AD/ECUREUIL/5 - Tail Rotor Control Fixed Plate - Inspection of Self Aligning Bearing
1AD/ECUREUIL/5 - Tail Rotor Control Fixed Plate - Inspection of Self Aligning Bearing
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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/5 Tail Rotor Control Fixed Plate - Inspection
of Self Aligning Bearing
8/79
Applicability: All model AS.350 not modified in accordance with AMS 350A.07.6513 and AMS 350A.07.8515.
Document: AS.350 SB 05.01.
Compliance: At periods not exceeding 50 hours time in service.
Background: Regular inspections are required to ensure that the tail rotor control self aligning bearing is correctly located in the bore of the fixed plate.