Federal Aviation Administration July 2008 – Federal Register Recent Federal Regulation Documents

Results 101 - 140 of 140
Airworthiness Directives; Boeing Model 777-200, -200LR, -300, and -300ER Series Airplanes Approved for Extended-Range Twin-Engine Operational Performance Standards (ETOPS)
Document Number: E8-15371
Type: Rule
Date: 2008-07-08
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for certain Boeing Model 777-200, -200LR, -300, and -300ER series airplanes. This AD requires a one-time inspection to determine the part number of the cargo compartment fire suppression filter/regulator. This AD also requires, for certain airplanes, a revision of the ``Maximum Diversion Time in Minutes'' for ETOPS operation specified in the Operations Specifications. For certain airplanes, this AD also provides for optional replacement of the cargo compartment fire suppression filter/ regulator, which would allow revision of the ``Maximum Diversion Time in Minutes'' for ETOPS operation specified in the Operations Specifications to restore the airplane's full ETOPS capability. This AD results from a report that the filter/regulator installed in the cargo fire suppression system did not meter the Halon for the certified duration during ETOPS flight tests. We are issuing this AD to prevent ETOPS operation with insufficient cargo fire suppression capability, which could result in an uncontained fire in the cargo compartment.
Airworthiness Directives; Dassault Model Falcon 2000 Airplanes
Document Number: E8-14579
Type: Rule
Date: 2008-07-08
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; APEX Aircraft Model CAP 10B Airplanes
Document Number: E8-14484
Type: Rule
Date: 2008-07-08
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; ATR Model ATR42 Airplanes and Model ATR72-101, -102, -201, -202, -211, and -212 Airplanes
Document Number: E8-14477
Type: Rule
Date: 2008-07-08
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 737-300 and -400 Series Airplanes
Document Number: E8-14475
Type: Rule
Date: 2008-07-08
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for certain Boeing Model 737-300 and -400 series airplanes. This AD requires testing and inspecting a certain web panel of the main wheel well pressure deck to determine the material type and thickness; and related investigative and corrective actions if necessary. This AD results from several reports indicating that cracks ranging from 0.8 to 8.0 inches long were found on a certain web panel of the main wheel well pressure deck. We are issuing this AD to prevent fatigue cracking in the web panel of the main wheel well pressure deck, which could result in venting and consequent decompression of the airplane.
Airworthiness Directives; McDonnell Douglas Model DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), DC-9-87 (MD-87), and MD-88 Airplanes
Document Number: E8-14472
Type: Rule
Date: 2008-07-08
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for all McDonnell Douglas Model DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD- 83), DC-9-87 (MD-87), and MD-88 airplanes. This AD requires repetitive inspections for cracking of the overwing frames from stations 845 to 905 (MD-87 stations 731 to 791), 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; Boeing Model 737-100, -200, -200C, -300, -400, and -500 Series Airplanes
Document Number: E8-14471
Type: Rule
Date: 2008-07-08
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for certain Boeing Model 737-100, -200, -200C, -300, -400, and -500 series airplanes. This AD requires various repetitive inspections for cracking of the upper frame to side frame splice of the fuselage, and other specified and corrective actions if necessary. This AD also provides for an optional preventive modification, which terminates the repetitive inspections. This AD results from a report that the upper frame of the fuselage was severed between stringers S-13L and S-14L at station 747, and the adjacent frame at station 767 had a 1.3-inch-long crack at the same stringer location. We are issuing this AD to detect and correct fatigue cracking of the upper frame to side frame splice of the fuselage, which could result in reduced structural integrity of the frame and adjacent lap joint. This reduced structural integrity can increase loading in the fuselage skin, which will accelerate skin crack growth and result in decompression of the airplane.
Airworthiness Directives; Lockheed Model 1329 Series Airplanes
Document Number: E8-14470
Type: Rule
Date: 2008-07-08
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for certain Lockheed Model 1329 series airplanes. This AD requires determining the part number on the steering cylinder assembly for the nose landing gear (NLG), determining the total flight cycles accumulated on the NLG steering cylinder assembly, repetitively replacing the assembly, inspecting for missing tow turning limit markings, and performing corrective actions if necessary. This AD results from reports of numerous failures of the NLG steering cylinder. We are issuing this AD to prevent the loss of hydraulic pressure and steering control.
Airworthiness Directives; Gulfstream Aerospace LP Model Astra SPX, 1125 Westwind Astra, and Gulfstream 100 Airplanes
Document Number: E8-14469
Type: Rule
Date: 2008-07-08
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 A330 Airplanes and Model A340-200 and -300 Series Airplanes
Document Number: E8-14468
Type: Rule
Date: 2008-07-08
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for certain Airbus Model A330 airplanes and Model A340-200 and -300 series airplanes. This AD requires revising the airplane flight manual (AFM) to prohibit the flightcrew from performing CAT 2 and CAT 3 automatic landings and roll-outs at certain airports. This AD also provides an optional terminating action for the AFM revision. This AD results from data showing that the magnetic variation table installed in certain Honeywell and Northrop Grumman air data inertial reference units (ADIRUs) is obsolete at certain airports. We are issuing this AD to prevent the airplane from departing the runway during a CAT 2 or CAT 3 automatic landing or roll-out, due to differences between actual magnetic variation and the values in the ADIRU magnetic variation tables.
Airworthiness Directives; Dassault Model Mystere-Falcon 900, Falcon 900EX, and Falcon 2000 Airplanes
Document Number: E8-15370
Type: Proposed Rule
Date: 2008-07-07
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; Lockheed Model 382, 382B, 382E, 382F, 382G, and 382J Series Airplanes
Document Number: E8-15181
Type: Rule
Date: 2008-07-07
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for all Lockheed Model 382, 382B, 382E, 382F, 382G, and 382J series airplanes. This AD requires, among other actions, an inspection to determine whether a certain upper engine mount bolt is installed, and replacement of any discrepant upper engine mount bolt with a new one. This AD results from a report indicating that several upper engine mount bolts manufactured by a certain supplier broke during installation. We are issuing this AD to prevent failure of the upper engine mount bolts, which could result in reduced structural capability of an engine mount, and possible separation of a strut and engine from the airplane during flight.
Agency Information Collection Activity Seeking OMB Approval
Document Number: E8-15063
Type: Notice
Date: 2008-07-07
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) revision of a current information collection. The Federal Register Notice with a 60-day comment period soliciting comments on the following collection of information was published on April 23, 2008, vol. 73, no. 79, page 21999. Part A of Subtitle VII of the Revised Title 49 U.S.C. authorizes the issuance of regulations governing the use of navigable airspace. Information is collected to determine compliance with Federal regulations.
Establishment of Class E Airspace; Pampa, TX
Document Number: E8-14923
Type: Rule
Date: 2008-07-07
Agency: Federal Aviation Administration, Department of Transportation
This action establishes Class E5 airspace at Pampa, TX. Controlled airspace is necessary to accommodate aircraft using new RNAV Global Positioning System (GPS) Standard Instrument Approach Procedures (SIAP) at Mesa Vista Ranch Airport. The FAA is proposing this action to enhance the safety and management of Instrument Flight Rules (IFR) aircraft operations at Mesa Vista Ranch Airport, Pampa, TX.
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 http://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: