1AD/FU24/12 - Rudder Lowr Rib - 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 Airparts (NZ) Ltd. FU 24 Series Aeroplanes

 

AD/FU24/12 Rudder Lowr Rib - Inspection 6/68

Applicability: All models not incorporating James Aviation Mod. HA/FU24/116.

 

Requirement: Detach the torque tube from the rudder and examine the rudder lower rib assembly P/N 242406 at the attachment of the rudder torque tube flange P/N 242410 for cracking and corrosion.

 

Compliance: At intervals not exceeding 500 hours time in service.