Federal Aviation Administration January 2011 – Federal Register Recent Federal Regulation Documents

Results 51 - 100 of 124
Amendment of VOR Federal Airways V-2 and V-21; Hawaii
Document Number: 2011-823
Type: Rule
Date: 2011-01-18
Agency: Federal Aviation Administration, Department of Transportation
This action amends two VHF Omnidirectional Range (VOR) Federal airway legal descriptions in the State of Hawaii. The FAA is taking this action to remove exclusions to restricted airspace areas that have been removed from the National Airspace System (NAS).
Airworthiness Directives; Eurocopter France (Eurocopter) Model SA-365N, SA-365N1, AS-365N2, AS 365 N3, and SA-366G1 Helicopters
Document Number: 2011-720
Type: Proposed Rule
Date: 2011-01-18
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for the specified Eurocopter model helicopters. This proposed AD would require an initial and recurring inspections of the inner angles and flanges of the 9-degree frame on the right-hand (RH) and left-hand (LH) sides for a crack. If a crack is found, this proposed AD would require, before further flight, repairing the frame. This proposed AD is prompted by the discovery of a crack in the 9-degree frame of a Eurocopter Model AS-365N2 helicopter. These cracks could also develop on the other specified model helicopters because they contain the same 9-degree frame. The actions specified by this proposed AD are intended to detect a crack in the 9-degree frame to prevent loss of structural integrity and subsequent loss of control of the helicopter.
Establishment of Class E Airspace; Lucin, UT
Document Number: 2011-593
Type: Rule
Date: 2011-01-18
Agency: Federal Aviation Administration, Department of Transportation
This action makes a minor correction to a final rule published in the Federal Register July 8, 2010, that establishes Class E en route domestic airspace for the Lucin VORTAC, Lucin, UT.
Notice of Passenger Facility Charge (PFC) Approvals and Disapprovals
Document Number: 2011-347
Type: Notice
Date: 2011-01-18
Agency: Federal Aviation Administration, Department of Transportation
The FAA publishes a monthly notice, as appropriate, of PFC approvals and disapprovals under the provisions of the Aviation Safety and Capacity Expansion Act of 1990 (Title IX of the Omnibus Budget Reconciliation Act of 1990) (Pub. L. 101-508) and Part 158 of the Federal Aviation Regulations (14 CFR Part 158). This notice is published pursuant to paragraph d of Sec. 158.29.
Amendment of Class E Airspace; Kwajalein Island, Marshall Islands, RMI
Document Number: 2011-867
Type: Rule
Date: 2011-01-14
Agency: Federal Aviation Administration, Department of Transportation
This action corrects a final rule; technical amendment published in the Federal Register. In that rule, errors were made in the airspace description. This action corrects those errors.
Eighty-Fourth Meeting: RTCA Special Committee 159: Global Positioning System (GPS)
Document Number: 2011-818
Type: Notice
Date: 2011-01-14
Agency: Federal Aviation Administration, Department of Transportation
The FAA is issuing this notice to advise the public of a meeting of RTCA Special Committee 159: Global Positioning System (GPS).
Proposed Amendment of Class E Airspace; Pueblo, CO
Document Number: 2011-812
Type: Proposed Rule
Date: 2011-01-14
Agency: Federal Aviation Administration, Department of Transportation
This action proposes to amend Class E airspace at Pueblo Memorial Airport, Pueblo, CO. Additional controlled airspace is necessary to facilitate vectoring of Instrument Flight Rules (IFR) traffic from en route airspace to Pueblo Memorial Airport. The FAA is proposing this action to enhance the safety and management of aircraft operations at the airport.
Receipt of Noise Compatibility Program and Request for Review for San Diego International Airport, San Diego, CA
Document Number: 2011-804
Type: Notice
Date: 2011-01-14
Agency: Federal Aviation Administration, Department of Transportation
The Federal Aviation Administration (FAA) announces that it is reviewing a proposed noise compatibility program that was submitted for San Diego International Airport under the provisions of 49 U.S.C. 47501 et seq. (the Aviation Safety and Noise Abatement Act, hereinafter referred to as ``the Act'') and 14 CFR part 150 by the San Diego County Regional Airport Authority, San Diego County, California. This program was submitted subsequent to a determination by FAA that associated noise exposure maps submitted under 14 CFR Part 150 for San Diego International Airport were in compliance with applicable requirements, effective November 10, 2009, 74 FR 66400-66401. The proposed noise compatibility program will be approved or disapproved on or before July 3, 2011.
