Federal Aviation Administration December 1, 2005 – Federal Register Recent Federal Regulation Documents
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Agency Information Collection Activity Under OMB Review, Request for Comments; Renewal of an Approved Information Collection Activity, Operating Requirements: Domestic, Flag, and Supplemental Operations, Part 121
The FAA invites public comments about our intention to request the Office of Management and Budget's (OMB) renewal of a current information collection. The Federal Register Notices with a 60-day comment period soliciting comments on the following collection of information was published on July 27, 2005, vol. 143, pages 43502-43503. 14 CFR Part 121 prescribes the requirements governing air carrier operations. The information collected is used to determine air operators' compliance with the minimum safety standards set out in the regulation and the applicant's eligibility for air operations certification.
Notice of Intent To Rule on Request To Release Airport Property at Shawnee Regional Airport, Shawnee, OK
FAA proposes to rule and invites public comment on the release of land at Shawnee Regional Airport under the provisions of Title 49 of US Code, Section 47153.
Public Notice for a Change in Use of Aeronautical Property at Owensboro-Daviess County Regional Airport, Owensboro, KY
Under the provisions of Title 49, U.S.C. 47153(c), the Federal Aviation Administration is requesting public comment on the Owensboro- Daviess County Regional Airport Board's request to change a portion (2.362 acres) of airport property from aeronautical use to non- aeronautical use. The property is to be sold to The City of Owensboro, Kentucky for the completion of a connector walkway to David C. Adkisson Greenbelt Park. The 2.362 acres is located on the northeast boundary of Owensboro- Daviess County Regional Airport; adjacent to and immediately west of the Wendell Ford Expressway, adjacent to and immediately south of Bittel Road, Daviess County, Kentucky.
Special Conditions; New Piper Aircraft, Inc.; PA-34; Protection of Systems for High Intensity Radiated Fields (HIRF)
These special conditions are issued to the New Piper Aircraft, Inc., Vero Beach, Florida, for a type design change for the PA-34 model airplanes. These airplanes will have novel and unusual design features when compared to the state of technology envisaged in the applicable airworthiness standards. These novel and unusual design features include the installation of electronic flight instrument system (EFIS) displays Model 700-00006-XXX(), manufactured by Avidyne Corporation, Inc. for which the applicable regulations do not contain adequate or appropriate airworthiness standards for the protection of these systems from the effects of high intensity radiated fields (HIRF). These special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to the airworthiness standards applicable to these airplanes.
Special Conditions; Cessna Aircraft Company; Protection of Systems for High Intensity Radiated Fields (HIRF)
These special conditions are issued to Cessna Aircraft Co., for the Type Certificate of Model 510 Mustang airplane. This airplane will have novel and unusual design features when compared to the state of technology envisaged in the applicable airworthiness standards. The novel and unusual design features include the installation of an Electronic Flight Instrumentation System (EFIS), Digital Air Data Computer (ADC), and a Full Authority Digital Engine Control (FADEC). The applicable regulations do not adequately consider failure of electrical and electronic systems performing critical functions from the effects of external HIRF. These special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to the airworthiness standards applicable to this airplane.
Airworthiness Directives; Boeing Model 737-100, -200, -200C, -300, -400, and -500 Series Airplanes
The FAA is revising an earlier proposed airworthiness directive (AD) for all Boeing Model 737-100, -200, -200C, -300, -400, and -500 series airplanes. The original NPRM would have required an inspection for chafing of certain wire bundles located above the center fuel tank, corrective actions if necessary, and replacement of wire bundle clamps with new clamps. The original NPRM resulted from fuel system reviews conducted by the manufacturer. This action revises the original NPRM by adding an inspection for damage to the fuel vapor barrier area located below the wire bundles and corrective action, if necessary. We are proposing this supplemental NPRM to prevent chafed wire bundles near the center fuel tank, which could cause electrical arcing through the tank wall and ignition of fuel vapor in the fuel tank, and result in a fuel tank explosion.
Airworthiness Directives; Airbus Model A318-100 Series Airplanes, Model A319-100 Series Airplanes, Model A320-111 Airplanes, Model A320-200 Series Airplanes, and Model A321-100 Series Airplanes
The FAA proposes to supersede an existing airworthiness directive (AD) that applies to certain Airbus Model A319, A320, and A321 series airplanes. The existing AD currently requires repetitive inspections to detect wear of the inboard flap trunnions, and to detect wear or de-bonding of the protective half-shells; corrective actions, if necessary; and terminating action. This proposed AD would remove the repetitive inspections to detect wear of the inboard flap trunnions and to detect wear or de-bonding of the protective half-shells; and corrective actions if necessary. This proposed AD would add repetitive detailed inspections of the inboard flap trunnions for any wear marks and of the sliding panels for any cracking at the long edges, and corrective actions if necessary. This proposed AD would also add airplanes to the applicability. This proposed AD results from reports of wear damage to the inboard flap trunnions after incorporation of the terminating modification. We are proposing this AD to detect and correct wear of the inboard flap trunnions, which could lead to loss of flap surface control and consequently result in the flap detaching from the airplane. A detached flap could result in damage to the tail of the airplane.
Airworthiness Directives; Airbus Model A319-131, -132, and -133; A320-232 and -233; and A321-131 and -231 Airplanes
The FAA proposes to adopt a new airworthiness directive (AD) for certain Airbus Model A319-131, -132, and -133; A320-232 and -233; and A321-131 and -231 airplanes. This proposed AD would require inspecting for cracks or failure of the primary load path components of the engine forward mount, and corrective action if necessary. This proposed AD also would require removing, re-installing, and re-torquing the attachment bolts for the secondary load path. This proposed AD results from a report that, during modification of certain engine forward mount assemblies of the left and right engines done at an engine shop visit, an incorrect torque was applied to the attachment bolts. We are proposing this AD to prevent structural failure of the secondary load path of the forward engine mount, which, if combined with failure of the primary load path, could result in separation of the engine from the airplane.
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