AD/DH114/31 - Rudder Control Pedal Reversal Lever - Inspection
1AD/DH114/31 - Rudder Control Pedal Reversal Lever - Inspection
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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 DH114 (Heron) Series Aeroplanes
AD/DH114/31 Rudder Control Pedal Reversal Lever - Inspection NK
Applicability: All models.
Document: Hawker Siddeley TNS Heron (114) No. CF.15.
Compliance: Within 100 hours time in service after 31 March 1971 and thereafter at intervals not exceeding 2400 hours time in service.