Airworthiness Directives; Rolls-Royce plc RB211-Trent 800 Series Turbofan Engines
Document Number: 2011-775
Type: Proposed Rule
Date: 2011-01-14
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for the products listed above. This proposed 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; MD Helicopters, Inc. (MDHI) Model MD900 Helicopters
Document Number: 2011-726
Type: Proposed Rule
Date: 2011-01-14
Agency: Federal Aviation Administration, Department of Transportation
This document proposes superseding an existing airworthiness directive (AD) for MDHI Model MD900 helicopters. That AD currently requires turning on both Vertical Stabilizer Control System (VSCS) switches and turning off the autopilot (AP/SAS) switch; pulling certain AP/SAS circuit breakers; installing a placard near the AP/SAS master switch; installing an airspeed limitation placard on the instrument panel; and making changes to the Rotorcraft Flight Manual (RFM). This action would retain those requirements and would provide an option of replacing each affected tube adapter with a newly-designed tube adapter, which would provide terminating action for the unsafe condition. This proposal is prompted by the manufacturer introducing an improved, newly-designed tube adapter. The actions specified by this AD are intended to prevent loss of yaw control and subsequent loss of control of the helicopter.
Petition for Exemption; Summary of Petition Received
Document Number: 2011-717
Type: Notice
Date: 2011-01-14
Agency: Federal Aviation Administration, Department of Transportation
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.
Agency Information Collection Activities: Requests for Comments; Clearance of Renewed Approval of Information Collection(s): Flight Engineers and Flight Navigators.
Document Number: 2011-594
Type: Notice
Date: 2011-01-13
Agency: Federal Aviation Administration, Department of Transportation
In accordance with the Paperwork Reduction Act of 1995, FAA invites public comments about our intention to request the Office of Management and Budget (OMB) approval to renew an information collection. The Federal Register Notice with a 60-day comment period soliciting comments on the following collection of information was published on September 22, 2010, vol. 75, no. 183, page 57828-57829. Information collected is used to determine certification eligibility of Flight Engineers and Flight Navigators.
Airworthiness Directives; Airbus Model A330-300, A340-200, and A340-300 Series Airplanes
Document Number: 2011-586
Type: Proposed Rule
Date: 2011-01-13
Agency: Federal Aviation Administration, Department of Transportation
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; BAE SYSTEMS (OPERATIONS) LIMITED Model BAe 146 Airplanes, and Model Avro 146-RJ Airplanes
Document Number: 2011-585
Type: Proposed Rule
Date: 2011-01-13
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for the products listed above that would supersede an existing AD. 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; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model ERJ 170 and ERJ 190 Airplanes
Document Number: 2011-584
Type: Proposed Rule
Date: 2011-01-13
Agency: Federal Aviation Administration, Department of Transportation
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; M7 Aerospace LP (Type Certificate Previously Held by Fairchild Aircraft Incorporated) Models SA26-AT, SA26-T, SA226-AT, SA226-T, SA226-T(B), SA226-TC, SA227-AC (C-26A), SA227-AT, SA227-BC (C-26A), SA227-CC, SA227-DC (C-26B), and SA227-TT Airplanes
Document Number: 2011-457
Type: Rule
Date: 2011-01-12
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for the products listed above. This AD requires repetitively inspecting the cockpit heated windshields for damage and replacing damaged windshields. This AD was prompted by reports from the windshield manufacturer of inner glass ply fracture. We are issuing this AD to detect and correct damage to the cockpit heated windshield, which could result in failure of the windshield with consequent rapid cabin decompression and loss of control of the airplane.
