AD/DAUPHIN/44 - Tail Rotor Hub Fairing
1AD/DAUPHIN/44 - Tail Rotor Hub Fairing
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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 Eurocopter SA 360 and SA 365 (Dauphin) Series Helicopters
AD/DAUPHIN/44 Tail Rotor Hub Fairing 9/95 TX
Applicability: Model SA 365C, C1, C2, and C3, and 365N.
Requirement: Action in accordance with Eurocopter Telex Service No. 01.34 or 01.43 as applicable.
Note: DGAC ADs 95-112-040(B) and 95-107-039(B) R1 refer.
Compliance: Prior to further flight after 7 July 1995, thereafter in accordance with the Requirement Document.
Background: There have been in service reports of ruptured springs, which both DGAC and Eurocopter consider to be an urgent airworthiness matter.