Monday July 18, 2011
Final Rules
- Airworthiness Directives; 328 Support Services GmbH (Type Certificate Previously Held by AvCraft Aerospace GmbH; Fairchild Dornier GmbH; Dornier Luftfahrt GmbH) Model 328– 100 and –300 Airplanes. 14 CFR Part 39
[Docket No. FAA–2011–0308; Directorate Identifier 2010–NM–233–AD; Amendment 39–16754; AD 2011–15–07]. Final rule. 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: During maintenance, it has been discovered that at the installation of the fixation brackets for rudder spring tabs and trim tabs an incorrect installation of the
fixation brackets may have occurred. * * * If the orientation of the fixation bracket is reversed or upside down the screws may not reach into the helicoil thread to a sufficient depth. An incorrect installation, if not detected and corrected, could lead to an in-flight failure of the fixation brackets for rudder
spring tabs and trim tabs resulting in and reduced control of the aeroplane.
* * * * * We are issuing this AD to require actions to correct the unsafe condition
on these products. DATES: This AD becomes effective August 22, 2011. The Director of the Federal Register approved the incorporation by reference of certain publications listed in this AD as of August 22, 2011. - Airworthiness Directives; Airbus Model A300 B4–600, B4–600R, and F4–600R
Series Airplanes, and Model A300 C4– 605R Variant F Airplanes (Collectively
Called A300–600 Series Airplanes); and Model A310 Series Airplanes. 14 CFR Part 39 [Docket No. FAA–2011–0309; Directorate Identifier 2010–NM–255–AD; Amendment 39–16755; AD 2011–15–08]. Final rule. 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: A specific failure case of the THSA [trimmable horizontal stabilizer actuator] upper primary attachment, which may result in a loading of the upper secondary attachment, has been identified by analysis. Primary load path failure can be caused by bearing migration from the upper attachment gimbal by failure or loss of a retention bolt. In case of failure of the THSA upper primary attachment, the THSA upper secondary attachment would engage. Because the upper attachment secondary load path can only withstand the loads for a limited period of time, the condition where it would be engaged could lead, if not detected, to the failure of the secondary load path, which would likely result in loss of control of the aeroplane. * * * * * We are issuing this AD to require actions to correct the unsafe condition on these products. DATES: This AD becomes effective August 22, 2011.
The Director of the Federal Register approved the incorporation by reference of certain publications listed in this AD as of August 22, 2011. - Airworthiness Directives; Airbus Model A318, A319, A320, and A321 Series Airplanes. 14 CFR Part 39 [Docket No. FAA–2011–0257; Directorate Identifier 2010–NM–122–AD; Amendment 39–16741; AD 2011–14–06]. Final rule. We are superseding an existing airworthiness directive (AD) that applies to 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: * * * * * The issue 10 of Airbus A318/A319/A320/ A321 ALI [Airworthiness Limitation Items] Document and issue 2 of Airbus A319 Corporate Jet ALI Document introduce more restrictive maintenance requirements/ airworthiness limitations. Failure to comply with this issue 10 constitutes an unsafe condition. * * * * * The unsafe condition is fatigue cracking, accidental damage, or corrosion in principal structural elements and possible failure of certain life limited parts, which could result in reduced structural integrity of the airplane. We are issuing this AD to require actions to correct the unsafe condition on these products. DATES: This AD becomes effective August 22, 2011. The Director of the Federal Register approved the incorporation by reference of certain publications listed in this AD as of August 22, 2011. The Director of the Federal Register previously approved the incorporation by reference of certain other publications, listed in this AD as of
November 7, 2007 (72 FR 56262, October 3, 2007). - Airworthiness Directives; Bombardier, Inc. Model DHC–8–400 Series
Airplanes. 14 CFR Part 39 [Docket No. FAA–2011–0718; Directorate Identifier 2011–NM–117–AD; Amendment 39–16756; AD 2011–15–09]. Final rule. We are adopting a new airworthiness directive (AD) for the products listed above that would supersede an existing AD. 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: Two cases of the main landing gear (MLG) alternate extension system (AES) cam mechanism failure were found during line checks. The cam mechanism operates the cable to open the MLG door and releases the MLG uplock in sequence. In the case where it is necessary to deploy the MLG using the AES, the failure of the MLG AES cam mechanism on one side will lead to an unsafe asymmetrical landing configuration. * * * * *
The unsafe condition is possible loss of control during landing. This AD requires actions that are intended to address the unsafe condition described in the MCAI.
