Federal Aviation Administration February 13, 2015 – Federal Register Recent Federal Regulation Documents
Results 1 - 7 of 7
Notice of Passenger Facility Charge (PFC) Approvals and Disapprovals
The FAA publishes a monthly notice, as appropriate, of PFC approvals and disapprovals under the provisions of the Aviation Safety and Capacity Expansion Act of 1990 (title IX of the Omnibus Budget Reconciliation Act of 1990) (Pub. L. 101-508) and part 158 of the Federal Aviation Regulations (14 CFR part 158). This notice is published pursuant to paragraph d of Sec. 158.29.
Sixty-Fifth Meeting: RTCA Special Committee 135, Environmental Conditions and Test Procedures for Airborne Equipment
The FAA is issuing this notice to advise the public of the Sixty-Fifth meeting of the RTCA Special Committee 135, Environmental Conditions and Test Procedures for Airborne Equipment.
Third Meeting: RTCA Special Committee 230, Airborne Weather Detection Systems Committee
The FAA is issuing this notice to advise the public of the third meeting of the Airborne Weather Detection Systems Committee.
Third Meeting: RTCA Special Committee 232, Airborne Selective Calling Equipment
The FAA is issuing this notice to advise the public of the third meeting of RTCA Special Committee 232, Airborne Selective Calling Equipment.
Airworthiness Directives; Airbus Airplanes
We propose to adopt a new airworthiness directive (AD) for all Airbus Model A330-243, A330-243F, A330-341, A330-342, and A330-343 airplanes. This proposed AD was prompted by reports indicating that certain hinge sleeves on the cowl doors of the thrust reverser units (TRUs) were not heat treated. This proposed AD would require replacing the sleeves of certain hinges on the cowl doors of the TRUs with new parts. We are proposing this AD to prevent, in the event of a fan- blade-off event due to high vibration, in-flight loss of TRU heavy components, which might damage airplane structure or control surfaces, and consequent reduced controllability of the airplane.
Airworthiness Directives; Airbus Airplanes
We propose to adopt a new airworthiness directive (AD) for certain Airbus Model A330-200, A330-200 Freighter, and A330-300 series airplanes; and all A340-200 and A340-300 series airplanes. This proposed AD was prompted by reports that a bracket that attaches the cockpit instrument panel to the airplane structure, does not sustain the fatigue loads of the design service goal. This proposed AD would require repetitive inspections of that bracket for cracking and to determine if both lugs are fully broken, an inspection for cracking of an adjacent bracket, if necessary, and corrective actions if necessary. This AD would also provide an optional modification, which would terminate the repetitive inspections. We are proposing this AD to detect and correct cracking on a bracket of the cockpit instrument panel, which, combined with failure of the horizontal beam, could lead to collapse of the cockpit panel, and reduced controllability of the airplane.
Airworthiness Directives; Airbus Airplanes
We propose to adopt a new airworthiness directive (AD) for certain Airbus Model A300 B4-2C, B4-103, and B4-203 airplanes; Airbus Model A300 B4-600 series airplanes; and Airbus Model A300 B4-600R series airplanes. This proposed AD was prompted by reports indicating that, on airplanes that received a certain repair following crack findings, cracks can re-initiate. This proposed AD would require repetitive inspections for cracking of the frame (FR) 40 forward fittings for airplanes previously repaired. We are proposing this AD to detect and correct cracking on the FR 40 forward fittings, which could result in rupture of the forward fittings and reduction of in-flight structural strength.
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