Federal Aviation Administration May 22, 2008 – Federal Register Recent Federal Regulation Documents
Results 1 - 6 of 6
Airworthiness Directives; Boeing Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-200C, 747-300, 747-400, 747-400D, and 747SR Series Airplanes
We are revising an earlier proposed airworthiness directive (AD) for certain Boeing Model 747-100, 747-100B, 747-100B SUD, 747- 200B, 747-200C, 747-300, 747-400, 747-400D, and 747SR series airplanes. For certain airplanes, the original NPRM would have required a material type inspection to determine if the lower forward corner reveal of the number 3 main entry doors (MEDs) is a casting. If the reveals are castings, the original NPRM would have required repetitive inspections of the reveals for cracking, and corrective action if necessary. If the reveals are not castings, the original NPRM would have required a detailed inspection of the reveals for a sharp edge and repetitive inspections of the reveals for cracking, and corrective action if necessary. For certain other airplanes, the original NPRM would have required only a detailed inspection of the reveals for a sharp edge and repetitive inspections of the reveals for cracking, and corrective action if necessary. For certain other airplanes, the original NPRM would have required repetitive inspections of the reveals for cracking only, and corrective action if necessary. The original NPRM resulted from reports of cracking and/or a sharp edge in the lower forward corner reveal of the number 3 MEDs. This action revises the original NPRM by reducing the compliance times for doing certain inspections and allowing a certain replacement as an optional action for the material type inspection for certain airplanes. We are proposing this supplemental NPRM to detect and correct fatigue cracking of the lower forward corner reveal of the number 3 MEDs, which could lead to the door escape slide departing the airplane when the door is opened and the slide is deployed, and consequent injuries to passengers and crew using the door escape slide during an emergency evacuation.
Airworthiness Directives; Dornier Model 328-100 Airplanes
The FAA proposes to supersede an existing airworthiness directive (AD) that applies to all AvCraft Dornier Model 328-100 airplanes. The existing AD currently requires modifying the electrical wiring of the fuel pumps; installing insulation at the hand flow control and shut-off valves, and other components of the environmental control system; and installing markings at fuel wiring harnesses. The existing AD also requires revising the Airworthiness Limitations section (ALS) of the Instructions for Continued Airworthiness to incorporate new inspections of the fuel tank system. This proposed AD would replace the flight-hour-based threshold for conducting certain initial inspections, with an 8-year threshold. This proposed AD results from fuel system reviews conducted by the manufacturer. We are proposing this AD to reduce the potential of ignition sources inside fuel tanks, which, in combination with flammable fuel vapors, could result in fuel tank explosions and consequent loss of the airplane.
RTCA Special Committee 218/Future ADS-B/TCAS Relationships
The FAA is issuing this notice to advise the public of a meeting of RTCA Special Committee 218/Future ADS-B/TCAS Relationships
Fourth Meeting, RTCA Special Committee 216: Aeronautical System Security
The FAA is issuing this notice to advise the public of a meeting of RTCA Special Committee 216: Aeronautical Systems Security.
Fourth Meeting, Special Committee 214: Standards for Air Traffic Data Communication Services Joint With EUROCAE Working Group 78 (WG-78)
The FAA is issuing this notice to advise the public of a first meeting of RTCA Special Committee 214, Standards for Air Traffic Data Communication Services Joint with EUROCAE Working Group 78 (WG-78).
Transport Airplane Wheels and Wheel and Brake Assemblies
This notice announces the availability of, and requests comment on proposed Technical Standard Order (TSO) C-135a, Transport Airplane Wheels and Wheel and Brake Assemblies. This proposed TSO tells persons seeking a TSO authorization or letter of design approval what minimum performance standards (MPS) their Transport Airplane Wheels and Wheel and Brake Assemblies must meet to be identified with the appropriate TSO marking.
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