Federal Aviation Administration 2011 – Federal Register Recent Federal Regulation Documents

This action proposes to amend Class E airspace at Hugo, CO. Decommissioning of the Hugo Tactical Air Navigation System (TACAN) has made this action necessary for the safety and management of Instrument Flight Rules (IFR) operations in the vicinity of the Hugo Very High Frequency Omni-Directional Radio Range/Distance Measuring Equipment (VOR/DME). This action also would make a minor adjustment to the geographic coordinates of the VOR/DME and make a correction to the regulatory text.

This action establishes Class D and E airspace and amends existing Class E airspace at Brooksville, FL, to accommodate a new air traffic control tower at Hernando County Airport This action enhances the safety and management of Instrument Flight Rules (IFR) operations for standard instrument approach procedures at the airport. This action also makes a minor adjustment to the geographic coordinates of the airport.

We are superseding an existing airworthiness directive (AD) that applies to certain Bombardier, Inc. Model DHC-8-300 series airplanes. 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:

We are adopting a new airworthiness directive (AD) for all Learjet Inc. Model 45 airplanes. This AD was prompted by a report of the potential for fatigue cracking of the end cap of the main landing gear (MLG) prior to the published life limitation. This AD requires revising the maintenance program to incorporate life limits for the MLG actuator end cap. We are issuing this AD to prevent fatigue cracking of the end cap of the MLG, which could result in the failure of the MLG actuator upon landing, and failure of the MLG to extend or retract during flight.

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.

As a result of recent legislation, the FAA has begun the process of amending the circumstances in which aircraft owners or operators can limit the dissemination of their aircraft data via the FAA's ASDI program. This Notice describes the immediate changes that the FAA has implemented. In a future Notice, the FAA will propose specific procedures by which owners or operators who want the FAA to block their aircraft data can express their preference regarding the FAA's release of that information via ASDI. At that time, the FAA will invite comments on the FAA's proposed procedures. In the interim, any aircraft that the FAA previously blocked under the Certified Security Concerns program published on June 3, 2011, will remain blocked. The FAA will address the future procedures concerning the blocking of those aircraft in its upcoming proposed and final procedures. In addition, the FAA is now accepting and implementing all direct requests of aircraft owners or operators to block their aircraft data from public display of ASDI and NASSI information.

Pursuant to Section 10(a)(2) of the Federal Advisory Committee Act (Pub. L. 92-463, 5 U.S.C. App. 2), notice is hereby given of a teleconference of the Commercial Space Transportation Advisory Committee (COMSTAC). The teleconference will take place on Thursday, January 5, 2012, starting at 11 a.m. Eastern Standard Time. Individuals who plan to participate should contact Susan Lender, Designated Federal Officer (DFO), (the Contact Person listed below) by phone or email for the teleconference call in number. The proposed agenda for this teleconference is to review and accept a report providing input to the United Nations Office of Outer Space Affairs. This report summarizes industry input to the United Nations Committee on Peaceful Uses of Outer Space (UN COPOUS). COMSTAC members will receive a copy of the final report on approximately January 3, 2012. Members of the public may request a copy from Susan Lender, DFO (the Contact Person listed below). Interested members of the public may submit relevant written statements for the COMSTAC members to consider under the advisory process. Statements may concern the issues and agenda items mentioned above or additional issues that may be relevant for the U.S. commercial space transportation industry. Interested parties wishing to submit written statements should contact Susan Lender, DFO, (the Contact Person listed below) in writing (mail or email) by December 29, 2011, so that the information can be made available to COMSTAC members for their review and consideration before the January 5, 2012, teleconference. Written statements should be supplied in the following formats: One hard copy with original signature or one electronic copy via email. An agenda will be posted on the FAA Web site at https://www.faa.gov/ go/ast. Individuals who plan to participate and need special assistance should inform the Contact Person listed below in advance of the meeting.

This action proposes to modify Class E airspace at Bisbee Douglas International Airport, Douglas, AZ. Decommissioning of the Cochise Very High Frequency Omni-Directional Radio Range Tactical Air Navigational Aid (VORTAC) has made this action necessary for the safety and management of aircraft operations at the airport. This action would also adjust the geographic coordinates of the airport.

We propose to adopt a new airworthiness directive (AD) for all The Boeing Company Model 777 airplanes. This proposed AD was prompted by four reports of retaining cross bolt hardware not fully engaged into the fuse pins of the forward trunnion lower housing of the main landing gear (MLG), which could result in an incorrect MLG emergency landing break-away sequence. This proposed AD would require a detailed inspection of the fuse pin cross bolts and fuse pins of the left and right MLG forward trunnion lower housing to verify that the cross bolts are correctly installed and that there are no missing fuse pins, and replacement of the fuse pins if necessary. We are proposing this AD to prevent an incorrect emergency landing MLG break-away sequence, which could result in puncturing of the wing box and consequent fuel leaks and an airplane fire. Failure of the fuse pins could also result in a premature landing gear collapse causing a runway excursion during take- off or landing.

This action modifies Class E airspace at The Dalles, OR. Controlled airspace is necessary to accommodate aircraft using Area Navigation (RNAV) Global Positioning System (GPS) standard instrument approach procedures at Columbia Gorge Regional/The Dalles Municipal Airport. This action also changes the airport name. This improves the safety and management of Instrument Flight Rules (IFR) operations at the airport.

This action proposes to amend Class E Airspace at Columbia, SC by removing Corporate Airport from the airspace designation, and would establish Class E Airspace at Pelion, SC, using the new airport name, as new Standard Instrument Approach Procedures have been developed at Lexington County Airport at Pelion. This action would enhance the safety and airspace management of Instrument Flight Rules (IFR) operations at the airport. This action also would update the geographic coordinates of the airport.

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.

Projects funded under the Airport Improvement Program (AIP) must meet the requirements of 49 U.S.C. 50101, Buy American Preferences. The Federal Aviation Administration (FAA) is considering issuing waivers to foreign manufacturers of certain airport lighting and navigation aid equipment that is lit with Light Emitting Diode (LED) lighting. This notice requests information from manufacturers of systems meeting the technical requirements to determine whether a waiver to the Buy American Preferences should be issued.

This notice announces the availability of a proposed Advisory Circular, regarding stall and stick pusher training for transport category airplanes for comment. This Advisory Circular provides guidance to training providers on stall event and stick pusher demonstration training, including recommendations and best practices for academic training, job performance training, and instructor training.

This action proposes to establish Class E Airspace at Piseco, NY, to accommodate new Area Navigation (RNAV) Global Positioning System (GPS) Standard Instrument Approach Procedures at Piseco Airport. This action would enhance the safety and airspace management of Instrument Flight Rules (IFR) operations at the airport.

This action modifies the Palm Beach International Airport, FL, Class C airspace area by raising the floor of Class C airspace over Palm Beach County Park Airport. The FAA is taking this action to enhance safety and increase the efficiency of air traffic operations in the Palm Beach, FL, terminal area.

This action proposes to amend Class E airspace at Omaha, NE. Additional controlled airspace is necessary to accommodate new Standard Instrument Approach Procedures (SIAP) at Eppley Airfield. The FAA is taking this action to enhance the safety and management of Instrument Flight Rules (IFR) operations for SIAPs at the airport.

We propose to supersede an existing airworthiness directive (AD) that applies to Turbomeca S.A. Arrius 2F turboshaft engines with P3 air pipe (first section) part number (P/N) 0 319 71 918 0, installed. The existing AD currently requires inspections of the P3 air pipe (first section) and right-hand (RH) rear half-wall for proper clearance, and readjustment of the pipe if necessary. Since we issued that AD, Turbomeca S.A. has redesigned the RH rear half-wall to ensure sufficient clearance between the P3 air pipe (first section) and RH rear half-wall. This proposed AD would require the same inspections for installed engines, eliminate readjusting of the P3 air pipe (first section), require replacement of the RH rear half-wall under certain conditions, and adding an optional terminating action. We are proposing this AD to prevent an uncommanded power loss to flight idle, which could result in an emergency autorotation landing or accident.

