Commonwealth legislation

AD/JT8D/6 - Replacement or Inspection of LP Turbine Shaft and No. 2 Hub

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Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

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This airworthiness directive mandates replacement or inspection of the low‑pressure turbine shaft and No. 2 hub on Pratt & Whitney JT8D‑1, ‑1A, ‑7 and ‑7A engines, but delegates the step‑by‑step requirements to referenced “Requirement Documents” (Pratt & Whitney Alert SB No. 4357 Rev. 3; FAA AD 75‑01‑01; AD/PW‑T/33).

It affects operators, owners and maintenance organisations for those engines and matters because compliance is mandatory, carrying maintenance, cost and downtime implications determined by the referenced documents.

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AD/JT8D/6 - Replacement or Inspection of LP Turbine Shaft and No. 2 Hub

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 106 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

View image in the official source Pratt and Whitney Turbine Engines - JT8D Series

AD/JT8D/6 Replacement or Inspection of LP Turbine Shaft and No. 2 Hub

Applicability: JT8D-1, -1A, -7, -7A engines.

Document: 1. Pratt & Whitney Alert SB No. 4357, Rev. 3; or

FAA AD 75-01-01 amendment 39-2358; or 3. AD/PW-T/33.

Compliance: As detailed in the Requirement Document.

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Source text

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