Procedures for Protests and Contracts Dispute
Document Number: 2011-397
Type: Proposed Rule
Date: 2011-01-12
Agency: Federal Aviation Administration, Department of Transportation
This action would update, simplify, and streamline the current regulations governing the procedures for bid protests brought against the FAA and contract disputes brought against or by the FAA. It would also add a voluntary dispute avoidance and early resolution process. This action is necessary to ensure the regulations reflect the changes that have evolved since 1999 when they were first implemented. The intended effect of this action is to streamline and further improve the protest and dispute process.
Airworthiness Directives; The Boeing Company Model 757 Airplanes
Document Number: 2011-371
Type: Rule
Date: 2011-01-12
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for Model 757-200, -200PF, -200CB, and -300 series airplanes. This AD requires an inspection of the two spring arms in the spin brake assemblies in the nose wheel well to determine if the spring arms are made of aluminum or composite material, and repetitive related investigative/corrective actions if necessary. This AD also provides options for terminating the repetitive actions. This AD results from reports of cracked and broken aluminum springs. We are issuing this AD to detect and correct cracked or broken springs. A cracked or broken spring could separate from the airplane and result in potential hazard to persons or property on the ground, or ingestion into the engine with engine damage and potential shutdown, or damage to the airplane.
Modification of Class E Airspace; Show Low, AZ
Document Number: 2011-356
Type: Rule
Date: 2011-01-12
Agency: Federal Aviation Administration, Department of Transportation
This action will amend Class E airspace at Show Low, AZ, to accommodate aircraft using a new Area Navigation (RNAV) Global Positioning System (GPS) Standard Instrument Approach Procedures at Show Low Regional Airport. This will improve the safety and management of Instrument Flight Rules (IFR) operations at the airport.
Establishment of Class E Airspace; Panguitch, UT
Document Number: 2011-353
Type: Rule
Date: 2011-01-12
Agency: Federal Aviation Administration, Department of Transportation
This action will establish Class E airspace at Panguitch, UT, to accommodate aircraft using a new Area Navigation (RNAV) Global Positioning System (GPS) Standard Instrument Approach Procedures at Panguitch Municipal Airport. This will improve the safety and management of Instrument Flight Rules (IFR) operations at the airport.
Airworthiness Directives; Short Brothers PLC Model SD3 Airplanes
Document Number: 2011-30
Type: Rule
Date: 2011-01-12
Agency: Federal Aviation Administration, Department of Transportation
We are superseding an existing airworthiness directive (AD) that applies to the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued by an airworthiness authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as
Airworthiness Directives; The Boeing Company Model MD-11 and MD-11F Airplanes
Document Number: 2011-271
Type: Rule
Date: 2011-01-12
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for the products listed above. This AD requires a one-time inspection to detect damage of the wire assemblies of the tail tank fuel system, a wiring change, and corrective actions if necessary. This AD also requires, for certain airplanes, a general visual inspection for correct installation of the self-adhering high-temperature electrical insulation tape; installation of a wire assembly support bracket and routing wire assembly; changing wire supports; and installation of a wire protection bracket. This AD was prompted by fuel system reviews conducted by the manufacturer. We are issuing this AD to detect and correct a potential of ignition sources inside fuel tanks, which, in combination with flammable vapors, could result in a fuel tank fire or explosion, and consequent loss of the airplane.
Airworthiness Directives; The Boeing Company Model DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), DC-9-87 (MD-87), and MD-88 Airplanes
Document Number: 2010-33345
Type: Rule
Date: 2011-01-12
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for the products listed above. This AD requires installing fuel level float and pressure switch in-line fuses on the wing forward spars and forward and aft auxiliary fuel tanks, depending on the airplane configuration. This AD was prompted by 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, could result in fuel tank explosions and consequent loss of the airplane.
