Fleet Air Arm

August 6, 2014 - 11:10am

The FAA is issuing an Airworthiness Directive for Airbus Helicopters (previously Eurocopter France) EC130B4 and EC130T2. The AD requires repetitive inspection of the fenestron-to-tailboom junction frame for a crack. This AD is prompted by reports of a crack propagating through the junction frame on two EC130B4 helicopters. These actions are intended to detect a crack and to prevent failure of the junction frame, which could result in loss of the fenestron and subsequent loss of control of the helicopter.

December 17, 2013 - 2:10pm

A helicopter emergency services (HEMS) weather summit will be held tomorrow in Washington, D.C. The event is sponsored by the National Center for Atmospheric Research in conjunction with the National EMS Pilots Association, FAA, National Weather Service and the International Helicopter Safety Team. An inaugural summit, held in 2006, resulted in the development of the aviation digital data service HEMS weather tool.

November 27, 2013 - 8:40am

The FAA has issued a final rule to adopt a new Airworthiness Directive (AD) for the sliding doors on the Eurocopter AS350B, AS350BA, AS350B1, AS350B2, AS350B3, AS350C, AS350D, AS350D1, AS355E, AS355F, AS355F1, AS355F2, AS355N and AS355NP. The AD does not apply to aircraft that have modification AL 4262. The AD, which requires removing specified nuts and washers from the lower ball-joint bolt, was prompted by a report of a sliding door detaching from the helicopter in flight.

March 27, 2013 - 12:40pm

The FAA has adopted a new Airworthiness Directive (AD) for all AgustaWestland A109, A109A, A109A II, A109C, A109K2, A109E, A109S and A119 helicopters. It was prompted by the failure of the tail rotor pitch control link assembly on an A109E, caused by a production defect. The AD requires inspecting the link assembly for freedom of movement and taking corrective action if rotation resistance or binding occurs.

March 6, 2013 - 6:49pm

The General Aviation Manufacturers Association (GAMA) held a meeting yesterday at Heli-Expo to share its experience with the government/industry working group designed to rewrite FAR Part 23 certification rules for fixed-wing aircraft and encourage the helicopter industry to apply the model for possible revision of Parts 27 and 29 helicopter certification standards.

March 6, 2013 - 4:25pm

The General Aviation Manufacturers Association (GAMA) held a meeting Tuesday at Heli-Expo to share its experience with the government/industry working group designed to rewrite the certification rules for Part 23 fixed-wing aircraft and encourage the helicopter industry to apply the model for possible revision of the helicopter certification standards under Parts 27 and 29.

March 4, 2013 - 2:20pm

The FAA has begun the process that could lead to rewriting the certification regulations for normal and transport category helicopters certified under Parts 27 and 29. On February 22 the FAA issued a request for public comment, due on or before May 23.

February 26, 2013 - 3:42pm

The FAA has begun the process that could lead to rewriting the standards for normal- and transport-category helicopters certified under Parts 27 and 29 of the FARs. On Friday, the agency formally issued a request for public comment due on or before May 23. Specifically, the FAA is seeking comments on whether it should revise the maximum weight and passenger-seat capacity for helicopters in both categories and make airworthiness standards “more efficient and adaptable to future technology.”

October 31, 2012 - 12:05pm

The FAA is proposing an Airworthiness Directive for the Eurocopter AS332C, L and L1 to require initial and repetitive inspections of the outer skin, butt strap and fuselage frame for a crack and modification of the helicopter. The proposed AD is prompted by an AD issued by the EASA that states a crack was discovered in a fuselage frame during a daily check.

September 5, 2012 - 12:55pm

The FAA is proposing an airworthiness directive for MD Helicopters 369Ds, 369Es, 369Fs and 369FFs with specific serial-numbered tailboom assemblies. The AD was prompted by the discovery of short-edge margin conditions on two tailboom assemblies.

 
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