Federal Aviation Administration 2008 – Federal Register Recent Federal Regulation Documents

Results 751 - 800 of 1,726
Establishment of Class E Airspace; Plains, TX
Document Number: E8-14921
Type: Rule
Date: 2008-07-07
Agency: Federal Aviation Administration, Department of Transportation
This action establishes Class E5 airspace at Plains, TX. Additional controlled airspace is necessary to accommodate aircraft using new RNAV Global Positioning System (GPS) Standard Instrument Approach Procedures (SIAP) at Yoakum County Airport, Plains, TX. This action will enhance the safety and management of Instrument Flight Rules (IFR) aircraft operations at Yoakum County Airport.
Airworthiness Directives; Stemme GmbH & Co. KG Model S10-VT Powered Sailplanes
Document Number: E8-15177
Type: Proposed Rule
Date: 2008-07-03
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:
Establishment of Low Altitude Area Navigation Route (T-Route); Southwest Oregon
Document Number: E8-15020
Type: Rule
Date: 2008-07-03
Agency: Federal Aviation Administration, Department of Transportation
This action establishes a low altitude Area Navigation (RNAV) route, designated T-274 in the State of Oregon. T-routes are low altitude Air Traffic Service (ATS) routes, based on RNAV, for use by aircraft having instrument flight rules (IFR)-approved Global Positioning System (GPS)/Global Navigation Satellite System (GNSS) equipment. The FAA is taking this action to enhance safety and improve the efficient use of the navigable airspace in Oregon.
Notice of Availability of the Final Environmental Impact Statement (Final EIS) for the Development and Extension of Runway 9R/27L and Other Associated Airport Projects at Fort Lauderdale-Hollywood International Airport (FLL)
Document Number: E8-15061
Type: Notice
Date: 2008-07-02
Agency: Federal Aviation Administration, Department of Transportation
The FAA is issuing this Notice of Availability to advise the public that a Final EIS will be available for public review beginning June 27, 2008. The document was prepared pursuant to a proposal presented to the FAA by the Broward County Board of County Commissioners, the owner and operator of FLL and identified in the Final EIS as the Airport Sponsor, for environmental review. The FAA prepared this Final EIS to analyze and disclose potential environmental impacts related to possible Federal actions at FLL. Numerous Federal actions would be necessary if airfield development were to be implemented. Proposed improvements include Runway 9R/27L development and extension and other airfield projects (see below). The Final EIS presents the purpose and need for the proposed Federal action, analysis of reasonable alternatives, including the No Action alternative, discussion of impacts for each reasonable alternative, the selection of the FAA's Preferred Alternative, proposed mitigation, and supporting appendices. The Airport Sponsor proposes to redevelop and expand Runway 9R/27L to an overall length of 8,000 feet and width of 150 feet (the reconstructed runway would be equipped with an Engineered Materials Arresting System (EMAS) at both runway ends); elevate Runway 9R end and Runway 27L end to provide 34.74 feet of vertical clearance over the Florida East Coast (FEC) Railway; construct a new full-length parallel taxiway 75 feet wide on the north side of Runway 9R/27L with separation of 400 feet from 9R/27L; construct an outer dual parallel taxiway that would be separated from the proposed north side parallel taxiway by 276 feet; construct connecting taxiways from the proposed full-length parallel taxiway to existing taxiways; construct a Category I Instrument Landing System (ILS) for landings on Runways 9R and 27L that includes a Medium Intensity Approach Light System with runway alignment indicator lights (MALSR), localizer, and glideslope. The Airport Sponsor also proposes to decommission Runway 13/31 and redevelop and expand terminal gate facilities. Connected actions associated with the Airport Sponsor's Proposed Project include closing Airport Perimeter Road located within the approach to Runway 9R; relocate ASR-9; acquire all, or a portion, of the Hilton Fort Lauderdale Airport Hotel (formerly Wyndham Fort Lauderdale Airport Hotel) and the Dania Boat Sales to the extent existing structures are within the Proposed Runway Protection Zone (RPZ) for extended Runway 9R/27L. Public Comment: The public comment period on the Final EIS starts June 27, 2008 and closes on July 28, 2008. Comments can only be accepted with the full name and address of the individual commenting. Mail and fax comments are to be submitted to Ms. Virginia Lane of the FAA, at the address shown in FOR FURTHER INFORMATION CONTACT. All comments must be postmarked or faxed no later than midnight, Monday, July 28, 2008. The Final EIS may be reviewed for comment during regular business hours at the following locations: 1. Broward County Governmental Center, 115 S. Andrews Avenue, Fort Lauderdale, FL 33301 (Telephone: 954-357-7000) 2. Broward County LibraryMain Branch, 100 S. Andrews Avenue, Fort Lauderdale, FL 33301 (Telephone: 954-354-7444) 3. Broward County LibraryFort Lauderdale Branch, 1300 E. Sunrise Boulevard, Fort Lauderdale, FL 33304 (Telephone: 954-765-4263) 4. Broward County LibraryHollywood Branch, 2600 Hollywood Boulevard, Hollywood, FL 33020 (Telephone: 954-926-2430) 5. Broward County LibraryDania Beach Paul DeMaio Branch, 255 E. Dania Beach Boulevard, Dania Beach, FL 33004 (Telephone: 954-926-2420) 6. Broward County LibraryDavie/Cooper City Branch, 4600 SW 82nd Avenue, Davie, FL 33328 (Telephone: 954-680-0050) 7. Broward County LibraryLauderhill Towne Centre, 6399 W. Oakland Park Boulevard, Lauderhill, FL 33313 (Telephone: 954-497-1630) 8. Broward County LibraryStirling Road Branch, 3151 Stirling Road, Hollywood, FL 33021 (Telephone: 954-985-2689) 9. Broward County LibraryPembroke Pines/Walter C. Young Branch, 955 NW 129th Avenue, Pembroke Pines, FL 33025 (Telephone: 954-437-2635) 10. Broward County LibraryWest Regional Branch, 8601 W. Broward Boulevard, Plantation, FL 33324 (Telephone: 954-831-3300) 11. Broward County LibrarySunrise Dan Pearl Branch, 10500 W. Oakland Park Boulevard, Sunrise, FL 33351 (Telephone: 954-749-2521) 12. Fort Lauderdale-Hollywood International Airport, Public Outreach Trailer, Broward County Aviation Department, 550 Northwest 10th Street, Dania Beach, FL 33315 (Telephone: 954-359-6977) 13. Broward County Administration Office, Broward County Governmental Center, 115 S. Andrews Avenue, Room 409, Fort Lauderdale, FL 33301 (Telephone: 954-357-7000) 14. Broward County Aviation Department, 100 Aviation Boulevard, Fort Lauderdale, FL 33315 (Telephone: 954-359-6199) A CD version of the Final EIS document will also be available at the following public locations. Broward County will be providing an electronic copy of the Final EIS on the Broward County web site at https://www.broward.org/airport/ 15. City of Lauderhill, Lauderhill City Hall, 2000 City Hall Drive, Lauderhill, FL 33313 (Telephone: 954-739-0100) 16. City of Pembroke Pines, Pembroke Pines City Hall, 10100 Pines Boulevard, Pembroke Pines, FL 33025 (Telephone: 954-431-4500) 17. City of Cooper City, Cooper City Hall, 9090 S.W. 50th Place, Cooper City, FL 33328 (Telephone: 954-434-4300) 18. City of Sunrise, 10770 W. Oakland Park Blvd., Sunrise, FL 33351 (Telephone: 954-741-2580) 19. City of Fort Lauderdale, 100 N. Andrews Avenue, Fort Lauderdale, FL 33301 (Telephone: 954-761-5000) 20. City of Plantation, Plantation City Hall, 400 N.W. 73rd Avenue, Plantation, FL 33317 (Telephone: 954-797-2221) 21. City of Hollywood, Hollywood City Hall, 2600 Hollywood Boulevard, Hollywood, FL 33020 (Telephone: 954-921-3473) 22. City of Dania Beach, Dania Beach City Hall, 100 W. Dania Beach Boulevard, Dania Beach, FL 33004 (Telephone: 954-924-3600) 23. Town of Davie, Davie Town Hall, 6591 S.W. 45th Street, Davie, FL 33314 (Telephone: 954-797-1000)
Agency Information Collection Activity Seeking OMB Approval
Document Number: E8-15023
Type: Notice
Date: 2008-07-02
Agency: Federal Aviation Administration, Department of Transportation
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 20, 2008, vol. 73, no. 55, page 15042. This project involves the random and representative sampling of Flight Attendants currently employed by U.S. air carriers.
Notice of Intent To Rule on Request To Release Airport Property at the Brownsville/South Padre Island International Airport, Brownsville, TX
Document Number: E8-15021
Type: Notice
Date: 2008-07-02
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to rule and invite public comment on the release of land at the Brownsville/South Padre Island International Airport under the provisions of Section 125 of the Wendell H. Ford Aviation Investment Reform Act for the 21st Century (AIR 21).
Proposed Establishment of Low Altitude Area Navigation Route (T-Route); Houston, TX
Document Number: E8-15018
Type: Proposed Rule
Date: 2008-07-02
Agency: Federal Aviation Administration, Department of Transportation
This action proposes to establish a low altitude Area Navigation (RNAV) route, designated T-254, in the Houston, TX, terminal area. T-routes are low altitude Air Traffic Service routes, based on RNAV, for use by aircraft that have instrument flight rules (IFR) approved Global Positioning System (GPS)/Global Navigation Satellite System (GNSS) equipment. This action would enhance safety and improve the efficient use of the navigable airspace in the Houston, TX, terminal area.
Airworthiness Directives; Fokker Model F.28 Mark 0070 and Mark 0100 Airplanes
Document Number: E8-14976
Type: Proposed Rule
Date: 2008-07-02
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to supersede an existing airworthiness directive (AD) that applies to certain Fokker Model F.28 Mark 0070 and 0100 airplanes. The existing AD currently requires a one-time inspection of the main landing gear (MLG) main fitting for cracks, and repair if necessary. The existing AD also currently requires installing a placard and revising the airplane flight manual to include procedures to prohibit the application of brakes during backward movement of the airplane. This proposed AD would require repetitive eddy current inspections of the MLG main fitting and rework before further flight as applicable. This proposed AD results from reports that a final solution eliminating the cause of the crack initiation mechanism is not yet available and that repetitive inspections are necessary. We are proposing this AD to detect and correct cracks in the MLG main fitting, which could result in reduced structural integrity of the MLG main fitting.
Airworthiness Directives; Boeing Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-200C, 747-200F, 747-300, 747-400, 747-400D, 747-400F, 747SR, and 747SP Series Airplanes
Document Number: E8-14974
Type: Proposed Rule
Date: 2008-07-02
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to supersede an existing airworthiness directive (AD) that applies to all Boeing Model 747 series airplanes. The existing AD currently requires repetitive detailed inspections of the aft pressure bulkhead for indications of ``oil cans'' and previous oil can repairs, and corrective actions, if necessary. An oil can is an area on a pressure dome web that moves when pushed from the forward side. This proposed AD would reduce the compliance time for the initial detailed inspection and clarify the applicability. This proposed AD results from a report that cracks in oil-canned areas were found during an inspection of the aft pressure bulkhead. We are proposing this AD to detect and correct the propagation of fatigue cracks in the vicinity of oil cans on the web of the aft pressure bulkhead, which could result in rapid decompression of the airplane and overpressurization of the tail section, and consequent loss of control of the airplane.
Airworthiness Directives; Fokker Model F.28 Mark 0070 and 0100 Airplanes
Document Number: E8-14969
Type: Proposed Rule
Date: 2008-07-02
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; Bombardier Model DHC-8-400, DHC-8-401, and DHC-8-402 Airplanes
Document Number: E8-14964
Type: Proposed Rule
Date: 2008-07-02
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:
Establishment of Class E Airspace; Salida, CO
Document Number: E8-14939
Type: Rule
Date: 2008-07-02
Agency: Federal Aviation Administration, Department of Transportation
This action will establish Class E airspace at Salida, CO. Controlled airspace is necessary to accommodate aircraft using a new Area Navigation (RNAV) Global Positioning System (GPS) Standard Instrument Approach Procedure (SIAP) at Harriet Alexander Field. This will improve the safety of Instrument Flight Rules (IFR) aircraft executing the new RNAV GPS SIAP at Harriet Alexander Field, Salida, CO.
Airworthiness Directives; Hartzell Propeller Inc. ( )HC-( )(2,3)Y(K,R)-2 Two- and Three-Bladed Compact Series Propellers
Document Number: E8-14312
Type: Rule
Date: 2008-07-02
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for Hartzell Propeller Inc. left-hand rotating ( )HC-( )(2,3)Y(K,R)-2 two- and three-bladed, aluminum hub, ``compact'' series propellers, with hubs having a non-suffix serial number, and lubrication holes located on the shoulder of the hub blade socket. These propellers are installed on Lycoming Engines LIO-360 series and LO-360 series reciprocating engines installed on Piper Aircraft, Inc. Seneca PA-34-200 and Seminole PA-44-180, and Hawker Beechcraft Corporation Model 76 Duchess, airplanes. This AD requires initial and repetitive eddy current inspections (ECI), of the area around the lubrication holes of the hub blade sockets. This AD results from four reports of propeller hub cracks, including two in-flight blade separation events. We are issuing this AD to prevent failure of the propeller hub, which could result in blade separation and loss of control of the airplane.
Airworthiness Directives; Turbomeca S.A. Arrius 2F Turboshaft Engines
Document Number: E8-14311
Type: Rule
Date: 2008-07-02
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) 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; Dornier Model 328-100 Airplanes
Document Number: E8-14205
Type: Rule
Date: 2008-07-02
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; ATR Model ATR42-200, -300, -320, -500 Airplanes; and Model ATR72-101, -201, -102, -202, -211, -212, and -212A Airplanes
Document Number: E8-14191
Type: Rule
Date: 2008-07-02
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; Boeing Model 757 Airplanes Equipped With Rolls Royce RB211-535E Engines
Document Number: E8-14190
Type: Rule
Date: 2008-07-02
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for certain Boeing Model 757 airplanes equipped with Rolls Royce RB211-535E engines. This AD requires repetitive inspections for signs of damage of the aft hinge fittings and attachment bolts of the thrust reversers, and related investigative and corrective actions if necessary. This AD results from reports of several incidents of bolt failure at the aft hinge fittings of the thrust reversers due to, among other things, high operational loads. We are issuing this AD to prevent failure of the attachment bolts and consequent separation of a thrust reverser from the airplane during flight, which could result in structural damage to the airplane.
Airworthiness Directives; Boeing Model 767-200, -300, and -400ER Series Airplanes
Document Number: E8-14189
Type: Rule
Date: 2008-07-02
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for certain Boeing Model 767-200, -300, and -400ER series airplanes. This AD requires an inspection to determine the manufacturer and manufacture date of the oxygen masks in the passenger service units and the flight attendant and lavatory oxygen boxes, as applicable. This AD also requires related investigative/corrective actions if necessary. This AD results from a report that several passenger masks with broken in-line flow indicators were found following a mask deployment. We are issuing this AD to prevent the in-line flow indicators of the passenger oxygen masks from fracturing and separating, which could inhibit oxygen flow to the masks and consequently result in exposure of the passengers and cabin attendants to hypoxia following a depressurization event.
Airworthiness Directives; Boeing Model 747-400, 747-400D, and 747-400F Series Airplanes
Document Number: E8-14188
Type: Rule
Date: 2008-07-02
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 747-400, 747-400D, and 747-400F series airplanes. This AD requires replacement of an electronic flight instrument system/ engine indicating and crew alerting system (EFIS/EICAS) interface unit (EIU) located on the E2-6 shelf of the main equipment center with a new or modified EIU. This AD results from two instances where all six integrated display units (IDUs) on the flight deck panels went blank in flight. We are issuing this AD to prevent loss of the IDUs due to failure of all three EIUs, which could result in the inability of the flightcrew to maintain safe flight and landing of the airplane.
Airworthiness Directives; Hawker Beechcraft Corporation (Type Certificates No. 3A15, No. 3A16, No. A23CE, and No. A30CE Previously Held by Raytheon Aircraft Company) F33 Series and Models G33, V35B, A36, A36TC, B36TC, 95-B55, D55, E55, A56TC, 58, 58P, 58TC, G58, and 77 Airplanes
Document Number: E8-14090
Type: Rule
Date: 2008-07-02
Agency: Federal Aviation Administration, Department of Transportation
The FAA adopts a new airworthiness directive (AD) for certain Hawker Beechcraft Corporation F33 series and Models G33, V35B, A36, A36TC, B36TC, 95-B55, D55, E55, A56TC, 58, 58P, 58TC, G58, and 77 airplanes. This AD requires you to replace certain circuit breaker toggle switches with improved design circuit breaker toggle switches. This AD results from reports of certain circuit breaker toggle switches used in various electrical systems throughout the affected airplanes overheating. We are issuing this AD to prevent failure of the circuit breaker toggle switch, which could result in smoke in the cockpit and the inability to turn off the switch.
