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Airworthiness Directives (ADs)

87-ATR-144

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
1998/07/15
Applicability
ATR42-200, -300, -320
Model Number
ATR
CAA AD Number
87-ATR-144
Aeronautics Authority of Original AD
FAA
Original AD Number
98-09-22
Effective Date
Subject
To prevent reduced structural integrity of the airplane resulting from fatigue cracking of the windshield frame structure.
Reference Publications (Revision/ATA/SB)
SB ATR42-53-0093
Remarks
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