Federal Aviation Administration 2008 – Federal Register Recent Federal Regulation Documents
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Airworthiness Directives; Cessna Aircraft Company Models 175 and 175A Airplanes
We are adopting a new airworthiness directive (AD) for certain Cessna Aircraft Company (Cessna) Models 175 and 175A airplanes. This AD requires you to check the airplane logbook to determine if the original engine mounting brackets have been replaced. If the original engine mounting brackets are still installed, this AD requires you to repetitively inspect those brackets for cracks and replace any cracked engine mounting bracket. After replacing all four original engine mounting brackets, no further action will be required by this AD. This AD was prompted by a report that the engine became detached from the firewall during landing on one of the affected airplanes. We are issuing this AD to detect and correct cracks in the engine mounting brackets, which could result in failure of the engine mounting bracket. This failure could lead to the engine detaching from the firewall.
Airworthiness Directives; MD Helicopters, Inc. Model MD900 (including the MD902 Configuration) Helicopters
This document proposes adopting a new airworthiness directive (AD) for the specified MD Helicopters, Inc. (MDHI) model helicopters that would require, within 30 days, reducing the current gross weight limit to a maximum gross weight limit of 5,400 pounds and inserting a copy of this AD into the Limitations section of the Rotorcraft Flight Manual (RFM) or making certain optional modifications that constitute terminating actions. This proposal is prompted by flight tests that show that the information currently listed in the Limitations section of the RFM is inconsistent with the actual performance of the helicopter. The actions specified by the proposed AD are intended to prevent loss of directional control of the helicopter.
Airworthiness Directives; Bell Helicopter Textron Canada Model 222, 222B, 222U, 230, and 430 Helicopters
This document proposes superseding an existing airworthiness directive (AD) for Bell Helicopter Textron Canada (BHTC) helicopters. That AD currently requires certain checks and inspections of the tail rotor blades. If a crack is found, the existing AD requires replacing the tail rotor blade (blade) with an airworthy blade before further flight. This action would require the same checks and inspections until they are required to be replaced and would remove certain serial numbered and specifically coded tail rotor blades from the applicability of the AD. This proposal is prompted by the approved rework of certain tail rotor blades and two newly redesigned tail rotor blades, which, if installed, constitutes terminating action for the inspection requirements. The actions specified by the proposed AD are intended to detect a crack in a blade, and to prevent loss of a blade and subsequent loss of control of the helicopter.
Consensus Standards, Light-Sport Aircraft
This notice announces the availability of three new consensus standards and a revision to a previously accepted consensus standard relating to the provisions of the Sport Pilot and Light-Sport Aircraft rule issued July 16, 2004, and effective September 1, 2004. ASTM International Committee F37 on Light Sport Aircraft developed the new and revised standards with Federal Aviation Administration (FAA) participation. By this notice, the FAA finds the new and revised standards acceptable for certification of the specified aircraft under the provisions of the Sport Pilot and Light-Sport Aircraft rule.
Airworthiness Directives; McDonnell Douglas Model DC-10-10, DC-10-10F, DC-10-15, DC-10-30, DC-10-30F (KC-10A and KDC-10), DC-10-40, DC-10-40F, MD-10-10F, MD-10-30F, MD-11, and MD-11F Airplanes
The FAA proposes to supersede an existing airworthiness directive (AD) that applies to certain McDonnell Douglas transport category airplanes. The existing AD currently requires modification of the installation wiring for the electric motor-operated auxiliary hydraulic pumps in the right wheel well area of the main landing gear; repetitive inspections of the numbers 1 and 2 electric motors of the auxiliary hydraulic pumps for electrical resistance, continuity, mechanical rotation, and associated airplane wiring resistance/voltage; and corrective actions if necessary. This proposed AD would, for certain airplanes, also require modifying and rerouting, as applicable, certain components of the wiring of the electric motor for the auxiliary hydraulic pump located in the right wheel well. This proposed AD results from reports of failure of the electric motor for the auxiliary hydraulic pump. We are proposing this AD to prevent failure of the electric motors of the hydraulic pump and associated wiring, which could result in fire at the auxiliary hydraulic pump and consequent damage to the adjacent electrical equipment and/or structure.
