Federal Aviation Administration 2007 – Federal Register Recent Federal Regulation Documents
Results 1,001 - 1,050 of 1,687
Amendment of Class E Airspace; Middlesboro, KY; Correction
This document contains a correction to the final rule (FAA- 2007-27262; 07-ASO-1), which was published in the Federal Register of May 8, 2007, (72 FR 25963), amending Class E airspace at Middlesboro, KY. This action corrects an error in the legal description for the Class E5 airspace at Middlesboro, KY.
Passenger Facility Charge Program, Debt Service, Air Carrier Bankruptcy, and Miscellaneous Changes
This final rule amends FAA regulations dealing with the Passenger Facility Charge (PFC) program to add more eligible uses for revenue, protect such revenue in bankruptcy proceedings, and eliminate charges to passengers on military charters. These changes respond to the Vision 100Century of Aviation Reauthorization Act. This final rule also revises current reporting requirements to reflect technological improvements, and to clarify and update existing references and regulations. This final rule further streamlines the existing policies of the PFC program.
Airworthiness Directives; Boeing Model 737-200, -300, -400, -500, -600, -700, -800, and -900 Series Airplanes; Boeing Model 757-200 and -300 Series Airplanes; and McDonnell Douglas Model DC-10-10, DC-10-10F, DC-10-30, DC-10-30F, DC-10-40, MD-10-30F, MD-11, and MD-11F Airplanes; Equipped With Reinforced Flight Deck Doors Installed in Accordance With Supplemental Type Certificate (STC) ST01335LA, STC ST01334LA, and STC ST01391LA, Respectively
The FAA is superseding an existing airworthiness directive (AD), which applies to certain transport category airplanes identified above. That AD currently requires modification of the reinforced flight deck door and other actions related to the reinforced flight deck door. Those other actions include modifying the door, inspecting and modifying wiring in the area, and revising the maintenance program to require more frequent testing of the decompression panels of the flight deck door. This new AD continues to require the existing requirements. This new AD adds airplanes to the existing requirement of a one-time inspection for chafing of wire bundles in the area of the flight deck door and corrective actions if necessary. This proposed AD also removes certain airplanes from the applicability. This AD results from a report of smoke and fumes in the cockpit of a Model 737-300 series airplane. We are issuing this AD to prevent inadvertent release of the decompression latch and consequent opening of the decompression panel in the flight deck door, or penetration of the flight deck door by smoke, any of which could result in injury to the airplane flightcrew. We are also proposing this AD to detect and correct wire chafing, which could result in arcing, fire, and/or reduced controllability of the airplane.
Airworthiness Directives; Robinson Helicopter Company Model R44 and R44 II Helicopters
This amendment adopts a new airworthiness directive (AD) for Robinson Helicopter Company (Robinson) Model R44 and R44 II helicopters that have a certain seat belt buckle (buckle) assembly installed, that requires removing the buckle assembly and the buckle assembly spacer, and replacing them with airworthy parts. This amendment is prompted by an accident in which a seat belt failed, and also by reports of cracking in the buckle assembly stainless support strap (support strap). The actions specified by this AD are intended to prevent cracking in the support strap and failure of a seat belt.
Airworthiness Directives; Airbus Model A300-600 Series Airplanes
The FAA is adopting a new airworthiness directive (AD) for all Airbus Model A300-600 series airplanes. This AD requires revising the Airworthiness Limitations section of the Instructions for Continued Airworthiness to incorporate new limitations for fuel tank systems. This AD results from fuel system reviews conducted by the manufacturer. We are issuing this AD to prevent the potential of ignition sources inside fuel tanks, which, in combination with flammable fuel vapors caused by latent failures, alterations, repairs, or maintenance actions, could result in fuel tank explosions and consequent loss of the airplane.
