AD/GAZELLE/13 - Main Gearbox Input Gear Slotted Nut - Inspection
1AD/GAZELLE/13 - Main Gearbox Input Gear Slotted Nut - Inspection
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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 SA341 and SA342 (Gazelle) Series Helicopters
AD/GAZELLE/13 Main Gearbox Input Gear Slotted Nut - Inspection
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Applicability: All SA 341 and SA 342 models fitted with main gearbox Part No. 341A 32.1000.01 through 06 with the embodiment of Modification A.M.S. 07.70.76/S.374.
Document: SA 341-342 Service Bulletin 65-24.
Note: For gearboxes not modified as above refer to AD/GAZELLE/9 and Service Bulletin 65.19.
Compliance: Within 100 hours time in service after 31st May 1983 carry out the inspection as per the requirement document.
Background: The manufacturer has introduced an inspection method to ensure that the correct torque load had been applied to the slotted nut which retains the input gear flange.