Federal Aviation Administration 2012 – Federal Register Recent Federal Regulation Documents

Results 1,351 - 1,400 of 1,440
Agency Information Collection Activities: Requests for Comments; Clearance of Renewed Approval of Information Collection: Report of Inspections Required by Airworthiness Directives
Document Number: 2012-1843
Type: Notice
Date: 2012-01-27
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 November 22, 2011, vol. 76, no. 225, page 72237. Airworthiness Directives are regulations issued to require correct corrective action to correct unsafe conditions in aircraft, engines, propellers, and appliances. Reports of inspections are often needed when emergency corrective action is taken to determine if the action was adequate to correct the unsafe condition. The respondents are aircraft owners and operators.
Agency Information Collection Activities: Requests for Comments; Clearance of Renewed Approval of Information Collection: ACSEP Evaluation Customer Feedback Report
Document Number: 2012-1842
Type: Notice
Date: 2012-01-27
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 November 22, 2011, vol. 76, no. 225, pages 72236-72237. The information is collected from holders of FAA production approvals and selected suppliers to obtain their input on how well the agency is performing the administration and conduct of the Aircraft Certification Systems Evaluation Program (ACSEP).
Agency Information Collection Activities: Requests for Comments; Clearance of Renewed Approval of Information Collection: Commercial Air Tour Limitations in the Grand Canyon National Park Special Flight Rules Area
Document Number: 2012-1841
Type: Notice
Date: 2012-01-27
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 November 22, 2011, vol. 76, no. 225, page 72239-72240. The FAA uses the information gathered from Grand Canyon National Park air tour operators to monitor their compliance with the Federal regulations.
Agency Information Collection Activities: Requests for Comments; Clearance of Renewed Approval of Information Collection: Certification of Repair Stations
Document Number: 2012-1839
Type: Notice
Date: 2012-01-27
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 November 22, 2011, vol. 76, no. 225, page 72240. Information is collected from applicants who wish to obtain repair station certification. Applicants must submit FAA form 8310-3 to the appropriate FAA flight standards district office for review.
FAA-Approved Portable Oxygen Concentrators; Technical Amendment
Document Number: 2012-1830
Type: Rule
Date: 2012-01-27
Agency: Federal Aviation Administration, Department of Transportation
The FAA is amending regulations relating to operating rules for FAA approved portable oxygen concentrators (POC) onboard aircraft. This document updates the names of two manufacturers of approved POCs listed in the Special Federal Aviation Regulation (SFAR).
Petition for Exemption; Summary of Petition Received
Document Number: 2012-1829
Type: Notice
Date: 2012-01-27
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.
Airworthiness Directives; Thielert Aircraft Engines GmbH Reciprocating Engines
Document Number: 2012-1607
Type: Rule
Date: 2012-01-27
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for all Thielert Aircraft Engines GmbH (TAE) TAE 125-02-99 and TAE 125-02-114 reciprocating engines. This AD was prompted by in-flight engine shutdown incidents reported on airplanes equipped with TAE 125 engines. We are issuing this AD to prevent in- flight engine shutdown, which could result in loss of control of the airplane.
Airworthiness Directives; The Boeing Company Airplanes
Document Number: 2012-838
Type: Rule
Date: 2012-01-25
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for certain Model 767-200 and 767-300 series airplanes. This AD was prompted by reports of water accumulation in the forward lower lobe of the forward cargo compartment. This AD requires installing cargo bulkhead supports, ceiling supports, a secondary dam support, drainage tubing, and ceiling panels to the forward lower lobe in the forward cargo compartment. We are issuing this AD to prevent water from accumulating in the forward lower lobe of the forward cargo compartment and entering the adjacent electronic equipment bay, which could result in an electrical short and the potential loss of several functions essential for safe flight.
Revision of Compulsory Reporting Points; Alaska
Document Number: 2012-1394
Type: Rule
Date: 2012-01-25
Agency: Federal Aviation Administration, Department of Transportation
This action revises the published description of two low altitude Alaskan compulsory reporting points; one in the vicinity of Homer and the other in the vicinity of Kenai. Specifically, the FAA is revising the description of CLAMS and SKILA to address recent technical adjustments to their actual locations.
