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AD/BELL 205/40 - Tail Rotor Pitch Horns - Inspection
1AD/BELL 205/40 - Tail Rotor Pitch Horns - Inspection
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Bell Helicopter Textron 205 Series Helicopters
AD/BELL 205/40 Tail Rotor Pitch Horns - Inspection 10/77
Applicability: All models fitted with pitch change horns P/N 212-010-716-5 or -9. Document: 1. Bell SB No. 205-77-5; or
- FAA AD 77-17-03.
Compliance: Within 25 hours time in service after 15 September 1977, and there- after at intervals not to exceed 100 hours.