We are adopting a new airworthiness directive (AD) for certain Continental Motors, Inc. (CMI) models TSIO-520, TSIO-550-K, TSIOF-550K, and IO-550-N series reciprocating engines. This emergency AD was sent previously to all known U.S. owners and operators of these engines. This AD requires replacing affected CMI starter adapters with starter adapters eligible for installation. This AD was prompted by 5 reports received of fractures in starter adapter shaft gears in certain part number (P/N) CMI starter adapters. We are issuing this AD to prevent failure of the starter adapter gear shaft, leading to an inoperable oil scavenge pump and engine in-flight shutdown.

We are superseding an existing airworthiness directive (AD) for all The Boeing Company 757-200, 757-200PF, 757-200CB, 757-300, 767- 200, 767-300, and 767-300F series airplanes. That AD currently requires revising the Limitations section of the airplane flight manual (AFM) to advise the flightcrew of procedures to follow to ensure that a fuel filter impending bypass condition due to gross fuel contamination is detected in a timely manner. This new AD requires installing new operating program software (OPS) (Version 7) of the engine indication and crew alerting system (EICAS) in the EICAS computers. This AD also requires various concurrent actions. This AD also retains the existing AD provision that relieves certain airplanes (those equipped with certain EICAS OPS versions) from the requirements. Accomplishment of the new actions terminates the requirements of the existing AD. This AD was prompted by an error in the EICAS OPS. The error prevents the display of an advisory message to the flightcrew of a left engine fuel filter contamination and imminent bypass condition, which may indicate an imminent multiple engine thrust loss or engine malfunction event due to fuel contamination. We are issuing this AD to correct the unsafe condition on these products.

We are adopting a new airworthiness directive (AD) for certain The Boeing Company Model MD-11 and MD-11F airplanes. This AD was prompted by a report that the rub strips attached to the horizontal stabilizer front spar access door location were manufactured improperly using anodized aluminum. This AD requires replacing the anodized rub strips with new alodined rub strips to prevent inadequate electrical bonding between the rub strips and the fuel access door, which can contribute to possible ignition of flammable fuel vapor in the tail fuel tank as a result of a lightning strike. We are issuing this AD to correct the unsafe condition on these products.

We propose to adopt a new airworthiness directive (AD) for all 328 Support Services GmbH (Type Certificate previously held by AvCraft Aerospace GmbH; Fairchild Dornier GmbH; Dornier Luftfahrt GmbH) Model 328-100 and -300 airplanes 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:

We are adopting a new airworthiness directive (AD) for International Aero Engines (IAE) V2500-A1, V2522-A5, V2524-A5, V2525- D5, V2527-A5, V2527E-A5, V2527M-A5, V2528-D5, V2530-A5, and V2533-A5 turbofan engines. This AD was prompted by three reports of high- pressure turbine (HPT) case burn-through events, numerous reports of loss of stage 1 blade outer air seal segments, and HPT case bulging. This AD requires initial and repetitive 360 degree borescope inspections of HPT stage 1 blade outer air seal segments for evidence of certain distress conditions. This AD also requires incorporation of improved durability stage 1 blade outer air seal segments at the next exposure to the HPT module subassembly as terminating action to the repetitive inspections. We are issuing this AD to prevent HPT case burn-through, uncontrolled under-cowl engine fire, and damage to the airplane.

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.

This action announces the effective date of a final rule published in the Federal Register of April 28, 2011 that amends Federal airways in Alaska. The FAA subsequently published a rule in the Federal Register of June 16, 2011 that delayed the effective date until further notice. An amendment, published in the Federal Register of October 20, 2011, further modified the rule. This action is the result of satisfactory flight inspections for the Federal airways affected by the relocation of the Anchorage VHF Omnidirectional Range (VOR).