Airworthiness Directives; Pilatus Aircraft Ltd. Models PC-6, PC-6-H1, PC-6-H2, PC-6/350, PC-6/350-H1, PC-6/350-H2, PC-6/A, PC-6/A-H1, PC-6/A-H2, PC-6/B-H2, PC-6/B1-H2, PC-6/B2-H2, PC-6/B2-H4, PC-6/C-H2, and PC-6/C1-H2 Airplanes
Document Number: 2010-33333
Type: Rule
Date: 2011-01-12
Agency: Federal Aviation Administration, Department of Transportation
We are revising 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:
Airworthiness Directives; Bombardier, Inc. Model CL-600-2C10 (Regional Jet Series 700, 701 & 702) Airplanes, Model CL-600-2D15 (Regional Jet Series 705) Airplanes, and Model CL-600-2D24 (Regional Jet Series 900) Airplanes
Document Number: 2011-368
Type: Proposed Rule
Date: 2011-01-11
Agency: Federal Aviation Administration, Department of Transportation
We are revising an earlier NPRM for the products listed above. This action revises the earlier NPRM by expanding the scope. 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; The Boeing Company Model 737-600, -700, -700C, -800, -900, and -900ER Series Airplanes
Document Number: 2011-367
Type: Proposed Rule
Date: 2011-01-11
Agency: Federal Aviation Administration, Department of Transportation
The FAA is revising an earlier NPRM for an airworthiness directive (AD) that applies to all Boeing Model 737-600, -700, -700C, - 800, and -900 series airplanes. The original NPRM would have superseded an existing AD that currently requires reviewing the airplane maintenance records to determine whether an engine has been removed from the airplane since the airplane was manufactured. For airplanes on which an engine has been removed, the existing AD also requires an inspection of the aft engine mount to determine if the center link assembly is correctly installed, and follow-on actions if necessary. The original NPRM proposed to require the same actions for airplanes on which the engine has not been previously removed. The original NPRM resulted from reports indicating that operators found that the center link assembly for the aft engine mount was reversed on several airplanes that had not had an engine removed since delivery. This new action revises the original NPRM by expanding the applicability to include Model 737-900ER airplanes. We are proposing this supplemental NPRM to prevent increased structural loads on the aft engine mount, which could result in failure of the aft engine mount and consequent separation of the engine from the airplane.
Amendment of Class E Airspace; Horseshoe Bay, TX
Document Number: 2011-205
Type: Rule
Date: 2011-01-11
Agency: Federal Aviation Administration, Department of Transportation
This action amends Class E airspace for Horseshoe Bay, TX. Decommissioning of the Horseshoe Bay Resort non-directional beacon (NDB) at Horseshoe Bay Resort Airport, Horseshoe Bay, TX, has made this action necessary to enhance the safety and management of Instrument Flight Rule (IFR) operations at the airport.
Amendment of Class D Airspace; Fort Worth NAS JRB (Carswell Field), TX
Document Number: 2011-204
Type: Rule
Date: 2011-01-11
Agency: Federal Aviation Administration, Department of Transportation
This action amends the geographic coordinates within the Fort Worth Naval Air Station (NAS) JRB (Carswell Field), TX, area and renames the navigation aids, at the request of the U.S. Navy, that are listed in the description. This action does not change the boundaries or operating requirements of the airspace.
Amendment of Class E Airspace; Sturgis, KY
Document Number: 2011-203
Type: Rule
Date: 2011-01-11
Agency: Federal Aviation Administration, Department of Transportation
This action amends Class E airspace at Sturgis, KY. The Tradewater Non-Directional Beacon (NDB) has been decommissioned and new Standard Instrument Approach Procedures (SIAPs) have been developed for Sturgis Municipal Airport. This action enhances the safety and airspace management of Instrument Flight Rules (IFR) operations at the airport.
Amendment of Class E Airspace; Savannah, TN
Document Number: 2011-202
Type: Rule
Date: 2011-01-11
Agency: Federal Aviation Administration, Department of Transportation
This action amends Class E airspace at Savannah, TN. The Pinhook Non-Directional Beacon (NDB) has been decommissioned and new Standard Instrument Approach Procedures (SIAPs) have been developed for Savannah-Hardin County Airport. This action enhances the safety and airspace management of Instrument Flight Rules (IFR) operations at the airport.
Airworthiness Directives; The Boeing Company Model 757-200, -200CB, and -300 Series Airplanes
Document Number: 2011-51
Type: Rule
Date: 2011-01-10
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for the products listed above. This AD requires repetitive inspections for cracking of the fuselage skin of the crown skin panel along the chem- milled step at stringers S-4 left and S-4 right, from stations (STA) 297 through 439, and repair if necessary. This AD also includes terminating action for the repetitive inspections of the repaired areas only. This AD was prompted by reports of cracking in the fuselage skin of the crown skin panel. We are issuing this AD to detect and correct fatigue cracking of the fuselage skin of the crown skin panel, which could result in pressure venting and consequent rapid decompression of the airplane.
