Federal Aviation Administration 2010 – Federal Register Recent Federal Regulation Documents
Results 851 - 900 of 1,625
Notice of Intent to Request Extension From the Office of Management and Budget of a Currently Approved Information Collection Activity, Request for Comments; Certification Procedures for Products and Parts
The FAA invites public comments about our intention to request the Office of Management and Budget (OMB) to approve a current information collection. CFR part 21 prescribes certification standards for aircraft, aircraft engines, propellors, products, and parts. The information collected is used to determine compliance and applicant eligibility.
Agency Information Collection Activity Seeking OMB Approval
The FAA invites public comments about our intention to request the Office of Management and Budget's (OMB) approval of a new information collection. The Federal Register Notice with a 60-day comment period soliciting comments on the following collection of information was published on March 18, 2010, vol. 75, no. 52, page 13204. This research is important for establishing the scientific basis for air tour management policy decisions in the National Parks as mandated by the National Parks Air Tour Management Act of 2000.
Airworthiness Directives; Gulfstream Aerospace LP (Type Certificate Previously Held by Israel Aircraft Industries, Ltd.) Model Galaxy and Gulfstream 200 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: Extension of airbrakes above 360 KIAS [knots indicated air speed]/0.79 Mi [Mach indicated] results in aerodynamic driven vibration of the airbrake which, if not limited per Revision 14 to the AFM [airplane flight manual], can lead to high cycle fatigue failure of the airbrake in board hinge. The unsafe condition is high cycle fatigue of the airbrake in-board hinge, which can result in loss of the airbrake, which in turn can lead to reduced controllability of the airplane. The proposed AD would require actions that are intended
Airworthiness Directives; McDonnell Douglas Corporation Model DC-8-31, DC-8-32, DC-8-33, DC-8-41, DC-8-42, and DC-8-43 Airplanes; Model DC-8-50 Series Airplanes; Model DC-8F-54 and DC-8F-55 Airplanes; Model DC-8-60 Series Airplanes; Model DC-8-61 Series Airplanes; Model DC-8-70 Series Airplanes; and Model DC-8-70F Series Airplanes
The FAA proposes to supersede an existing airworthiness directive (AD) that applies to all of the McDonnell Douglas Corporation airplanes identified above. The existing AD currently requires revising the maintenance program to incorporate new airworthiness limitations for fuel tank systems to satisfy Special Federal Aviation Regulation No. 88 requirements. This proposed AD would add requirements to revise the maintenance program to incorporate specific Critical Design Configuration Control Limitations (CDCCL) information and install fuel tank float switch in-line fuses. This proposed AD would also add two Airworthiness Limitations inspections (ALIs). This proposed AD results from a design review of the fuel tank systems. 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; Fokker Services B.V. Model F.28 Mark 0070 and 0100 Airplanes
We are adopting a new airworthiness directive (AD) for the products listed above. 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:
Airworthiness Directives; Piper Aircraft, Inc. Models PA-32R-301T and PA-46-350P Airplanes
We are adopting a new airworthiness directive (AD) for certain Piper Aircraft, Inc. Models PA-32R-301T and PA-46-350P airplanes. This AD requires you to replace any spot-welded, V-band exhaust coupling with a riveted, V-band exhaust coupling. This AD results from reports that spot-welded, V-band exhaust couplings are failing. We are issuing this AD to prevent failure of the V-band exhaust coupling, which could cause the exhaust pipe to detach from the turbocharger. This failure could result in release of high-temperature gases inside the engine compartment and possibly cause an in-flight fire. An in-flight fire could lead to loss of control.
