Commonwealth legislation

AD/B727/70 - Main Landing Gear Down-Lock Torque Shaft P/N 65-23366 - Replacement

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Plain English Summary

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This AD requires replacement of the main landing‑gear down‑lock torque shaft (P/N 65‑23366) on specified Boeing 727s, and delegates the detailed procedure and timing to FAA AD 72‑12‑01 and Boeing SB No. 32‑180 Rev. 1.

It affects operators, maintenance organisations and parts suppliers—operators pay for parts, labour and downtime and must schedule the work, while reliance on the FAA/Boeing documents and parts availability are the main implementation risks.

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AD/B727/70 - Main Landing Gear Down-Lock Torque Shaft P/N 65-23366 - Replacement

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

View image in the official source Boeing 727 Series Aeroplanes

AD/B727/70 Main Landing Gear Down-Lock Torque Shaft

P/N 65-23366 - Replacement

10/75

Applicability: All models listed in Boeing SB No. 32-180 Rev. 1. with main landing gear down-lock torque shaft P/No. 65-23366.

Document: FAA AD 72-12-01, Boeing Amdt. 39-2353. Compliance: As detailed in the requirement document.

Source text

Sourced from the Federal Register of Legislation (legislation.gov.au), CC BY 4.0.