Federal Aviation Administration February 25, 2010 – Federal Register Recent Federal Regulation Documents

Airworthiness Directives; Bombardier, Inc. Model CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), and CL-600-2B16 (CL-601-3A, CL-601-3R, and CL-604 Variants) Airplanes
Document Number: 2010-3827
Type: Proposed Rule
Date: 2010-02-25
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 EMB-135ER, -135KE, -135KL, and -135LR Airplanes; and EMBRAER Model EMB-145, -145ER, -145MR, -145LR, -145XR, -145MP, and -145EP Airplanes
Document Number: 2010-3826
Type: Proposed Rule
Date: 2010-02-25
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; The Boeing Company Model 747-100, -200B, and -200F Series Airplanes
Document Number: 2010-3819
Type: Proposed Rule
Date: 2010-02-25
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to supersede an existing airworthiness directive (AD) that applies to certain Model 747-100, 747-200B, and - 200F series airplanes. The existing AD currently requires inspections to detect cracking in the upper row of fasteners holes of the skin lap joints in the fuselage lower lobe, and repair, if necessary. This proposed AD would reduce the maximum interval of the post-modification inspections. This proposed AD results from reports of fatigue cracking on modified airplanes. We are proposing this AD to detect and correct fatigue cracking in the longitudinal lap joints of the fuselage lower lobe, which could lead to the rapid decompression of the airplane and the inability of the structure to carry fail-safe loads.
Airworthiness Directives; Airbus Model A300, A300-600, and A310 Airplanes
Document Number: 2010-3817
Type: Proposed Rule
Date: 2010-02-25
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; Airbus Model A300 Series Airplanes, Airbus Model A300 B4-600 Series Airplanes, Airbus Model A300 B4-600R Series Airplanes, and A310 Series Airplanes
Document Number: 2010-3816
Type: Proposed Rule
Date: 2010-02-25
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: During a maintenance check performed by an A310 operator, the recommended modification of the lower attachment beam of rack 101VU by accomplishment of Airbus Service Bulletin (SB) A310-53-2076 was embodied on the aeroplane, leading the operator to find three cracks on the FR15A crossbeam above the NLG [nose landing gear] box at the splicing with rack 107VU fitting. This condition, if not detected and corrected, could degrade the structural integrity of the crossbeam on NLG FR15A web attachment fitting of rack 107VU. Rack 107VU contains major airworthiness system components whose functioning could be adversely affected by the loss of the attachment fitting. As the A300 and A300-600 aeroplanes share this design feature, they are also affected. The proposed AD would require actions that are intended to
Revocation of Class D and E Airspace; Brunswick, ME
Document Number: 2010-3741
Type: Rule
Date: 2010-02-25
Agency: Federal Aviation Administration, Department of Transportation
This action removes the Class D and E Airspace at Brunswick NAS Airport, Brunswick, ME, as the airport has closed and the associated Standard Instrument Approach Procedures (SIAPs) removed, eliminating the need for controlled airspace.
Amendment of Class E Airspace; Llano, TX
Document Number: 2010-3738
Type: Rule
Date: 2010-02-25
Agency: Federal Aviation Administration, Department of Transportation
This action amends Class E airspace for Llano, TX, adding additional controlled airspace to accommodate Area Navigation (RNAV) Standard Instrument Approach Procedures (SIAPs) at Llano Municipal Airport, Llano, TX, and updates the airport's geographic coordinates. The FAA is taking this action to enhance the safety and management of Instrument Flight Rule (IFR) operations at the airport.
Amendment of Class E Airspace; Lima, OH
Document Number: 2010-3727
Type: Rule
Date: 2010-02-25
Agency: Federal Aviation Administration, Department of Transportation
This action amends Class E airspace at Lima, OH, to accommodate Area Navigation (RNAV) Standard Instrument Approach Procedures (SIAPs) at Lima Allen County Airport, Lima, OH. The FAA is taking this action to enhance the safety and management of Instrument Flight Rule (IFR) operations at the airport.
Amendment of Class E Airspace; Stamford, TX
Document Number: 2010-3716
Type: Rule
Date: 2010-02-25
Agency: Federal Aviation Administration, Department of Transportation
This action amends Class E airspace for Stamford, TX, adding additional controlled airspace to accommodate Area Navigation (RNAV) Standard Instrument Approach Procedures (SIAPs) at Arledge Field Airport, Stamford, TX. The FAA is taking this action to enhance the safety and management of Instrument Flight Rule (IFR) operations at the airport.
Establishment of Class E Airspace; Langdon, ND
Document Number: 2010-3708
Type: Rule
Date: 2010-02-25
Agency: Federal Aviation Administration, Department of Transportation
This action establishes Class E airspace for Langdon, ND to accommodate Area Navigation (RNAV) Standard Instrument Approach Procedures (SIAPs) at Robertson Field Airport, Langdon, ND. The FAA is taking this action to enhance the safety and management of Instrument Flight Rule (IFR) operations at the airport.
Airworthiness Directives; ATR-GIE Avions de Transport Régional Model ATR42 and ATR72 Airplanes
Document Number: 2010-3558
Type: Rule
Date: 2010-02-25
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) 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; PILATUS AIRCRAFT LTD. Model PC-12/47E Airplanes
Document Number: 2010-3521
Type: Rule
Date: 2010-02-25
Agency: Federal Aviation Administration, Department of Transportation
We are superseding an existing airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:
Airworthiness Directives; Airbus Model A340-541 and -642 Airplanes
Document Number: 2010-3485
Type: Rule
Date: 2010-02-25
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) 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; Airbus Model A340-200 and A340-300 Series Airplanes
Document Number: 2010-3472
Type: Rule
Date: 2010-02-25
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) 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 ATP Airplanes
Document Number: 2010-3470
Type: Rule
Date: 2010-02-25
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for the products listed above that would supersede an existing AD. 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; McDonnell Douglas Corporation Model MD-90-30 Airplanes
Document Number: 2010-3469
Type: Rule
Date: 2010-02-25
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for all Model MD-90-30 airplanes. This AD requires repetitive inspections for cracking of the overwing frames at stations 883, 902, 924, 943, and 962, left and right sides, and corrective actions if necessary. This AD results from reports of cracked overwing frames. We are issuing this AD to detect and correct such cracking, which could sever the frame, increase the loading of adjacent frames, and result in damage to adjacent structure and loss of overall structural integrity of the airplane.
Airworthiness Directives; Bombardier, Inc. Model CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), and CL-600-2B16 (CL-601-3A, CL-601-3R, and CL-604) Airplanes
Document Number: 2010-3463
Type: Rule
Date: 2010-02-25
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) 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:
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