Source: https://regulations.justia.com/regulations/fedreg/agencies/department-of-transportation/federal-aviation-administration/2005?page=5&registers=between&min-day=1&min-month=1&max-day=31&max-month=12
Timestamp: 2020-08-07 19:19:50
Document Index: 767200042

Matched Legal Cases: ['art 150', 'art 150', 'art 150', 'art 150', 'art 150', 'art 150', 'art 150']

Results 201 - 250 of 2,027
Document Number: 05-22791
https://regulations.justia.com/regulations/fedreg/2005/11/21/05-22791.html
Document Number: 05-22790
The FAA is adopting a new airworthiness directive (AD) for all British Aerospace Model HS 748 airplanes. This AD requires repetitive inspections for fatigue cracking, corrosion, and other related discrepancies of the rear pressure bulkhead and associated areas, and the fin attachment fittings, particularly the fin link beam; and related investigative and corrective actions. This AD results from a structural integrity audit of the airplane that showed the importance of inspecting for fatigue cracking and corrosion of these areas. We are issuing this AD to detect and correct cracking, corrosion, and other related discrepancies of the rear pressure bulkhead and associated areas, and the fin attachment fittings, particularly the fin link beam, which could result in damage to the airplane structure or injury to airplane occupants.
https://regulations.justia.com/regulations/fedreg/2005/11/21/05-22790.html
Document Number: 05-22789
The FAA is adopting a new airworthiness directive (AD) for all Airbus Model A340-200 and A340-300 series airplanes. This AD requires repetitive inspections for cracking of the junction between the thrust reverser forward frame and the 12 o'clock and 6 o'clock beams; the thrust reverser common fittings; and the thrust reverser J-ring structure at the 12 o'clock and 6 o'clock positions; and related investigative and corrective actions. This AD results from fatigue and damage tolerance testing of the engine thrust reversers which revealed fatigue cracking of the junction between the thrust reverser forward frame and the 12 o'clock beam, and of the thrust reverser J-ring structure. We are issuing this AD to detect and correct such fatigue cracking, which could result in rupture of the J-ring, forward frame, or common fittings; loss of the thrust reverser system; or inadvertent deployment of a thrust reverser in flight and consequent reduced controllability of the airplane.
https://regulations.justia.com/regulations/fedreg/2005/11/21/05-22789.html
Document Number: 05-22918
https://regulations.justia.com/regulations/fedreg/2005/11/18/05-22918.html
Document Number: 05-22917
https://regulations.justia.com/regulations/fedreg/2005/11/18/05-22917.html
Document Number: 05-22916
https://regulations.justia.com/regulations/fedreg/2005/11/18/05-22916.html
Document Number: 05-22915
https://regulations.justia.com/regulations/fedreg/2005/11/18/05-22915.html
Document Number: 05-22872
The FAA adopts a new airworthiness directive (AD) for all CENTRAIR 101 series gliders. This AD requires you to make pen and ink changes to the Limitations Section of the glider maintenance manual to eliminate contradictory information concerning the structural life limit. This AD results from a review by FAA of the Limitations Section of the CENTRAIR Model 101AP glider maintenance manual that revealed conflicting information concerning the structural life limit. We are issuing this AD to assure that the published life limit is adhered to and to prevent structural failure of the glider once this life limit is reached.
https://regulations.justia.com/regulations/fedreg/2005/11/18/05-22872.html
Document Number: 05-22775
https://regulations.justia.com/regulations/fedreg/2005/11/17/05-22775.html
Document Number: 05-22774
https://regulations.justia.com/regulations/fedreg/2005/11/17/05-22774.html
Document Number: 05-22773
https://regulations.justia.com/regulations/fedreg/2005/11/17/05-22773.html
Document Number: 05-22772
This action proposes to establish new Class E airspace at Koyuk, AK. Two revised procedures and one new Standard Instrument Approach Procedure (SIAP) are being published for the Koyuk Airport. Additional Class E Airspace is needed to contain aircraft executing instrument approaches at Koyuk Airport. Additionally, one small section of Class G airspace surrounded by Class E airspace will be converted to Class E airspace by this action. Adoption of this proposal would result in creation of additional Class E airspace upward from 700 feet (ft.) and 1,200 ft. above the surface at Koyuk, AK.
