Federal Aviation Administration May 19, 2006 – Federal Register Recent Federal Regulation Documents

Availability of Partially Exclusive, Exclusive or Non Exclusive License
Document Number: Z6-7331
Type: Notice
Date: 2006-05-19
Agency: Department of Defense, Employee Benefits Security Administration, Department of Labor, Department of Energy, Federal Aviation Administration, Department of Transportation, Management and Budget Office, Department of the Army, Corps of Engineers, Engineers Corps, Army Department
Airworthiness Directives; Raytheon Aircraft Company Model B300 Airplanes
Document Number: E6-7636
Type: Proposed Rule
Date: 2006-05-19
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for certain Raytheon Aircraft Company (Raytheon) Model B300 airplanes. This proposed AD would require you to modify the cabin passenger seats by installing a modification kit on each passenger seat, removing the existing technical standard order (TSO) label, and re-identifying each modified passenger seat assembly with a new part number. This proposed AD results from the seats not meeting the ultimate load requirements of 14 CFR part 23 during structural testing of the seat with design changes. We are issuing this proposed AD to prevent the passenger seats from failing during emergency landing conditions when high inertial loadings occur. Passenger seat failure may result in occupant injury.
Airworthiness Directives; Boeing Model 757-200, -200CB, and -300 Series Airplanes
Document Number: E6-7633
Type: Proposed Rule
Date: 2006-05-19
Agency: Federal Aviation Administration, Department of Transportation
The FAA is revising an earlier proposed airworthiness directive (AD) for certain Boeing Model 757-200, -200CB, and -300 series airplanes. The original NPRM would have required repetitive detailed inspections for proper functioning of the girt bar leaf springs for the escape slides to ensure the leaf springs retain the sliders and the required 0.37-inch minimum engagement between the sliders and floor fittings is achieved at passenger doors 1, 2, and 4, and corrective actions if necessary. The original NPRM resulted from a report that the escape slides failed to deploy correctly during an operator's tests of the escape slides. This action revises the original NPRM by stating that this proposed AD would not include procedures from the airplane maintenance manuals and component maintenance manuals that allow bending the girt bar retention springs. We are proposing this supplemental NPRM to prevent escape slides from disengaging from the airplane during deployment or in use, which could result in injuries to passengers or flightcrew.
Airworthiness Directives; The Cessna Aircraft Company Models 208 and 208B Airplanes
Document Number: C6-2544
Type: Rule
Date: 2006-05-19
Agency: Federal Aviation Administration, Department of Transportation
Airworthiness Directives; Hamilton Sundstrand Model 14RF-9 Propellers; Correction
Document Number: 06-4679
Type: Rule
Date: 2006-05-19
Agency: Federal Aviation Administration, Department of Transportation
This document makes a correction to Airworthiness Directive (AD) 2006-10-07. That AD applies to Hamilton Sundstrand Model 14RF-9 propellers. We published AD 2006-10-07 in the Federal Register on May 12, 2006 (71 FR 27600). An incorrect phrase was used in the compliance section, which impacts the intent of the compliance. This document corrects that phrase. In all other respects, the original document remains the same.
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