AD/HU 269/78 - Tail Rotor Pitch Control Link Assembly
1AD/HU 269/78 - Tail Rotor Pitch Control Link Assembly
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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 269/78 Tail Rotor Pitch Control Link Assembly 6/86
DM
Applicability: All model 269A, 269A-1 and 269C Helicopters.
Requirement: Action in accordance with Schweizer Service Information Notice No. N198. Compliance: Within 50 hours time in service after 16 May 1986.
For spares, before installation in an aircraft.
Background: The inspection and rework procedure called for ensures correct clearance between tail rotor pitch links and pitch control housing assembly.