CTHRepealedLegislation
AD/PT6A/8 - Compressor Rear Hub Hardness - CANCELLED
Pratt and Whitney Canada Turbine EnginesPratt and Whitney Canada Turbine Engines - PT6A Series
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Pratt and Whitney Canada Turbine Engines - PT6A Series
| AD/PT6A/8 | Compressor Rear Hub Hardness | 7/2009 |
|---|
| Requirement: | CANCELLED. |
|---|---|
| This AD is cancelled on 2 July 2009. | |
| Background: | This unique Australian AD specified action in accordance with UACL SB No. 62 or SB No. 1035 before installation in an aircraft following re-conditioning after November 1969. The AD is no longer required. |
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James Coyne
Delegate of the Civil Aviation Safety Authority
18 May 2009