Airworthiness Directives; Bombardier Model DHC-8-400 Series Airplanes
Document Number: E8-13728
Type: Rule
Date: 2008-07-02
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:
Advisory Circulars: Extended Operations (ETOPS) and Polar Operations, AC 121-42B and Extended Operations (ETOPS) and Operations in the North Polar Area, AC 135-42
Document Number: E8-14879
Type: Notice
Date: 2008-07-01
Agency: Federal Aviation Administration, Department of Transportation
The issuance of Advisory Circular (AC) 121-42B, Extended Operations (ETOPS) and Polar Operations, provides certificate holders with guidance for obtaining operational approval to conduct ETOPS under 14 CFR part 121. The issuance of AC 135-42, Extended Operations (ETOPS) and Operations in the North Polar Area, provides certificate holders with guidance for obtaining operational approval to conduct Extended Operations (ETOPS) under 14 CFR part 135.
Airworthiness Directives; Eurocopter France Model AS 355 N Helicopters
Document Number: E8-14717
Type: Rule
Date: 2008-07-01
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for Eurocopter France Model AS 355 N helicopters. 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 European Aviation Safety Agency (EASA), the technical agent for France, with which we have a bilateral agreement, states in the MCAI: ``This Airworthiness Directive (AD) is issued because it was found that the power drawn by the starter generators from the engines is above the consumption capacity at altitudes above 3,000 meters, declared for the engines of AS 355 N helicopters. Excessive power consumption of the starter generators reduces the engine surge margin, which can result in engine failure.'' After engine start, the starter generator functions as the normal operational electrical generator. We are issuing this AD to require actions that are intended to address this unsafe condition.
Standard Instrument Approach Procedures, and Takeoff Minimums and Obstacle Departure Procedures; Miscellaneous Amendments
Document Number: E8-14172
Type: Rule
Date: 2008-07-01
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.
Airworthiness Directives; Viking Air Limited Models DHC-6-1, DHC-6-100, DHC-6-200, and DHC-6-300 Airplanes
Document Number: E8-13848
Type: Rule
Date: 2008-07-01
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) 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; Viking Air Limited Models DHC-6-1, DHC-6-100, DHC-6-200, and DHC-6-300 Airplanes
Document Number: E8-13844
Type: Rule
Date: 2008-07-01
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) 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; Eurocopter France Model AS355E, F, F1, F2, and N Helicopters
Document Number: E8-14723
Type: Proposed Rule
Date: 2008-06-30
Agency: Federal Aviation Administration, Department of Transportation
This document revises an earlier proposed superseding airworthiness directive (AD) for the specified Eurocopter France (ECF) model helicopters. That AD currently requires certain checks of the magnetic chip detector plug (chip detector) and the main gearbox (MGB) oil-sight glass, certain inspections of the lubrication pump (pump), and replacing the MGB and the pump with an airworthy MGB and pump, if necessary. Also, the AD requires that before a pump or MGB with any hours time-in-service (TIS) can be installed, it must meet the AD requirements. The earlier proposed superseding AD proposed retaining those requirements but proposed adding all serial-numbered pumps to the applicability. This supplemental proposal is prompted by an improved procedure for detecting oil pump wear earlier and is considered more accurate than the procedure proposed previously. The actions specified by the proposed AD are intended to implement improved procedures to detect a failing MGB oil pump, to prevent failure of the MGB pump, seizure of the MGB, loss of drive to an engine and main rotor, and subsequent loss of control of the helicopter.
