Department of Transportation April 13, 2005 – Federal Register Recent Federal Regulation Documents
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Change 1 to AC 23-15A, Small Airplane Certification Compliance Program
This notice announces the issuance of change 1 to AC 23-15A, Small Airplane Certification Compliance Program. Change 1 to AC 23-15A deletes the fourth sentence in paragraph 5n(2)(e) and deletes ``fatigue properties'' in fifth sentence in paragraph 5n(2)(e). This change is required since the paragraph was misinterpreted by some, to mean that no fatigue testing is required for composites. A parallel was drawn between the failure phenomenon (at a micro level) of wood and composites. Since the comparison created confusion, all mention of composites is eliminated.
Vessel Documentation: Lease Financing for Vessels Engaged in the Coastwise Trade; Second Rulemaking
The Coast Guard and the Maritime Administration (MARAD) are withdrawing their joint notice of proposed rulemaking on documentation, under the lease-financing provisions, of vessels engaged in the coastwise trade. The joint notice of proposed rulemaking was superseded by legislation. A new notice of proposed rulemaking addressing the provisions of the new legislation will be published in the future.
Civilian Use of, and Requirements for, the Next Generation of GPS for Automotive Safety
The U.S. Department of Transportation (DOT) is working closely with the U.S. Department of Defense (DOD) in modernizing the Global Positioning System (GPS). In this document, the National Highway Traffic Safety Administration (NHTSA) is requesting comments and information to help us determine the civilian specifications for the next generation of the GPS (GPS III) based on future automotive safety needs that could be enhanced by a modernized GPS.
Special Conditions; Twin Commander Aircraft Models 690C, 690D, 695, 695A, and 695B; Protection of Systems for High Intensity Radiated Fields (HIRF)
These special conditions are issued to Twin Commander Aircraft LLC. 19010 59th DR. NE. Arlington, WA. 98223 for a Supplemental Type Certificate for the Twin Commander Aircraft Models 690C, 690D, 695, 695A, and 695B. These airplanes will have novel and unusual design features when compared to the state of technology envisaged in the applicable airworthiness standards. The novel and unusual design features include the installation of dual Innovative Solutions & Support (IS&S) Air Data Display Units (ADDU) for which the applicable regulations do not contain adequate or appropriate airworthiness standards for the protection of these systems from the effects of high intensity radiated fields (HIRF). These special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to the airworthiness standards applicable to these airplanes.
Notice of Availability of Draft Environmental Impact Statement (DEIS), Notice of Public Comment Period for the DEIS and Schedule of Public Information Meetings and Public Hearings for Proposed Development Activities at the Juneau International Airport, Juneau, AK
The Federal Aviation Administration is issuing this notice to advise the public that a Draft Environmental Impact Statement (DEIS) for Proposed Development Activities at the Juneau International Airport (JNU) has been prepared and is available for public review and comment. Written requests for the DEIS and written comments on the DEIS can be submitted to the individual listed in the section FOR FURTHER INFORMATION CONTACT. Public information meetings and public hearings will be held on June 1 and June 2, 2005. The public comment period will commence on April 29, 2009 and will close on June 30, 2005. Public Comment and Information Meetings/Public Hearings: The start of the public comment period on the DEIS will be April 29, 2005 and will end on June 30, 2005. Two combined public Information meetings and public hearings will be held on June 1 and June 2, 2005, at different times to accommodate differences in availability of interested parties. The public information meeting on Wednesday, June 1 will begin at 3 p.m. (ADT) and will last until 5 p.m. (ADT). The public hearing on that date will begin shortly after the public information meeting, at 5:30 p.m. (ADT). The public information meeting on Thursday, June 2 will begin at 5 p.m. (ADT) and will last until 7 p.m. (ADT). The public hearing on that date will begin shortly after the public information meeting, at 7:30 p.m. (ADT). The location for both of the Public Information Meetings/Public Hearings is Centennial Hall, 101 Egan Drive, Juneau, AK 99801.
Special Conditions; Lancair LC41-550FG and LC42-550FG for the Protection of Systems From High Intensity Radiated Fields (HIRF)
These special conditions are issued to The Lancair Company, 22550 Nelson Road, Bend, Oregon 97701, for a Type Design Change for the Lancair LC41-550FG and LC42-550FG airplanes. These airplanes have novel and unusual design features when compared to the state of technology envisaged in the applicable airworthiness standards. These novel and unusual design features include the installation of electronic flight instrument system (EFIS) displays Model 700-00006-XXX-( ) manufactured by Avidyne Corporation for which the applicable regulations do not contain adequate or appropriate airworthiness standards for the protection of these systems from the effects of high intensity radiated fields (HIRF). These special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to the airworthiness standards applicable to these airplanes.
Notice of Intent To Rule on Application To Impose and Use the Revenue From a Passenger Facility Charge (PFC) at Key Field Airport, Meridian, MS
The FAA proposes to rule and invites public comment on the application to impose and use the revenue from a PFC at Key Field Airport 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).
Airworthiness Directives; General Electric Company (GE) CF6-45 and CF6-50 Series Turbofan Engines
The FAA is adopting a new airworthiness directive (AD) for GE CF6-45 and CF6-50 series turbofan engines. This AD requires reviewing accumulated cyclic-life records of 10 life-limited rotating parts, correcting those records, and removing from service parts that exceed the low-cycle-fatigue (LCF) life limits published in the Engine Manual Chapter 5, Airworthiness Limitations Section (ALS). This AD results from an error in a tracking database that subtracted flight cycles of certain serial number (SN) parts from the actual accumulated cycles. We are issuing this AD to prevent rotating parts that may have exceeded their LCF life limit from failing, leading to uncontained engine failure.
Airworthiness Directives; GROB-WERKE Model G120A Airplanes
The FAA proposes to adopt a new airworthiness directive (AD) for all GROB-WERKE (GROB) Model G120A airplanes. This proposed AD would require you to repetitively inspect the nose landing gear (NLG) assembly, paying special attention to the NLG swivel tube and the engine truss in the area of the NLG attachment, for cracks and damaged (defective) welding seams. If you find cracks or defects during any inspection, this proposed AD would require you to replace the cracked or defective part. This proposed AD results from mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. We are issuing this proposed AD to detect and correct cracks and defects in the NLG assembly, which could result in failure of the NLG. This failure could lead to a hard landing and/or loss of control of the airplane during landing operations.
Airworthiness Directives; Pilatus Aircraft Ltd. Models PC-12 and PC-12/45 Airplanes
The FAA proposes to adopt a new airworthiness directive (AD) for certain Pilatus Aircraft Ltd. (Pilatus) Models PC-12 and PC-12/45 airplanes. This proposed AD would require you to insert a temporary revision into the Limitations Section of the Pilot Operating Handbook (POH). This proposed AD would also require you to replace the pitch actuator with an improved design pitch actuator and make the necessary wiring and circuit breaker changes, as applicable. Installing the improved design pitch actuator terminates the need for the temporary revision in the POH. This proposed AD results from mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Switzerland. We are issuing this proposed AD to prevent an out-of- trim condition from occurring when the flaps are at a 40-degree flight phase and the pilot disconnects the autopilot. This condition could lead to reduced ability to control the airplane.
Airworthiness Directives; Boeing Model 747-100, -200B, -200F, -200C, -100B, -300, -100B SUD, -400, -400D, and -400F Series Airplanes; and Model 747SR Series Airplanes
The FAA proposes to supersede two existing airworthiness directives (AD) for certain Boeing transport category airplanes. One AD currently requires doing certain inspections to detect cracks and corrosion around the lower bearing of the actuator attach fittings of the inboard and outboard flaps; repairing if necessary; and either overhauling the fittings or replacing them, which when done on certain actuator attach fittings ends the repetitive inspections. The other AD currently requires certain other inspections to detect discrepancies of the fittings of the flaps, and follow-on and corrective actions if necessary, which ends the repetitive inspections of the first AD. For certain airplanes, this proposed AD would require new inspections for discrepancies of the attach fittings of the flaps, and follow-on and corrective actions if necessary, which ends the repetitive inspections of both existing ADs. For all airplanes, this proposed AD would require repetitive overhaul/replacements of the fittings of both the inboard and outboard flaps. This proposed AD is prompted by reports of cracks of the attach fittings of the trailing edge flaps. We are proposing this AD to prevent cracking and other damage of the actuator attach fittings of the trailing edge flaps, which could result in abnormal operation or retraction of a trailing edge flap, and possible loss of controllability of the airplane.
Office of Small and Disadvantaged Business Utilization; Notice of Request for New Data Collection
In accordance with the Paperwork Reduction Act of 1995 (44 U.S.C. 3501 et seq.), this notice announces that the Information Collection Request (ICR) abstracted below has been forwarded to the Office of Management and Budget (OMB) for approval and comment. The ICR describes the nature of the information collection and its expected cost and burden. The Federal Register Notice with a 60-day comment period soliciting comments on the following collection of information was published on January 7, 2005 [FR Vol. 70, No. 5, page 1500-1501]. No comments were received.
Office of Small and Disadvantaged Business Utilization; Notice of Request for New Data Collection
In accordance with the Paperwork Reduction Act of 1995 (44 U.S.C. 3501 et seq.), this notice announces that the Information Collection Request (ICR) abstracted below has been forwarded to the Office of Management and Budget (OMB) for approval and comment. The ICR describes the nature of the information collection and its expected cost and burden. The Federal Register Notice with a 60-day comment period soliciting comments on the following collection of information was published on December 30, 2004 [Volume 69, Number 250] and January 7, 2005 [FR Vol. 70, No. 5, page 1501] (correction). No comments were received.
Agency Information Collection; Activity Under OMB Review; Report of Financial and Operating Statistics for Small Aircraft Operators
In compliance with the Paperwork Reduction Act of 1995 (44 U.S.C. 3501 et seq.), this notice announces that the Information Collection Request (ICR) abstracted below has been forwarded to the Office of Management and Budget (OMB) for extension of currently approved collections. The ICR describes the nature of the information collection and its expected burden. The Federal Register Notice with a 30-day comment period soliciting comments on the following collection of information was published on December 17, 2004 (69 FR 75601).
Notice of Order Adjusting the Standard Foreign Fare Level Index
The Department revises the Standard Foreign Fare Level (SFFL) to reflect the latest available fuel and non fuel cost changes experienced by carriers, as required by 40 U.S.C. 41509(e).
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