Airworthiness Directives (ADs)
CAA-2009-03-008
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
- 2009/03/30
-
Applicability
- General Electric Company (GE) CF6-80C2 and CF6-80E1 series turbofan
engines with high-pressure compressor rotor (HPCR) spool shaft stage 14 disks, part number (P/N)
1703M49G02, 1703M49G03, or 1509M71G10 installed. These engines are installed on, but not
limited to, Airbus A300-600R/F, A310-200/300, and A330-200/300, and Boeing 747-
200B/300/400/400D/400F, 767-200/300/400F/400ER, and MD-11 airplanes.
-
Model Number
- General Electric Company CF6-80C2 and CF6-80E1 Series
-
CAA AD Number
- CAA-2009-03-008
-
Aeronautics Authority of Original AD
- FAA
-
Original AD Number
- 2009-07-03
-
Effective Date
- 2009/04/30
-
Subject
- To prevent cracks from propagating to an uncontained
failure of the disk and damage to the airplane.
-
Reference Publications (Revision/ATA/SB)
- CF6-80C2 S/B 72-A1122,R1 & CF6-80E1 S/B 72-A0258,R1.
-
Remarks
-
Download
-