RNP SAAAR Approval Consultant Opportunities
The Federal Aviation Administration (FAA) announced today that it is seeking to identify qualified industry consultants to assist 14 Code of Federal Regulations (CFR) part 91, 121, 125, 129, 135 applicants as they pursue approval to conduct ``Required Navigation Performance Special Aircraft and Aircrew Authorization Required'' (RNP SAAAR) approaches. Provisions for gaining those approvals are contained within FAA Advisory Circular 90-101, ``Approval Guidance for RNP Procedures with SAAAR.'' Applicants who meet certain qualifications will be permitted to enter into an agreement with the FAA to be listed as RNP SAAAR Approval Consultants.
Parachute Equipment and Packing
The FAA is considering rulemaking to change the packing interval for certain types of parachutes. Currently, the FAA requires that most parachutes may not be used or carried aboard an aircraft and available for emergency use unless they have been packed within the previous 120 days. New reliability data from the parachute industry and other sources indicate it is time to review the packing interval, and the FAA is asking for public comment on a proposal to lengthen the interval from 120 to 180 days. The effect of the proposal is to ensure the rules reflect the safest parachute packing interval. In this rulemaking, we are also proposing several correcting amendments to the rules related to parachute operations.
Airworthiness Directives; Boeing Model 737-100, -200, -200C, -300, -400, and -500 Series Airplanes
The FAA is superseding an existing airworthiness directive (AD) that applies to all Model 737-100, -200, -300, -400, and -500 series airplanes. The existing AD currently requires repetitive detailed inspections for damage of the electrical wire and sleeve that run through a conduit in the fuel tank to the fuel boost pump, and related investigative and corrective actions; as applicable. This new AD removes certain inspection requirements. This new AD adds 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. This AD also adds airplanes to the applicability. Accomplishment of the initial new inspection and the sleeve installation terminates the requirements of the existing AD. This new AD results from a report of a fuel tank explosion on a Model 727-200F airplane on the ground, and a report of chafed wires and a damaged power cable sleeve of a fuel boost pump discovered during an inspection on a Model 737-300 airplane. We are issuing this AD to detect and correct chafing of the fuel boost pump electrical wiring and leakage of fuel into the conduit, and to prevent electrical arcing between the wiring and the surrounding conduit, which could result in arc-through of the conduit, and consequent fire or explosion of the fuel tank.
Airworthiness Directives; Boeing Model 727 Airplanes
The FAA is superseding an existing airworthiness directive (AD) that applies to all Boeing Model 727 airplanes. The existing AD requires a boost pump dry bay inspection to detect leakage of fuel through an arced-through conduit, and corrective action as necessary. The existing AD also requires repetitive inspections of the in-tank fuel boost pump wiring to detect chafing of the wire insulation, evidence of electrical arcing, or arc-through of the conduit wall, and applicable corrective action; and installation of sleeving over the in- tank fuel boost pump wires as a method to protect the wiring from chafing. This new AD removes certain inspection requirements from the existing AD. This new AD adds new repetitive 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; applicable investigative and corrective actions; and a new repetitive engine fuel suction feed operational test. Initiation of the new inspections terminates the requirements of the existing AD. This AD results from reports of a fuel tank explosion on a Model 727-200F airplane on the ground; and of chafed wires and a damaged power cable sleeve of a fuel boost pump that were discovered during an inspection required by an existing AD on a Model 737-300 airplane. We are issuing this AD to detect and correct chafing of the fuel boost pump electrical wiring and leakage of fuel into the conduit, and to prevent electrical arcing between the wiring and the surrounding conduit, which could result in arc-through of the conduit, and consequent fire or explosion of the fuel tank.
Proposed Revision of Class E Airspace; Ruby, AK
This action proposes to revise Class E airspace at Ruby, AK. Two Standard Instrument Approach Procedures (SIAPs) are being amended for the Ruby Airport at Ruby, AK. Adoption of this proposal would result in revision of existing Class E airspace upward, from 700 feet (ft.) and 1,200 ft. above the surface, at the Ruby Airport, Ruby, AK.