Airworthiness Directives; Air Tractor, Inc. Models AT-802 and AT-802A Airplanes
We are adopting a new airworthiness directive (AD) to supersede AD 2006-08-09, which applies to all Air Tractor, Inc. (Air Tractor) Models AT-802 and AT-802A airplanes. AD 2006-08-09 currently requires you to repetitively inspect (using the eddy current method) the two outboard fastener holes in both of the wing main spar lower caps at the center splice joint for cracks and repair or replace any cracked spar cap. Since we issued AD 2006-08-09, we have determined we need to clarify the serial numbers (SNs) of the Models AT-802 and AT- 802A airplanes affected by that AD. Additionally, we are adding an option of modifying the wing main spar lower caps to extend the safe life limit on the affected airplanes. Consequently, this AD would keep the actions of AD 2006-08-09, clarify the affected SNs, and add a modification option to extend the safe life limit. We are issuing this AD to detect and correct cracks in the wing main spar lower cap at the center splice joint, which could result in failure of the spar cap and lead to wing separation and loss of control of the airplane.
Airworthiness Directives; Bombardier, Inc. Model DHC-8-400 Series Airplanes
We are adopting a new airworthiness directive (AD) for the products listed above. 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:
Standard Instrument Approach Procedures, and Takeoff Minimums and Obstacle Departure Procedures; Miscellaneous Amendments
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.
Airworthiness Directives; McDonnell Douglas Corporation Model DC-10-10, DC-10-10F, and MD-10-10F Airplanes
We are adopting a new airworthiness directive (AD) for certain Model DC-10-10, DC-10-10F, and MD-10-10F airplanes. This AD requires a one-time high frequency eddy current inspection of fastener holes for cracks at the left and right side wing rear spar lower cap at station Xors=345, and other specified and corrective actions if necessary. This AD results from a report of three instances of Model DC-10-10F airplanes having fuel leaks in the wing rear spar lower cap at station Xors=345. We are issuing this AD to prevent cracks in the spar cap, which could lead to cracking of the lower wing skin, fuel leaks, and the inability of the structure to sustain limit load.
Standard Instrument Approach Procedures, and Takeoff Minimums and Obstacle Departure Procedures; Miscellaneous Amendments
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; Bombardier, Inc. Model CL-600-2C10 (Regional Jet Series 700 & 701) Airplanes, Model CL-600-2D15 (Regional Jet Series 705) Airplanes, and Model CL-600-2D24 (Regional Jet Series 900) Airplanes
We are adopting a new airworthiness directive (AD) for the products listed above. 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:
Airworthiness Directives; The Boeing Company Model 777-200LR and -300ER Series Airplanes
We are adopting a new airworthiness directive (AD) for certain Model 777-200LR and -300ER series airplanes. This AD requires doing a high frequency eddy current inspection for cracking of the keyway of the fuel tank access door cutout on the left and right wings between wing rib numbers 8 (wing station 387) and 9 (wing station 414.5), and related investigative and corrective actions if necessary. This AD results from reports of cracks emanating from the keyway of the fuel tank access door cutout of the lower wing skin between wing rib numbers 8 and 9. We are issuing this AD to prevent loss of the lower wing skin load path, which could cause catastrophic structural failure of the wing.
Airworthiness Directives; Fokker Services B.V. Model F.27 Mark 500 and 600 Airplanes
We are adopting a new airworthiness directive (AD) for the products listed above. 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:
Airworthiness Directives; Honeywell International Inc. TPE331-10 and TPE331-11 Series Turboprop Engines
The FAA proposes to supersede an existing airworthiness directive (AD) for Honeywell International Inc. TPE331-10 and TPE331-11 series turboprop engines. That AD currently requires removing certain first stage turbine disks from service. This proposed AD would require the same actions, and would also require performing fluorescent penetrant inspections (FPI) and eddy current inspections (ECI) on certain first stage turbine disks that have a serial number (S/N) listed in this proposed AD. This proposed AD results from our determination that we need to expand the affected population to include other disks from the same heat lot as the failed first stage turbine disk, and that certain inspections are also required. We are proposing this AD to prevent uncontained failure of the first stage turbine disk and damage to the airplane.
