AD/B727/22 - Main Landing Gear Actuator Beam - Inspection and Modification
1AD/B727/22 - Main Landing Gear Actuator Beam - Inspection and 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 727 Series Aeroplanes
AD/B727/22 Main Landing Gear Actuator Beam - Inspection and Modification
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Applicability: All models. Document: Boeing SB No. 32-76.
Compliance: Inspect before 3,000 hours total time in service and thereafter at intervals not exceeding 200 hours time in service until modified in accordance with SB No. 32-76.