Petition for Exemption; Summary of Petition Received
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.
Notice of Intent To Rule on Request To Release Airport Property at the Liberal Mid-America Regional Airport, Liberal, KS
The FAA proposes to rule and invites public comment on the release of land at the Liberal Mid-America Regional Airport under the provisions of Section 125 of the Wendell H. Ford Aviation Investment Reform Act for the 21st Century (AIR 21).
Notice of Intent To Rule on Request To Release Airport Property at the Rialto Municipal Airport, Rialto, San Bernardino County, CA
The FAA proposes to rule and invite public comment on the release of land at the Rialto Municipal Airport under the provisions of section 125 of the Wendell H. Ford Aviation Investment Reform Act for the 21st Century (AIR 21).
Petition for Exemption; Summary of Petition Received
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.
Petition for Exemption; Summary of Petition Received
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.
Revision of Class E Airspace; Kivalina, AK
This action revises Class E airspace at Kivalina, AK, to provide adequate controlled airspace to contain aircraft executing Standard Instrument Approach Procedures (SIAPs) and Obstacle Departure Procedures (ODPs). Two SIAPs are being amended for the Kivalina Airport. Additionally, one textual ODP is being developed. This action revises existing Class E airspace upward from 700 feet (ft.) and 1,200 ft. above the surface at Kivalina Airport, Kivalina, AK.
Establishment of Class E Airspace; Eek, AK
This action establishes Class E airspace at Eek, AK to provide adequate controlled airspace to contain aircraft executing Standard Instrument Approach Procedures (SIAPs) and Obstacle Departure Procedures (ODPs). Two SIAPs and a textual ODP are being developed for the Eek Airport at Eek Alaska. This action establishes Class E airspace upward from 700 feet (ft.) above the surface at the Eek Airport, Eek, AK.
Revision of Class E Airspace; Kake, AK
This action revises Class E airspace at Kake, AK to provide adequate controlled airspace to contain aircraft executing public and private (Special) Instrument Approach and Departure Procedures. A Standard Instrument Approach Procedure (SIAP) and Standard Instrument Departure (SID) procedure are being developed for the Kake Airport. Additionally, a Special Area Navigation (RNAV) SID and two SIAPs are being amended. This action revises existing Class E airspace upward from 700 feet (ft.) above the surface at Kake Airport, Kake, AK.
Revision of Class E Airspace; Gulkana, AK
This action revises Class E airspace at Gulkana, AK to provide adequate controlled airspace to contain aircraft executing Standard Instrument Approach Procedures (SIAPs). Two SIAPs are being amended for the Gulkana Airport. This action revises existing Class E airspace upward from 700 feet (ft.) and 1,200 ft. above the surface at Gulkana Airport, Gulkana, AK. The present Class E2 Surface Area is not being amended.
Amendment of Class E Airspace; Salyer Farms, CA
This action will amend Class E airspace at Salyer Farms, CA. The El Rico Airport mentioned in the published description has been abandoned, making it necessary to realign the Class E Airspace area at Salyer Farms Airport. This action also makes a minor correction by removing the Salyer Farms RBN in the airport description.
Revision of Class E Airspace; Red Dog, AK
This action revises Class E airspace at Red Dog, AK, to provide adequate controlled airspace to contain aircraft executing Special Instrument Approach Procedures (IAPs) and Special Obstacle Departure Procedures (ODPs). A Special IAP and a Special Obstacle Departure Procedure (ODP) are being developed for the Red Dog Airport. Additionally, a Special IAP is being amended. This action revises existing Class E airspace upward from 700 feet (ft.) and 1,200 ft. above the surface at Red Dog Airport, Red Dog, AK.
