Federal Aviation Administration 2008 – Federal Register Recent Federal Regulation Documents

The FAA is revising an earlier proposed airworthiness directive (AD) for certain Boeing Model 767 airplanes. The original NPRM would have required repetitive inspections for cracking of the wing skin, and related investigative/corrective actions if necessary. The original NPRM resulted from reports of cracks found in the lower wing skin originating at the forward tension bolt holes of the aft pitch load fitting. This action revises the original NPRM by revising certain compliance times. We are proposing this supplemental NPRM to detect and correct cracking in the lower wing skin for the forward tension bolt holes at the aft pitch load fitting, which could result in a fuel leak and 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:

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.

The FAA is issuing this notice to advise the public of a meeting of RTCA Special Committee 218/Future ADS-B/TCAS Relationships

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).

We are adopting a new airworthiness directive (AD) for all Boeing Model 737-100, -200, -200C, -300, -400, and -500 series airplanes. This AD requires repetitive inspections for cracking in and around the upper and lower hinge cutouts of the forward entry and forward galley service doorways, and corrective actions if necessary. This AD results from multiple reports of cracks found in the skin, bearstrap, and/or frame outer chord in the hinge cutout areas of the forward entry and forward galley service doorways. We are issuing this AD to detect and correct such cracking, which could result in rapid decompression of the airplane.

We are adopting a new airworthiness directive (AD) for all Boeing Model 737-100, -200, and -200C series airplanes. This AD requires revising the FAA-approved maintenance inspection program to include inspections that will give no less than the required damage tolerance rating for each structural significant item (SSI), doing repetitive inspections to detect cracks of all SSIs, and repairing cracked structure. This AD results from a report of incidents involving fatigue cracking in transport category airplanes that are approaching or have exceeded their design service objective. We are issuing this AD to maintain the continued structural integrity of the entire fleet of Model 737-100, -200, and -200C series airplanes.

We are adopting a new airworthiness directive (AD) for all Lockheed Model L-1011 series airplanes. This AD requires revising the FAA-approved maintenance program by incorporating new airworthiness limitations for fuel tank systems to satisfy Special Federal Aviation Regulation No. 88 requirements. This AD also requires the accomplishment of certain fuel system modifications, the initial inspections of certain repetitive fuel system limitations to phase in those inspections, and repair if necessary. This AD results from a design review of the fuel tank systems. We are issuing this AD to prevent the potential for ignition sources inside fuel tanks caused by latent failures, alterations, repairs, or maintenance actions, which, in combination with flammable fuel vapors, could result in a fuel tank explosion and consequent loss of the airplane.

In a proposed order published on March 18, 2008, the Federal Aviation Administration (FAA) tentatively identified the parameters of an order that would temporarily limit scheduled flight operations at Newark Liberty International Airport (EWR).\1\ The FAA issued the proposal as a result of persistent congestion and delays at EWR during the peak operating hours, as well as a dramatic projected increase in flight delays at the airport during the summer of 2008 if proposed schedules were implemented as requested by carriers. After evaluating the written comment submitted to the public docket in this matter, the FAA is issuing this final Order, which will take effect at 6 a.m., Eastern Time, on June 20, 2008.

We are adopting a new airworthiness directive (AD) for certain Boeing Model 747-100, 747-100B, 747-200B, 747-200C, 747-200F, 747-300, 747SR, and 747SP series airplanes. This AD requires an inspection to determine if acceptable external skin doublers are installed at the stringer 6 (S-6) lap splices, between station (STA) 340 and STA 400. For airplanes without the acceptable external skin doublers, this AD requires repetitive related investigative actions and corrective actions if necessary. This AD also provides an optional terminating modification for the repetitive related investigative actions. This AD results from a report of cracked fastener holes at the right S-6 lap splice between STA 340 and STA 380. We are issuing this AD to detect and correct cracking in the fuselage skin, which could result in rapid decompression and loss of structural integrity.

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 Lycoming Engines (formerly Textron Lycoming) models 320, 360, and 540 series, ``Parallel Valve'' reciprocating engines, with certain Engine Components Inc. (ECi) cylinder assemblies, part number (P/N) AEL65102 series ``Titan'', installed. This proposed AD would require initial and repetitive visual inspections and compression tests to detect cracks at the head-to-barrel interface, replacement of cylinder assemblies found cracked, and replacement of certain cylinder assemblies, at new reduced times-in-service. This proposed AD results from reports of 45 failures with head separations of ECi cylinder assemblies. We are proposing this AD to prevent loss of engine power due to cracks at the head-to-barrel interface in the cylinder assemblies and possible engine failure caused by separation of a cylinder head, which could result in loss of control of the aircraft.