Airworthiness Directives; Dowty Propellers Models R354/4-123-F/13; R354/4-123-F/20; R354/4-123-F/21; R375/4-123-F/21; R389/4-123-F/25; R354/4-123-F/26; and R390/4-123-F/27 Propellers
Document Number: E8-14715
Type: Proposed Rule
Date: 2008-06-30
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) issued by the European Aviation Safety Agency (EASA) to identify and correct an unsafe condition on Dowty Propellers models R354/4-123-F/13; R354/4-123-F/20; R354/4-123-F/21; R375/4-123-F/21; R389/4-123-F/25; R354/4-123-F/26; and R390/4-123-F/27 propellers. The MCAI describes the unsafe condition as:
Executive Committee of the Aviation Rulemaking Advisory Committee; Meeting
Document Number: E8-14573
Type: Notice
Date: 2008-06-30
Agency: Federal Aviation Administration, Department of Transportation
The FAA is issuing this notice to advise the public of a meeting of the Executive Committee of the Aviation Rulemaking Advisory Committee.
Petition for Exemption; Summary of Petition Received
Document Number: E8-14572
Type: Notice
Date: 2008-06-30
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; Avions Marcel Dassault-Breguet Model Falcon 10 Airplanes
Document Number: E8-14575
Type: Proposed Rule
Date: 2008-06-27
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to supersede an existing airworthiness directive (AD) that applies to all Avions Marcel Dassault-Breguet Model Falcon 10 airplanes. The existing AD currently requires either revising the airplane flight manual (AFM) and installing a placard in the flight deck to prohibit flight into known or forecasted icing conditions, or repetitively inspecting for delamination of the flexible hoses in the wing (slat) anti-icing system and performing corrective actions if necessary. The existing AD also requires replacement of the flexible hoses installed in the slat anti-icing systems, which ends the repetitive inspections. This proposed AD would continue to require replacement of the flexible hoses installed in the slat anti-icing systems with new hoses, but at intervals defined in flight hours instead of flight cycles. This proposed AD results from information we received from operators and the airplane manufacturer indicating that the repetitive interval for the required replacement deviated from the referenced service information. We are proposing this AD to prevent collapse of the flexible hoses in the slat anti-icing system, which could lead to insufficient anti-icing capability and, if icing is encountered in this situation, could result in reduced controllability of the airplane.
IFR Altitudes; Miscellaneous Amendments
Document Number: E8-14543
Type: Rule
Date: 2008-06-27
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.
Amendment of Class E Airspace; Gettysburg, PA
Document Number: E8-14384
Type: Rule
Date: 2008-06-27
Agency: Federal Aviation Administration, Department of Transportation
This action confirms the effective date of a direct final rule published in the Federal Register (73 FR 8593) that modifies Class E Airspace at Gettysburg, PA. Additional controlled airspace at Gettysburg Regional Airport will now provide the controlled airspace required to support the new Copter Area Navigation (RNAV) Global Positioning System (GPS) 070 Point in Space (PinS) approach developed to facilitate helicopter medical flight arrivals and departures at Gettysburg Hospital, Gettysburg, PA.
Amendment of Class E Airspace; Indianapolis, IN
Document Number: E8-14381
Type: Rule
Date: 2008-06-27
Agency: Federal Aviation Administration, Department of Transportation
This action confirms the effective date of a direct final rule that establishes additional Class E airspace at Indianapolis, IN, published in the Federal Register April 2, 2008 (73 FR 17887) Docket No. FAA-2008-0163. This action also makes a minor correction to the geographic coordinates of Hendricks County Gordon Graham Field.
Establishment of Class E Airspace; Philippi, WV
Document Number: E8-14164
Type: Rule
Date: 2008-06-27
Agency: Federal Aviation Administration, Department of Transportation
This action establishes Class E airspace at Philippi, WV, to accommodate a new Area Navigation (RNAV) Global Positioning System (GPS) Standard Instrument Approach Procedures (SIAP) Runways (RWY) 08- 26 that has been developed for Philippi/Barbour County Regional Airport. As a result, controlled airspace extending upward from 700 feet Above Ground Level (AGL) is needed to contain the SIAP and for Instrument Flight Rule (IFR) operations at Philippi/Barbour County Regional Airport. The operating status of the airport will change from Visual Flight Rules (VFR) to include IFR operations concurrent with the publication of the SIAP.