Revision of Class E Airspace; Prospect Creek, AK
This action revises Class E airspace at Prospect Creek, AK, to provide adequate controlled airspace to contain aircraft executing Special Instrument Approach Procedures (IAPs) and Special Obstacle Departure Procedures (ODPs). Three Special IAPs are being developed for the Prospect Creek Airport. Addtionally, two Special IAPs and a Special ODP are being amended. This action revises existing Class E airspace upward from 700 feet (ft.) and 1,200 ft. above the surface at Prospect Creek Airport, Prospect Creek, AK.
Notification of Policy Revisions, and Requests for Comments on the Percentage of Fabrication and Assembly That Must Be Completed by an Amateur Builder To Obtain an Experimental Airworthiness Certificate for an Amateur-Built Aircraft; Extension of Comment Period
This notice announces an extension of the comment period for the proposed revisions to Chapter 4, Special Airworthiness Certification, Section 9 of the FAA Order 8130.2F, Airworthiness Certification of Aircraft and Related Products, and Advisory Circular (AC) 20-27G, Certification and Operation of Amateur-Built Aircraft (AC 20-27G is the result of combining AC 20-27F and AC 20-139, Commercial Assistance During Construction of Amateur-Built Aircraft), as well as for comments on the percentage of fabrication and assembly that must be completed by an amateur builder to obtain an experimental airworthiness certificate for an amateur-built aircraft. These and other related documents are located on the FAA main Web page. The Web link is: https://www.faa.gov/ aircraft/draft_docs/display_docs/index.cfm?DocType=Pubs.
Modification of Certain Medical Standards and Procedures and Duration of Certain Medical Certificates
This rule extends the duration of first- and third-class medical certificates for certain individuals. A first-class medical certificate is required when exercising airline transport pilot privileges and at least a third-class medical certificate when exercising private pilot privileges. Certain conforming amendments to medical certification procedures and some general editorial amendments are also adopted. The intent of this action is to improve the efficiency of the medical certification program and service provided to medical certificate applicants.
Petition for Exemption; Summary of Petition Received
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; General Electric Company CF34-1A, -3A, -3A1, -3A2, -3B, and -3B1 Turbofan Engines
The FAA proposes to adopt a new airworthiness directive (AD) for General Electric Company (GE) CF34-1A, -3A, -3A1, -3A2, -3B, and - 3B1 turbofan engines with high-pressure (HP) rotor 4-step air balance piston stationary seals (4-step seals), part numbers 4923T54G01, 6019T90G03, 6037T99G01, 6037T99G02, and 6037T99G03, installed. This proposed AD would require removing the 4-step seals and incorporating an 8-step seal at the next piece-part exposure. This proposed AD results from the investigation of an airplane accident. Both engines experienced high- altitude flameouts. Rotation of the HP rotors was not maintained during descent and the engines could not be restarted. We are proposing this AD to prevent the inability to restart both engines after flameout due to excessive friction of the 4-step seal, which could result in subsequent forced landing of the airplane.
Airworthiness Directives; General Electric Company (GE) CT58 Series Turboshaft Engines
The FAA proposes to adopt a new airworthiness directive (AD) for certain GE CT58 series turboshaft engines. This proposed AD would require recalculating the lives of certain part numbered compressor spools using a new repetitive heavy lift (RHL) multiplying factor. This proposed AD results from reports of cracks originating from the inner faces of the locking screw holes in the compressor spool. We are proposing this AD to prevent cracks due to RHL missions. Cracks could result in an uncontained rotor burst and damage to, or loss of, the helicopter and serious injuries to any person onboard.
Standard Instrument Approach Procedures, and Takeoff Minimums and Obstacle Departure Procedures; Miscellaneous Amendments
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.
Removal of Class E5 Airspace; Madison, CT
This action removes Class E5 airspace at Griswold Airport, Madison, CT, (N04). The VHF Omnidirectional Range (VOR) approach into Griswold Airport has been discontinued; eliminating the need for Class E5 700 foot controlled airspace.
