This is a list of United States Code sections, Statutes at Large, Public Laws, and Presidential Documents, which provide rulemaking authority for this CFR Part.
This list is taken from the Parallel Table of Authorities and Rules provided by GPO [Government Printing Office] .
It is not guaranteed to be accurate or up-to-date, though we do refresh the database weekly. More limitations on accuracy are described at the GPO site.
United States Code U.S. Code: Title 49 - TRANSPORTATION
Title 14 published on 2015-01-01
The following are ALL rules, proposed rules, and notices (chronologically) published in the Federal Register relating to 14 CFR Part 23 after this date.
2015-12-09; vol. 80 # 236 - Wednesday, December 9, 2015 80 FR 76379 - Special Conditions: Cirrus Aircraft Corporation, SF50; Auto Throttle
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions. The effective date of these special conditions is December 9, 2015 and are applicable on December 2, 2015. 14 CFR Part 23 Summary These special conditions are issued for the Cirrus Aircraft Corporation Model SF50 airplane. This airplane will have a novel or unusual design feature(s) associated with installation of an Auto Throttle System. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. 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.
2015-11-04; vol. 80 # 213 - Wednesday, November 4, 2015 80 FR 68281 - Special Conditions: Kestrel Aircraft Company, Model K-350 Turboprop, Lithium Batteries
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Notice of proposed special conditions. Send your comments on or before December 21, 2015. 14 CFR Part 23 Summary This action proposes special conditions for the Kestrel Aircraft Company, Model K-350 Turboprop airplane. This airplane will have a novel or unusual design feature associated with the installation of a rechargeable lithium battery. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. 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.
2015-10-30; vol. 80 # 210 - Friday, October 30, 2015 80 FR 66788 - Special Conditions: Honda Aircraft Company (Honda) Model HA-420, HondaJet; Cruise Speed Control System
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions. These special conditions are effective October 30, 2015 and are applicable on October 26, 2015. 14 CFR Part 23 Summary These special conditions are issued for the Honda Aircraft Company HA-420 airplane. This airplane will have a novel or unusual design feature(s) associated with the use of a cruise speed control system. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. 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.
2015-09-23; vol. 80 # 184 - Wednesday, September 23, 2015 80 FR 57289 - Special Conditions: Cirrus Design Corporation, SF50; Full Authority Digital Engine Control (FADEC) System
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. The effective date of these special conditions is September 23, 2015. We must receive your comments by October 23, 2015. 14 CFR Part 23 Summary These special conditions are issued for the Cirrus Design Corporation SF50 airplane. This airplane will have a novel or unusual design feature(s) associated with the use of an electronic engine control system instead of a traditional mechanical control system. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. 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.
80 FR 57291 - Special Conditions: Honda Aircraft Company, Model HA-420 HondaJet, Lithium-ion Batteries
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions. These special conditions are effective September 23, 2015. 14 CFR Part 23 Summary These special conditions are issued for the Honda Aircraft Company, Model HA-420 airplane. This airplane will have a novel or unusual design feature associated with the installation of lithium-ion (Li-ion) batteries. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. 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.
80 FR 57312 - Special Conditions: Honda Aircraft Company (Honda) Model HA-420, HondaJet; Cruise Speed Control System
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Notice of proposed special conditions. Send your comments on or before October 23, 2015. 14 CFR Part 23 Summary This action proposes special conditions for the Honda Aircraft Company HA-420 airplane. This airplane will have a novel or unusual design feature(s) associated with the use of a cruise speed control system. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. 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.
2015-09-11; vol. 80 # 176 - Friday, September 11, 2015 80 FR 54713 - Special Conditions: Korea Aerospace Industries, Ltd., Model K-100; Full Authority Digital Engine Control (FADEC) System
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. The effective date of these special conditions is September 11, 2015. We must receive your comments by October 26, 2015. 14 CFR Part 23 Summary These special conditions are issued for the Korea Aerospace Industries, Ltd., Model K-100 airplane. This airplane will have a novel or unusual design feature(s) associated with the use of an electronic engine control system instead of a traditional mechanical control system. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. 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.
2015-08-21; vol. 80 # 162 - Friday, August 21, 2015 80 FR 50808 - Special Conditions: Cirrus Aircraft Corporation, SF50; Auto Throttle.
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Notice of proposed special conditions. Send your comments on or before October 5, 2015. 14 CFR Part 23 Summary This action proposes special conditions for the Cirrus Aircraft Corporation Model SF50 airplane. This airplane will have a novel or unusual design feature(s) associated with installation of an Auto Throttle System. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. 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.
2015-08-20; vol. 80 # 161 - Thursday, August 20, 2015 80 FR 50587 - Revisions to Operational Requirements for the Use of Enhanced Flight Vision Systems (EFVS) and to Pilot Compartment View Requirements for Vision Systems; Reopening of Comment Period
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Notice of proposed rulemaking; reopening of comment period. The comment period for the NPRM published on June 11, 2013 (78 FR 34935) closed October 15, 2013, and is reopened until September 21, 2015. 14 CFR Part 1, 23, 25, 27, 29, 61, 91, 121, 125, 135 Summary This action reopens the comment period for the regulatory evaluation associated with the FAA's June 11, 2013 Notice of Proposed Rulemaking (NPRM), Revisions to Operational Requirements for the Use of Enhanced Flight Vision Systems (EFVS) and to Pilot Compartment View Requirements for Vision Systems. The regulatory evaluation associated with the NPRM was not posted to the docket prior to the close of the comment period. Therefore, the FAA is reopening the comment period to allow the public the opportunity to adequately analyze the full regulatory evaluation for the NPRM. The FAA will accept comments on the regulatory evaluation only; and not on the regulatory changes proposed in the NPRM.
2015-08-12; vol. 80 # 155 - Wednesday, August 12, 2015 80 FR 48242 - Special Conditions: Honda Aircraft Company, Model HA-420, HondaJet; Ventilation Requirements in High Altitude Operations
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. The effective date of these special conditions is August 12, 2015. We must receive your comments by September 11, 2015 14 CFR Part 23 Summary These special conditions are issued for the Honda Aircraft Company, Model HA-420 airplane. This airplane will have a novel or unusual design feature associated with high altitude operations above 41,000 feet. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. 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.
2015-06-16; vol. 80 # 115 - Tuesday, June 16, 2015 80 FR 34242 - Special Conditions: Honda Aircraft Company, Model HA-420; Fire Extinguishing for Overwing Pylon Mounted Engines
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. The effective date of these special conditions is June 16, 2015. We must receive your comments by July 16, 2015. 14 CFR Part 23 Summary These special conditions are issued for the Honda Aircraft Company model HA-420 airplane. This airplane will have a novel or unusual design feature associated with mounting the engines on the wings in close proximity to the aft fuselage. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. 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.
2015-05-21; vol. 80 # 98 - Thursday, May 21, 2015 80 FR 29205 - Special Conditions: Cirrus Design Corporation Model SF50 airplane; Full Authority Digital Engine Control (FADEC) System; Withdrawal
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; withdrawal. Effective May 21, 2015, the special condition published on April 20, 2010 (75 FR 20518) is withdrawn. 14 CFR Part 23 Summary The FAA is withdrawing a previously published document granting special conditions for the Cirrus Design Corporation model SF50 airplane. We are withdrawing Special Condition No. 23-246-SC through mutual agreement with Cirrus Design Corporation.
2015-04-27; vol. 80 # 80 - Monday, April 27, 2015 80 FR 23229 - Special Conditions: Honda Aircraft Company Model HA-420 Hondajet, Fire Extinguishing; Withdrawal
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; withdrawal. This special condition published on September 23, 2008 (73 FR 54675) is withdrawn, effective April 27, 2015. 14 CFR Part 23 Summary The FAA is withdrawing a previously published notice granting special conditions for the Honda Aircraft Company model HA-420 jet airplane. We are withdrawing Special Condition No. 23-227-SC through mutual agreement with Honda Aircraft Company.
80 FR 23229 - Special Conditions: Honda Aircraft Company Model HA-420 Hondajet, Protection of Systems for High Intensity Radiated Fields (HIRF); Withdrawal
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; withdrawal. This special condition published on December 10, 2007 (72 FR 69572) is withdrawn, effective April 27, 2015. 14 CFR Part 23 Summary The FAA is withdrawing a previously published notice granting special conditions for the Honda Aircraft Company model HA-420 jet airplane. We are withdrawing Special Condition No. 23-217-SC through mutual agreement with Honda Aircraft Company.
2015-04-14; vol. 80 # 71 - Tuesday, April 14, 2015 80 FR 19889 - Special Conditions: Honda Aircraft Company, Model HA-420 HondaJet, Lithium-Ion Batteries
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Notice of proposed special conditions. Send your comments on or before May 4, 2015. 14 CFR Part 23 Summary This action proposes special conditions for the Honda Aircraft Company, Model HA-420 airplane. This airplane will have a novel or unusual design feature associated with the installation of lithium-ion (Li-ion) batteries. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. 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.
2015-04-01; vol. 80 # 62 - Wednesday, April 1, 2015 80 FR 17310 - Special Conditions: Honda Aircraft Company Model HA-420; Single-Place Side-Facing Seat Dynamic Test Requirements
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. The effective date of these special conditions is April 1, 2015, and is applicable on March 25, 2015. We must receive your comments by May 1, 2015. 14 CFR Part 23 Summary These special conditions are issued for the Honda Aircraft Company HA-420 airplane. This airplane will have a novel or unusual design feature(s) associated with a side-facing passenger seat. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. 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.
80 FR 17312 - Special Conditions: Honda Aircraft Company (Honda) Model HA-420, HondaJet; Full Authority Digital Engine Control (FADEC) System
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. The effective date of these special conditions is April 1, 2015, and is applicable on March 25, 2015. We must receive your comments by May 1, 2015. 14 CFR Part 23 Summary These special conditions are issued for the Honda Aircraft Company HA-420 airplane. This airplane will have a novel or unusual design feature associated with the use of an electronic engine control system instead of a traditional mechanical control system. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. 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.
