Agency: Federal Aviation Administration
Years: 20002001200220032004200520062007200820092010201120122013[FR Doc 03-32087] 1. Modification of Class E Airspace; Johnson, KS
This document confirms the effective date of the direct final rule which revises Class E airspace at Johnson, KS.
Published: 2003-12-31 DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration
[FR Doc 03-32082] 2. Standard Instrument Approach Procedures; Miscellaneous Amendments
This amendment establishes, amends, suspends, or revokes Standard Instrument Approach Procedures (SIAPs) 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
Published: 2003-12-31 DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration
[FR Doc 03-32134] 3. Airworthiness Directives; Boeing Model 737-600, -700, 700C, -800, and -900
This document proposes the adoption of a new airworthiness directive (AD) that is applicable to certain Boeing Model 737600, 700, 700C, 800, and 900 series airplanes. This proposal would require replacement of the proximity switch electronics unit with a new, improved unit. This action is necessary to prevent a malfunction of the aural warning for
Published: 2003-12-31 DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration
[FR Doc 03-32133] 4. Airworthiness Directives; Bombardier Model DHC-8-102, -103, -106, -201, -202,
This document proposes the adoption of a new airworthiness directive (AD) that is applicable to certain Bombardier Model DHC8 102, 103, 106, 201, 202, 301, 311, and 315 airplanes. This proposal would require inspection of the fitting assemblies located on the vent and scavenge lines routed immediately below the fuel tank access covers on both wings
Published: 2003-12-31 DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration
[FR Doc 03-32135] 5. Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER)
This document proposes the adoption of a new airworthiness directive (AD) that is applicable to certain EMBRAER Model EMB135 and EMB145 series airplanes. This proposal would require inspection of the housings of the main landing gear (MLG) leg strut bushings; repair of the housings if necessary; and replacement of the MLG leg strut bushings with
Published: 2003-12-31 DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration
[FR Doc 03-32083] 6. Proposed Revision of VOR Federal Airway 137
This action proposes to revise VOR Federal Airway 137 (V-137) between the Thermal, CA, Very High Frequency Omnidirectional Radio Range and Tactical Air Navigation Aids (VORTAC) intersection and the Imperial, CA, VORTAC. The current route segment between the Thermal, CA, VORTAC, and the Imperial, CA, VORTAC is aligned to avoid a restricted area
Published: 2003-12-31 DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration
[FR Doc 03-32084] 7. Petitions for Exemption; Summary of Petitions Received; Dispositions of
Pursuant to FAA's rulemaking provisions governing the application, processing, and disposition of petitions for exemption part 11 of Title 14, Code of Federal Regulations (14 CFR), this notice contains a summary of certain dispositions of certain petitions previously received. The purpose of this notice is to improve the public's awareness of, and
Published: 2003-12-31 DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration
[FR Doc 03-32090] 8. Notice of Intent To Rule on Application 04-05-C-00-BUF To Impose and Use the
The FAA proposes to rule and invites public comment on the application to impose and use the revenue from a PFC at Buffalo Niagara International Airport under the provisions of the 49 U.S.C. 40117 and part 158 of the Federal Aviation Regulations (14 CFR part 158).
Published: 2003-12-31 DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration
[FR Doc 03-31849] 9. Airworthiness Directives; Agusta S.p.A. Model A109E Helicopters
This amendment adopts a new airworthiness directive (AD) for Agusta S.p.A. (Agusta) Model A109E helicopters. This action requires certain inspections of the rodend of the main rotor head damper for freedom of movement, and depending on the torque required to move the rodend, either further inspection for a crack or replacing the rod end. This
Published: 2003-12-31 DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration
[FR Doc 03-32091] 10. Notice of Intent To Rule on Application 04-07-C-00-EYW To Impose and Use the
The FAA proposes to rule and invites public comment on the application to impose and use the revenue from a PFC at Key West International and use the revenue from a PFC at Florida Keys Marathon Airports under the provisions of the 49 U.S.C. 40117 and part 158 of the Federal Aviation Regulations (14 CFR part 158).