https://regulations.justia.com/regulations/fedreg/2005/11/17/05-22772.html
Document Number: 05-22771
https://regulations.justia.com/regulations/fedreg/2005/11/17/05-22771.html
Document Number: 05-22770
https://regulations.justia.com/regulations/fedreg/2005/11/17/05-22770.html
Establishment of Class E Airspace; Nenana, AK
Document Number: 05-22767
This action revises Class E airspace at Nenana, AK to provide adequate controlled airspace to contain aircraft executing Standard Instrument Approach Procedures (SIAPs). This rule results in revised Class E airspace upward from 700 feet (ft.) above the surface at Nenana Municipal Airport, AK.
https://regulations.justia.com/regulations/fedreg/2005/11/17/05-22767.html
Document Number: 05-22766
https://regulations.justia.com/regulations/fedreg/2005/11/17/05-22766.html
Document Number: 05-22712
The FAA proposes to adopt a new airworthiness directive (AD) for McCauley Propeller Systems models 3A32C406/82NDB-X and D3A32C409/ 82NDB-X propellers, installed on Teledyne Continental Motors (TCM) IO- 520, TSIO-520, or IO-550 reciprocating engines. These propellers are herein referred to as C406 and C409 propellers, respectively. This proposed AD would require adding an operational revolutions per minute (rpm) restriction on the C406 and C409 propellers, and installing an rpm restriction placard in the cockpit. This proposed AD would also add a 10,000-hour total time-in-service (TIS) life limit for these propellers. This proposed AD would also remove from service any propeller that has 10,000 hours or more total TIS, or that has an unknown total TIS. Also, this proposed AD would require initial and repetitive propeller blade inspections for damage, and repair if necessary. This proposed AD results from testing by the manufacturer that identified stress conditions that affect the fatigue life and damage tolerance of C406 and C409 propellers, when installed on TCM IO- 520, TSIO-520, or IO-550 reciprocating engines. We are proposing this AD to prevent blade or hub failure that could result in separation of a propeller blade and loss of control of the airplane.
https://regulations.justia.com/regulations/fedreg/2005/11/16/05-22712.html
Document Number: 05-22652
The FAA is making available an EA and FONSI for the evaluation of environmental impacts associated with a proposed corporate hangar construction at Cincinnati Municipal Airport-Lunken Field, located in Cincinnati, Ohio. Point of Contact: Mr. Brad Davidson, Environmental Protection Specialist, FAA Great Lakes Region, Detroit Airports District Office, 11677 South Wayne Road, Suite 107, Romulus, MI 48174, (734) 229-2900.
https://regulations.justia.com/regulations/fedreg/2005/11/16/05-22652.html
Document Number: 05-22651
https://regulations.justia.com/regulations/fedreg/2005/11/16/05-22651.html
Document Number: 05-22650
The FAA invites public comments about our intention to request the Office of Management and Budget's (OMB) renewal of a current information collection. The information collected on the FAA Form 8120- 11 will be reported voluntarily by manufacturers, repair stations, aircraft owner/operators, air carriers, and the general public who wish to report suspected ``unapproved'' parts to the FAA for review. The information will be used to determine if an ``unapproved'' part investigation is warranted.
https://regulations.justia.com/regulations/fedreg/2005/11/16/05-22650.html
Document Number: 05-22649
https://regulations.justia.com/regulations/fedreg/2005/11/16/05-22649.html
Document Number: 05-22593
The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 737-600, -700, -700C, -800, and -900 series airplanes. This AD requires modification of certain wire bundles located above the center fuel tank. This AD results from fuel system reviews conducted by the manufacturer. We are issuing this AD to prevent chafed wire bundles near the center fuel tank, which could cause electrical arcing through the tank wall and ignition of fuel vapor in the fuel tank, and result in a fuel tank explosion.
