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Airworthiness Directives (ADs)

85-MD11-053

The aircraft owner or operator shall comply with Airworthiness Directives issued by the CAA or the aeronautics authority of the State of Design (SoD) of the aviation products, appliances and parts, and take all necessary actions thereto.

Issue Date
1996/10/09
Applicability
Model Number
MD11
CAA AD Number
85-MD11-053
Aeronautics Authority of Original AD
FAA
Original AD Number
96-19-03
Effective Date
Subject
To prevent stress corrosion cracking in fasteners in the inboard flap track, which could result in bending of flap and inability of the flap to extend or retract.
Reference Publications (Revision/ATA/SB)
SB DC-10-57-134,MD11-57-031
Remarks
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