DATES: This AD becomes effective August 2, 2011. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in the AD as of August 2, 2011. The Director of the Federal Register approved the incorporation by reference of a certain other publication listed in the AD as of March 25, 2011 (76 FR 13080, March 10, 2011). We must receive comments on this AD by September 1, 2011. - Airworthiness Standards; Rotor Overspeed Requirements. 14 CFR Part 33
[Docket No. FAA–2010–0398; Amendment No. 33–31]. Final rule. This rule will amend the aircraft turbine engine rotor overspeed type certification standards. This action establishes uniform rotor overspeed design and test requirements for aircraft engines and turbochargers certificated by the FAA and the European Aviation Safety Agency (EASA). The rule also establishes uniform standards for the design and testing of engine rotor parts in the United States and in Europe,
eliminating the need to comply with two differing sets of requirements. DATES: This amendment becomes effective September 16, 2011.
Notices
- Notice of Final Federal Agency Actions on Proposed Highway in California. Notice. The FHWA, on behalf of Caltrans, is issuing this notice to announce actions taken by Caltrans, and USACE that are final within the meaning of 23 U.S.C. 139(l)(1). The actions relate to a proposed highway project at the Genesee Avenue Interchange on Interstate 5 (I–5) in the City and County of San Diego, State of California. Those actions grant licenses, permits, and approvals for the project. DATES: By this notice, the FHWA, on behalf of Caltrans, is advising the public of final agency actions subject to 23 U.S.C. 139(l)(1). A claim seeking
judicial review of the Federal agency actions on the highway project will be
barred unless the claim is filed on or before January 14, 2012. If the Federal
law that authorizes judicial review of a claim provides a time period of less
than 180 days for filing such claim, then that shorter time period still applies.
Final Rules
- Establishment of Class E Airspace; Brunswick, ME. 14 CFR Part 71
[Docket No. FAA–2011–0116; Airspace Docket No. 11–ANE–1]. Final rule. This action corrects the effective date of a final rule correction, that was published in the Federal Register on July 6, 2011. The effective date in that Final Rule; Correction. inadvertently listed the wrong effective date in the Correction to Final Rule section. DATES: Effective Date: 0901 UTC, July 28, 2011.
Proposed Rules
- Airworthiness Directives; Airbus Model A330–201, –202, –203, –223, –243,
–301, –302, –303, –321, –322, –323, –341, –342, and –343 Airplanes; and
Model A340–200 and –300 Series Airplanes. 14 CFR Part 39 [Docket No. FAA–2011–0717; Directorate Identifier 2010–NM–108–AD]. Proposed rules. 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: During A330 and A340 aeroplanes fatigue tests, cracks appeared on the right (RH) and left (LH) sides between the crossing area of the keel beam fitting and the front spar of the
Centre Wing Box (CWB). This condition, if not corrected, could lead to keel beam
rupture which would affect the area structural integrity. * * * * * The proposed AD would require actions that are intended to address the unsafe condition described in the MCAI. DATES: We must receive comments on this proposed AD by September 2, 2011. - Airworthiness Directives; The Boeing Company Model 767–200, –300, and –400ER Series Airplanes. 14 CFR Part 39 [Docket No. FAA–2011–0719; Directorate Identifier 2010–NM–087–AD]. Proposed rule. We propose to supersede an existing airworthiness directive (AD) that applies to the products listed above. The existing AD currently requires replacing the separation link assembly on the applicable entry and service doors with an improved separation link assembly, and doing related investigative and corrective actions if necessary. Since we issued that AD, we have received a report that an additional airplane is subject to the unsafe condition. This proposed AD would add that airplane to the applicability and also remove certain other airplanes from the applicability. We are proposing this AD to prevent failure of an entry or service door to open fully in the event of an emergency evacuation, which could impede exit from the airplane. This condition could result in injury to passengers or crewmembers.