https://regulations.justia.com/regulations/fedreg/2005/11/16/05-22593.html
Document Number: 05-22592
The FAA is adopting a new airworthiness directive (AD) for all British Aerospace Model BAC 1-11 200 and 400 series airplanes. This AD requires revising the airplane flight manual (AFM) to contain applicable AFM amendments, which advise the flightcrew of information pertaining to safely operating the fuel system. The AD also requires revising the FAA-approved maintenance program to include certain repetitive maintenance tasks intended to improve the safety of the fuel system. This AD results from fuel system reviews conducted by the manufacturer. We are issuing this AD to prevent potential ignition sources inside the fuel system, which, in combination with flammable fuel vapors, could result in a fuel tank explosion and consequent loss of the airplane.
https://regulations.justia.com/regulations/fedreg/2005/11/16/05-22592.html
Document Number: 05-22591
The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 737 airplanes. This AD requires, for certain airplanes, a one-time detailed inspection for interference between a clamp assembly and the wires behind the P15 refuel panel, and corrective actions if necessary. For certain other airplanes, this AD requires a one-time detailed inspection for discrepancies of the wires behind the P15 refuel panel; and corrective and related investigative actions if necessary. This AD is prompted by evidence of chafed wiring behind the P15 refuel panel and arcing to the back of the P15 refuel panel and adjacent wing structure. We are issuing this AD to detect and correct chafing of the wiring behind the P15 refuel panel, which could lead to arcing and fire with consequent airplane damage and injury to refueling personnel.
https://regulations.justia.com/regulations/fedreg/2005/11/16/05-22591.html
Document Number: 05-22589
The FAA is adopting a new airworthiness directive (AD) for all Fokker Model F27 Mark 050 airplanes. This AD requires a one-time inspection of the bleed air supply ducts to determine if blanking plugs are present and a one-time inspection of the entire area of the engine nacelle for heat damage; and corrective actions if necessary. This AD also requires replacement of the blanking plugs with clamping devices. This AD results from heat damage in areas adjacent to the bleed air supply duct assembly. We are issuing this AD to prevent rupture of the bleed air supply duct, which could lead to hot bleed air leaking into the engine controls area and result in heat damage to control cables, electrical wiring, hydraulic components, and fuel lines, and consequent fire.
https://regulations.justia.com/regulations/fedreg/2005/11/16/05-22589.html
Document Number: 05-22578
https://regulations.justia.com/regulations/fedreg/2005/11/16/05-22578.html
Document Number: 05-22590
https://regulations.justia.com/regulations/fedreg/2005/11/15/05-22590.html
Document Number: 05-22588
The FAA proposes to adopt a new airworthiness directive (AD) for all Airbus Model A330-200, A330-300, A340-200, and A340-300 series airplanes; and A340-541 and A340-642 airplanes. This proposed AD would require operators to revise the Airworthiness Limitations section of the Instructions for Continued Airworthiness to incorporate new information. This information includes, for all affected airplanes, decreased life limit values for certain components; and for Model A330-200 and -300 series airplanes, new inspections, compliance times, and new repetitive intervals to detect fatigue cracking, accidental damage, or corrosion in certain structures. This proposed AD results from a revision to subsection 9-1 of the Airbus A330 and A340 Maintenance Planning Documents (MPD) for Life Limits/Monitored parts, and subsection 9-2 of the Airbus A330 MPD for Airworthiness Limitations Items. We are proposing this AD to ensure the continued structural integrity of these airplanes.
https://regulations.justia.com/regulations/fedreg/2005/11/15/05-22588.html
Document Number: 05-22587
https://regulations.justia.com/regulations/fedreg/2005/11/15/05-22587.html
Document Number: 05-22577
The FAA is requesting public comment on the City of Manchester, New Hampshire's request to sell a portion (3.98 acres) of Airport property. The property is located in the area of the Northeast Ramp off Perimeter Road and is identified as Tax Map 721, Lot 17E. The land is currently unimproved. The parcel will be swapped with another parcel of equal value needed for Airport development. Upon sale, the land will be utilized for hangar development. A portion of the property (2.58 acres) was acquired under the Surplus Property Act via deed dated August 16, 1968. The disposition of proceeds from the disposal of 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.
