AD/S-PUMA/1 - Main Rotor Shaft
1AD/S-PUMA/1 - Main Rotor Shaft
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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 AS 332 (Super Puma) Series Helicopters
AD/S-PUMA/1 Main Rotor Shaft 2/91
Applicability: Versions C, C1, L and L1 which are fitted with main rotor shafts P/Nos 330A31 1222.05 or .06 modified per AMS 07.43069 and 330A31 1222.08, .09, .11 or .12.
Requirement: Action in accordance with the technical requirements of DGAC AD 83-095-006(B) Revision 1, dated 19 September 1990.
Note: Aerospatiale AS 332 SB No 05.01 R2 approved 31 August 1990, refers.
Compliance: In accordance with the Requirement Document.