Airworthiness Directives (ADs)
CAA-2010-01-008
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
- 2010/01/26
-
Applicability
- Boeing Company Model 747-100B SUD, -200B, -300, -400, and -
400D series airplanes。
-
Model Number
- Boeing Company Model 747-100B SUD, -200B, -300, -400, and -
400D Series Airplanes
-
CAA AD Number
- CAA-2010-01-008
-
Aeronautics Authority of Original AD
- FAA
-
Original AD Number
- 2010-01-02
-
Effective Date
- 2010/02/24
-
Subject
- To detect
and correct fatigue cracking in certain fuselage stringers, which, if left undetected, could result in
fuselage skin cracking that reduces the structural integrity of the skin panel, and consequent rapid
depressurization of the airplane.
-
Reference Publications (Revision/ATA/SB)
- This AD supersedes AD 2005-15-08(CAA-2005-07-020).Ref:Boeing Service Bulletin 747-53A2484, Revision 1.
-
Remarks
-
Download
-