Approval of Noise Compatibility Program; Orlando Executive Airport, Orlando, FL
The Federal Aviation Administration (FAA) announces its findings on the Noise Compatibility Program submitted by the Greater Orlando Aviation 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 December 31, 2007, the FAA determined that the noise exposure maps submitted by the Greater Orlando Aviation Authority under Part 150 were in compliance with applicable requirements. On June 23, 2008, the FAA approved the Orlando Executive Airport noise compatibility program. All of the recommendations of the program were approved.
Executive Committee of the Aviation Rulemaking Advisory; Meeting Cancellation
The FAA is issuing this notice to advise the public the July 23, 2008, meeting of the Executive Committee of the Aviation Rulemaking Advisory Committee (73 FR 36952, June 30, 2008) has been cancelled. The meeting will be rescheduled in a subsequent Federal Register notice.
Standard Instrument Approach Procedures, and Takeoff Minimums and Obstacle Departure Procedures; Miscellaneous Amendments
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; Maryland Air Industries, Inc., Model Fairchild F-27 and FH-227 Series Airplanes
We propose to adopt a new airworthiness directive (AD) for all Maryland Air Industries, Inc., Model Fairchild F-27 and FH-227 series airplanes. This proposed AD would require operators to modify their airplanes and revise their inspection or maintenance programs to incorporate instructions for maintenance and inspection of the fuel tank systems, as appropriate, by December 16, 2008, using information developed in accordance with SFAR 88. This proposed AD results from fuel system safety reviews done on similar airplane models in accordance with SFAR 88. These safety reviews identified potential unsafe conditions on Model Fairchild F-27 and FH-227 series airplanes for which the type certificate holder, Maryland Air Industries, Inc., has not conducted SFAR 88 safety reviews, has not provided corrective actions, and does not plan to do so. We are proposing this AD to reduce the potential of ignition sources inside fuel tanks, which, in combination with flammable fuel vapors, could result in fuel tank explosions and consequent loss of the airplane.
Proposed Establishment and Revocation of Class E Airspace; Lake Havasu, AZ
This action proposes to establish Class E airspace at the new Lake Havasu City Airport, Lake Havasu, AZ. Additional controlled airspace is necessary to accommodate aircraft using VHF Omni- Directional Radio Range/Distance Measuring Equipment (VOR/DME) Global Positioning System (GPS) Standard Instrument Approach Procedure (SIAP) at Lake Havasu City Airport, Lake Havasu, AZ. This action also would revoke Class E airspace at the old Lake Havasu Airport, Lake Havasu, AZ, as that airport has been abandoned. The FAA is proposing this action to enhance the safety and management of aircraft operations at Lake Havasu City Airport, Lake Havasu, AZ.
Revocation of Class E Airspace; Luke AFB, Phoenix, AZ
This action will revoke Class E airspace at Luke AFB, Phoenix, AZ. The United States Air Force (USAF) is closing the airport to Instrument Flight Rules (IFR) operations when the Air Traffic Control Tower (ATCT) is closed.
Establishment of Class E Airspace; Carson City, NV
This action will establish Class E airspace at Carson City, NV. Controlled airspace is necessary to accommodate aircraft using a new Area Navigation (RNAV) Global Positioning System (GPS) Standard Instrument Approach Procedure (SIAP) at Carson City Airport, Carson City, NV. This will improve the safety of Instrument Flight Rules (IFR) aircraft executing the new RNAV GPS SIAP at Carson City Airport, Carson City, NV.
Airworthiness Directives; Boeing Model 737-300, -400, and -500 Series Airplanes
We are adopting a new airworthiness directive (AD) for all Boeing Model 737-300, -400, and -500 series airplanes. This AD requires inspecting to determine if certain carriage spindles are installed, repetitive inspections for corrosion and indications of corrosion on affected carriage spindles, and if necessary, related investigative action and corrective action. This AD also provides optional terminating action. This AD results from a report of corrosion found on carriage spindles that are located on the outboard trailing edge flaps. We are issuing this AD to detect and correct corrosion of the carriage spindle, which could result in fracture. Fracture of both the inboard and outboard carriage spindles, in the forward ends through the large diameters, on a flap, could adversely affect the airplane's continued safe flight and landing.
