Do you want to access to this and other private contents?
Log in if you are a subscriber or click here to request service
FAA AD on McDonnell Douglas model DC-9-10, DC-9- 20, DC-9-30, DC-9-40, and DC-9-50 series airplanes (2006-07-08)
Washington, Usa - To detect and correct stress corrosion cracking of the main fuselage frame, which could result in extensive damage to adjacent structure and reduced structural integrity of the airplane
Airworthiness Directive Federal Register Information [Federal Register: March 31, 2006 (Volume 71, Number 62)] [Page 16201-16203] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-23197; Directorate Identifier 2005-NM-109-AD; Amendment 39-14535; AD 2006-07-08] RIN 2120-AA64 Airworthiness Directives;...
fra/pec - 138768
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency