AD/PT6A/8 Compressor Rear Hub Hardness Cancelled (Cth)
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AIRWORTHINESS DIRECTIVE
On the effective date specified below, and for the reasons set out in the background section, the CASA delegate whose signature appears below revokes Airworthiness Directive AD/PT6A/8.
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. |
James Coyne
Delegate of the Civil Aviation Safety Authority
18 May 2009
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