Federal Aviation Administration 2007 – Federal Register Recent Federal Regulation Documents

This action proposes to establish Class E airspace at Gould Peterson Municipal Airport, Tarkio, MO. The development of an Area Navigation (RNAV) Standard Instrument Approach Procedure (SIAP) to serve flights operating into the Gould Peterson Municipal Airport during Instrumental Flight Rules (IFR) conditions makes this action necessary. Controlled airspace extending upward from 700 feet Above Ground Level (AGL) is needed to contain aircraft executing an approach. The area would be depicted on aeronautical charts for pilot reference.

The FAA is publishing notice of proposed release of 0.81 acres of land at the Lonesome Pine Airport, Wise, Virginia to the town of Wise or Wise county Industrial Development Authority (Property Map Parcel 35). The release of land will transfer the responsibility (and potential liability) for maintenance and security of the water tank site to the appropriate governmental entity. Releasing the land does not adversely impact theAirport and the land is not needed for airport development as shown on the Airport Layout Plan. Fair Market Value of the land has been assessed and will be provided to The Cumberlands Airport Commission for Airport and commission operational expenses.

We propose to adopt a new airworthiness directive (AD) for the products listed above. This proposed AD results from mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:

We propose to adopt a new airworthiness directive (AD) for the products listed above. This proposed AD results from mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:

This action proposes to modify Class E airspace at Helena, MT. Additional controlled airspace is necessary to accommodate aircraft using a new Localizer (LOC) Back Course (BC)-C Standard Instrument Approach Procedures (SIAP) at Helena Regional Airport. The FAA is proposing this action to enhance the safety and management of aircraft operations at Helena Regional Airport, Helena, MT.

The FAA is correcting a typographical error in an existing airworthiness directive (AD) that was published in the Federal Register on May 22, 2007 (72 FR 28597). The error resulted in a confusing compliance time. This AD applies to all Boeing Model 737-100, -200, - 200C, -300, -400, and -500 series airplanes. This AD requires repetitive detailed inspections for damage of the electrical wire and sleeve that run to the fuel boost pump through a conduit in the fuel tank, and arcing damage of the conduit and signs of fuel leakage into the conduit; replacement of the sleeve with a new, smaller-diameter sleeve; and related investigative and corrective actions, as applicable.

The FAA is adopting a new airworthiness directive (AD) for all Boeing Model 767 airplanes. This AD requires repetitive detailed inspections of the wire bundles, power drive unit (PDU) wiring, and wire attaching hardware, supports, and sleeving located in the forward and aft lower lobe cargo compartments, and corrective actions as necessary. This AD results from a fire in the forward lower lobe cargo compartment found shortly after airplane arrival. We are issuing this AD to detect and correct damage to wires in the forward and aft lower lobe cargo compartments, which could result in a potential short circuit and consequent fire in the forward and aft lower lobe cargo compartments.

This amendment adopts a new airworthiness directive (AD) for Sikorsky Aircraft Corporation (Sikorsky) Model S92-A helicopters. This action requires, within a specified time, borescope inspecting a certain part-numbered tail rotor pitch change shaft and bearing assembly (shaft and bearing assembly) and also inspecting after any installation. This amendment is prompted by an incident involving failure of a shaft and bearing assembly and servo clevis shaft resulting in loss of tail rotor control. The actions specified in this AD are intended to prevent failure of a shaft and bearing assembly, loss of tail rotor pitch and yaw control, and subsequent loss of control of a helicopter.

We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued by the aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:

We propose to adopt a new airworthiness directive (AD) for the products listed above. This proposed AD results from mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:

We propose to adopt a new airworthiness directive (AD) for the products listed above. This proposed AD results from mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:

The FAA proposes to adopt a new airworthiness directive (AD) for all Airbus Model A310 series airplanes. This proposed AD would require revising the Airworthiness Limitations section of the Instructions for Continued Airworthiness to incorporate new and revised structural inspections and inspection intervals. This proposed AD results from issuance of new and revised structural inspections and inspection intervals. We are proposing this AD to detect and correct fatigue cracking, which could result in reduced structural integrity of the airplane.

We propose to adopt a new airworthiness directive (AD) for the products listed above. This proposed AD results from mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:

The FAA is revising an earlier NPRM for an airworthiness directive (AD) that applies to all Airbus Model A330-200, A330-300, A340-200, and A340-300 series airplanes; and Model A340-541 and A340- 642 airplanes. The original NPRM would have superseded an existing AD that currently requires operators to revise the Airworthiness Limitations section (ALS) of the Instructions for Continued Airworthiness (ICA) to incorporate new information. This information includes, for all affected airplanes, decreased life limit values for certain components; and for Model A330-200 and -300 series airplanes, new inspections, compliance times, and new repetitive intervals to detect fatigue cracking, accidental damage, or corrosion in certain structures. The original NPRM proposed to revise the ALS, for all affected airplanes, by adding new Airworthiness Limitations Items (ALIs) to incorporate service life limits for certain items and inspections to detect fatigue cracking, accidental damage or corrosion in certain structures, in accordance with the revised ALS of the ICA. The original NPRM resulted from the issuance of new and more restrictive service life limits and structural inspections based on fatigue testing and in-service findings. This new action revises the original NPRM by adding airplanes, adding new requirements, and including more restrictive compliance thresholds and intervals. We are proposing this supplemental NPRM to detect and correct fatigue cracking, accidental damage, or corrosion in principal structural elements, and to prevent failure of certain life-limited parts, which could result in reduced structural integrity of the airplane.