Airworthiness Directives; 328 Support Services GmbH Airplanes
Document Number: 2012-1126
Type: Rule
Date: 2012-01-25
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for all 328 Support Services GmbH (Type Certificate previously held by AvCraft Aerospace GmbH; Fairchild Dornier GmbH; Dornier Luftfahrt GmbH) Model 328-100 and 328-300 airplanes. This AD was prompted by a manufacturer safety analyses review on flight control which resulted in recommendations for reduced repetitive inspection intervals for the flight controls certification maintenance requirements (CMR) of the tab-to-actuator linkage. This AD requires revising the airplane maintenance program by incorporating certain CMR tasks. We are issuing this AD to prevent failure of these components or their constituent parts which could lead to reduced control of the airplane.
Airworthiness Directives; The Boeing Company Airplanes
Document Number: 2012-1125
Type: Rule
Date: 2012-01-25
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for certain The Boeing Company Model 757-200, -200CB, and -300 series airplanes with off-wing escape slide systems installed. This AD was prompted by reports of in-flight loss of the off-wing escape slide. This AD requires modifying the door latch fittings and witness mark placards of the off-wing escape slide systems; and for certain airplanes, replacing the bearings and lockbase retainer in the door latch assembly, relocating and adjusting the sensor target and the sensor proximity switch, and testing to ensure positive door locking and corrective action if necessary. For certain airplanes, this AD would also require installing a bumper assembly and placards. We are issuing this AD to prevent the in-flight loss of the off-wing escape slide, which could result in the unavailability of the escape slide during an emergency evacuation. Additionally, the departed slide could cause damage to the fuselage, wing, flaps, or stabilizer, which could degrade flight control.
Airworthiness Directives; Cirrus Design Corporation Airplanes
Document Number: 2012-1122
Type: Rule
Date: 2012-01-25
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for certain Cirrus Design Corporation (Cirrus) Model SR22T airplanes. This AD was prompted by reports of partial loss of engine power due to a dislodged rubber gasket/seal being ingested into the turbocharger. This AD requires inspection and modification of the air box flange welds and slots and installation of induction system air box seals as applicable. We are issuing this AD to correct the unsafe condition on these products.
Airworthiness Directives; Agusta S.p.A. Helicopters
Document Number: 2012-366
Type: Rule
Date: 2012-01-24
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for all Agusta S.p.A. (Agusta) model A109S and AW109SP helicopters. This AD is prompted by a fatigue crack found in the left elevator assembly along the riveting of the upper skin to the fourth rib on an Agusta A109S helicopter. These actions are intended to detect a crack, which could lead to a failure of the elevator, reduced maneuverability of the helicopter, and subsequent loss of control of the helicopter.
Airworthiness Directives; Eurocopter France (ECF) Model AS350B, B1, B2, B3, BA, and D; and AS355E, F, F1, F2, and N Helicopters
Document Number: 2012-365
Type: Rule
Date: 2012-01-24
Agency: Federal Aviation Administration, Department of Transportation
We are superseding an existing airworthiness directive (AD) for the specified ECF model helicopters. This AD results from a mandatory continuing airworthiness information (MCAI) AD issued by the European Aviation Safety Agency (EASA), which is the Technical Agent for the Member States of the European Union. The MCAI AD states that some cracks have been discovered in the spar of the upper fin on Model AS355N helicopters. Due to the fin design similarity between AS350 and AS355 helicopters, this AD action applies to both helicopter models. Modifying the upper and lower fin attachment is intended to prevent failure of a spar, loss of a fin, a separated fin hitting a rotor, and subsequent loss of control of a helicopter.
Amendment of Restricted Areas R-3704A and R-3704B; Fort Knox, KY
Document Number: 2012-1397
Type: Rule
Date: 2012-01-24
Agency: Federal Aviation Administration, Department of Transportation
This action makes several editorial corrections to the descriptions of restricted areas R-3704A and R-3704B, Fort Knox, KY.
Proposed Modification, Revocation and Establishment of Air Traffic Service Routes; Windsor Locks Area; CT
Document Number: 2012-1395
Type: Proposed Rule
Date: 2012-01-24
Agency: Federal Aviation Administration, Department of Transportation
This action proposes to modify four VOR Federal airways, revoke one VOR Federal airway, and establish three area navigation (RNAV) routes in the vicinity of Windsor Locks, CT. The FAA is proposing this action to adjust the airway route structure due to the planned decommissioning of the Bradley VHF omnirange/tactical air navigation (VORTAC) aid located on Bradley International Airport property, Windsor Locks, CT.
