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FAA AD on Learjet model 23, 24, 24A, 24B, 24B-A, 24D, 24D-A, 24E, 24F, 25, 25A, 25B, 25C, 25D, and 25F airplanes modified by Supplemental Type Certificate SA1731SW, SA1669SW, or SA1670SW (2005-23-06)
Washington, Usa - To prevent failure of the thrust reverser accumulators, due to fatigue cracking on the female threads, which could result in the loss of hydraulic power and damage to the surrounding airplane structure
Airworthiness Directive Federal Register Information [Federal Register: November 14, 2005 (Volume 70, Number 218)] [Page 69059-69061] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-20947; Directorate Identifier 2004-NM-245-AD; Amendment 39-14364; AD 2005-23-06] RIN 2120-AA64 Airworthiness Directives;...
fra/pec - 131102
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency