Airworthiness Directives (ADs)
CAA-2006-05-001A
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
- 2006/12/12
-
Applicability
- Boeing Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-300, 747-400, 747-400D, and 747SR series airplanes, certificated in any category; as identified in Boeing Alert Service Bulletin 747-53A2408, Revision 1, dated April 4, 2002.
-
Model Number
- Boeing Model 747-100, 747-100B, 747- 100B SUD, 747-200B, 747-300, 747-400, 747-400D, and 747SR Series Airplanes
-
CAA AD Number
- CAA-2006-05-001A
-
Aeronautics Authority of Original AD
- FAA
-
Original AD Number
- 2006-09-06R1
-
Effective Date
- 2006/06/07
-
Subject
- To detect and correct fatigue cracking of certain lower lobe fuselage frames, which could lead to fatigue cracks in the fuselage skin, and consequent rapid decompression of the airplane.
-
Reference Publications (Revision/ATA/SB)
- Revises AD 2006-09-06(CAA-2006-05-001)
Ref. Boeing Alert Service Bulletin 747-53A2408 or Boeing Alert Service Bulletin 747-53A2408, Revision 1
-
Remarks
-
Download
-