Receipt of Noise Compatibility Program and Request for Review for Philadelphia International Airport, Philadelphia, PA
Document Number: 2012-1206
Type: Notice
Date: 2012-01-24
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 Philadelphia International Airport under the provisions of 49 U.S.C. 47504 (the Aviation Safety and Noise Abatement Act, hereinafter referred to as ``the Act'') and 14 Code of Federal Regulations (CFR) Part 150 (hereinafter referred to as ``Part 150'') by the City of Philadelphia. This program was submitted subsequent to a determination by FAA that associated noise exposure maps submitted under Part 150 for Philadelphia International Airport were in compliance with applicable requirements, effective June 1, 2010, and published in the Federal Register at 75 FR 44046 (July 27, 2010). The proposed noise compatibility program will be approved or disapproved on or before July 17, 2012.
Standard Instrument Approach Procedures, and Takeoff Minimums and Obstacle Departure Procedures; Miscellaneous Amendments
Document Number: 2012-804
Type: Rule
Date: 2012-01-23
Agency: Federal Aviation Administration, Department of Transportation
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.
Standard Instrument Approach Procedures, and Takeoff Minimums and Obstacle Departure Procedures; Miscellaneous Amendments
Document Number: 2012-803
Type: Rule
Date: 2012-01-23
Agency: Federal Aviation Administration, Department of Transportation
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.
Airborne Radar Altimeter Equipment (For Air Carrier Aircraft)
Document Number: 2012-1243
Type: Notice
Date: 2012-01-23
Agency: Federal Aviation Administration, Department of Transportation
This notice announces the FAA's intent to cancel TSO-C67, Airborne Radar Altimeter Equipment (For Air Carrier Aircraft). The effect of the cancelled TSO will result in no new TSO-C67 design or production approvals. However, cancellation will not affect any current production of an existing TSO authorization (TSOA). Articles produced under an existing TSOA can still be installed per the existing airworthiness approvals, and all applications for new airworthiness approvals will still be processed.
Airworthiness Directives; Bombardier, Inc. Airplanes
Document Number: 2012-1210
Type: Proposed Rule
Date: 2012-01-23
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-400 series airplanes. This proposed AD was prompted by test reports showing that failure of a retract port flexible hose of a main landing gear (MLG) retraction actuator could cause excessive hydraulic fluid leakage. This proposed AD would require a detailed inspection for defects and damage of the retract port flexible hose on the left and right MLG retraction actuator, and replacement of the flexible hose if needed. We are proposing this AD to detect and correct defects and damage of the retract port flexible hose which could lead to an undamped extension of the MLG and could result in MLG structural failure, leading to an unsafe asymmetric landing configuration.
Proposed Establishment of Class E Airspace; Grasonville, MD
Document Number: 2012-1203
Type: Proposed Rule
Date: 2012-01-23
Agency: Federal Aviation Administration, Department of Transportation
This action proposes to establish Class E Airspace at Grasonville, MD, to accommodate a new Area Navigation (RNAV) Global Positioning System (GPS) special Standard Instrument Approach Procedure (SIAP) serving Queen Anne E.R. Heliport. This action would enhance the safety and airspace management of Instrument Flight Rules (IFR) operations within the National Airspace System.
Airworthiness Directives; the Boeing Company Airplanes
Document Number: 2012-1202
Type: Proposed Rule
Date: 2012-01-23
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for certain Model 767-200 and -300 series airplanes. This proposed AD was prompted by reports of fatigue cracking on the lower main sill inner chord of the hatch opening of the overwing emergency exit. This proposed AD would require repetitive inspections for cracking, corrosion damage, and any other irregularity of the lower main sill inner chord and surrounding structure, and repair if necessary. We are proposing this AD to detect and correct fatigue cracking on the lower main sill inner chord of the hatch opening of the overwing emergency exit, which could result in reduced structural integrity of the hatch opening of the overwing emergency exit and consequent rapid decompression of the airplane.
Airworthiness Directives; Bombardier, Inc. Airplanes
Document Number: 2012-1197
Type: Proposed Rule
Date: 2012-01-23
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for certain Bombardier, Inc. Model CL-600-2B19 (Regional Jet Series 100 & 440) airplanes. This proposed AD was prompted by a report of a fire which started in the vicinity of an electrical panel that was fed by oxygen escaping from a damaged third crew person oxygen line that occurred while the airplane was on the ground. This proposed AD would require replacing and changing the routing of the flexible oxygen hose of the third crew person oxygen line and modifying the entrance compartment assembly. We are proposing this AD to prevent the possibility of damage to the third crew person oxygen line and an oxygen-fed fire in the airplane.
Airworthiness Directives; BRP-POWERTRAIN GMBH & CO KG Rotax Reciprocating Engines
Document Number: 2012-1133
Type: Rule
Date: 2012-01-23
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for BRP POWERTRAIN GMBH & CO KG Rotax 914 F2, 914 F3, and 914 F4 reciprocating engines. This 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 isolated manufacturing deviations reportedly found on the threads of a certain batch of fuel pressure regulators, part number (P/N) 887130, installed on Rotax 914 F series engines, which could result in fuel leakage during engine operation. We are issuing this AD to prevent fuel leaks, which could result in an in-flight fire and damage to the aircraft.
Airworthiness Directives; General Electric Company Turbofan Engines
Document Number: 2012-1132
Type: Rule
Date: 2012-01-23
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for General Electric Company (GE) CF34-10E series turbofan engines. This AD was prompted by a report of heavy wear found on the seating surface of the center vent duct (CVD) (commonly referred to as center vent tube) support ring and on the inside diameter of the fan drive shaft at the mating location. This AD requires removing from service all CVD support assemblies and any fan drive shaft on the affected engines if wear is found on either the CVD support ring or the fan drive shaft. We are issuing this AD to prevent fan drive shaft failure, leading to uncontained engine failure and damage to the airplane.
Release of Airport Property: Fort Myers International Airport, Fort Myers, FL
Document Number: 2012-1064
Type: Notice
Date: 2012-01-23
Agency: Federal Aviation Administration, Department of Transportation
The FAA hereby provides notice of intent to release certain airport properties 0.55 acres at the Fort Myers International Airport, Fort Myers, FL from the conditions, reservations, and restrictions as contained in all grant agreements between the FAA and the Lee County Port Authority. The release of property will allow the Lee County Port Authority, owner of Fort Myers International Airport, to dispose of the property for other than aeronautical purposes. The property is located north of Daniels Parkway and Chana Court, near the intersection of Chamberlin Parkway, in Fort Myers, Florida. The parcels are currently designated as non-aeronautical use. The property will be released of its federal obligations to transfer ownership to Lee County. The release of the airport properties will facilitate the construction of a new direct interchange access to the airport from Interstate 75. Lee County will also transfer ownership of 1.93 acres of property north of Daniels Parkway and Chana Court to be used for drainage for the airport access road. The airport parcels to be released have an appraised Fair Market Value of $41,622. The value of the parcel to be received is $5,000, and the value of the proposed airport access improvement is estimated to be $500,620. Documents reflecting the Sponsor's request are available, by appointment only, for inspection at the Fort Myers International Airport and the FAA Airports District Office.
Release of Airport Property: Page Field, Fort Myers, FL
Document Number: 2012-1053
Type: Notice
Date: 2012-01-23
Agency: Federal Aviation Administration, Department of Transportation
The FAA hereby provides notice of intent to release certain airport properties 1.52 acres at Page Field, Fort Myers, FL from the conditions, release certain properties from all terms, conditions, reservations and restrictions of a Quitclaim Deed agreement, dated June 4, 1947, between the subject airport and the Federal Aviation Administration. The release of property will allow the Lee County Port Authority, owner of Page Field, to dispose of the property for other than aeronautical purposes. The property is located in the southwest corner of airport property, north of South Road, in Lee County, Florida. The parcel is currently designated as non-aeronautical use. The property will be released of its federal obligations to sell the property at Fair Market Value to Lee County for municipal purposes. The appraised Fair Market Value of the parcel is $64,628. Documents reflecting the Sponsor's request are available, by appointment only, for inspection at the Lee County Port Authority Offices at Fort Myers International Airport and the FAA Airports District Office.
