AD/F28/51 - Main Landing Gear Bay Cracking
1AD/F28/51 - Main Landing Gear Bay Cracking
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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 Fokker F28 Series Aeroplanes
AD/F28/51 Main Landing Gear Bay Cracking 2/86
Applicability: All model F28 with S/Nos 11003 to 11091, 11094 to 11135, 11991 and 11992. Requirement: Action in accordance with Fokker SB F28/57-76.
Note: RLD AD 85-87 refers.
Compliance: Prior to 31 March 1986.
The manufacturer reports an instance of a crack in the area of Station 2635 and the rear spar.