The FAA proposes to supersede an existing airworthiness directive (AD) that applies to various aircraft equipped with certain Honeywell Primus II RNZ-850( )/-851( ) integrated navigation units (INUs). The existing AD, as one alternative for compliance, provides for a one-time inspection to determine whether a certain modification has been installed on the Honeywell Primus II NV-850 navigation receiver module (NRM), which is part of the INU. In lieu of accomplishing this inspection, and for aircraft found to have an affected NRM, that AD provides for revising the aircraft flight manual to include new limitations for instrument landing system approaches. That AD also requires an inspection to determine whether certain other modifications have been done on the NRM; and doing related investigative, corrective, and other specified actions, as applicable; as well as further modifications to address additional anomalies. This proposed AD would extend the compliance time for a certain inspection and associated actions. This proposed AD would also revise the applicability to include additional affected INUs. This proposed AD results from reports indicating that erroneous localizer and glideslope indications have occurred on certain aircraft equipped with the subject INUs. We are proposing this AD to ensure that the flight crew has accurate localizer and glideslope deviation indications. An erroneous localizer or glideslope deviation indication could lead to the aircraft making an approach off the localizer, which could result in impact with an obstacle or terrain.

This notice contains a summary of a petition seeking relief from specified requirements of 14 CFR. The purpose of this notice is to improve the public's awareness of, and participation in, this aspect of FAA's regulatory activities. Neither publication of this notice nor the inclusion or omission of information in the summary is intended to affect the legal status of the petition or its final disposition.

This action amends the Class E airspace area at Waynesburg, PA, to accommodate a new Standard Instrument Approach Procedure (SIAP) that has been developed for Green County Airport. As a result, controlled airspace extending upward from 700 feet Above Ground Level (AGL) will be expanded to contain the SIAP and other Instrument Flight Rules (IFR) operations at Green County Airport. The operating status of the airport will change from Visual Flight Rules (VFR) to include IFR operations concurrent with the publication of the SIAP. A minor correction is also being made in the geographic position coordinates of the Green County Airport.

The FAA invites public comments about our intention to request the Office of Management and Budget (OMB) to approve a current information collection. SFAR 36 (to part 121) relieves qualifying applicants involved in aircraft repair of the burden to obtain FAA approval of data developed by them for the major repairs on a case-by- case basis; and provides for one-time approvals.

The FAA invites public comments about our intention to request the Office of Management and Budget (OMB) to approve a current information collection. Respondents conducting general operation and flight of aircraft or any activity that could encroach on airspace must apply for approval.

The FAA invites public comments about our intention to request the Office of Management and Budget (OMB) to approve a current information collection. Aircraft operators seeking operational approval to conduct RVSM operations within the 48 contiguous United States (U.S.), Alaska and a portion of the Gulf of Mexico must submit an application to the Certificate Holding District Office.

This action confirms the effective date of a direct final rule published in the Federal Register (73 FR 9443) that modifies Class E Airspace at Bradford, PA. The modified controlled airspace from nearby Bradford Regional Airport will now adequately support the Area Navigation (RNAV) Global Positioning System (GPS) Special Instrument Approach Procedure (IAP) developed for medical flight operations for the University of Pittsburgh.

The FAA invites public comments about our intention to request the Office of Management and Budget (OMB) to approve a current information collection. Pursuant to Public Law 104-50, the FAA implements an acquisition management system that addresses the unique needs of the agency. This document established the policies and internal procedures for the FAA's acquisition system.

The FAA invites public comments about our intention to request the Office of Management and Budget (OMB) to approve a current information collection. The information to be collected includes data required for performing launch site location analysis.

The FAA invites public comments about our intention to request the Office of Management and Budget (OMB) to approve a current information collection. The Advanced Qualification Program (AQP) incorporates data driven quality control processes for validating and maintaining the effectiveness of air carrier training program curriculum content.

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 allows the FAA to evaluate its certification standards, maintenance programs, and regulatory requirements. It is also the basis for issuance of Airworthiness Directives designed to prevent unsafe conditions and accidents.

This Rule establishes, amends, suspends, or revokes STANDARD Instrument Approach Procedures (SIAPs) and associated Takeoff Minimums and Obstacle Departure Procedures for operations at certain airports. These regulatory actions are needed because of the adoption of new or revised criteria, or because of changes occurring in the National Airspace System, such as the commissioning of new navigational facilities, adding new obstacles, or changing air traffic requirements. These changes are designed to provide safe and efficient use of the navigable airspace and to promote safe flight operations under instrument flight rules at the affected airports.