IFR Altitudes; Miscellaneous Amendments
Document Number: 2012-1046
Type: Rule
Date: 2012-01-23
Agency: Federal Aviation Administration, Department of Transportation
This amendment adopts miscellaneous amendments to the required IFR (instrument flight rules) altitudes and changeover points for certain Federal airways, jet routes, or direct routes for which a minimum or maximum en route authorized IFR altitude is prescribed. This regulatory action is needed because of changes occurring in the National Airspace System. These changes are designed to provide for the safe and efficient use of the navigable airspace under instrument conditions in the affected areas.
Airworthiness Directives; Airbus Airplanes
Document Number: 2012-1131
Type: Proposed Rule
Date: 2012-01-20
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for all Airbus Model A310 series airplanes. This proposed AD was prompted by a report of an electrical arc and hydraulic haze in the wheel bay of the left-hand main landing gear (MLG) possibly resulting from chafing between the hydraulic high pressure hose and electrical wiring of the green electrical motor pump (EMP). This proposed AD would require prohibiting in-flight use of the green EMPs; revising the airplane flight manual (AFM) limitations section; installing a placard in the cockpit overhead panel; doing a one-time general visual inspection for correct condition and installation of hydraulic pressure hoses, electrical conduits, feeder cables, and associated clamping devices; and corrective action if necessary. We are proposing this AD to detect and correct chafing of hydraulic pressure hoses and electrical wiring of the green EMPs, which in combination with a system failure, could cause an uncontrolled and undetected fire in the MLG bay.
Airworthiness Directives; Turbomeca S.A. Turboshaft Engines
Document Number: 2012-1129
Type: Proposed Rule
Date: 2012-01-20
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for all Turbomeca S.A. Arriel 2B and 2B1 turboshaft engines. This proposed AD was prompted by the discovery of non-conformities of certain power turbine (PT) blade fir-tree roots. This proposed AD would require removing the affected PT blades from service on or before reaching a new reduced life limit for those certain PT blades. We are proposing this AD to prevent PT blade rupture, which could result in an uncommanded in-flight engine shutdown, forced autorotation landing, or accident.
Airworthiness Directives; Rolls-Royce plc (RR) Turbofan Engines
Document Number: 2012-1128
Type: Proposed Rule
Date: 2012-01-20
Agency: Federal Aviation Administration, Department of Transportation
We are revising an earlier proposed airworthiness directive (AD) for all RR RB211-Trent 553-61, 553A2-61, 556-61, 556A2-61, 556B- 61, 556B2-61, 560-61, 560A2-61, 768-60, 772-60, 772B-60, 875-17, 877- 17, 884-17, 884B-17, 892-17, 892B-17, and 895-17 turbofan engines. That NPRM proposed to supersede an existing AD that requires inspecting the intermediate-pressure (IP) compressor rotor shaft rear balance land for cracks, which could lead to engine failure. This action revises that NPRM by changing the optional terminating action for RB211-Trent 700 and RB211-Trent 800 engines to mandatory terminating action. Since these actions impose an additional burden over that proposed in the NPRM, we are reopening the comment period to allow the public the chance to comment on these proposed changes.
Airworthiness Directives; Agusta S.p.A. Helicopters
Document Number: 2012-1121
Type: Proposed Rule
Date: 2012-01-20
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for Agusta S.p.A. (Agusta) Model AB139 and AW139 helicopters with a certain generator control unit (GCU). This proposed AD was prompted by laboratory tests which revealed a potential fault in the overvoltage protection on a certain part-numbered GCU. This proposed AD would require replacing each affected GCU with an airworthy GCU. In addition, any affected GCU is not approved for installation on any helicopter. We are proposing this AD to prevent failure of the overvoltage protection of the GCU, degraded performance of the electrical power generation and distribution systems, a fire, and subsequent loss of control of the helicopter.