Published: 2003-12-31 DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration
[FR Doc 03-31666] 11. Airworthiness Directives; Anjou Aeronautique Safety Belts and Restraint
The FAA adopts a new airworthiness directive (AD) for certain Anjou Aeronautique (ANJOU) (formerly TRW Repa S.A., formerly L'AIGLON) safety belts and restraint systems that are installed in aircraft. This AD requires you to inspect safety belts and restraint systems for defects and service life limits, and, if necessary, repair safety belts and
Published: 2003-12-31 DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration
[FR Doc 03-32092] 12. Notice of Intent To Rule on Applications 03-04-C-00-SGF To Impose and Use the
The FAA proposes to rule and invites public comment on the
application to impose and use the revenue from a PFC at Springfield
Branson Regional Airport under the provisions of the Aviation Safety
and Capacity Expansion Act of 1990 (Title IX of the Omnibus Budget [[Page 75712]]
Reconciliation Act of 1990) (Pub. L. 101508) and part 158 of the
Federal
Published: 2003-12-31 DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration
[FR Doc 03-31853] 13. Airworthiness Directives; Boeing Model 737-100, -200, -200C, - 300, -400, and
This amendment adopts a new airworthiness directive (AD), applicable to certain Boeing Model 737100, 200, 200C, 300, 400, and 500 series airplanes, that requires replacing the existing pressure relief valve on the potable water tank with a new, improved pressure relief valve, which is made of stainless steel and is non adjustable. For certain
Published: 2003-12-31 DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration
[FR Doc 03-32089] 14. Geosynchronous Orbit Aeronautical Mobile Satellite Services Aircraft Earth
This announces the availability of and request comments on a proposed Technical Standard Order (TSO) C132, Geosynchronous Orbit Aeronautical Mobile Satellite Services Aircraft Earth Station Equipment. The proposed TSO tells manufacturers seeking TSO authorization or letter of design approval what minimum performance standard (MPS) their equipment
Published: 2003-12-31 DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration
[FR Doc 03-31851] 15. Airworthiness Directives; McDonnell Douglas MD-90-30 Airplanes
This amendment adopts a new airworthiness directive (AD), applicable to certain McDonnell Douglas Model MD9030 airplanes, that requires a onetime general visual inspection of the circuit breakers to determine if discrepant circuit breakers are installed, and corrective action if necessary. This action is necessary to prevent internal overheating
Published: 2003-12-31 DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration
[FR Doc 03-32088] 16. TSO-C163, VDL Mode 3 Communications Equipment Operating Within the Frequency
This notice announces the availability of, and request comments, on a proposed Technical Standard order (TSO) for VDL Mode 3 Communications Equipment Operating within the Frequency Range 117.975 to 137.000 Megahertz (MHz). The proposed TSO tells manufacturers seeking TSO authorization or letter of design approval what minimum performance standard
Published: 2003-12-31 DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration
[FR Doc 03-32155] 17. Airworthiness Directives; Pratt & Whitney JT9D-3A, -7, -7A, -7F, -7H, -7AH,
The FAA is revising an existing airworthiness directive (AD) for Pratt & Whitney (PW) JT9D3A, 7, 7A, 7F, 7H, 7AH, and 7J turbofan engines, with gearbox pressure tube, part number (P/N) 697896, and No. 4 bearing front pressure manifold, P/N 670663, installed. That AD currently requires a onetime visual inspection of the gearbox pressure tube and
Published: 2003-12-31 DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration
[FR Doc 03-32156] 18. Airworthiness Directives; Pratt & Whitney PW4074, PW4074D, PW4077, PW4077D,
The FAA is superseding an existing airworthiness directive (AD) for Pratt & Whitney PW4074, PW4074D, PW4077, PW4077D, PW4084, PW4084D, PW4090, PW4090D, PW40903, and PW4098 turbofan engines. That AD requires initial and repetitive visual and borescope inspections of the No. 3 bearing weep tube and turbine exhaust case (TEC), and removal of the high
Published: 2003-12-31 DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration
[FR Doc 03-32085] 19. Airworthiness Standards; Bird Ingestion; Correction
This document contains corrections to the final regulations for bird ingestion type certification standards that the Federal Aviation Administration (FAA) published in the Federal Register on September 14, 2000 (65 FR 55848), with an effective date of December 13, 2000. These regulations revised the bird ingestion type certification standards for
Published: 2003-12-31 DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration
[FR Doc 03-32086] 20. Modification of Class D Airspace; and Modification of Class E Airspace;
This document confirms the effective date of the direct final rule which revises Class D and Class E airspace at Topeka, Philip Billard Municipal Airport, KS.
Published: 2003-12-31 DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration
[FR Doc 03-31883] 21. Service Difficulty Reports
The Federal Aviation Administration (FAA) is further delaying the effective date of a final rule that amends the reporting requirements for air carriers and certificated domestic and foreign repair station operators concerning failures, malfunctions, and defects of aircraft, aircraft engines, systems, and components. This action is prompted by the
Published: 2003-12-30 DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration
[FR Doc 03-31667] 22. Airworthiness Directives; Cessna Aircraft Company Models 172R, 172S, 182S,
This document makes a correction to Airworthiness Directive
(AD) 20032413, which was published in the Federal Register on
December 4, 2003 (68 FR 67789), and applies to certain Cessna Aircraft
Company (Cessna) Models 172R, 172S, 182S, 182T, T182T, 206H, and T206H [[Page 75115]]
airplanes that are equipped with a Honeywell KAP 140 autopilot computer
Published: 2003-12-30 DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration
[FR Doc 03-31850] 23. Airworthiness Directives; Titeflex Corporation; Correction
This document makes corrections to Airworthiness Directive (AD) 20032305 applicable to certain Titeflex Corporation hoses installed on Boeing 737300, 400, 500, 600, 700, 700C, 800, 900, 747400, 757200, 300, 767200, 300, and 300F airplanes, that was published in the Federal Register on November 19, 2003 (68 FR 65157). The AD number is incorrect in
Published: 2003-12-30 DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration
[FR Doc 03-31978] 24. Airworthiness Directives; GARMIN International Inc. GTX 330 Mode S
The FAA proposes to adopt a new airworthiness directive (AD) for certain GARMIN International Inc. GTX 330/GTX 330D Mode S transponders. This proposed AD would require you to install GTX 330/ 330D Software Upgrade Version 3.03. This proposed AD is the result of observations that the GTX 330 and GTX 330D may detect, from other aircraft, the S1
Published: 2003-12-30 DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration
[FR Doc 03-31847] 25.Airworthiness Directives; AeroSpace Technologies of Australia Pty Ltd Airplanes
The FAA proposes to adopt a new airworthiness directive (AD) for all AeroSpace Technologies of Australia Pty Ltd Model N22B, N22S, and N24A airplanes. This proposed AD would require you to inspect the forward and aft face of the rear fuselage frame for cracks and to repair or modify accordingly. This proposed AD is the result of mandatory continuing
Published: 2003-12-29 DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration
Years: 20002001200220032004200520062007200820092010201120122013