The FAA proposes to adopt a new airworthiness directive (AD) for certain Boeing Model 737-300, -400, and -500 series airplanes. This proposed AD would require, among other actions, modifying the door- mounted escape system of the forward right side door slide compartment. This proposed AD results from reports indicating that the forward right escape slide inflated 90 degrees out of alignment after deployment from the forward right side slide compartment. We are proposing this AD to prevent the escape slide from being unusable during an emergency evacuation and consequent injury to passengers or crewmembers.

The FAA proposes to adopt a new airworthiness directive (AD) for certain Boeing Model 737-100, -200, -200C, -300, -400, and -500 series airplanes. This proposed AD would require repetitive detailed and high-frequency eddy current inspections for cracking around the heads of the fasteners on the forward fastener row of certain areas of the station (STA) 259.5 circumferential butt splice, and repair if necessary. This proposed AD would also require a preventive modification, which would eliminate the need for the repetitive inspections. This proposed AD results from a report that an operator found multiple cracks in the fuselage skin of a Model 737-200 airplane, at the forward fastener row of the STA 259.5 circumferential butt splice between stringers 19 and 24. We are proposing this AD to prevent cracking of the STA 259.5 circumferential butt splice, which could result in loss of structural integrity of the fuselage skin and possible loss of cabin pressure.

The FAA proposes to adopt a new airworthiness directive (AD) for certain Boeing airplanes listed above. This proposed AD would require an inspection of certain lighted pushbutton switches in the flight compartment for configuration `D' master modules and part numbers and corrective action if necessary. This proposed AD also provides an option to inspect panel assemblies for part numbers. This proposed AD results from a report indicating that the integrated drive generator failed in flight due to a possible switch malfunction. We are proposing this AD to ensure that certain lighted pushbutton switches in the flight compartment do not malfunction and cause the flightcrew to be unable to control critical airplane systems and continue safe airplane operation.

The FAA proposes to adopt a new airworthiness directive (AD) for certain Boeing Model 767-300F series airplanes. This proposed AD would require replacing the rotomolded duct(s) of the mix manifold system with new duct(s). This proposed AD results from a report of failures of the duct joint seal of the mix manifold system. We are proposing this AD to prevent air conditioning leakage into the mix manifold bay. Such leakage could decrease the air flow to the flight compartment and main cabin or could allow smoke into the flight compartment in the event of a fire in the main cabin or forward cargo compartment.

This document denies the request to extend the comment period on the FAA's notice of proposed amendments to its December 12, 2006, order that places temporary limitations on flight operations at New York's LaGuardia Airport. The notice of proposed amendments was published in the Federal Register on August 7, 2007.

This final rule amends Federal Aviation Administration (FAA) regulations by requiring operators of passenger-carrying transport category airplanes used in domestic, flag, and supplemental operations to have a means for flightcrew to visually monitor the door area outside the flightdeck. This means will allow the flightcrew to identify persons requesting entry into the flightdeck and detect suspicious behavior or potential threats. This final rule also amends FAA regulations to require that, for operations requiring the presence of flight attendants, the flight attendants have a means to discreetly notify the flightcrew of suspicious activity or security breaches in the cabin. This final rule addresses standards adopted by the International Civil Aviation Organization (ICAO) following the September 11, 2001 terrorist attacks.

These special conditions are issued for the Adam Aircraft, Model A700 airplane. This airplane will have a novel or unusual design feature(s) associated with aft mounted engine fire protection. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. These special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards.

The FAA is issuing this notice to advise the public of RTCA Special Committee 215, Aeronautical Mobile Satellite (Route) Services, Next Generation Satellite Services and Equipment.

The FAA invites public comments about our intention to request the Office of Management and Budget (OMB) to approve a current information collection. Title 49 U.S.C. Sections 47702 and 44703 authorize the issuance of airman certificates. FAR part 65 prescribes requirements for mechanics, repairmen, parachute riggers, and inspection authorizations.

The FAA invites public comments about our intention to request the Office of Management and Budget (OMB) to approve a current information collection. This information collection is used to allocate slots and maintain accurate records of slot transfers at High Density Traffic Airports.

The FAA invites public comments about our intention to request the Office of Management and Budget (OMB) to approve a current information collection. Per this rule, aircraft operators need to add a statement to the seat back pocket card stating the country of origin of final assembly of the aircraft.