Airworthiness Directives; Bombardier Model DHC-8-400 Series Airplanes
Document Number: E8-14482
Type: Proposed Rule
Date: 2008-06-26
Agency: Federal Aviation Administration, Department of Transportation
The FAA is revising an earlier NPRM for an airworthiness directive (AD) that applies to certain Bombardier Model DHC-8-400 series airplanes. The original NPRM would have superseded an existing AD that currently requires inspecting all barrel nuts to determine if the barrel nuts have a certain marking, inspecting affected bolts to determine if the bolts are pre-loaded correctly, and replacing all hardware if the pre-load is incorrect. For airplanes on which the pre- load is correct, the existing AD requires doing repetitive visual inspections for cracking of the barrel nuts and cradles and replacing all hardware for all cracked barrel nuts. The existing AD also requires replacement of all hardware for certain affected barrel nuts that do not have cracking, which would end the repetitive inspections for those airplanes. The existing AD also provides an optional replacement for all affected barrel nuts. The original NPRM proposed to require replacement of all affected barrel nuts. The original NPRM resulted from reports of cracking in the barrel nuts at the four primary front spar wing-to-fuselage attachment joints. This new action revises the original NPRM by adding, for certain airplanes, application of a certain compound to the affected barrel nuts and bolts. We are proposing this supplemental NPRM to detect and correct cracking of the barrel nuts at the wing front spar wing-to-fuselage joints, which could result in reduced structural integrity of the wing-to-fuselage attachments and consequent detachment of the wing.
Airworthiness Directives; Airbus Model A330 and A340 Airplanes
Document Number: E8-14480
Type: Proposed Rule
Date: 2008-06-26
Agency: Federal Aviation Administration, Department of Transportation
The FAA is revising an earlier supplemental NPRM (SNPRM) for an airworthiness directive (AD) that applies to all Airbus Model A330- 200, A330-300, A340-200, and A340-300 series airplanes; and Model A340- 541 and A340-642 airplanes. The original NPRM would have superseded an existing AD that currently requires operators to revise the Airworthiness Limitations section (ALS) of the Instructions for Continued Airworthiness (ICA) 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. The original NPRM proposed to revise the ALS, for all affected airplanes, by adding new Airworthiness Limitations Items (ALIs) to incorporate service life limits for certain items and inspections to detect fatigue cracking, accidental damage or corrosion in certain structures, in accordance with the revised ALS of the ICA. The original NPRM resulted from the issuance of new and more restrictive service life limits and structural inspections based on fatigue testing and in-service findings. The first supplemental NPRM revised the original NPRM by adding airplanes, adding new requirements, and including more restrictive compliance thresholds and intervals. This new action revises the first supplemental NPRM by adding a new weight variant configuration, and including more restrictive compliance thresholds and intervals. We are proposing this second supplemental NPRM to detect and correct fatigue cracking, accidental damage, or corrosion in principal structural elements, and to prevent failure of certain life-limited parts, which could result in reduced structural integrity of the airplane.
Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model ERJ 170 and ERJ 190 Airplanes
Document Number: E8-14476
Type: Proposed Rule
Date: 2008-06-26
Agency: Federal Aviation Administration, Department of Transportation
We are revising an earlier NPRM for the products listed above. This action revises the earlier NPRM by expanding the scope. 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:
Public Notice For Waiver of Aeronautical Land-Use Assurance; MBS International Airport, Saginaw, Michigan
Document Number: E8-14386
Type: Notice
Date: 2008-06-26
Agency: Federal Aviation Administration, Department of Transportation
The Federal Aviation Administration (FAA) is considering a proposal to change a portion of the MBS International Airport (MBS) from aeronautical use to non-aeronautical use and to authorize the sale of the airport property. The proposal consists of the sale of vacant, unimproved land owned by the MBS International Airport Commission (Commission). The Commission has requested from FAA a ``Release from Federal agreement obligated land covenants'' to sell a portion of Parcel 6 which was acquired on March 14, 1949, under Instrument of Transfer from the United States of America, acting by and through the War Assets Administrator, to the Cities of Saginaw, Bay City, and Midland (recorded in Liber 802, pages 206-216). There are no impacts to the airport by allowing the Commission to dispose of the vacant property. Approval does not constitute a commitment by the FAA to financially assist in the disposal of the airport property nor a determination of eligibility for grant-in-aid funding from the FAA. The disposition of proceeds from the disposal 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.