Proposed Establishment of Class E Airspace; Creighton, NE
Document Number: 2011-213
Type: Proposed Rule
Date: 2011-01-10
Agency: Federal Aviation Administration, Department of Transportation
This action proposes to establish Class E airspace at Creighton, NE. Controlled airspace is necessary to accommodate new Standard Instrument Approach Procedures (SIAP) at Creighton Municipal Airport. The FAA is taking this action to enhance the safety and management of Instrument Flight Rules (IFR) operations for SIAPs at the airport.
Proposed Amendment of Class E Airspace; Mosby, MO
Document Number: 2011-212
Type: Proposed Rule
Date: 2011-01-10
Agency: Federal Aviation Administration, Department of Transportation
This action proposes to amend Class E airspace at Mosby, MO. Decommissioning of the Mosby non-directional beacon (NDB) at Midwest National Air Center Airport, Mosby, MO, has made this action necessary for the safety and management of Instrument Flight Rules (IFR) operations at Midwest National Air Center Airport.
Proposed Amendment of Class E Airspace; Kokomo, IN
Document Number: 2011-210
Type: Proposed Rule
Date: 2011-01-10
Agency: Federal Aviation Administration, Department of Transportation
This supplemental notice of proposed rulemaking would expand Class E airspace to include the Regional Health System Heliport, Kokomo, IN. In an NPRM published in the Federal Register August 18, 2010, the FAA proposed to amend controlled airspace at Kokomo Municipal Airport, Kokomo, IN. The FAA has reassessed the proposal to include controlled Class E airspace for new standard instrument approach procedures (SIAP) at the heliport. This action is necessary to further the safety and management of Instrument Flight Rules (IFR) operations in the Kokomo, IN area.
Airworthiness Directives; The Boeing Company Model 727, 727C, 727-100, 727-100C, 727-200, and 727-200F Series Airplanes
Document Number: 2011-188
Type: Rule
Date: 2011-01-10
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for the products listed above. This AD requires repetitive detailed inspections of the aft pressure bulkhead web for cracking, and repair if necessary. For certain airplanes, this AD also provides for an optional preventative modification of the aft pressure bulkhead web, which would terminate certain repetitive detailed inspections. This AD was prompted by reports of cracks in the aft pressure bulkhead web. We are issuing this AD to detect and correct cracking in the aft pressure bulkhead web, which could adversely affect the structural integrity of the airplane, resulting in difficulty maintaining cabin pressurization or rapid decompression of the airplane.
Airworthiness Directives; Cessna Aircraft Company (Cessna) (Type Certificate A00003SE Previously Held by Columbia Aircraft Manufacturing (Previously The Lancair Company)) Models LC41-550FG and LC42-550FG Airplanes
Document Number: 2010-33336
Type: Rule
Date: 2011-01-10
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for the products listed above. This emergency AD was sent previously to all known U.S. owners and operators of these airplanes. This AD requires obtaining written approval from the Manager, Wichita Aircraft Certification Office (ACO), to operate the airplane. This written approval must clearly state that operation is approved per Emergency AD 2010-26-54. This AD was prompted by a Cessna Model LC41-550FG airplane that suffered a significant structural failure in the wing during a production acceptance flight test. We are issuing this AD to prevent catastrophic failure of the wing due to disbonding of the wing skin from the wing spar.
Airworthiness Directives; Airbus Model A300, A300-600, A310, A318, A319, A320, A321, A330-300, A340-200, A340-300, A340-500, A340-600, and A380-800 Series Airplanes; and Model A330-201, A330-202, A330-203, A330-223, A330-243 Airplanes
Document Number: 2010-33318
Type: Rule
Date: 2011-01-10
Agency: Federal Aviation Administration, Department of Transportation
This document publishes in the Federal Register an amendment adopting airworthiness directive (AD) 2010-02-05 that was sent previously by individual notices to the known U.S. owners and operators of affected airplanes identified above. This AD requires modifying the flight deck door. This AD was prompted by a report indicating that certain equipment of the flight deck door is defective. We are issuing this AD to prevent failure of this equipment, which could jeopardize flight safety.