DATES: We must receive comments on this proposed AD by September 2, 2011. - Airworthiness Directives; Lycoming Engines Model TIO 540–A Series Reciprocating Engines. 14 CFR Part 39 [Docket No. FAA–2011–0691; Directorate
Identifier 2011–NE–26–AD]. Proposed rule. We propose to rescind an airworthiness directive (AD) for Lycoming Engines model TIO 540–A
series reciprocating engines. The existing AD, AD 71–13–01 (Amendment
39–1231) resulted from a report of a failed fuel injector tube assembly.
Since we issued AD 71–13–01, we became aware that Lycoming Engines no
longer supports Service Bulletin (SB) No. 335A, which was incorporated by
reference in AD 71–13–01. The intent of the requirements of that SB is now in
Lycoming Engines Mandatory SB No. 342F. This proposal to rescind AD 71–
13–01 allows the public the opportunity to comment on the FAA’s determination
of the duplication of requirements in another AD, before we rescind the engine-level AD. DATES: We must receive comments on this proposed AD by September 2, 2011. - Airworthiness Directives; Turbomeca Arriel 1 Series Turboshaft Engines. 14 CFR Part 39 [Docket No. FAA–2010–0710; Directorate Identifier 2010–NE–26–AD]. Proposed rule. We propose to revise an existing airworthiness directive (AD) that applies to the products listed above. The existing AD currently requires removing from service certain gas generator second stage turbine discs, part number (P/N) 0 292 25 040 0, that are not marked with ‘‘CFR’’ before the discs exceed 2,500 cycles-in-service (CIS) since-new or within 20 CIS from the effective date of the AD, whichever occurs later. That AD also requires removing from service certain gas generator second stage turbine discs, P/N 0 292 25 040 0, that are marked
with ‘‘CFR’’ before the discs exceed 3,500 CIS since-new. Since we issued that AD, Turbomeca has restored all or part of the life limits of the affected discs, and the European Aviation Safety Agency (EASA) issued AD 2010– 0101R2, dated March 24, 2011 to do the same. This proposed AD would still prevent disc failure but extends the life limits of the affected discs. We are proposing this AD to prevent failure of the gas generator second stage turbine disc which could result in the release of high energy debris and damage to the helicopter. DATES: We must receive comments on this proposed AD by September 2, 2011.
Notices
- Final Written Re-Evaluation for Environmental Impact Statement: Sikorsky Memorial Airport, Stratford, CT. Notice. The FAA is issuing this notice to advise the public that a Writetn Re- Evaluation of a Final Environmental Impact Statement (FEIS) has been completed for Sikorsky Memorial Airport in Stratford, Connecticut.
Wednesday July 20, 2011
Final Rules
- Update of August 2001 Overflight Fees. 14 CFR Part 187 [Docket No.: FAA–2010–0326; Amendment No. 187–35]. Final rule. This final rule updates
existing Overflight Fees using more current FAA cost accounting data and
air traffic activity data. Overflight Fees are charges for aircraft flights that transit
U.S.-controlled airspace, but neither land in nor depart from the United States. These fees have not been updated in nearly a decade and are based upon 1999 cost accounting and activity data. This action is necessary because operational costs have increased steadily since the fees were last updated. This adjustment of
Overflight Fees will result in an increased level of cost recovery for the services being provided. DATES: Effective October 1, 2011.
Notice
- Notice of Final Federal Agency Actions on Proposed Highway in Indiana. Notice. This notice announces actions taken by the FHWA and the USACE that are final within the meaning of 23 U.S.C. 139(l)(1). The actions relate to proposed highway projects, including I–69 from Evansville to Indianapolis in the Counties of Vanderburgh, Warrick, Gibson, Pike, Daviess, Greene, Monroe, Morgan, Johnson and Marion, State of Indiana, and a 13.1 mile segment of I–69 in the Counties of Warrick and Gibson, State of Indiana. These actions grant or amend licenses, permits, and approvals for the projects. DATES: By this notice, the FHWA is
advising the public of final agency actions subject to 23 U.S.C. 139(l)(1) and
are final within the meaning of that law. A claim seeking judicial review of those
Federal agency actions that are covered by this notice will be barred unless the
claim is filed on or before January 17, 2012. If the Federal law that authorizes
judicial review of a claim provides a time period of less than 180 days for
filing such claim, then the shorter time period applies.
