Airworthiness Directives (ADs)
88-747-291
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
- 1999/01/12
-
Applicability
- 747-100,-200,-300,-400
-
Model Number
- 747
-
CAA AD Number
- 88-747-291
-
Aeronautics Authority of Original AD
- FAA
-
Original AD Number
- 98-26-13
-
Effective Date
-
Subject
- To detect and correct stress corrosion cracking of the stop support fittings of the main entry doors and the resultant failure of the stop support fitting, which could result in loss of a main entry door and consequent rapid decompression of the airplane.
-
Reference Publications (Revision/ATA/SB)
- SB 747-53-2358
-
Remarks
-
Download
-