Establishment of Class E Airspace; Canon, GA
Document Number: E8-14168
Type: Rule
Date: 2008-06-26
Agency: Federal Aviation Administration, Department of Transportation
This action establishes Class E Airspace at Canon, GA, to accommodate the new Area Navigation (RNAV) Global Positioning System (GPS) Standard Instrument Approach Procedures (SIAPs) that have been developed for Franklin County Airport. Controlled airspace extending upward from 700 feet Above Ground Level (AGL) is needed to contain the SIAP and for Instrument Flight Rule (IFR) operations at Franklin County Airport. The operating status of the airport will change from Visual Flight Rules (VFR) to include IFR operations concurrent with the publication of the SIAP.
Amendment of Class E Airspace; Danville, KY
Document Number: E8-14167
Type: Rule
Date: 2008-06-26
Agency: Federal Aviation Administration, Department of Transportation
This action confirms the effective date of a direct final rule published in the Federal Register (73 FR 15058) that amends the Class E airspace area to support Area Navigation (RNAV) Global Positioning System (GPS) Standard Instrument Approach Procedures (IAPs) that were developed to serve the Stuart Powell Field Airport. Additionally, the direct final rule made a technical amendment addressing the airport's name change from Goodall Field Airport to Stuart Powell Field Airport.
Establishment of Class E Airspace; Susquehanna, PA
Document Number: E8-14165
Type: Rule
Date: 2008-06-26
Agency: Federal Aviation Administration, Department of Transportation
This action confirms the effective date of a direct final rule published in the Federal Register (73 FR 14679) that establishes Class E Airspace at Susquehanna, PA, to support a new Area Navigation (RNAV) Global Positioning System (GPS) Special Instrument Approach Procedure (IAP) that has been developed for medical flight operations into the Susquehanna High School Heliport.
Establishment of Class E Airspace; Sunbury, PA
Document Number: E8-14163
Type: Rule
Date: 2008-06-26
Agency: Federal Aviation Administration, Department of Transportation
This action confirms the effective date of a direct final rule published in the Federal Register (73 FR 14677) that establishes Class E Airspace at Sunbury, PA to support a new Area Navigation (RNAV) Global Positioning System (GPS) Special Instrument Approach Procedure (IAP) that has been developed for medical flight operations into the Sunbury Community Hospital Airport.
Standard Instrument Approach Procedures, and Takeoff Minimums and Obstacle Departure Procedures; Miscellaneous Amendments
Document Number: E8-14162
Type: Rule
Date: 2008-06-26
Agency: Department of Transportation, Federal Aviation Administration
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.
Special Conditions: Embraer S.A. Model EMB-500; Full Authority Digital Engine Control (FADEC) System.
Document Number: E8-14383
Type: Rule
Date: 2008-06-25
Agency: Federal Aviation Administration, Department of Transportation
These special conditions are issued for the Embraer S.A. Model EMB-500 airplane. This airplane will have a novel or unusual design feature(s) associated with the use of an electronic engine control system instead of a traditional mechanical control system. 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.
Special Conditions; Honda Aircraft Company, Model HA-420 HondaJet Airplane; Fire Extinguishing
Document Number: E8-14380
Type: Proposed Rule
Date: 2008-06-25
Agency: Federal Aviation Administration, Department of Transportation
This notice proposes special conditions for the Honda Aircraft Company, Model HA-420 HondaJet Airplane. This new airplane will have novel and unusual design features not typically associated with normal, utility, acrobatic, and commuter category airplanes. These design features include turbofan engines and engine location, for which the applicable regulations do not contain adequate or appropriate airworthiness standards. These proposed special conditions contain the additional airworthiness standards that the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards.
Airworthiness Directives; Turbomeca S.A. Models Arriel 1E2, 1S, and 1S1 Turboshaft Engines
Document Number: E8-14321
Type: Proposed Rule
Date: 2008-06-25
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) 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; Pratt & Whitney Canada PW206A, PW206B, PW206B2, PW206C, PW206E, PW207C, PW207D, and PW207E Turboshaft Engines
Document Number: E8-14320
Type: Proposed Rule
Date: 2008-06-25
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) issued by the 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. PC-6 Series Airplanes
Document Number: E8-14106
Type: Rule
Date: 2008-06-25
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) 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; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-135BJ Airplanes
Document Number: E8-13926
Type: Rule
Date: 2008-06-25
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:
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