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Airworthiness Directives (ADs)

2002-02-013

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
2002/02/18
Applicability
Hamilton Sundstrand
Model Number
QE
CAA AD Number
2002-02-013
Aeronautics Authority of Original AD
FAA
Original AD Number
2002-04-52
Effective Date
Subject
To prevent blade failure due to corrosion-induced fatigue, which could result in blade separation and possible loss of airplane control.
Reference Publications (Revision/ATA/SB)
Hamilton Sundstrand ASB 568F-61-A35
Remarks
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