Proposed Establishment of Low Altitude Area Navigation Route T-209; GA
This action proposes to establish a low altitude Global Positioning System (GPS)/Global Navigation Satellite System (GNSS) area navigation (RNAV) route, designatedT-209, in the vicinity of Augusta, GA. The FAA is proposing this action to enhance the safe and efficient use of the navigable airspace. The proposed route would reduce air traffic controller workload and provide a nonradar route that ensures clearance from the Bulldog A Military Operations Area (MOA).
Proposed Revision of Class E Airspace; Kotzebue, AK
This action proposes to revise Class E airspace at Kotzebue, AK. Eight (8) Standard Instrument Approach Procedures (SIAPs) are being amended for the Ralph Wien Memorial Airport at Kotzebue, AK. A Departure Procedure (DP) is also being amended. Adoption of this proposal would result in revision of existing Class E airspace upward from the surface, from 700 feet (ft.) and 1,200 ft. above the surface, at the Ralph Wien Memorial Airport, Kotzebue, AK.
Proposed Revision of Class E Airspace; Fort Yukon, AK
This action proposes to revise Class E airspace at Fort Yukon, AK. One Standard Instrument Approach Procedure (SIAP) is being amended and three new SIAPs are being developed for the Fort Yukon Airport. A Departure Procedure (DP) and a Direction Finding (DF) procedure (used by Flight Service Station personnel) is also being amended. Adoption of this proposal would result in revision of existing Class E airspace upward from the surface, from 700 feet (ft.) and 1,200 ft. above the surface, at Fort Yukon Airport, Fort Yukon, AK.
Proposed Revision of Class E Airspace; Noatak, AK
This action proposes to revise Class E airspace at Noatak, AK. One Standard Instrument Approach Procedure (SIAP) is being amended for the Noatak Airport at Noatak, AK. A Departure Procedure (DP) is also being amended. Adoption of this proposal would result in revision of existing Class E airspace upward, from 700 feet (ft.) and 1,200 ft. above the surface, at the Noatak Airport, Noatak, AK.
Airworthiness Directives; Turbomeca Arrius 2F Turboshaft Engines
The FAA is superseding an existing airworthiness directive (AD) for Turbomeca Arrius 2F turboshaft engines. That AD currently requires removing from service certain serial number (SN) fuel control units (FCUs) or replacing the constant delta pressure (delta P) diaphragm in those FCUs. This AD requires replacing all FCUs not incorporating modification Tf 55 with FCUs that incorporate modification Tf 55. This AD results from the European Aviation Safety Agency (EASA) and Turbomeca expanding the applicability to the full population of FCUs installed on Arrius 2F turboshaft engines. FCUs not incorporating modification Tf 55 are susceptible to having an improperly assembled constant delta P diaphragm. We are issuing this AD to prevent an uncommanded engine in-flight shutdown on a single-engine helicopter, resulting in a forced autorotation landing or an accident.
Airworthiness Directives; Pratt & Whitney Canada (P&WC) PW535A Turbofan Engines; Correction
The FAA is correcting airworthiness directive (AD) 2006-24-08. That AD applies to Pratt & Whitney Canada (P&WC) PW535A turbofan engines. We published that AD in the Federal Register on December 4, 2006 (71 FR 70284). The fuel manifold part number (P/N) 3025267-01 listed in paragraph (c) is incorrect. This document corrects that P/N. In all other respects, the original document remains the same.
Airworthiness Directives; Reims Aviation S.A. Model F406 Airplanes
We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued 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:
Airworthiness Directives; Dornier Luftfahrt GmbH Model 228 Series Airplanes
We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued 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:
Airworthiness Directives; British Aerospace Regional Aircraft Model HP.137 Jetstream Mk.1, Jetstream Series 200, Jetstream Series 3101, and Jetstream Model 3201 Airplanes
We are superseding an existing airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued 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:
RTCA Government/Industry Air Traffic Management Advisory Committee
The FAA is issuing this notice to advise the public of a meeting of RTCA Government/Industry Air Traffic Management Advisory Committee.