Reduction of Fuel Tank Flammability in Transport Category Airplanes
This final rule amends FAA regulations that require operators and manufacturers of transport category airplanes to take steps that, in combination with other required actions, should greatly reduce the chances of a catastrophic fuel tank explosion. The final rule does not direct the adoption of specific inerting technology either by manufacturers or operators, but establishes a performance-based set of requirements that set acceptable flammability exposure values in tanks most prone to explosion or require the installation of an ignition mitigation means in an affected fuel tank. Technology now provides a variety of commercially feasible methods to accomplish these vital safety objectives.
Airworthiness Directives; Cessna Aircraft Company 150 Series Airplanes
We propose to adopt a new airworthiness directive (AD) for certain Cessna Aircraft Company 150 series airplanes with the BRS-150 Parachute System installed via Supplemental Type Certificate (STC) SA64CH. This proposed AD would require the replacement of the pick-up collar support and nylon screws for the BRS-150 Parachute System. This proposed AD results from notification by Ballistic Recovery Systems, Inc. (BRS) that the pick-up collar assembly may prematurely move off the launch tube and adversely affect rocket trajectory during deployment. We are proposing this AD to prevent premature separation of the collar. This condition could result in the parachute failing to successfully deploy.
Establishment of Class E Airspace; Removal of Class E Airspace; Roanoke Rapids, NC
This action establishes Class E airspace at Halifax- Northampton Regional Airport, (IXA), Roanoke Rapids, NC and removes Class E airspace at Halifax County Airport, Roanoke Rapids, NC, (RZZ). The operating status of the airport will include Instrument Flight Rule (IFR) operations. This action will enhance the safety and airspace management of Halifax-Northampton Regional Airport.
Amendment of Class E Airspace; Black River Falls, WI
A direct final rule, published in the Federal Register April 2, 2008 (73 FR 17888) docket No. FAA-2008-0024, adding additional Class E airspace at Black River Falls, WI is being removed. Although the rule became effective June 5, 2008, charting of this airspace was never completed. A new rulemaking will be forthcoming with an effective date that coincides with the new charting date.
Amendment of Class E Airspace; Lexington, OK
A direct final rule, published in the Federal Register April 16, 2008 (73 FR 20526) Docket No. FAA-2008-0003, adding additional Class E airspace at Lexington, OK is being removed. Although the rule became effective April 10, 2008, charting of this airspace was never completed. A new rulemaking will be forthcoming with an effective date that coincides with the new charting date.
Petition for Exemption; Summary of Petition Received
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.
Petition for Exemption; Summary of Petition Received
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; Pacific Aerospace Limited Model FU-24 Airplanes
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-120, -120ER, -120FC, -120QC, and -120RT Airplanes
This amendment adopts a new airworthiness directive (AD), applicable to all EMBRAER Model EMB-120 series airplanes, that requires revising the airplane flight manual to include operational limitations for use of the autopilot, installing two placards that advise the flight crew to check the pitch trim before descent, and modifying the elevator trim system, which would terminate the requirements of the AD. The actions specified by this AD are intended to prevent pitch trim upsets if the pitch trim actuators jam or freeze, which could result in reduced controllability of the airplane. This action is intended to address the identified unsafe condition.
