Airworthiness Directives (ADs)
CAA-2010-07-003
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
- 2010/07/05
-
Applicability
- The Boeing Company Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-200C, 747-200F, 747-300, 747-400, 747-400D, 747-400F, 747SR, and 747SP series airplanes, certificated in any category, line numbers 1 though 1307 inclusive.
-
Model Number
- The Boeing Company Model 747 Airplanes
-
CAA AD Number
- CAA-2010-07-003
-
Aeronautics Authority of Original AD
- FAA
-
Original AD Number
- 2010-14-07
-
Effective Date
- 2010/08/05
-
Subject
- To prevent fatigue cracking of the BS 2598 bulkhead structure, which could result in inability of the structure to carry horizontal stabilizer flight loads, and loss of controllability of the airplane.
-
Reference Publications (Revision/ATA/SB)
- This AD supersedes AD 2006-05-06(CAA-2006-03-006),Ref:Boeing Alert Service Bulletin 747-53A2467,Boeing Alert Service Bulletin 747-53A2473 R2,Boeing Service Bulletin 747-53A2427 R5,Boeing Service Bulletin 747-53A2449 R1,Boeing Service Bulletin 747-53A2449 R2 & Boeing Service Bulletin 747-53A2467 R1.
-
Remarks
-
Download
-