Proposed Establishment of Class E Airspace; Centreville, AL
This notice proposed to establish Class E airspace at Centreville, AL. An Area Navigation (RNAV) Global Positioning System (GPS) Standard Instrument Approach Procedure (SIAP) Runway (RWY) 10 has been developed for Bibb County Airport. As a result, controlled airspace extending upward from 700 feet Above Ground Level (AGL) is needed to contain the SIAP and for Instrument Flight Rules (IFR) operations at Bibb 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.
Proposed Establishment of Class E Airspace; Vero Beach, FL
This notice proposes to establish Class E2 airspace at Vero Beach, FL. As a result of an evaluation, it has been determined Class E Airspace Designated as Surface Areas should be established for Vero Beach Municipal Airport. Miami Air Route Traffic Control Center has communications capabilities and weather observation reporting when the Vero Beach tower is closed. Therefore, the airport will meet criteria for Class E2 airspace. Class E2 surface area airspace is required when the control tower is closed to contain Standard Instrument Approach Procedures (SIAPs) and other Instrument Flight Rules (IFR) operations at the airport. This action would establish Class E2 airspace extending upward from the surface to and including 2,500 feet MSL within a 4.2- mile radius of the airport and within 3.2 miles each side of the 261[deg] bearing from the Vero Beach Nondirectional Radio Beacon (NDB) extending from the 4.2 mile radius of the Vero Beach Municipal Airport to 7 miles west of the NDB.
Public Notice for Waiver of Aeronautical Land-Use Assurance Rickenbacker International Airport Columbus, OH
The Federal Aviation Administration (FAA) is considering a proposal to change a portion of the airport from aeronautical use to non-aeronautical use and to authorize the release of 188.653 acres of vacant airport property previously used for agricultural purposes for the proposed development of bulk warehouse/distribution facilities as a component of the Rickenbacker Global Logistics Park. The land was acquired by the Rickenbacker Port Authority through three Quitclaim Deeds from the United States of American dated March 30, 1984, September 22, 2004 (amended and restated August 26, 2005) and May 16, 2005. There are no impacts to the airport by allowing the airport to dispose of the property. Approval does not constitute a commitment by the FAA to financially assist in the disposal of the subject airport property nor a determination of eligibility for grant-in-aid funding from the FAA. The CRAA will receive $4,245,000 for the parcel. In accordance with section 47107(h) of title 49, United States Code, this notice is required to be published in the Federal Register 30 days before modifying the land-use assurance that requires the property to be used for an aeronautical purpose.
Airworthiness Directives; Eurocopter France Model EC130 B4 Helicopters
This document proposes adopting a new airworthiness directive (AD) for Eurocopter France (Eurocopter) Model EC 130 B4 helicopters, with certain twist grip assemblies installed. This proposal would require inspecting the pilot and co-pilot collective levers for proper bonding between the twist grip drive tubes and the control pinions and if debonding is present, replacing the collective levers before further flight. This proposal is prompted by one incident in which the engine remained at idle speed although the twist grip had been turned to the flight position. The actions specified by this proposed AD are intended to detect debonding between the twist grip drive tubes and the control pinions on the pilot and co-pilot collective levers to prevent loss of cockpit throttle control of the engine, and subsequent loss of control of the helicopter.
Airworthiness Directives; Pratt & Whitney (PW) PW4164, PW4168, and PW4168A Turbofan Engines
The FAA proposes to adopt a new airworthiness directive (AD) for PW PW4164, PW4168, and PW4168A turbofan engines with certain low pressure turbine (LPT) stage 4 disks, part number (P/N) 51N404, installed. This proposed AD would require removing certain LPT stage 4 disks, listed by serial number at the next piece-part exposure or within 7,500 cycles-since-new (CSN), whichever occurs first. This proposed AD results from a report of improperly manufactured LPT stage 4 disks. We are proposing this AD to prevent an uncontained engine failure due to low-cycle fatigue (LCF), which could result in damage to the airplane.
