AD/HU 269/51 Amdt 1 - Tail Rotor Control System Pedal Installation - Inspection and Modification
1AD/HU 269/51 Amdt 1 - Tail Rotor Control System Pedal Installation - Inspection and 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 Schweizer (Hughes) 269 Series Helicopters
AD/HU 269/51
Amdt 1
Tail Rotor Control System Pedal Installation - Inspection and Modification
1/78
Applicability: All models.
Document: Hughes SIN Co. N-121.1. Compliance: As per requirement document.