Thursday July 21, 2011
Final Rules
- Amendment of Class E Airspace; Fulton, MO. 14 CFR Part 71 [Docket No. FAA–2011–0121; Airspace Docket No. 11–ACE–2]. Final rule. This action amends Class E airspace for Fulton, MO. Decommissioning of the Guthrie nondirectional beacon (NDB) at Elton Hensley Memorial Airport, Fulton, MO,
has made this action necessary to enhance the safety and management of Instrument Flight Rule (IFR) operations at the airport. DATES: Effective date: 0901 UTC, October 20, 2011. The Director of the Federal Register approves this
incorporation by reference action under 1 CFR part 51, subject to the annual
revision of FAA Order 7400.9 and publication of conforming amendments. - Amendment of Class E Airspace; Staunton, VA. 14 CFR Part 71 [Docket No. FAA–2010–1285; Airspace Docket No. 10–AEA–27]. Final rule. This action amends Class E surface airspace extending upward from 700 feet above the surface at Shenandoah Valley Regional Airport, Staunton, VA. The Bridgewater Non- Directional Beacon (NDB) has been decommissioned and new Standard
Instrument Approach Procedures have been developed for the airport. This
action enhances the safety and airspace management of Instrument Flight Rules
(IFR) operations at the airport. DATES: Effective 0901 UTC, October 20, 2011. The Director of the Federal Register approves this incorporation by reference action under title 1, Code of Federal Regulations, part 51, subject to the annual revision of FAA Order 7400.9 and publication of conforming amendments. - Amendment of Class E Airspace; Hannibal, MO. 14 CFR Part 71 [Docket No. FAA–2011–0046; Airspace Docket No. 11–ACE–1]. Final rule. This action amends Class E airspace for Hannibal, MO. Decommissioning of the Hannibal nondirectional beacon (NDB) at Hannibal Regional Airport, Hannibal, MO, has
made this action necessary to enhance the safety and management of Instrument Flight Rule (IFR) operations at the airport. This action also changes the airport name and updates the geographic coordinates of the airport. DATES: Effective date: 0901 UTC, October 20, 2011. The Director of the Federal Register approves this incorporation by reference action under 1 CFR part 51, subject to the annual
revision of FAA Order 7400.9 and publication of conforming amendments. - Amendment of Class E Airspace; Staunton, VA. 14 CFR Part 71 [Docket No. FAA–2010–1285; Airspace Docket No. 10–AEA–27]. Final rule. This action amends Class E surface airspace extending upward from 700 feet above the surface at Shenandoah Valley Regional Airport, Staunton, VA. The Bridgewater Non- Directional Beacon (NDB) has been decommissioned and new Standard
Instrument Approach Procedures have been developed for the airport. This
action enhances the safety and airspace management of Instrument Flight Rules
(IFR) operations at the airport. DATES: Effective 0901 UTC, October 20, 2011. The Director of the Federal Register approves this incorporation by reference action under title 1, Code of Federal Regulations, part 51, subject to the annual revision of FAA Order 7400.9 and publication of conforming amendments. - Standard Instrument Approach Procedures, and Takeoff Minimums and Obstacle Departure Procedures; Miscellaneous Amendments. 14 CFR Part 97 [Docket No. 30793; Amdt. No. 3435]. Final rule. 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. DATES: This rule is effective July 21, 2011. The compliance date for each SIAP, associated Takeoff Minimums, and ODP is specified in the amendatory provisions. The incorporation by reference of certain publications listed in the regulations is approved by the Director of the Federal Register as of July 21, 2011. - Standard Instrument Approach Procedures, and Takeoff Minimums and Obstacle Departure Procedures; Miscellaneous Amendments. 14 CFR Part 97 [Docket No. 30792; Amdt. No. 3434]. Final rule. This 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. DATES: This rule is effective July 21, 2011. The compliance date for each SIAP, associated Takeoff Minimums, and ODP is specified in the mandatory provisions. The incorporation by reference of certain publications listed in the regulations is approved by the Director of the Federal Register as of July 21, 2011.