Airworthiness Directives; The Boeing Company Model 747-100, 747-200B, and 747-200F Series Airplanes
The FAA proposes to supersede two existing airworthiness directives (AD) that apply to certain Model 747-100, 747-200B, and 747- 200F series airplanes. The existing ADs currently require inspections to detect fatigue-related skin cracks and corrosion of the skin panel lap joints in the fuselage upper lobe, and repair if necessary. One of the existing ADs, AD 94-12-09, also requires modification of certain lap joints and inspection of modified lap joints. The other AD, AD 90- 15-06, requires repetitive detailed external visual inspections of the fuselage skin at the upper lobe skin lap joints for cracks and evidence of corrosion, and related investigative and corrective actions. This proposed AD would reduce the maximum interval of the post-modification inspections, and adds post-repair inspection requirements for certain airplanes. This proposed AD results from reports of cracking on modified airplanes. We are proposing this AD to detect and correct fatigue cracking and corrosion in the fuselage upper lobe skin lap joints, which could lead to rapid decompression of the airplane and inability of the structure to carry fail-safe loads.
Airworthiness Directives; Robert E. Rust, Jr. Model DeHavilland DH.C1 Chipmunk 21, DH.C1 Chipmunk 22, and DH.C1 Chipmunk 22A Airplanes
We propose to adopt a new airworthiness directive (AD) for all Robert E. Rust, Jr. Model DeHavilland DH.C1 Chipmunk 21, DH.C1 Chipmunk 22, and DH.C1 Chipmunk 22A airplanes. This proposed AD would require a one-time inspection of the flap operating system for an unauthorized latch plate design installation. This proposed AD results from a report of a latch plate failing in service that was not made in accordance with the applicable de Havilland drawing. We are proposing this AD to detect and correct unauthorized latch plate design installation, which could result in an un-commanded retraction of the flaps. This failure could lead to a stall during a landing approach.
Airworthiness Directives; GA 8 Airvan (Pty) Ltd Models GA8 and GA8-TC320 Airplanes
We propose to adopt a new airworthiness directive (AD) for the products listed above that would revise 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: Inspection of a high time aircraft has revealed cracks in the Horizontal Stabilizer rear spar splice plate and inboard main ribs around the area of the Horizontal Stabilizer rear pivot attachment. Additionally, failure of some attach bolts in service may be due to improper assembly. This amendment is issued to include an applicability matrix (Table 1, page 2) in the compliance section of the service bulletin for improved clarity. The
Existence of Proposed Airworthiness Design Standards for Acceptance Under the Primary Category Rule; Orlando Helicopter Airways (OHA), Inc., Models Cessna 172I, 172K, 172L, and 172M
This notice announces the existence of and requests comments on the proposed airworthiness design standards for acceptance of the OHA, Inc., Models Cessna 172I, 172K, 172L, and 172M airplanes under the regulations for primary category aircraft.
Approval of Noise Compatibility Program for Buckeye Municipal Airport, Town of Buckeye, AZ
The Federal Aviation Administration (FAA) announces its findings on the noise compatibility program submitted by the Town of Buckeye under the provisions of 49 U.S.C. 47501 et seq. (formerly 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''). On September 22, 2008, the FAA determined that the noise exposure maps submitted by the Town of Buckeye under Part 150 were in compliance with applicable requirements. On May 13, 2010, the FAA approved the Buckeye Municipal Airport noise compatibility program. All of the recommendations of the program were approved.
Airworthiness Directives; CFM International, S.A. CFM56-5, -5B, and -7B Series Turbofan Engines
The FAA is adopting a new airworthiness directive (AD) for CFM International, S.A. CFM56-5, -5B, and -7B series turbofan engines. This AD requires removing from service, nine stage 3 low-pressure turbine (LPT) disks, identified by serial number (S/N). This AD results from the discovery of a material nonconformity requiring removal of the disk before the certified disk life of certain stage 3 LPT disks. We are issuing this AD to prevent uncontained failure of the stage 3 LPT disk and damage to the airplane.
