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 Schweizer Aircraft Corporation model 269A, 269A-1, 269B, 269C, and TH-55A helicopters
Washington, Usa - To prevent failure of a tailboom support strut or lug on a cluster fitting, which could cause rotation of a tailboom into the main rotor blades, and subsequent loss of control of the helicopter
![](https://www.avionews.it/layout/elements/default.jpg)
Airworthiness Directives Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-SW-25-AD; Amendment 39-13217; AD 2003-13-15] RIN 2120-AA64 Airworthiness Directives; Schweizer Aircraft Corporation Model 269A, 269A-1, 269B, 269C, and TH-55A Helicopters PDF Copy (If Available): Preamble...
fra/pec - 47688
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency