Federal Aviation Administration 2009 – Federal Register Recent Federal Regulation Documents
Results 301 - 350 of 1,434
Airworthiness Directives; Airbus Model A300 B4-601, B4-603, B4-605R, B4-620, B4-622, B4-622R, F4-605R, F4-622R, and C4-605R Variant F Series Airplanes Equipped With Simmonds Precision Products, Inc., Fuel Quantity Indicating System Sensors and In-Tank Harnesses Installed in Accordance With Supplemental Type Certificate (STC) ST00092BO
We are adopting a new airworthiness directive (AD) for certain Airbus model series airplanes listed above. This AD requires revising the Airworthiness Limitations Section of the Instructions for Continuing Airworthiness to incorporate new fuel system limitations for airplanes modified in accordance with Supplemental Type Certificate (STC) ST00092BO. This AD also requires a general visual inspection for tank unit separation and compensator separation of the center, inner, and outer fuel tanks, and trim fuel tanks of the tank units, and corrective actions if necessary. This AD results from fuel system reviews conducted by the manufacturer. We are issuing this AD to prevent a potential of ignition sources inside fuel tanks, which in combination with flammable fuel vapors, could result in a fuel tank fire or explosion and consequent loss of the airplane.
Airworthiness Directives; Rolls-Royce plc RB211 Trent 700 Series Turbofan Engines
The FAA proposes to supersede an existing airworthiness directive (AD) for Rolls-Royce plc (RR) RB211 Trent 700 series turbofan engines. That AD currently requires initial and repetitive borescope inspections of the high pressure-and-intermediate pressure (HP-IP) turbine internal and external oil vent tubes for coking and carbon buildup, and cleaning or replacing the vent tubes if necessary. This proposed AD would require the same actions, but would add additional inspections of the vent flow restrictor. This proposed AD results from further analysis that the cleaning of the vent tubes required by AD 2007-02-05 could lead to loosened carbon fragments, causing a blockage downstream in the vent flow restrictor. We are proposing this AD to prevent internal oil fires due to coking and carbon buildup that could cause uncontained engine failure and damage to the airplane.
Airworthiness Directives; International Aero Engines AG (IAE) V2500-A1, V2527E-A5, V2530-A5, and V2528-D5 Turbofan Engines
The FAA is adopting a new airworthiness directive (AD) for International Aero Engines AG (IAE) V2500-A1, V2527E-A5, V2530-A5, and V2528-D5 turbofan engines. This AD requires reducing the published life limit of certain high-pressure compressor (HPC) stage 9-12 disc assemblies. This AD also removes from service those HPC stage 9-12 disc assemblies using a drawdown schedule. This AD results from IAE updating the low-cycle-fatigue (LCF) life analysis for certain HPC stage 9-12 disc assemblies. We are issuing this AD to prevent an uncontained failure of the HPC stage 9-12 disc assembly, resulting in an in-flight engine shutdown and possible damage to the airplane.
Proposed Establishment of Area Navigation Route Q-37; Texas
This action proposes to establish a high altitude area navigation (RNAV) route, designated Q-37, extending between the Pueblo, CO, very high frequency omnidirectional range/tactical air navigation (VORTAC) navigation aid and the Fort Stockton, TX, VORTAC. The new route would provide pilots and air traffic controllers with an efficient alternative route around potentially constrained airspace during convective weather events in west Texas.
Notice of Intent To Request Reinstatement From the Office of Management and Budget of an Expired Information Collection Activity, Request for Comments; Flight Attendant Duty/Rest/Fatigue Field Study
The FAA invites public comments about our intention to request the Office of Management and Budget (OMB) to reinstate an expired information collection. In response to a Congressional directive to conduct a flight attendant fatigue study, FAA's Civil Aerospace Medical Institute, has initiated a comprehensive analysis of fatigue in flight attendants across a range of operational conditions.
Establishment of Class E Airspace; Noorvik, AK
This action establishes Class E airspace at Noorvik, AK to provide adequate controlled airspace to contain aircraft executing Standard Instrument Approach Procedures (SIAPs). Two SIAPs are being developed for the Robert (Bob) Curtis Memorial Airport at Noorvik, AK. Additionally, one textual Obstacle Departure Procedure (ODP) is being developed. This action establishes Class E airspace upward from 700 feet (ft.) above the surface at Robert (Bob) Curtis Memorial Airport, Noorvik, AK.
Amendment of Federal Airways V-163 and V-358 in the Lampasas, TX, Area
This action amends the legal descriptions of two Federal airways that have ``Lampasas, TX, very high frequency omnidirectional range/tactical air navigation (VORTAC)'' included as part of their route structure. Currently, the Lampasas VORTAC and the Lampasas Airport share the same location name and identifier (LZZ). To eliminate confusion and potential flight safety issues, the ``Lampasas VORTAC'' (LZZ) will be renamed the ``Gooch Springs VORTAC'' (AGJ). All airways with Lampasas [VORTAC] included in their legal descriptions will be amended, concurrent with the effective date of this final rule, to reflect the name change.
Aircraft Noise Impacts Research Roadmap
This notice advises interested persons that the FAA is conducting workshops to develop an aircraft noise impacts research roadmap. The roadmap is intended to advance our scientific knowledge in
Establishment of Class D and E Airspace and Modification of Class E Airspace; State College, PA
This action proposes to establish Class D and E airspace and modify existing Class E airspace at State College, PA. The University Park Airport is building a new air traffic control tower and the FAA is directed by law to establish and/or modify controlled surface airspace for the support of air traffic operations. This action would enhance the safety and airspace management around University Park Airport, State College, PA.
Eleventh Meeting: RTCA Special Committee 216: Aeronautical Systems Security
The FAA is issuing this notice to advise the public of a meeting of RTCA Special Committee 216: Aeronautical Systems Security.
Special Conditions: Model C-27J Airplane; Class E Cargo Compartment Lavatory
This action proposes special conditions for the Alenia Model C-27J airplane. This airplane has novel or unusual design features when compared to the state of technology described in the airworthiness standards for transport-category airplanes. These design features include a lavatory in the Class E cargo compartment. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for these design features. These proposed special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards. We have issued additional special conditions for other novel or unusual design features of the C-27J.
Proposed Revision of Area Navigation (RNAV) Route Q-108; Florida
This action proposes to make a revision to the alignment of high altitude RNAV route Q-108, which currently extends between the GADAY and CLAWZ waypoints (WP) in Florida. The FAA is proposing this action to enhance the efficiency of the National Airspace System in the northern Florida area.
Proposed Modification of Jet Route J-20; Florida
This action proposes to modify Jet Route J-20 by terminating the route at the Orlando, FL, very high frequency omnidirectional range/tactical air navigation (VORTAC) facility, thereby eliminating the segment between the Orlando VORTAC and the Virginia Key, FL, very high frequency omnidirectional range/distance measuring equipment (VOR/ DME) facility. This modification would eliminate a portion of J-20 that is no longer needed.
Airworthiness Directives; AeroSpace Technologies of Australia Pty Ltd Models N22B, N22S, and N24A Airplanes
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:
Airworthiness Directives; Eurocopter France Model AS350B, BA, B1, B2, B3, C, D, D1, AS355E, F, F1, F2, and N Helicopters
We propose to adopt a new airworthiness directive (AD) for the specified Eurocopter France (Eurocopter) model helicopters. This proposed AD results from a mandatory continuing airworthiness information (MCAI) AD issued by the European Aviation Safety Agency (EASA), which is the Technical Agent for the Member States of the European Community. The AD MCAI states ``EASA issued Airworthiness Directive (AD) 2006-0251 and its revisions following a case of total failure and a case of a crack discovered on the support shaft of the sliding door rear roller. Metallurgical and metallographic analyses revealed a nonconformity concerning the heat treatment of the material. Since then, other cases of cracks and failures of the roller support shaft rear attach fitting had been reported. This condition, if not corrected, could lead to the loss of the sliding door in flight.''
Airworthiness Directives; MD Helicopters, Inc. Model MD-900 Helicopters
This document proposes superseding an existing airworthiness directive (AD) for MD Helicopters, Inc. (MDHI) Model MD-900 helicopters. That AD currently requires applying serial numbers to certain parts, increasing the life limit for various parts, maintaining a previously established life limit for a certain vertical stabilizer control system (VSCS) bellcrank assembly and bellcrank arm, and correcting the part number for the VSCS bellcrank arm. This proposal would require the same actions, except it would reduce the life limit of the swashplate spherical slider bearing (slider bearing). It would further correct what was described as a ``bellcrank arm'' life limit in the current AD and correctly describe it as another ``bellcrank assembly'' life limit. This proposal is prompted by two reports of cracks in the slider bearing that occurred well before the previously increased retirement life of 2,030 hours time-in-service (TIS) was reached. The actions specified by the proposed AD are intended to establish appropriate life limits for various parts, and to prevent fatigue failure of those parts and subsequent loss of control of the helicopter.
Special Conditions: Alenia Model C-27J Airplane; Liquid Oxygen System
These special conditions are issued for the Alenia Model C-27J airplane. This airplane will have novel or unusual design features when compared to the state of technology described in the airworthiness standards for transport-category airplanes. These design features include a liquid-oxygen (LOX) system. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for oxygen systems that use liquid oxygen. These special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards.
Standard Instrument Approach Procedures, and Takeoff Minimums and Obstacle Departure Procedures; Miscellaneous Amendments
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.
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.
Notice of Intent To Rule on Request To Release Airport Property at the Punxsutawney Municipal Airport, Punxsutawney, PA
The FAA proposes to rule and invite public comment on the release of land at the Punxsutawney Municipal Airport, Punxsutawney, Pennsylvania under the provisions of Section 47125(a) of Title 49 United States Code (U.S.C.).
Pilot, Flight Instructor, and Pilot School Certification; Correction
The Federal Aviation Administration (FAA) is making several corrections to its ``Pilot, Flight Instructor, and Pilot School Certification'' final rule published in the Federal Register on August 21, 2009. The FAA corrections include standardizing certain part 61 time period durations from ``60 days'' to now read ``2 calendar months.'' We are also correcting an omission and errors to the prerequisite eligibility requirements for use of flight simulators. Additionally, we are correcting the duration of a student pilot certificate to 60 calendar months for a student pilot seeking a sport pilot certificate. Finally, we are correcting a sentence in the preamble to conform with the final rule regarding the use of flight training devices.
Proposed Amendment of Class D Airspace; St Louis, MO
This action proposes to amend Class D airspace at St Louis, MO. Additional controlled airspace is necessary to accommodate new Standard Instrument Approach Procedures (SIAPs) at Spirit of St Louis Airport, St Louis, MO. The FAA is taking this action to enhance the safety and management of Instrument Flight Rules (IFR) operations for SIAPs at Spirit of St Louis Airport.
Establishment of VOR Federal Airway V-626; UT
This action establishes VOR Federal Airway 626 (V-626) located between the Myton, UT, Very High Frequency Omnidirectional Range/ Tactical Air Navigation (VORTAC) and the Salt Lake City terminal area. This route will improve aircraft flow during busy traffic periods into the Salt Lake City terminal area, and provide a more precise means of navigation and reduce controller workload.
Modification of Restricted Areas and Other Special Use Airspace; Fallon, NV
This action amends the time of designation and using agency of nine restricted areas located in the vicinity of the Fallon Naval Air Station (NAS), Fallon, NV, as part of a Department of the Navy initiative to standardize the operating hours throughout the Fallon Airspace Complex. The times of use are being expanded to meet the critical need of the Navy for additional nighttime training, and the using agency changes are administrative in accordance with a Navy realignment of functions. Additionally, this action modifies the times of use of the four military operation areas (MOAs) in the Fallon Airspace Complex. Unlike restricted areas, which are designated under 14 CFR part 73, MOAs are not rulemaking airspace actions. The MOA changes described here were published in the National Flight Data Digest (NFDD). The Navy requested these airspace changes to provide additional night training time to meet combat readiness requirements currently being carried out in accordance with 14 CFR 99.7.
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; Thielert Aircraft Engines GmbH (TAE) Models TAE 125-02-99 and TAE 125-01 Reciprocating Engines
We propose to adopt a new airworthiness directive (AD) for the products listed above. This proposed AD results from mandatory continuing airworthiness information (MCAIs) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAIs describe the unsafe condition as:
Aviation Rulemaking Advisory Committee-New Task
The FAA assigned the Aviation Rulemaking Advisory Committee (ARAC) a new task to provide advice and recommendations to the FAA about the current ARAC process. This notice informs the public of the new ARAC activity.
Airworthiness Directives; Airbus Model A330-200 and -300, and Model A340-300 Series Airplanes
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; Boeing Model 757 Airplanes
We propose to adopt a new airworthiness directive (AD) for certain Boeing Model 757 airplanes. This proposed AD would require replacing the power control relays for the fuel boost pumps and override pumps with new relays having a ground fault interrupt (GFI) feature. This proposed AD results from fuel system reviews conducted by the manufacturer. We are proposing this AD to prevent damage to the fuel pumps caused by electrical arcing that could introduce an ignition source in the fuel tank, which, in combination with flammable fuel vapors, could result in a fuel tank explosion and consequent loss of the airplane.
Airworthiness Directives; Boeing Model 737-600, -700, -700C, -800, and -900 Series Airplanes
We propose to adopt a new airworthiness directive (AD) for certain Boeing Model 737-600, -700, -700C, -800, and -900 series airplanes. This proposed AD would require inspections for scribe lines in the fuselage skin at lap joints, the splice strap at certain butt joints, the skin or doubler at certain approved repair doublers, and the skin at decal locations; and related investigative and corrective actions if necessary. This proposed AD results from reports of scribe line damage found adjacent to the skin lap joints, decals, and wing-to- body fairings. We are proposing this AD to detect and correct scribe lines, which can develop into fatigue cracks in the skin. Undetected fatigue cracks can grow and cause sudden decompression of the airplane.
Airworthiness Directives; Boeing Model 757 Airplanes
We are revising an earlier proposed airworthiness directive (AD) for all Boeing Model 757-200, -200PF, -200CB, and -300 series airplanes. The original NPRM would have required an inspection of the two spring arms in the spin brake assemblies in the nose wheel well to determine if the spring arms are made of aluminum or composite material, and repetitive related investigative/corrective actions if necessary. The original NPRM resulted from reports of cracked and broken aluminum springs. This action revises the original NPRM to include a parts installation paragraph and to provide options for terminating the repetitive actions. We are proposing this supplemental NPRM to detect and correct cracked or broken springs. A cracked or broken spring could separate from the airplane and result in potential hazard to persons or property on the ground, or ingestion into the engine with engine damage and potential shutdown, or damage to the airplane.
Modification of Class E Airspace; Beckley, WV
This action modifies Class E airspace at Beckley, WV. Controlled airspace is being expanded to contain the Area Navigation (RNAV) Global Positioning System (GPS) Standard Instrument Approach Procedures (SIAPs) that have been developed for Raleigh County Memorial Airport. This action enhances the National Airspace System by providing controlled airspace in the vicinity of Beckley, WV.
Establishment of Class E Airspace; Spencer, WV
This action establishes Class E Airspace at Spencer, WV. This action enhances the safety and airspace management of Boggs Field Airport, Spencer, WV.
Amendment of Class E Airspace; Minden, NE
This action amends Class E airspace at Minden, NE. Additional controlled airspace is necessary to accommodate Area Navigation (RNAV) Standard Instrument Approach Procedures (SIAPs) at Pioneer Village Field Airport, Minden, NE. The FAA is taking this action to enhance the safety and management of Instrument Flight Rule (IFR) operations at Pioneer Village Field Airport.
Amendment of Class E Airspace; Peoria, IL
This action amends Class E airspace for the Peoria, IL area. Additional controlled airspace is necessary to accommodate Area Navigation (RNAV) Standard Instrument Approach Procedures (SIAP) at Mount Hawley Auxiliary Airport, Peoria, IL. The FAA is taking this action to enhance the safety and management of Instrument Flight Rule (IFR) operations at Mount Hawley Auxiliary Airport.
Amendment of Class E Airspace; Winona, MN
This action amends Class E airspace at Winona, MN. Additional controlled airspace is necessary to accommodate Area Navigation (RNAV) Standard Instrument Approach Procedures (SIAP) at Winona Municipal AirportMax Conrad Field, Winona, MN. The FAA is taking this action to enhance the safety and management of Instrument Flight Rule (IFR) operations at Winona Municipal AirportMax Conrad Field.
Amendment of Class E Airspace; St. Louis, MO
This action amends Class E airspace for the St. Louis, MO area. Additional controlled airspace is necessary to accommodate Area Navigation (RNAV) Standard Instrument Approach Procedures (SIAP) at Spirit of St. Louis Airport, St. Louis, MO. Also, this action makes minor adjustments to the geographic coordinates for the Lambert-St. Louis International Airport, St. Louis VORTAC, and the Foristell VORTAC. The FAA is taking this action to enhance the safety and management of Instrument Flight Rule (IFR) operations at Spirit of St. Louis Airport.
Amendment of Class E Airspace; Tioga, ND
This action amends Class E airspace at Tioga, ND. Additional controlled airspace is necessary to accommodate Area Navigation (RNAV) Standard Instrument Approach Procedures (SIAP) at Tioga Municipal Airport, Tioga, ND. This action also amends the geographic coordinates of Tioga Municipal Airport. The FAA is taking this action to enhance the safety and management of Instrument Flight Rule (IFR) operations at Tioga Municipal Airport.
Airworthiness Directives; BAE Systems (Operations) Limited Model BAe 146 and Avro 146-RJ Airplanes
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: Reports have been received of finding corrosion at the Frame 29 wing-to-fuselage attachment lug plate joint. This condition, if not detected and corrected, could result in a degradation of the structural integrity of Frame 29 and the wing-to-fuselage attachment.