Membership in the National Parks Overflights Advisory Group Aviation Rulemaking Committee
Document Number: 2012-1051
Type: Notice
Date: 2012-01-20
Agency: Federal Aviation Administration, Department of Transportation
By Federal Register notice (See 76 FR 65319; October 20, 2011) the National Park Service (NPS) and the Federal Aviation Administration (FAA) invited interested persons to apply to fill a vacant position on the National Parks Overflights Advisory Group (NPOAG) Aviation Rulemaking Committee (ARC). That previous notice invited interested persons to apply to fill the vacancy representing Native American tribal concerns due to the incumbent member's completion of a three- year term appointment on April 2, 2012. This notice informs the public of the person selected to fill the vacancy on the NPOAG ARC.
Twentieth Meeting: RTCA Special Committee 203, Unmanned Aircraft Systems
Document Number: 2012-1049
Type: Notice
Date: 2012-01-20
Agency: Federal Aviation Administration, Department of Transportation
The FAA is issuing this notice to advise the public of the twentieth meeting of RTCA Special Committee 203, Unmanned Aircraft Systems.
Twenty-Eighth Meeting: RTCA Special Committee 206: Aeronautical Information and Meteorological Data Link Services
Document Number: 2012-1048
Type: Notice
Date: 2012-01-20
Agency: Federal Aviation Administration, Department of Transportation
The FAA is issuing this notice to advise the public of the twenty-eighth meeting of RTCA Special Committee 206: Aeronautical Information and Meteorological Data Link Services
Release of Airport Property: Tampa International Airport, Tampa, FL
Document Number: 2012-1047
Type: Notice
Date: 2012-01-20
Agency: Federal Aviation Administration, Department of Transportation
The FAA hereby provides notice of intent to release certain airport properties, approximately 3.407 acres, at the Tampa International Airport, Tampa, FL from the conditions, reservations, and restrictions as contained in federal grant assurances. The release of property will allow the Hillsborough County Aviation Authority to dispose of the property for other than aeronautical purposes. The property is located southwest corner airport property, adjacent to Highway 60. The parcel is currently designated as non-aeronautical use. The property will be released of its federal obligations to grant a perpetual utlility easement to the Tampa Electric Company (TECO) for relocation of transmission lines serving the Skyway Substation located off airport. The fair market value of the parcel has been determined by appraisal to be $695,000. Documents reflecting the Sponsor's request are available, by appointment only, for inspection at the Tampa International Airport and the FAA Airports District Office.
Airworthiness Directives; Glasflugel Gliders
Document Number: 2012-928
Type: Proposed Rule
Date: 2012-01-19
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for Glasflugel Models Standard Libelle-201B, Club Libelle 205, Mosquito, and Kestrel gliders. 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 corrosion damage to the elevator control rod that could lead to failure of the elevator control rod, possibly resulting in loss of control of the glider. We are issuing this proposed AD to require actions to address the unsafe condition on these products.
Airworthiness Directives; The Boeing Company Airplanes
Document Number: 2012-859
Type: Proposed Rule
Date: 2012-01-19
Agency: Federal Aviation Administration, Department of Transportation
We propose to supersede an existing airworthiness directive (AD) that applies to certain The Boeing Company Model 737-300, -400, and -500 series airplanes. The existing AD currently requires repetitive inspections for cracking of the crown area of the fuselage skin, and corrective actions if necessary. Since we issued that AD, we received additional reports of cracking at the horizontal chem-mill steps away from the lap joints over the entire crown area, and vertical chem-mill cracks adjacent to the butt joints. This proposed AD would add repetitive inspections for cracking using different inspection methods and would inspect additional areas, and corrective actions if necessary. This proposed AD would also require additional repairs to previously repaired areas and repetitive inspections for loose fasteners and replacement if necessary in certain previously repaired areas. This proposed AD would also reduce certain compliance times and extend certain other compliance times. We are proposing this AD to detect and correct fatigue cracking of the fuselage skin, which could cause the fuselage skin to fracture and fail, and result in rapid decompression of the airplane.
Airworthiness Directives; The Boeing Company Airplanes
Document Number: 2012-858
Type: Proposed Rule
Date: 2012-01-19
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for all The Boeing Company Model 717-200 airplanes. This proposed AD was prompted by reports of cracks found on the center section ribs of the horizontal stabilizers. This proposed AD would require repetitive inspections for cracking of the aft face of the left and right rib hinge bearing lugs of the center section of the horizontal stabilizer; and crack measurement, repairs, and installation of a new center section rib if necessary. We are proposing this AD to detect and correct cracks in the left and right bearing lugs of the rib hinge spreading at the same time, which could result in failure of both hinge bearing lugs. Failure of the hinge bearing lugs could result in the inability of the horizontal stabilizer to sustain flight loads and therefore reduce the controllability of the airplane.
