AD/CESSNA 400/22 - Rudder Pedal Torque Tube - Modification
1AD/CESSNA 400/22 - Rudder Pedal Torque Tube - Modification
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text Cessna 400 Series Aeroplanes
AD/CESSNA 400/22 Rudder Pedal Torque Tube - Modification 5/71
Applicability: All models with S/Nos. as listed in requirement document. Document: Cessna SL ME71-1.
Compliance: 1. For aircraft fitted with internal rudder gust lock - within 100 hours time in service after 30 June 1971.
2. For aircraft not fitted with internal rudder gust lock -
(a) Within 100 hours time in service after 30 June 1971 for aircraft in excess of 1000 hours time in service as at 30 June 1971.
(b) Before exceeding 1100 hours time in service for aircraft with less than 1000 hours time in service.