Airworthiness Directives; McDonnell Douglas Corporation 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
We propose to adopt a new airworthiness directive (AD) for certain 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. This proposed AD would require 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 proposed AD results from fuel system reviews conducted by the manufacturer. We are proposing 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; The Boeing Company Model 777-200, -300, and -300ER Series Airplanes
We are revising an earlier proposed airworthiness directive (AD) for certain Model 777-200, -300, and -300ER series airplanes. The original NPRM would have required installing Teflon sleeving under the clamps of certain wire bundles routed along the fuel tank boundary structure, and cap sealing certain penetrating fasteners of the main and center fuel tanks. The original NPRM resulted from fuel system reviews conducted by the manufacturer. This action revises the original NPRM by adding airplanes and adding and removing certain requirements. We are proposing this supplemental NPRM to prevent electrical arcing on the fuel tank boundary structure or inside the fuel tanks, which could result in a fire or explosion.
Airworthiness Directives; Bombardier, Inc. Model CL-600-2B19 (Regional Jet Series 100 & 440) Airplanes; 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
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: Two cases of a crack on a ``dry'' ADG [air driven generator] (Hamilton Sundstrand part number in the 761339 series), in the aft area of the strut and generator housing assembly, have been reported on CL-600-2B19 aircraft. The same part is also installed on CL-600-2C10, -2D15 and -2D24 aircraft. Investigation determined that the crack was in an area of the strut where the wall thickness of the casting was below specification, due to a manufacturing anomaly in a specific batch of ADGs. Structural failure and departure of the ADG during deployment could possibly result in damage to the aircraft structure. If deployment was activated by a dual engine shutdown, ADG structural failure would also result in loss of hydraulics for the flight controls. The proposed AD would require actions that are
Revocation of Class D and E Airspace; Big Delta, AK
This action revokes Class D and E airspace at Big Delta, AK, to eliminate duplicated controlled airspace serving Allen Army Airfield. The FAA is taking this action to enhance safety and management of Instrument Flight Rules (IFR) operations at Allen Army Airfield.
Airworthiness Directives; McCauley Propeller Systems Five-Blade Propeller Assemblies
The FAA proposes to supersede an existing airworthiness directive (AD) for certain McCauley Propeller Systems propeller assemblies. That AD currently requires removing certain propeller hubs from service at new, reduced life limits and eddy current inspections (ECIs) of the propeller hub. This proposed AD would require removing certain propeller hubs from service before they exceed 6,000 hours time-since-new (TSN). This proposed AD results from a report of a crack in a propeller hub. We are proposing this AD to prevent cracked propeller hubs, which could cause failure of the propeller hub, blade separation, and loss of control of the airplane.
Proposed Amendment of Class E Airspace; Williston, ND
This action proposes to amend Class E airspace at Williston, ND. Additional controlled airspace is necessary to accommodate new Standard Instrument Approach Procedures (SIAPs) at Sloulin Field International Airport, Williston, ND. The FAA is taking this action to enhance the safety and management of Instrument Flight Rules (IFR) operations at the airport. Adjustments to the geographic coordinates of the airport also would be made.
Proposed Establishment of Class E Airspace; Port Clarence, AK
This action proposes to establish Class E airspace at Port Clarence Coast Guard Station (CGS), AK. The United States Coast Guard operates into this airstrip and has developed a military-use instrument approach procedure. This instrument approach development at the Port Clarence CGS Airport has made this action necessary to enhance safety and management of Instrument Flight Rules (IFR) operations.
