AD/BEECH 99/6 - Wing Structural Fatigue Limitations
1AD/BEECH 99/6 - Wing Structural Fatigue Limitations
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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 Beechcraft 99 Series Aeroplanes
AD/BEECH 99/6 Wing Structural Fatigue Limitations 12/96
Applicability: All model 99 aircraft.
Requirement: Inspect and retire the wing structural components in accordance with the Beechcraft 99 Airliner Series Continued Airworthiness Program Inspection Manual P/N 98- 30131 Rev. A1, Sections 57-10 and 57-20.
Note: FAA AD 92-15-13 refers.
Compliance: This Directive takes effect 7 November 1996.
Background: This Directive requires life limited components to be retired to prevent fatigue failure of the wing spar and associated structure.