Proposed Rules
- Proposed Amendment of Class E Airspace; Spearfish, SD. 14 CFR Part 71
[Docket No. FAA–2011–0431; Airspace Docket No. 11–AGL–11]. Proposed rules. This action proposes to amend Class E airspace at Spearfish, SD. Additional controlled airspace is necessary to accommodate new Standard Instrument Approach Procedures (SIAP) at Black Hills Airport-Clyde Ice Field. The geographic coordinates of the airport also would be updated. The FAA is taking this action to enhance the safety and management of Instrument Flight Rules (IFR) operations for SIAPs at the airport. DATES: 0901 UTC. Comments must be
received on or before September 6, 2011. - Proposed Amendment of Class E Airspace; Bryan, OH. 14 CFR Part 71
[Docket No. FAA–2011–0606; Airspace Docket No. 11–AGL–14]. Proposed rule. This action proposes to amend Class E airspace at Bryan, OH. Decommissioning of the Bryan nondirectional beacon (NDB) at Williams County Airport, Bryan, OH, has made this action necessary for the safety and management of Instrument Flight Rules (IFR) operations at Williams County Airport. DATES: 0901 UTC. Comments must be received on or before September 6, 2011. - Proposed Amendment of Class E Airspace; Evansville, IN. 14 CFR Part 71
[Docket No. FAA–2011–0429; Airspace Docket No. 11–AGL–9]. Proposed rule. This action proposes to amend Class E airspace at Evansville, IN. Additional controlled airspace is necessary to accommodate new Standard Instrument Approach Procedures at Evansville Regional Airport. The FAA is taking this action to enhance the safety and management of Instrument Flight Rules (IFR)
operations for SIAPs at the airport. DATES: 0901 UTC. Comments must be
received on or before September 6, 2011. - Proposed Amendment of Class E Airspace; Sturgis, SD. 14 CFR Part 71
[Docket No. FAA–2011–0430; Airspace Docket No. 11–AGL–10]. Proposed rule. This action proposes to amend Class E airspace at Sturgis, SD. Additional controlled airspace is necessary to accommodate new Standard Instrument Approach Procedures (SIAP) at Sturgis Municipal Airport. The FAA is taking this action to enhance the safety and management of Instrument Flight Rules (IFR)
operations for SIAPs at the airport. DATES: 0901 UTC. Comments must be
received on or before September 6, 2011. - Proposed Amendment of Class E Airspace; Valley City, ND. 14 CFR Part 71
[Docket No. FAA–2011–0605; Airspace Docket No. 11–AGL–13]. Proposed rule. This action proposes to amend Class E airspace at Valley City, ND. Decommissioning of the Valley City non-directional beacon (NDB) at Barnes
County Municipal Airport, Valley City, ND, has made this action necessary for
the safety and management of Instrument Flight Rules (IFR) operations at the airport. DATES: 0901 UTC. Comments must be received on or before September 6, 2011.
Friday July 22, 2011
Final Rules
- Amendment of Class E Airspace; Ava, MO. 14 CFR Part 71 [Docket No. FAA–2011–0122; Airspace Docket No. 11–ACE–3]. Final rule. This action amends Class E airspace for Ava, MO. Decommissioning of the Bilmart non-directional beacon (NDB) at Ava Bill Martin Memorial Airport, Ava, MO, has made this action necessary to enhance the safety and management of Instrument Flight Rule (IFR) operations at the airport. DATES: Effective date: 0901 UTC,
October 20, 2011. The Director of the Federal Register approves this incorporation by reference action under 1 CFR part 51, subject to the annual
revision of FAA Order 7400.9 and publication of conforming amendments. - Amendment of Class E Airspace; Drummond Island, MI. 14 CFR Part 71
[Docket No. FAA–2010–0609; Airspace Docket No. 10–AGL–9]. Final rule. This action amends Class E airspace for Drummond Island, MI, to accommodate new Area Navigation (RNAV) Standard Instrument Approach Procedures at Drummond Island Airport. The FAA is taking this action to enhance the safety and management of Instrument Flight Rule (IFR) operations at the airport.
DATES: Effective date: 0901 UTC, October 20, 2011. The Director of the
Federal Register approves this incorporation by reference action under 1 CFR part 51, subject to the annual revision of FAA Order 7400.9 and publication of conforming amendments. - Establishment of Class E Airspace; Hearne, TX. 14 CFR Part 71 [Docket No. FAA–2011–0214; Airspace Docket No. 11–ASW–2]. Final rule. This action establishes Class E airspace for Hearne, TX, to accommodate new Area Navigation (RNAV) Standard Instrument Approach Procedures at Hearne Municipal Airport. The FAA is taking this action to enhance the safety and management of Instrument Flight Rule (IFR) operations at the airport.