Standard Instrument Approach Procedures, and Takeoff Minimums and Obstacle Departure Procedures; Miscellaneous Amendments
Document Number: 2010-33224
Type: Rule
Date: 2011-01-10
Agency: Federal Aviation Administration, Department of Transportation
This 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.
Standard Instrument Approach Procedures, and Takeoff Minimums and Obstacle Departure Procedures; Miscellaneous Amendments
Document Number: 2010-33219
Type: Rule
Date: 2011-01-10
Agency: Department of Transportation, Federal Aviation Administration
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.
Airworthiness Directives; GROB-WERKE GMBH & CO KG Models G102 ASTIR CS, G102 CLUB ASTIR III, G102 CLUB ASTIR IIIb, and G102 STANDARD ASTIR III Gliders
Document Number: 2010-32753
Type: Rule
Date: 2011-01-10
Agency: Federal Aviation Administration, Department of Transportation
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; Gulfstream Aerospace Corporation Model G-1159 Airplanes
Document Number: 2011-54
Type: Proposed Rule
Date: 2011-01-06
Agency: Federal Aviation Administration, Department of Transportation
This action withdraws a notice of proposed rulemaking (NPRM) that proposed a new airworthiness directive (AD) to supersede an existing AD, applicable to certain Gulfstream Aerospace Corporation Model G-1159 airplanes. The existing AD requires an inspection to detect cracks or corrosion in the wing structure in the area of Fuselage Station (FS) 452 inboard clothespin attachment fitting, and repair if necessary. The proposed AD would have required repetitive inspections to detect corrosion or cracks in the forward and aft wing attach fittings at FS 345 and 452, respectively, and adjacent wing beam and wing plank areas, and repair if necessary; and the application of corrosion protection treatment. Since the issuance of the NPRM, the Federal Aviation Administration (FAA) has received new data that indicate the aircraft maintenance manual has been revised to include additional inspections that address the unsafe condition detailed in the NPRM and that the full fleet is in compliance with the inspection and applicable repair required by the existing AD. Accordingly, the proposed rule is withdrawn.
Harmonization of Airworthiness Standards for Transport Category Airplanes-Landing Gear Retracting Mechanisms and Pilot Compartment View
Document Number: 2010-33347
Type: Proposed Rule
Date: 2011-01-05
Agency: Federal Aviation Administration, Department of Transportation
The Federal Aviation Administration proposes to amend the airworthiness standards for transport category airplanes on landing gear retracting mechanisms and the pilot compartment view. This proposal would adopt the 1-g stall speed as a reference stall speed instead of the minimum speed obtained in a stalling maneuver, and would add an additional requirement to keep the landing gear and doors in the correct retracted position in flight. This proposal would also revise the requirements for pilot compartment view in precipitation conditions. Adopting these proposals would eliminate regulatory differences between the airworthiness standards of the U.S. and the European Aviation Safety Agency (EASA), without affecting current industry design practices.
Airworthiness Directives; Fokker Services B.V. Model F.28 Mark 1000, 2000, 3000, and 4000 Airplanes
Document Number: 2010-33337
Type: Proposed Rule
Date: 2011-01-05
Agency: Federal Aviation Administration, Department of Transportation
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; Lockheed Martin Corporation/Lockheed Martin Aeronautics Company Model 382, 382B, 382E, 382F, and 382G Airplanes
Document Number: 2010-33335
Type: Proposed Rule
Date: 2011-01-05
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to supersede an existing airworthiness directive (AD) that applies to all Model 382, 382B, 382E, 382F, and 382G airplanes. The existing AD currently 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. That 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 proposed AD would correct certain part number references, add an additional inspection area, and for certain airplanes, require certain actions to be re- accomplished according to revised service information. This proposed AD results from a report of incorrect accomplishment information in the service information cited by the existing AD. We are proposing 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.