Airworthiness Directives; Rolls-Royce plc RB211 Trent 800 Series Turbofan Engines
The FAA is superseding an existing airworthiness directive (AD) for Rolls-Royce plc RB211 Trent 875-17, Trent 877-17, Trent 884- 17, Trent 892-17, Trent 892B-17, and Trent 895-17 turbofan engines with high-pressure (HP) compressor rotor rear stage 5 and 6 discs and cone shafts, part numbers (P/Ns) FK25230 and FK27899 installed. That AD currently requires removal from service of these HP compressor rotor rear stage 5 and 6 discs and cone shafts before reaching newly reduced life limits. This AD requires removing these parts at new reduced cycle limits. This AD results from Rolls-Royce plc reducing the lives of these parts and changing the life calculating method to use ``Standard Duty Cycles'' with ``Multiple Flight Profile Monitoring'' and ``Flight Cycles'' with ``Heavy Flight Profile Monitoring''. We are issuing this AD to prevent stage 5 and 6 disc crack initiation and propagation that might lead to uncontained disc failure and damage to the airplane.
Airworthiness Directives; Turbomeca S.A. ARRIUS 1A Turboshaft Engines
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:
Production and Airworthiness Approvals, Part Marking, and Miscellaneous Amendments
The FAA is amending its certification procedures and identification requirements for aeronautical products and articles. The amendments will update and standardize those requirements for production approval holders (PAHs), revise export airworthiness approval requirements to facilitate global manufacturing, move all part marking requirements from part 21 to part 45, and amend the identification requirements for products and articles. The intent of these changes is to continue to promote safety by ensuring that aircraft, and products and articles designed specifically for use in aircraft, wherever manufactured, meet appropriate minimum standards for design and construction. As a result of this action, the FAA's regulations now better reflect the current global aircraft and aircraft products and articles manufacturing environment.
Notice of Intent To Request Revision From the Office of Management and Budget of a Currently Approved Information Collection Activity, Request for Comments; Safe Disposition of Life-Limited Aircraft Parts
The FAA invites public comments about our intention to request the Office of Management and Budget (OMB) to approve a current information collection. This action responds to the Wendall Fl. Ford Investment and Reform Act for the 21st Century by requiring that all persons who remove any life-limited aircraft part have a method to prevent the installation of that part after it has reached its life limit.
Notice of Intent To Request Revision From the Office of Management and Budget of a Currently Approved Information Collection Activity, Request for Comments; Pilot Schools-FAR 141
The FAA invites public comments about our intention to request the Office of Management and Budget (OMB) to approve a current information collection. 49 CFR Part 44707 authorizes certification of civilian schools giving instruction in flying. Information collected is used for certification and to determine applicant compliance.
Notice of Intent To Request Revision From the Office of Management and Budget of a Currently Approved Information Collection Activity, Request for Comments; Representatives of the Administrator, 14 CFR Part 183
The FAA invites public comments about our intention to request the Office of Management and Budget (OMB) to approve a current information collection. Title 49, United States Code, Section 44702 authorizes the appointment of appropriately qualified persons to be representatives of the Administrator to allow those persons to examine, test and certify other persons for the purpose of issuing them pilot and instructor certificates.
Notice of Intent To Request Revision From the Office of Management and Budget of a Currently Approved Information Collection Activity, Request for Comments; Notice of Landing Area Proposal
The FAA invites public comments about our intention to request the Office of Management and Budget (OMB) to approve a current information collection. FAR Part 157 requires that each person who intends to construct, deactivate, or change the status of an airport, runway, or taxiway must notify the FAA of such activity.
Notice of Intent To Request Revision From the Office of Management and Budget of a Currently Approved Information Collection Activity, Request for Comments; Anti-Drug Program for Personnel Engaged in Specified Aviation Activities
The FAA invites public comments about our intention to request the Office of Management and Budget (OMB) to approve a current information collection. The FAA uses this information for determining program compliance or non-compliance of regulated aviation employers, oversight planning, determining who must provide annual MIS testing information, and communicating with entities subject to the program regulations.
Notice of Intent To Request Revision From the Office of Management and Budget of a Currently Approved Information Collection Activity, Request for Comments; Application for Employment With the Federal Aviation Administration
The FAA invites public comments about our intention to request the Office of Management and Budget (OMB) to approve a current information collection. This collection is necessary for gathering data concerning potential new hires for the FAA.
Notice of Intent To Request Revision From the Office of Management and Budget of a Currently Approved Information Collection Activity, Request for Comments; National Air Tour Safety Standards
The FAA invites public comments about our intention to request the Office of Management and Budget (OMB) to approve a current information collection. This final rule sets safety and oversight rules for a broad variety of sightseeing and commercial air tour flights.
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