CTHRepealedLegislation
AD/PA-31/58 - Auto Pilot Servo Bridle Clamp Bolt Torque - Modification - CANCELLED
Piper PA-31 Series AeroplanesPiper PA-31 Series Aeroplanes
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Piper PA-31 Series Aeroplanes
| AD/PA-31/58 | Auto Pilot Servo Bridle ClampBolt Torque - Modification | 8/2008 |
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| Requirement: | CANCELLED. |
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| This AD is cancelled on 31 July 2008. | |
| Background: | This unique Australian AD required once-only modification of the autopilot servo bridle clamp bolt in accordance with Piper SB No. 558. The AD required compliance within 100 hours TIS after September 1977. All affected aircraft have now been modified. |
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James Coyne
Delegate of the Civil Aviation Safety Authority
12 June 2008