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Fly Neighborly - Noise Abatement
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| Go to the My Rotor.com page for information on receiving RotorNews by e-mail and contributing news stories including press releases online. To view stories online in a particular category, click one of the following links: Advisory Circulars, Affiliate, Airworthiness Directives, Government, HAI Happenings, Helicopters Saving Lives, Industry Press Releases, Legislative, Maintenance Update (members only), Operations Update (members only), Preliminary Accident Reports (members only), Safety, and Security. |
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| Airworthiness Directives; Bell Helicopter Textron Canada Model 222, 222B, 222U, 230, and 430 Helicopters | Friday, September 12, 2008 (1294 reads) AD 2008-19-02
SUMMARY: We are superseding an existing airworthiness directive (AD) for Bell Helicopter Textron Canada (Bell) Model 222, 222B, 222U, 230, and 430 helicopters. That AD currently requires visually inspecting the main rotor hydraulic actuator support (support) to verify the presence of all dowel pins and sealant between the support and transmission and verifying the proper torque of each attaching nut (nut). This AD requires the same actions as the existing AD and also requires repetitive actions at intervals not to exceed 600 hours time-in-service (TIS) or 12 months, whichever occurs first.
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| Special Airworthiness Information Bulletin: Lycoming Direct-Drive Reciprocating Engines | Wednesday, September 10, 2008 (1242 reads) This Special Airworthiness Information Bulletin alerts you, owners, operators, and certificated repair facilities that, all Lycoming Engines (Lycoming) direct-drive reciprocating engines, including VO-360 and IVO-360; except O-320-H, O-360-E, LO-360-E, TO-360-E, LTO-360-E, and TIO- 541 series engines, must be in compliance with Airworthiness Directive (AD) 2004-10-14 if they have had a propeller strike.
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| EC135 Emergency Airworthiness Directive | Saturday, December 15, 2007 (1170 reads) ADMINISTRATOR'S AIRWORTHINESS DIRECTIVE ALERT
SUBJECT: Eurocopter Deutschland Model EC135 Helicopters.
BACKGROUND: The Rotorcraft Directorate will issue an emergency airworthiness directive (EAD) that is prompted by the failure of a tail rotor control rod which resulted in an accident that occurred in Japan.
UNSAFE CONDITION: The EAD is intended to prevent failure of a tail rotor control rod and subsequent loss of control of the helicopter. The Civil Aviation Bureau of Japan (JCAB) and European Aviation Safety Agency (EASA) have issued their own Airworthiness Directives.
ACTION: The EAD will require, within the next 5 hours time-in-service, inspecting the control rod and adjoining ball pivot and replacing any unairworthy parts before further flight.
IMPACT: U.S.-registered fleet: 163
Worldwide fleet: 2315
Labor Cost per Helicopter: $80 per work hour. We estimate 1 work hour to inspect the control rod and ball pivot and 3 work hours to replace a control rod or ball pivot, if necessary.
Parts Cost per Helicopter: $400 for the control rod and $675 for the ball pivot
Total Estimated Cost Impact: $32,765, assuming 15 helicopters require replacing parts.
AFFECTED U.S. OPERATORS: General Aviation (Air Tour Operators, Powerline/Pipeline Survey), Law Enforcement.
NEWS VALUE/MEDIA INTEREST: General press interest.
Regional Duty Officer: (817) 222-5006
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