Airworthiness Directives; Eurocopter France Model EC130 B4 Helicopters
This amendment proposes adopting a new airworthiness directive (AD) for Eurocopter France (ECF) Model EC130 B4 helicopters. This proposal would require, within 100 hours time-in-service (TIS), modifying and testing the wiring of the battery overheat sensing circuit. This proposal is prompted by a malfunction in the battery overheat sensing circuit found during a scheduled inspection. The actions specified by this proposed AD are intended to correct the connection of the thermal switch to the cockpit indicator light, to notify the flight crew of an overheated battery, and to prevent a thermal runaway of the battery, an in-flight fire, and subsequent loss of control of the helicopter.
Ninth Meeting: RTCA Special Committee 206/EUROCAE WG 76 Plenary
The FAA is issuing this notice to advise the public of a meeting of RTCA Special Committee 206: Aeronautical Information Services Data Link.
Airworthiness Directives; British Aerospace Regional Aircraft Model Jetstream HP.137 Jetstream Mk.1, Jetstream Series 200, Jetstream Series 3101, and Jetstream Model 3201 Airplanes
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:
Airworthiness Directives; Pacific Aerospace Limited, Model 750XL Airplanes
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:
Airworthiness Directives; British Aerospace Regional Aircraft Jetstream Model 3201 Airplanes
We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued 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:
Airworthiness Directives; Diamond Aircraft Industries GmbH Model DA 40 and DA 40F Airplanes
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:
Human Space Flight Requirements for Crew and Space Flight Participants
This notice announces the Office of Management and Budget's (OMB) approval of the information collection requirement in the final rule published on December 15, 2006. The sections of the final rule pending approval of this information collection request are effective upon publication of this notice.
Petitions for Exemption; Summary of Petitions Received
This notice contains a summary of a certain 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 any petition or its final disposition.
Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-145LR, -145XR, and -145MP Airplanes; and Model EMB-135BJ and -135LR Airplanes
The FAA is adopting a new airworthiness directive (AD) for certain EMBRAER Model EMB-145LR, -145XR, and -145MP airplanes; and Model EMB-135BJ and -135LR airplanes. This AD requires replacing the electrical bonding clamps inside the fuel tanks and adjacent areas. This AD results from a report of the failure of a fitting clamp of an electrical bonding cable for the fuel tubing. We are issuing this AD to prevent loss of bonding protection in the interior of the fuel tanks or adjacent areas, and a consequent potential source of ignition in a fuel tank and possible fire or explosion.
Airworthiness Directives; Cessna Aircraft Company Models 208 and 208B Airplanes
The FAA is adopting a new airworthiness directive (AD) to supersede AD 2006-06-06, which applies to certain Cessna Aircraft Company (Cessna) Models 208 and 208B airplanes. AD 2006-06-06 currently requires you to incorporate information into the applicable section of the Airplane Flight Manual (AFM) and Pilot's Operating Handbook (POH) and requires you to install placards. Since we issued AD 2006-06-06, Cessna issued new S1 Known Icing Equipment AFM supplements and developed a low airspeed awareness system. Consequently, this AD requires you to incorporate the applicable AFM supplement revision and temporarily retain the requirements of AD 2006-06-06 until the above revisions are incorporated. One of the AFM requirements is the installation of a functional low airspeed awareness system to operate the airplane in known icing conditions. We are issuing this AD to assure that the pilot has enough information and the necessary equipment to prevent loss of control of the airplane while in-flight during icing conditions.
Airworthiness Directives; Boeing Model 747-400 Series Airplanes
The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 747-400 series airplanes. This AD requires repetitive inspections for any crack in the upper deck floor beam at station 400, which include inspecting the floor beam web and chords, certain fastener holes at the intersection of the floor beam and frame on both sides of the airplane, and certain floor panel attachment fastener holes at the floor beam upper chords. This AD also requires corrective action if necessary. This AD results from several reports indicating that fatigue cracking was found in upper deck floor beams made from 7000 series aluminum alloy. We are issuing this AD to detect and correct cracking in the upper deck floor beam at station 400, which could extend and sever the floor beam. A severed floor beam could result in loss of controllability and rapid decompression of the airplane.
