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FAA AD on Learjet model 23, 24, 24A, 24B, 24B-A, 24C, 24D, 24D-A, 24E, 24F, 24F-A, 25, 25A, 25B, 25C, 25D, and 25F airplanes

Usa - To prevent failure of the spherical accumulator for the main hydraulic system, due to fatigue cracking on the threads, which could result in the loss of hydraulic power, damage to the surrounding airplane structure, and loss of airplane control

Airworthiness Directive Federal Register Information [Federal Register: November 14, 2005 (Volume 70, Number 218)] [Page 69069-69071] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-22169; Directorate Identifier 2005-NM-094-AD; Amendment 39-14361; AD 2005-23-03] RIN 2120-AA64 Airworthiness Directives;...

fra/pec - 131100
Rome, Italy, 11/16/2005 12:15
AVIONEWS - World Aeronautical Press Agency

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