Operating Limitations for Unscheduled Operations at John F. Kennedy International Airport and Newark Liberty International Airport
The FAA tentatively has determined that it is necessary to temporarily limit unscheduled aircraft operations at John F. Kennedy International Airport (JFK) and Newark Liberty International Airport (EWR). By Orders dated January 15 and May 15, 2008, the FAA restricted the number of scheduled operations respectively at JFK and EWR. These orders were a result of persistent congestion and delays at JFK and EWR during the peak operating hours, as well as a dramatic projected increase in fight delays at both airports during the summer of 2008 if proposed schedules were implemented as requested by carriers. The FAA recently published a notice of proposed rulemaking that addresses the operating limits of scheduled and unscheduled operations at both airports for the longer term. The FAA believes that in the interim it is necessary to limit unscheduled operations, as even the addition of a few operations in the critical peak hours can result in added congestion and delay. The intended effect of this action would be consistent with the previously issued Orders governing scheduled operations. This final Order would take effect at 6 a.m., Eastern Time, on August 28, 2008, and would expire at 11:59 p.m., Eastern Time, on October 24, 2009. This proposed Order would implement a reservation system to limit unscheduled operations at the airports and includes special provisions for public charter operations. A final Order would be enforceable under the FAA's civil penalty authority.
Notice of Passenger Facility Charge (PFC) Approvals and Disapprovals
The FAA publishes a monthly notice, as appropriate, of PFC approvals and disapprovals under the provisions of the Aviation Safety and Capacity Expansion Act of 1990 (Title IX of the Omnibus Budget Reconciliation Act of 1990) (Pub. L. 101-508) and Part 158 of the Federal Aviation Regulations (14 CFR Part 158). This notice is published pursuant to paragraph (d) of Sec. 158.29.
Approval of Noise Compatibility Program; Ocala International Airport; Ocala, FL
The Federal Aviation Administration (FAA) announces its findings on the Noise Compatibility Program submitted by the City of Ocala 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 December 28, 2008, the FAA determined that the noise exposure maps submitted by the City of Ocala under part 150 were in compliance with applicable requirements. On June 23, 2008, the FAA approved the Ocala International Airport noise compatibility program. All of the recommendations of the program were approved. No program elements relating to new or revised flight procedures for noise abatement were proposed by the airport operator.
Airworthiness Directives; Fokker Model F27 Mark 050 Airplanes
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 747-400 and 747-400D Series Airplanes
We are adopting a new airworthiness directive (AD) for certain Boeing Model 747-400 and 747-400D series airplanes. This AD requires a general visual inspection of the power feeder wire bundle of the auxiliary power unit (APU) where it crosses the hydraulic system 4 return tube to determine if parts are installed to provide separation between the wire bundle and hydraulic tube. This AD also requires related investigative and corrective actions if necessary. This AD results from a report that the power feeder wire bundle of the APU was found touching the hydraulic system return tube during inspection of an airplane. We are issuing this AD to prevent insufficient clearance between the wire bundle and hydraulic tube that could lead to chafing of the wire bundle, which could cause arcing and a consequent hydraulic fluid fire in an area outside of the smoke detection and fire extinguishing zone; this condition could result in an uncontrolled fire on the airplane.
Airworthiness Directives; 328 Support Services GmbH Dornier Model 328-100 and -300 Airplanes
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 A330-200 and A340-300 Series Airplanes
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; Agusta S.p.A. Model A109E and A119 Helicopters
We are adopting a new airworthiness directive (AD) for Agusta S.p.A. (Agusta) Model A109E and A119 helicopters. 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 European Aviation Safety Agency (EASA), the Technical Agent for Italy, with which we have a bilateral agreement, states in the MCAI: ``Some cases of interference between the hydraulic pipe, P/N 109-0761-65-103, and the tail rotor control rod assembly have been detected on Model A109E helicopters * * * The interference, if not corrected, could damage the hydraulic pipes and lead to the loss of the hydraulic system No. 1 in flight. This AD * * * is issued to extend the same mandatory corrective actions to A119 model due to its design similarity with A109E.'' This AD requires actions that are intended to address this unsafe condition.
Establishment of Class E Airspace; Fort Collins, CO
This action will establish Class E airspace at Fort Collins- Loveland Municipal Airport, Fort Collins, CO. Controlled airspace is necessary to accommodate Instrument flight rules (IFR) operations from this airport located in mountainous terrain and enable positive control at Fort Collins-Loveland Municipal Airport, Fort Collins, CO. This will enhance the safety and management of aircraft operations at Fort Collins-Loveland Municipal Airport, Fort Collins, CO.
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