Commonwealth legislation

AD/CF700/3 - Compressor Rotor Assembly

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

4/10 complexity

This Airworthiness Directive requires owners and operators of CF700-2C engines to carry out the work specified in General Electric SB (CF700) 72-49 or the alternate AD/GE-T/7 to address the compressor rotor assembly. Issued by the Civil Aviation Safety Authority and enforceable under its Schedule of Airworthiness Directives, the mandated actions must be completed before 17 November 1967, with operators bearing the inspection/repair costs.

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Direct links to the current provisions in AD/CF700/3 - Compressor Rotor Assembly.

AD/CF700/3 - Compressor Rotor Assembly

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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 General Electric Turbine Engines - CF700 Series

AD/CF700/3 Compressor Rotor Assembly 9/85

Applicability: All CF700-2C.

Document: General Electric SB (CF700) 72-49; or

AD/GE-T/7.

Compliance: Before 17 November 1967.

Source text

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