Airworthiness Directives; APEX Aircraft (Type Certificate No. A36EU Formerly Held by AVIONS MUDRY et CIE) Model CAP 10 B Airplanes
We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued 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:
Airworthiness Directives; Cirrus Design Corporation Models SR20 and SR22 Airplanes
We propose to adopt a new airworthiness directive (AD) for certain Cirrus Design Corporation (CDC) Models SR20 and SR22 airplanes. This proposed AD would require you to replace the pick-up collar support and nylon screws, of the Cirrus Airplane Parachute System (CAPS), with a new design pick-up collar support and custom tension screws. This proposed AD results from a CDC report of an in-flight CAPS activation where the parachute failed to successfully deploy. We are proposing this AD to correct pick-up collar support fasteners of the CAPS, which could result in the premature separation of the collar. This condition, if not corrected, could result in the parachute failing to successfully deploy (CAPS failure).
Airworthiness Directives; Allied Ag Cat Productions, Inc. (Type Certificate No. 1A16 Formerly Held by Schweizer Aircraft Corp.) G-164 Series Airplanes
We propose to supersede Airworthiness Directive (AD) 82-07-04, which applies to certain Allied Ag Cat Productions, Inc. (Ag Cat) G-164 series airplanes. AD 82-07-04 currently requires you to modify the fuel shut-off valve control by installation of a new stop-plate. Since we issued AD 82-07-04, we have determined the need to add airplane models and serial numbers that were not previously included in the applicability. Consequently, this proposed AD would retain the actions of AD 82-07-04 and add airplane models and serial numbers to the applicability. We are proposing this AD to prevent turning the fuel shut-off valve clockwise past the ``ON'' position stop which, if not corrected, could allow the fuel valve to be rotated to an unplacarded ``OFF'' position. This condition could lead to reduced fuel flow and consequent loss of engine power.
Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-135BJ Airplanes
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: It has been found cases in which the drain mast of the water and waste system does not meet the SFAR-88 (Special Federal Aviation Regulation No. 88) requirements. In case of fuel leakage or fuel vapor release, the proximity of this mast with the fuel tank may cause fuel ignition, leading to a possible tank explosion.
Airworthiness Directives; Airbus Model A300-600 Series Airplanes and Model A310 Series Airplanes
The FAA proposes to supersede an existing airworthiness directive (AD) that applies to certain Airbus Model A300-600, A310-200, and A310-300 series airplanes. The existing AD currently requires inspecting for certain serial numbers on elevators, and doing a detailed inspection, visual inspection with a low-angle light, and tap- test inspection of the upper and lower surfaces of the external skins on certain identified elevators for any damage (i.e., debonding of the graphite fiber reinforced plastic/Tedlar film protection, bulges, debonding of the honeycomb core to the carbon fiber reinforced plastic, abnormal surface reflections, and torn-out plies), and doing corrective actions if necessary. This proposed AD would also require inspecting for damage of the identified elevators in accordance with a new repetitive inspection program, at new repetitive intervals; and would provide an optional terminating action for the repetitive inspections. This proposed AD results from reports of damage caused by moisture/water inside the elevator. We are proposing this AD to detect and correct debonding of the skins on the elevators, which could cause reduced structural integrity of an elevator and reduced controllability of the airplane.
Airworthiness Directives; Boeing Model 757-200 and 757-300 Series Airplanes
The FAA proposes to adopt a new airworthiness directive (AD) for certain Boeing Model 757-200 and 757-300 series airplanes. This proposed AD would require installing a copper bonding jumper between a ground and the clamp on the tube of the forward and aft gray water composite drain masts. This proposed AD results from a report of charred insulation blankets and burned wires around the forward gray water composite drain mast found during an inspection of the forward cargo compartment on a Model 767-300F airplane. We are proposing this AD to prevent a fire near a composite drain mast and possible disruption of the electrical power system due to a lightning strike on a composite drain mast, which could result in the loss of several functions essential for safe flight.
Standard Instrument Approach Procedures, Weather Takeoff Minimums; Miscellaneous Amendments
This amendment establishes, amends, suspends, or revokes Standard Instrument Approach Procedures (SIAPs) and/or Weather Takeoff Minimums 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, addition of new obstacles, or changes in 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.