Airworthiness Directives; Dassault-Aviation Model FALCON 7X Airplanes
Document Number: 2010-33334
Type: Proposed Rule
Date: 2011-01-05
Agency: Federal Aviation Administration, Department of Transportation
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; Bombardier, Inc. Model CL-600-2A12 (CL-601) and CL-600-2B16 (CL-601-3A, CL-601-3R, and CL-604 Variants) Airplanes
Document Number: 2010-33329
Type: Proposed Rule
Date: 2011-01-05
Agency: Federal Aviation Administration, Department of Transportation
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
Marking Meteorological Evaluation Towers
Document Number: 2010-33310
Type: Proposed Rule
Date: 2011-01-05
Agency: Federal Aviation Administration, Department of Transportation
The FAA is considering revising its current Advisory Circular on Obstruction Marking and Lighting to include guidance for Meteorological Evaluation Towers (METs). These towers are erected in remote and rural areas, often are less than 200 feet above ground level (AGL), and fall outside of FAA regulations governing tall structures and their impact on navigable airspace. The proposed marking guidance would enhance the conspicuity of the towers and address the safety related concerns of low level agricultural operations. The FAA seeks comment on the proposed guidance.
Proposed Modification of the Minneapolis, MN, Class B Airspace Area; Public Meetings
Document Number: 2010-33305
Type: Proposed Rule
Date: 2011-01-05
Agency: Federal Aviation Administration, Department of Transportation
This notice announces four fact-finding informal airspace meetings to solicit information from airspace users and others concerning a proposal to revise the Class B airspace area at Minneapolis, MN. The purpose of these meetings is to provide interested parties an opportunity to present views, recommendations, and comments on the proposal. All comments received during these meetings will be considered prior to any revision or issuance of a notice of proposed rulemaking.
Commercial Space Transportation Advisory Committee-Public Teleconference
Document Number: 2010-33301
Type: Notice
Date: 2011-01-05
Agency: Federal Aviation Administration, Department of Transportation
Pursuant to Section 10(a)(2) of the Federal Advisory Committee Act (Pub. L. 92-463, 5 U.S.C. App. 2), notice is hereby given of a teleconference of the Commercial Space Transportation Advisory Committee (COMSTAC). The teleconference will take place on Thursday, January 20, 2011, starting at 1:30 p.m. Eastern Standard Time. Individuals who plan to participate should contact Susan Lender, DFO, (the Contact Person listed below) by phone or e-mail for the teleconference call in number. The proposed agenda for this teleconference is to review the structure of the COMSTAC Working Groups. The Committee will examine the current Working Groups and discuss whether it should make changes to the current structure. If changes are necessary, what should they be? Interested members of the public may submit relevant written statements for the COMSTAC members to consider under the advisory process. Statements may concern the issues and agenda items mentioned above or additional issues that may be relevant for the U.S. commercial space transportation industry. Interested parties wishing to submit written statements should contact Susan Lender, DFO, (the Contact Person listed below) in writing (mail or e-mail) by January 14, 2011, so that the information can be made available to COMSTAC members for their review and consideration before the January 20, 2011, teleconference. Written statements should be supplied in the following formats: one hard copy with original signature or one electronic copy via e-mail. An agenda will be posted on the FAA Web site at https://www.faa.gov/ go/ast. Individuals who plan to participate and need special assistance should inform the Contact Person listed below in advance of the meeting.
Airworthiness Directives; The Boeing Company Model 737-300, -400, and -500 Series Airplanes
Document Number: 2010-33003
Type: Rule
Date: 2011-01-05
Agency: Federal Aviation Administration, Department of Transportation
We are superseding an existing airworthiness directive (AD) for the products listed above. That AD currently requires repetitive inspections for discrepancies of the fuse pins of the inboard and outboard midspar fittings of the nacelle strut, and corrective actions if necessary. This new AD requires replacing the midspar fuse pins with new, improved fuse pins, which would terminate the repetitive inspections. This AD was prompted by a report of corrosion damage of the chrome runout on the head side found on all four midspar fuse pins of the nacelle strut. Additionally, a large portion of the chrome plate was missing from the corroded area of the shank. We are issuing this AD to prevent damage of the fuse pins of the inboard and outboard midspar fittings of the nacelle strut, which could result in reduced structural integrity of the fuse pins, and consequent loss of the strut and separation of the engine from the airplane.
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