Airworthiness Directives; Bombardier, Inc. Airplanes
Document Number: 2012-857
Type: Proposed Rule
Date: 2012-01-19
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for certain Bombardier, Inc. Model CL-600-2C10 (Regional Jet Series 700, 701, & 702); CL-600-2D15 (Regional Jet Series 705); CL-600-2D24 (Regional Jet Series 900); and CL-600-2E25 (Regional Jet Series 1000) airplanes. This proposed AD was prompted by reports of deformation of the pressure regulator on the oxygen cylinder, which was attributed to batches of raw material that did not meet required tensile strength. This proposed AD would require an inspection to determine if certain oxygen pressure regulators are installed, and replacement of oxygen cylinder and regulator assemblies (CRAs) containing pressure regulators that do not meet required material properties. We are proposing this AD to prevent elongation of the pressure regulator neck, which could result in rupture of the oxygen cylinder, and in the case of cabin depressurization, oxygen would not be available when required.
Airworthiness Directives; The Boeing Company Airplanes
Document Number: 2012-856
Type: Proposed Rule
Date: 2012-01-19
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for certain The Boeing Company Model 777 airplanes. This proposed AD was prompted by reports that escape slides/rafts did not deploy due to galvanic corrosion of the door-mounted slide/raft packboard release mechanisms. This proposed AD would require doing a general visual inspection of the housing assembly of the packboard release mechanism to determine if its surface treatment has been sealed, and if unsealed, replacing the housing assembly with a new or serviceable housing assembly. We are proposing this AD to detect and correct corrosion of the packboard release mechanisms, which could interfere with escape slide/raft deployment, prohibit doors from opening in the armed mode, and cause consequent delay and injury during evacuation of passengers and crew from the cabin in the event of an emergency.
Airworthiness Directives; Cessna Aircraft Company Airplanes
Document Number: 2012-855
Type: Proposed Rule
Date: 2012-01-19
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for certain Cessna Aircraft Company Model 560XL airplanes. This proposed AD was prompted by reports of wheel inserts becoming loose and damaging brake assemblies on Model 560XL airplanes. This proposed AD would require an inspection of the torque lug and surrounding components (wheel base, side rim, lock ring) for damage (such as corrosion, cracks, dents, bent areas, damaged or missing paint or primer, or wear on the metal), and of the bearing cup for corrosion, turned cup, or clearance that exceeds limits, and repair as applicable; measuring the torque lugs for width and replacing screws and inserts with new, improved screws and inserts; and re-identifying the wheel assemblies. We are proposing this AD to correct the unsafe condition on these products.
Airworthiness Directives; Bombardier, Inc. Airplanes
Document Number: 2012-854
Type: Proposed Rule
Date: 2012-01-19
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-400 series airplanes. This proposed AD was prompted by chafing on high pressure fuel lines due to improper installation of an expandable pin on the lower cowl assembly. This proposed AD would require installing spring clips and repositioning the lanyard attachment points at the forward end and the forward firefloor of the lower cowl. We are proposing this AD to prevent chafing of the high pressure fuel lines, which if not corrected, could cause fuel leakage in a fire zone.
Air Traffic Procedures Advisory Committee
Document Number: 2012-802
Type: Notice
Date: 2012-01-18
Agency: Federal Aviation Administration, Department of Transportation
The FAA is issuing this notice to advise the public that a meeting of the Federal Aviation Administration Air Traffic Procedures Advisory Committee (ATPAC) will be held to review present air traffic control procedures and practices for standardization, revision, clarification, and upgrading of terminology and procedures.