Notice of the U.S. Air Force Supplemental Final Environmental Impact Statement and FAA Approval of the Record of Decision for the Realistic Bomber Training Initiative (RBTI)
The FAA is announcingadoption of the United States Air Force (USAF) Final Supplemental Environmental Impact Statement (SEIS) for the Realistic Bomber Training Initiative (RBTI), and approval of the FAA Record of Decision (ROD). The USAF proposal was to create airspace that allows B-52 and B-1 aircrews to receive much needed realistic combat training while maximizing their training time. RBTI includes the Lancer Military Operating Area (MOA) and the Instrument Military Training Route 178 (IR-178).
Notice of Adoption of the U.S. Air Force Final Environmental Impact Statement and Approval of the Federal Aviation Administration Record of Decision for the New Mexico Training Range Initiative (NMTRI)
The FAA is announcing its Adoption of the United States Air Force (USAF) Final Environmental Impact Statement (FEIS) for the New Mexico Training Range Initiative and approval of the FAA Record of Decision (ROD). The New Mexico Training Range Initiative (NMTRI) is the USAF initiative to create airspace that allows mainly F-16 and aircrews to receive much needed realistic combat training while maximizing their training time. NMTRI includes the Pecos MOA complex.
Modification of Class E Airspace; Canby, MN
This action amends Title 14 Code of Federal Regulations, part 71 (14 CFR 71) by modifying Class E airspace at Canby, Myers Field, MN. Standard Instrument Approach Procedures have been developed by Canby, Myers Field, MN. Additional controlled airspace extending upward from the surface and upward from 700 feet above the surface of the earth is needed to contain aircraft executing these approaches. This action increases the area of the existing controlled airspace for Canby, Myers Field, MN.
Modification of Class E Airspace; Manhattan, KS
This action amends Title 14 Code of Federal Regulations, part 71 (14 CFR 71) by modifying the legal description of Class D airspace and Class E airspace at Manhattan Municipal Airport, KS. The establishment of adjacent Class D airspace at Fort Riley, Marshall Army Airfield, KS requires this modification. The intended effect of this rule is to provide controlled airspace of appropriate dimensions to protect aircraft operating in these areas.
Modification of Class E Airspace; Monticello, IA
This action amends Title 14 Code of Federal Regulations, part 71 (14 CFR 71) by modifying the Class E airspace area at Monticello Regional Airport, IA. The cancellation of the Non Directional Beacon (NDB) Instrument Approach Procedure (IAP) and subsequent decommissioning of the Monticello NDB requires modification of the Class E airspace area extending upward from 700 feet above the surface of the earth. The intended effect of this rule is to provide controlled airspace of appropriate dimensions to protect aircraft executing Standard Instrument Approach Procedures (SIAP) to Monticello Regional Airport, IA.
Modification of Class E Airspace; Marshalltown, IA
This action amends Title 14 Code of Federal Regulations, part 71q (14 CFR 71) by modifying the Class E airspace area at Marshalltown Municipal Airport, IA. The cancellation of the Non Directional Beacon (NDB) Instrument Approach Procedure (IAP) and subsequent decommissioning of the Marshalltown NDB requires modification of the Class E airspace area extending upward from 700 feet above the surface of the earth. The intended effect of this rule is to provide controlled airspace of appropriate dimensions to protect aircraft executing Standard Instrument Approach Procedures (SIAP) to Marshalltown Municipal Airport, IA.
Modification of Class E Airspace; Canby, MN
This action amends Title 14 Code of Federal Regulations, part 71 (14 CFR part 71) by modifying Class E airspace at Canby, Myers Field, MN. Standard Instrument Approach Procedures have been developed for Canby, Myers Field, MN. Additional controlled airspace extending upward from the surface and upward from 700 feet above the surface of the earth is needed to contain aircraft executing these approaches. This action increases the area of the existing controlled airspace for Canby, Myers Field, MN.
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