https://regulations.justia.com/regulations/fedreg/2005/11/15/05-22577.html
Document Number: 05-22494
https://regulations.justia.com/regulations/fedreg/2005/11/15/05-22494.html
Document Number: 05-22493
https://regulations.justia.com/regulations/fedreg/2005/11/15/05-22493.html
Document Number: 05-22523
https://regulations.justia.com/regulations/fedreg/2005/11/14/05-22523.html
Document Number: 05-22522
https://regulations.justia.com/regulations/fedreg/2005/11/14/05-22522.html
Document Number: 05-22521
These special conditions are issued for Cessna Model 650 airplanes modified by Elliott Aviation Technical Product Development, Inc. These modified airplanes will have a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. The modification incorporates the installation of electronic flight display systems manufactured by Universal Avionics Systems Corporation. The electronic flight display systems perform critical functions. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for the protection of these systems from the effects of high-intensity radiated fields (HIRF). 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.
https://regulations.justia.com/regulations/fedreg/2005/11/14/05-22521.html
Document Number: 05-22492
The Federal Aviation Administration (FAA) announces its findings on the noise compatibility program submitted by the Lehigh- Northampton Airport Authority under the provisions of 49 U.S.C. (the Aviation Safety and Noise Abatement Act, hereinafter referred to as ``the Act'') and 14 CFR Part 150. These findings are made in recognition of the description of Federal and nonfederal responsibilities in Senate Report No. 96-52 (1980). On May 14, 2004 the FAA determined that the noise exposure maps submitted by the Lehigh- Northampton Airport Authority under Part 150 were in compliance with applicable requirements. On October 7, 2005, the FAA approved the Lehigh Valley International Airport's updated noise compatibility program. Most of the recommendations of the program update were approved. One program element relating to revised flight procedures for noise abatement was proposed by the airport operator and was approved in part, as a voluntary measure, and disapproved in part. Only one noise abatement element was disapproved for purposes of Part 150 pending submission of additional information needed to make an informed analysis. The Lehigh-Northampton Airport Authority has also requested under FAR Part 150, section 150.35(f), that FAA determine that the revised five-year forecast condition NEM submitted with the noise compatibility program and showing noise contours as a result of the implementation of the noise compatibility program is in compliance with applicable requirements of FAR Part 150. The FAA announces its determination that the revised five-year forecast condition NEW for the Lehigh Valley International Airport for the year 2008 submitted with the noise compatibility program is in compliance with applicable requirements of FAR Part 150 effective October 31, 2005. The documentation that constitutes the revised five-year forecast condition NEM as defined in Sec. Sec. 150.7 and 150.101(e) of Part 150 includes but is not limited to: Sections 2.2 and 2.3, Figure 3, and Table 3 in the NCP Update, and Figure 11 and Figures 36 through 45 in the NEM volume. The FAA has determined that this revised five-year forecast condition NEM and accompanying documentation are in compliance with applicable requirements.
https://regulations.justia.com/regulations/fedreg/2005/11/14/05-22492.html
Document Number: 05-22442
https://regulations.justia.com/regulations/fedreg/2005/11/14/05-22442.html
Document Number: 05-22309
https://regulations.justia.com/regulations/fedreg/2005/11/14/05-22309.html
Document Number: 05-22308
The FAA is adopting a new airworthiness directive (AD) for certain EMBRAER Model EMB-135 airplanes, and Model EMB-145, -145ER, - 145MR, -145LR, -145XR, -145MP, and -145EP airplanes. This AD requires modification of the logic of the steering system of the nose landing gear (NLG) wheel. This AD results from reports of the loss of directional control of the airplane on the ground after an internal failure of the NLG wheel steering system. We are issuing this AD to prevent failure of the NLG wheel steering system, which could result in reduced controllability of the airplane.