Public Notice for Waiver of Aeronautical Land-Use Assurance; Gerald R. Ford International Airport, Grand Rapids, MI
Document Number: 2012-800
Type: Notice
Date: 2012-01-18
Agency: Federal Aviation Administration, Department of Transportation
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 lease of the airport property. The proposal consists of 2 parcels of land with the lease portion totaling approximately 5.4 acres. Current use and present condition is partially developed land compatible with local commercial/ industrial zoning classification. The land was acquired under the FAA Project Numbers 9-20-072-6001, 3-26-0039-02, and 3-26-0055-44208. There are no impacts to the airport by allowing the airport to lease the property, since the land is no longer needed for aeronautical use. Subject land will provide for the development and expansion of the west Michigan Aviation Academy (WMAA); and through its lease would result in generating a predictable long-term revenue stream for the airport. 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 disposition of proceeds from the lease of the airport property will be in accordance FAA's Policy and Procedures Concerning the Use of Airport Revenue, published in the Federal Register on February 16, 1999. 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.
Special Conditions: Gulfstream Aerospace Corporation, Model GVI Airplane; Rechargeable Lithium Batteries and Rechargeable Lithium-Battery Systems
Document Number: 2012-798
Type: Rule
Date: 2012-01-18
Agency: Federal Aviation Administration, Department of Transportation
These special conditions are issued for the Gulfstream Aerospace Corporation (GAC) Model GVI airplane. This airplane will have a novel or unusual design feature associated with the installation of rechargeable lithium batteries and rechargeable lithium-battery systems. 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.
Public Notice for Waiver of Aeronautical Land-Use Assurance; Willow Run Airport; Detroit, MI
Document Number: 2012-796
Type: Notice
Date: 2012-01-18
Agency: Federal Aviation Administration, Department of Transportation
The Federal Aviation Administration (FAA) is considering a proposal to authorize the release of approximately 29.5 acres of airport property for sale. The land consists of portions of the original airport parcels. These parcels were acquired by the Wayne County Road Commissioners of Wayne County, Michigan, its successors and assigns (Wayne County Airport Authority) from the U.S. Government, General Services Administration without federal participation. This property was previously released for non-aeronautical use. There are no requirements to retain the land for airport use. There are no impacts to the airport by allowing the Wayne County Airport Authority to sell the property. The land is not needed for aeronautical use. Approval does not constitute a commitment by the FAA to financially assist in the sale of the subject airport property nor a determination of eligibility for grant-in-aid funding from the FAA. The disposition of proceeds from the sale of the airport property will be in accordance with FAA's Policy and Procedures Concerning the Use of Airport Revenue, published in the Federal Register on February 16, 1999. 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; Hawker Beechcraft Corporation Models 1900, 1900C, and 1900D Airplanes
Document Number: 2012-604
Type: Rule
Date: 2012-01-18
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for certain Hawker Beechcraft Corporation Models 1900, 1900C, and 1900D airplanes. This emergency AD was sent previously to all known U.S. owners and operators of these airplanes. This AD requires inspecting the elevator bob-weight and attaching linkage for correct installation and for damage or deformation to the weight and/or weight bracket with corrective action as necessary. This AD was prompted by reports of the elevator bob-weight (stabilizer weight) traveling past its stop bolt, which allowed the attaching linkage to move over-center, resulting in reduced nose down elevator control, which could result in loss of control of the airplane. We are issuing this AD to detect and correct conditions that could result in reduced nose down elevator control and loss of control of the airplane.
Airworthiness Directives; The Boeing Company Airplanes
Document Number: 2012-468
Type: Rule
Date: 2012-01-18
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for The Boeing Company Model 767 airplanes. This AD requires installing new panel assemblies in the main equipment center or on the forward cargo compartment sidewall and removing certain relays from some panels in the main equipment center. This AD also requires revising the maintenance program to incorporate Airworthiness Limitations (AWLs) No. 28-AWL-27 and No. 28-AWL-28. This AD also includes an alternative location for the installation of the new panel assemblies for airplanes that have the optional water system drain plumbing and changing the interconnecting wiring between the P141 panel and the P36 and P37 panels. For airplanes with a deactivated center fuel tank, this AD also requires an alternative functional test for the left and right override/jettison pumps. We are issuing this AD to prevent possible sources of ignition in a fuel tank caused by electrical fault or uncommanded dry operation of the main tank boost pumps and center auxiliary tank override and jettison pumps. This AD was prompted by fuel system reviews conducted by the manufacturer. An ignition source in the fuel tank could result in a fire or an explosion and consequent loss of the airplane.
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