Federal Aviation Administration April 29, 2005 – Federal Register Recent Federal Regulation Documents

Airworthiness Directives; Boeing Model 737-100, -200, -200C, -300, -400, -500 Series Airplanes
Document Number: 05-8578
Type: Proposed Rule
Date: 2005-04-29
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for all Boeing Model 737-100, -200, -200C, -300, -400, and -500 series airplanes. This proposed AD would require a one-time inspection for scribe lines and cracks in the fuselage skin at certain lap joints, butt joints, external repair doublers, and other areas; and related investigative/corrective actions if necessary. This proposed AD is prompted by reports of fuselage skin cracks adjacent to the skin lap joints on airplanes that had scribe lines. Scribe line damage can also occur at many other locations, including butt joints, external doublers, door scuff plates, the wing-to-body fairing, and areas of the fuselage where decals have been applied or removed. We are proposing this AD to prevent rapid decompression of the airplane due to fatigue cracks resulting from scribe lines on pressurized fuselage structure.
Policy on Substantiation of Secondary Composite Structures
Document Number: 05-8537
Type: Notice
Date: 2005-04-29
Agency: Federal Aviation Administration, Department of Transportation
This notice announces the issuance of a Federal Aviation Administration (FAA) policy to provide some guidelines for certifying secondary structures made from composite materials. This notice is necessary to advise the public, especially manufacturers of normal, utility, and acrobatic category airplanes, and commuter category airplanes and their suppliers, that the FAA has adopted a policy on composite applications that range from secondary structures to non- structural parts such as interiors.
Revision of VOR Federal Airway 208
Document Number: 05-8536
Type: Rule
Date: 2005-04-29
Agency: Federal Aviation Administration, Department of Transportation
This action modifies Federal Airway 208 (V-208) by changing the originating point of the airway from the Santa Catalina, CA, Very High Frequency Omnidirectional Range/Tactical Air Navigation (VORTAC) to the Ventura, CA, VORTAC. This modification extends V-208 by incorporating a route segment that air traffic control (ATC) frequently assigns to aircraft arriving in the Los Angeles, CA, terminal area. This action will enhance air safety, simplify routings, and reduce controller workload in the Southern California area.
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