DATES: Effective date: 0901 UTC, October 20, 2011. The Director of the
Federal Register approves this incorporation by reference action under
1 CFR part 51, subject to the annual revision of FAA Order 7400.9 and
publication of conforming amendments. - Amendment of Class E Airspace; Ava, MO. 14 CFR Part 71 [Docket No. FAA–2011–0122; Airspace Docket No. 11–ACE–3]. Final rule. This action amends Class E airspace for Ava, MO. Decommissioning of the Bilmart non-directional beacon (NDB) at Ava Bill Martin Memorial Airport, Ava, MO, has made this action necessary to enhance the safety and management of Instrument Flight Rule (IFR) operations at the airport. DATES: Effective date: 0901 UTC,
October 20, 2011. The Director of the Federal Register approves this incorporation by reference action under 1 CFR part 51, subject to the annual
revision of FAA Order 7400.9 and publication of conforming amendments. - Launch Safety: Lightning Criteria for Expendable Launch Vehicles. 14 CFR Part 417 [Docket No.: FAA–2011–0181; Amendment No. 417–2]. Final rule.This action confirms the effective date of July 25, 2011, for the direct final rule issued June 8, 2011. No comments were received on this final rule. This action amends flight criteria for mitigating against naturally occurring lightning and lightning triggered by the flight of an expendable launch vehicle through or near an electrified environment in or near a cloud. These changes also increase launch
availability and implement changes already adopted by the United States Air Force. DATES: The direct final rule published June 8, 2011 (76 FR 33139) is effective on July 25, 2011. - Revision of Class E Airspace; Talkeetna, AK. 14 CFR Part 71 [Docket No. FAA–2011–0444; Airspace Docket No. 11–AAL–07]. Final Rule. This action revises Class E airspace at Talkeetna, AK, to accommodate the amendment of four Standard Instrument Approach Procedures and the Obstacle Departure
Procedure at Talkeetna Airport. The FAA is taking this action to enhance
safety and management of Instrument Flight Rules (IFR) operations at the
Talkeetna Airport. DATES: Effective 0901 UTC, October 20, 2011. The Director of the Federal Register approves this incorporation by reference action under title 1, Code of Federal Regulations, part 51, subject to the annual revision of FAA Order
7400.9 and publication of conforming amendments. - Revision of Class E Airspace; Yakutat, AK. 14 CFR Part 71 [Docket No. FAA–2011–0244 Airspace Docket No. 11–AAL–05]. Final rule. This action revises Class E airspace at the Yakutat Airport, Yakutat, AK. The amendment of eight Standard Instrument Approach Procedures (SIAPs) has made this action necessary to enhance safety and air traffic management of Instrument Flight Rules (IFR) operations at the airport. DATES: Effective 0901 UTC, October 20,
2011. The Director of the Federal Register approves this incorporation by reference action under title 1, Code of Federal Regulations, part 51, subject to
the annual revision of FAA Order 7400.9 and publication of conforming amendments.
Notices
- Agency Information Collection Activities: Requests for Comments; Clearance of Renewed Approval of Information Collection: General Operating and Flight Rules. Notice. In accordance with the Paperwork Reduction Act of 1995, FAA
invites public comments about our intention to request the Office of Management and Budget (OMB) approval to renew an information collection. The Federal Register Notice with a 60-day comment period soliciting comments on the following collection of information was published on May 25, 2011, vol. 76, no. 101, page 30421– 30422. 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. Respondents are individual airmen, state or local governments, and businesses.
DATES: Written comments should be submitted by August 22, 2011. - Agency Information Collection Activities: Requests for Comments; Clearance of Renewed Approval of Information Collection: Certification of Airmen for the Operation of Light- Sport Aircraft. Notice. In accordance with the Paperwork Reduction Act of 1995, FAA invites public comments about our intention to request the Office of Management and Budget (OMB) approval to renew an information collection. Regulation generates a need for new designated pilot examiners and designated airworthiness representatives to support the
certification of new light-sport aircraft, pilots, flight instructors, and ground
instructors. DATES: Written comments should be submitted by September 20, 2011.