Airworthiness Directives; Honeywell International Inc. Auxiliary Power Unit Models GTCP36-150(R) and GTCP36-150(RR)
The FAA is adopting a new airworthiness directive (AD) for Honeywell International Inc. auxiliary power unit (APU) models GTCP36- 150(R) and GTCP36-150(RR). This AD requires inspecting the fuel control unit (FCU) differential pressure (Delta P) sleeve bore for erosion, replacing the FCU if it fails the inspection, and installing a fuel deflector on the Delta P sleeve of the FCU. This AD results from eight reports of fuel leakage from the FCU. We are issuing this AD to prevent fuel leakage in the APU compartment, which could lead to ignition of fuel vapor, creating a fire and explosion hazard resulting in injury, and damage to the APU and the airplane.
Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-135ER, -135KE, -135KL, and -135LR Airplanes; and EMBRAER Model EMB-145, -145ER, -145MR, -145LR, -145XR, -145MP, and -145EP Airplanes
We are adopting a new airworthiness directive (AD) for the products listed above. 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:
Airworthiness Directives; Cessna Aircraft Company Model 525A Airplanes
We are adopting a new airworthiness directive (AD) to supersede AD 2009-24-13, which applies to certain Cessna Aircraft Company (Cessna) Model 525A airplanes. AD 2009-24-13 currently requires you to repetitively inspect the thrust attenuator paddle assemblies for loose and damaged fasteners and for cracks. AD 2009-24-13 also requires you to replace loose or damaged fasteners and replace cracked thrust attenuator paddles found during any inspection. Since we issued AD 2009-24-13, Cessna has developed new design thrust attenuator paddles and universal head rivets as terminating action for the repetitive inspections. Consequently, this AD would retain the requirements of AD 2009-24-13 until replacement of both thrust attenuator paddles and the eight countersunk fasteners with new design thrust attenuator paddles and universal head rivets. We are issuing this AD to detect and correct loose and damaged fasteners and cracks in the thrust attenuator paddles, which could result in in-flight departure of the thrust attenuator paddles. This failure could lead to rudder and elevator damage and result in loss of control.
Airworthiness Directives; Mitsubishi Heavy Industries, Ltd. Various Models MU-2B Airplanes
We are adopting a new airworthiness directive (AD) to supersede Airworthiness Directive (AD) 2006-17-01, AD 2006-15-07, AD 2000-02-25, and AD 97-25-02, which applies to certain Mitsubishi Heavy Industries, Ltd. (MHI) various Models MU-2B airplanes. An FAA MU-2B safety evaluation resulted in the standardization of the MU-2B specific training and the FAA-accepted pilot operating checklists through a special Federal aviation regulation (SFAR). MHI revised the airplane flight manuals (AFMs) to align them with the information in that training and the checklists. In addition, incorporating all AFM revisions up to and including this latest AFM revision will incorporate all AFM compliance actions required by the four above-mentioned ADs. This AD would retain from AD 2006-17-01 the inspection of the engine torque indication system and possible recalibration of the torque pressure transducers and would require incorporating all revisions up to and including the latest revisions of the AFM. We are issuing this AD to correct inconsistencies in critical operating procedures between the MU-2B specific training, the FAA-accepted pilot operating checklists, and the AFMs, which, if not corrected, could result in the pilot inadvertently taking inappropriate actions in critical operating conditions.
Airworthiness Directives; Eurocopter France Model AS 350 B, BA, B1, B2, B3, and D, and Model AS355 E, F, F1, F2, and N Helicopters
We propose to adopt a new airworthiness directive (AD) for the Eurocopter France Model AS 350 B, BA, B1, B2, B3, and D, and Model AS355 E, F, F1, F2, and N helicopters, with certain main rotor servo- controls and tail rotor servo-controls. This proposed AD would require replacing all servo-controls that are identified in the Applicability section of this proposed AD. This proposed AD is prompted by an internal review conducted by the manufacturer which revealed that some main and tail rotor servo-controls do not conform to the approved design. The actions specified by this proposed AD are intended to prevent the distributor slide valve jamming in its sleeve, leading to reduced controllability of the rotors and subsequent loss of control of the helicopter.
