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Airworthiness Directives (ADs)

87-F28-040A

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
1998/06/08
Applicability
F28 MK0100
Model Number
F28
CAA AD Number
87-F28-040A
Aeronautics Authority of Original AD
FAA
Original AD Number
98-06-07
Effective Date
Subject
To prevent stabilized engine operation in a certain engine speed range on the ground, which could result in uncontained engine fan blade failure due to high cycle fatigue cracking.
Reference Publications (Revision/ATA/SB)
Remarks
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