https://regulations.justia.com/regulations/fedreg/2005/11/14/05-22308.html
Document Number: 05-22220
https://regulations.justia.com/regulations/fedreg/2005/11/14/05-22220.html
Document Number: 05-22219
https://regulations.justia.com/regulations/fedreg/2005/11/14/05-22219.html
Document Number: 05-22218
The FAA is adopting a new airworthiness directive (AD) for certain Saab Model SAAB 2000 airplanes. This AD requires modifying the manual feather-and-unfeather system for the propellers to make the design of the system more robust. This AD results from reports of in- flight engine shutdown caused by uncommanded operation of the feather pump of the propeller. We are issuing this AD to prevent uncommanded feathering of the propeller, which could result in the shutdown of an engine during flight and consequent reduced controllability of the airplane.
https://regulations.justia.com/regulations/fedreg/2005/11/14/05-22218.html
Document Number: 05-22217
The FAA is superseding an existing airworthiness directive (AD), which applies to certain Airbus Model A319-100, A320-200, and A321-100 and -200 series airplanes. That AD currently requires modification of the telescopic girt bar of the escape slide/raft assembly, and follow-on actions. This new AD requires a new modification of the telescopic girt bar and the installation of placards on the modified girt bars, which terminates the repetitive functional tests required by the existing AD. This AD results from development of a new, improved modification. We are issuing this AD to prevent failure of the escape slide/raft to deploy correctly, which could result in the slide being unusable during an emergency evacuation and consequent injury to passengers or airplane crewmembers.
https://regulations.justia.com/regulations/fedreg/2005/11/14/05-22217.html
Airworthiness Directives; Airbus Model A300 B4-600 and A300 B4-600R Series Airplanes; and A300 F4-605R and A300 C4-605R Variant F Airplanes
Document Number: 05-22216
The FAA is superseding an existing airworthiness directive (AD), which applies to all Airbus Model A300 B4-600 and A300 B4-600R series airplanes, and all Model A300 F4-605R airplanes. That AD currently requires repetitive inspections to detect cracks of certain attachment holes, installation of new fasteners, follow-on inspections or repair if necessary, and modification of the angle fittings of fuselage frame FR47. This new AD revises certain inspection thresholds and intervals. This new AD also adds inspections to detect cracks of additional attachment holes. This AD results from reports of cracks found before the inspection thresholds in the existing AD and cracks found in nearby areas not inspected by the existing AD. We are issuing this AD to prevent fatigue cracking of the forward fitting of fuselage frame FR47, which could result in reduced structural integrity of the frame.
https://regulations.justia.com/regulations/fedreg/2005/11/14/05-22216.html
Document Number: 05-22215
https://regulations.justia.com/regulations/fedreg/2005/11/14/05-22215.html
Document Number: 05-22213
https://regulations.justia.com/regulations/fedreg/2005/11/14/05-22213.html
Document Number: 05-22457
https://regulations.justia.com/regulations/fedreg/2005/11/10/05-22457.html
Document Number: 05-22456
In this direct final rule, the FAA is amending its regulation on the use of pilot supplemental oxygen. The amendment changes the flight level at which the remaining pilot at the controls of the airplane must put on and use his oxygen mask if the other pilot at any time leaves his control station of the airplane. This amendment revises that altitude to ``above flight level 350'' from ``above flight level 250.'' It will also eliminate the needless use of oxygen that is not otherwise required to provide for safety in air carrier operations. This will reduce needless expenditures to replace oxygen equipment that is subject to excessive wear and tear.
https://regulations.justia.com/regulations/fedreg/2005/11/10/05-22456.html
Document Number: 05-22445
The FAA proposes to adopt a new airworthiness directive (AD) for certain Bombardier Model CL-600-1A11 (CL-600), CL-600-2A12 (CL- 601), and CL-600-2B16 (CL-601-3A, CL-601-3R, & CL-604) airplanes. This proposed AD would require modifying the rudder balance spring assembly by installing a new adjustable balance spring, and rigging the assembly to suit the rudder of each airplane. This proposed AD results from production inspections that showed that the spring assembly that controls rudder balance may not have the correct pre-load on some airplanes. We are proposing this AD to prevent uncommanded yaw movements and consequent reduced controllability of the airplane.
https://regulations.justia.com/regulations/fedreg/2005/11/10/05-22445.html
Document Number: 05-22444
https://regulations.justia.com/regulations/fedreg/2005/11/10/05-22444.html