Wing Leading Edge Flap System - Modification 1/81
Applicability: All models 747.
Document: 1. FAA AD 80-19-05, Amdt. 39-3906; or
- Boeing SB No. 747-27-2204.
Compliance: As per requirement document No. 1.
Background: Investigation has revealed that a single electrical fault in the leading edge flap circuits could cause an unscheduled deployment of the flaps.