AD/ECUREUIL/53 - Cyclic Pitch Change Rod
1AD/ECUREUIL/53 - Cyclic Pitch Change Rod
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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 350 (Ecureuil) Series Helicopters
AD/ECUREUIL/53 Cyclic Pitch Change Rod 11/94
Applicability: Models B, BA, D, B1 and B2 fitted with cyclic pitch change control rod P/No 704A34-113-279, and not fitted with an auto-pilot.
Requirement: Action in accordance with Eurocopter AS 350 Service Bulletin 01-42.
Note: DGAC AD 94-180-069(B) refers.
Compliance: Within 100 hours time in service after 13 October 1994.
Background: The manufacturer has determined that some control rods may not be “in safety”.