The Future of Aviation Advisory Committee (FAAC) Subcommittee on Financing; Notice of Meeting
The Department of Transportation, Office of the Secretary of Transportation, announces a meeting of the FAAC Financing Subcommittee, which will be held at the offices of the Cessna Aircraft Company, in Wichita, Kansas. This notice announces the date, time, and location of the meeting, which will be open to the public. The purpose of the FAAC is to provide advice and recommendations to the Secretary of Transportation to ensure the competitiveness of the U.S. aviation industry and its capability to manage effectively the evolving transportation needs, challenges, and opportunities of the global
The Future of Aviation Advisory Committee (FAAC) Subcommittee on Competitiveness and Viability; Notice of Meeting
The Department of Transportation (DOT), Office of the Secretary of Transportation, announces a meeting of the FAAC Subcommittee on Competitiveness and Viability, which will be held in Washington, DC on June 30, 2010. This notice provides details on the date, time, and location of the meeting, which will be open to the public. The purpose of the FAAC is to provide advice and recommendations to the Secretary of Transportation to ensure the competitiveness of the U.S. aviation industry and its capability to manage effectively the evolving transportation needs, challenges, and opportunities of the global economy. The Subcommittee on Competitiveness and Viability is charged with examining changes in the operating and competitive structures of the U.S. airline industry; considering innovative strategies to open up new international markets and expand commercial opportunities in existing markets; investigating strategies to encourage the development of cost-effective, cutting-edge technologies and equipment that are critical for a competitive industry coping with increasing economic and environmental challenges; and
Airworthiness Directives; Rolls-Royce plc (RR) RB211-524 Series and RB211 Trent 500, 700, and 800 Series Turbofan Engines
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:
Amendment of Class D and E Airspace; Victorville, CA
This action will amend Class D and E airspace at Victorville, CA, to accommodate aircraft using Instrument Flight Rules (IFR) operations at Southern California Logistics Airport, allowing aircraft operations outside Class D airspace at Adelanto Airport. This will improve the safety and management of Instrument Flight Rules (IFR) operations at both airports. This action also will note a change in the airport name and geographic coordinates of Southern California Logistic Airport.
Proposed Amendment of Class E Airspace; Port Angeles, WA
This action proposes to amend Class E airspace at William R. Fairchild International Airport, Port Angeles, WA. The Ediz Hook Nondirectional Radio Beacon (NDB) has been decommissioned and removed. The FAA is proposing this action for the safety and management of Instrument Flight Rules (IFR) operations at the airport.
Proposed Establishment of Class E Airspace; Fillmore, UT
This action proposes to establish Class E airspace at Fillmore, UT, to accommodate aircraft using a new Area Navigation (RNAV) Global Positioning System (GPS) Standard Instrument Approach Procedure (SIAP) at Fillmore Municipal Airport. The FAA is proposing this action to enhance the safety and management of aircraft operations at the airport.
Proposed Establishment of Class E Airspace; Toledo, WA
This action proposes to establish Class E airspace at Toledo, WA, to accommodate aircraft using a new Area Navigation (RNAV) Global Positioning System (GPS) Standard Instrument Approach Procedure (SIAP) at Ed Carlson Memorial Field-South Lewis County Airport. The FAA is proposing this action to enhance the safety and management of instrument flight rules (IFR) operations at the airport.
Proposed Establishment of Class E Airspace and Amendment to Class D Airspace; Troutdale, OR
This action proposes to establish Class E airspace at Troutdale, OR, to accommodate aircraft using Non-directional Radio Beacon (NDB) Global Positioning System (GPS) Standard Instrument Approach Procedures (SIAPs) at Portland-Troutdale Airport. This action would enhance the safety and management of instrument flight rules (IFR) operations at the airport. This action also would amend the geographic coordinates of the Class D airspace area at the airport.
