AD/BELL 206/19 Amdt 1 - Tail Rotor Pedal Controls - Inspection
1AD/BELL 206/19 Amdt 1 - Tail Rotor Pedal Controls - 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 Bell Helicopter Textron Canada (BHTC) 206 and Agusta Bell 206 Series Helicopters
AD/BELL 206/19
Amdt 1
Tail Rotor Pedal Controls - Inspection 6/70
Applicability: All model AB-206A fitted with hydraulically boosted tail rotor pitch control; and All model 206A with S/Nos. 4 to 497.
Requirement: Check the tail rotor pedal spring and friction adjustment and re- adjust as necessary in accordance with the requirements of Section IV the Maintenance and Overhaul Instructions.
Compliance: At intervals not exceeding 100 hours time in service. Background: AD/Agusta 206/10A equivalent.