AD/BELL 212/33 - Main Rotor Grip/Blade Bolt - Inspection and Rework
1AD/BELL 212/33 - Main Rotor Grip/Blade Bolt - Inspection and Rework
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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 Bell Helicopter Textron 212 Series Helicopters
AD/BELL 212/33 Main Rotor Grip/Blade Bolt - Inspection and Rework
Applicability: All BHTI reworked grips which have had grip bushing(s) replaced. Requirement: Bell Alert S.B. No. 212-85-37.
3/85
Compliance: Within 100 hours time in service after 31 March 1985 or at the next scheduled inspection for maintenance release issued after 31 March 1985 whichever is the later.
Background: There have been reports where an improper clearance was evident between the blade bolt head flange and the grip bushing. These reports have only pertained to grip assemblies returned to BHTI for repair/overhaul.