Proposed Modification of Class E Airspace; Willcox, AZ
This action proposes to modify Class E airspace at Willcox, AZ, to accommodate aircraft using a new Area Navigation (RNAV) Global Positioning System (GPS) Standard Instrument Approach Procedure (SIAP) at Cochise County Airport. The FAA is proposing this action to enhance the safety and management of aircraft operations at the airport.
Special Conditions: AeroMech, Incorporated; Hawker Beechcraft Corporation, Model B200 and Other Aircraft Listed in Table 1, Approved Model List (AML); Installation of MD835 Lithium Ion Battery
This action proposes special conditions for the AeroMech, Incorporated; Hawker Beechcraft Corporation, model B200 and other part 23 aircraft listed on the AML. These airplanes as modified by AeroMech, Incorporated will have a novel or unusual design feature(s) associated with installation of the Mid-Continent Instruments MD835 Lithium Ion (Li-ion) battery. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. These proposed 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.
Modification of Jet Routes J-32, J-38, and J-538; Minnesota
This action modifies Jet Routes J-32 and J-38 by terminating portions of the routes that are no longer needed at the Duluth, MN, VHF omnidirectional range/tactical air navigation (VORTAC) that are no longer needed. This action also modifies the J-538 airway description to align it with the corresponding segment of J-538 contained in Canadian airspace. This action is necessary for the safety and management of instrument flight rules (IFR) operations within the National Airspace System (NAS).
Revision of Class E Airspace; Galena, AK
This action revises Class E airspace at Galena, AK, to accommodate three amended Standard Instrument Approach Procedures (SIAPs) and the development of one Obstacle Departure Procedure (ODP) at the Edward G. Pitka Sr. Airport. The FAA is taking this action to enhance safety and management of Instrument Flight Rules (IFR) operations at Edward G. Pitka Sr. Airport.
Notice of Passenger Facility Charge (PFC) Approvals and Disapprovals
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. 1A158.29.
Airworthiness Directives; Microturbo Saphir 20 Model 095 Auxiliary Power Units (APUs)
We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued by the European Aviation Safety Agency (EASA) to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:
Airworthiness Directives; Bell Helicopter Textron Canada Model 222, 222B, 222U, 230, and 430 Helicopters
This amendment supersedes an existing airworthiness directive (AD) for the specified Bell Helicopter Textron Canada (BHTC) helicopters, that currently requires certain checks and inspections of the tail rotor blades. If a crack is found, the existing AD requires replacing the tail rotor blade (blade) with an airworthy blade before further flight. This amendment requires the same checks and inspections of the blades until they are required to be replaced and removes certain serial numbered and specifically coded blades from the applicability of the AD. This amendment is prompted by the approved rework of certain blades and two newly redesigned blades, which, if installed, constitute terminating action for the inspection requirements. The actions specified by this AD are intended to detect a crack in a blade, and to prevent loss of a blade and subsequent loss of control of the helicopter.
Orders Limiting Scheduled Operations at John F. Kennedy International Airport and Newark Liberty International Airport
This action announces a limited waiver of the requirements to use Operating Authorizations (slots) at John F. Kennedy International Airport (JFK) and Newark Liberty International Airport (EWR). The FAA will treat as used any Operating Authorization that was scheduled for an operation between JFK or EWR and points in Europe from April 14 through April 26, 2010. The FAA also will grant similar relief on an individual carrier basis following notification for scheduled flights between JFK or EWR and points in Europe canceled due to volcanic ash from April 27 through October 30, 2010. This policy is effective from April 14, 2010 through October 30, 2010.
Notice of Intent To Request Extension From the Office of Management and Budget of a Currently Approved Information Collection Activity, Request for Comments; Certification of Airmen for the Operation of Light-Sport Aircraft
The FAA invites public comments about our intention to request the Office of Management and Budget (OMB) to approve a current information collection. This rule generates a need for new designated pilot examiners and designated airworthiness representatives to support the certification of these new aircraft, pilots, flight instructors, and ground instructors.
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