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FAA AD on Airbus model A-300B2 and A-300B4; A-300 B4-600, B4-600R and F4-600R, A-300C4-605R Variant F; A-310/200 and -300 series airplanes (2005-20-06)
To prevent loss of the integral lighting due to failure of the normal electrical power circuit, which could result in inability of the pilot to read the backup attitude information during takeoff, and possible deviation from the intended flight path
Airworthiness Directive Federal Register Information [Federal Register: September 29, 2005 (Volume 70, Number 188)] [Page 56814-56818] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-20796; Directorate Identifier 2004-NM-160-AD; Amendment 39-14299; AD 2005-20-06] RIN 2120-AA64 Airworthiness Directives;...
fra/pec - 127998
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency