Source: http://www.law.cornell.edu/cfr/text/14/25/subpart-I?quicktabs_7=0
Timestamp: 2013-12-20 06:08:44
Document Index: 199438781

Matched Legal Cases: ['art 25', '§ 25', 'art 25', 'art 25', 'art 25', 'art 25', 'art 25', 'art 25', 'art 25', 'art 25', 'art 25', 'art 25', 'art 25', 'art 25', 'art 25', 'art 25', 'art 25', 'art 25', 'art 25', 'art 25', 'art 25', 'art 25', 'art 25', 'art 25']

14 CFR 25, Subpart I - Special Federal Aviation Regulations | Title 14 - Aeronautics and Space | Code of Federal Regulations | LII / Legal Information Institute
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14 CFR 25, Subpart I - Special Federal Aviation Regulations
§ 25.1801 — SFAR No. 111—Lavatory Oxygen Systems.
Title 14 published on 2013-01-01The following are only the Rules published in the Federal Register after the published date of Title 14.For a complete list of all Rules, Proposed Rules, and Notices view the Rulemaking tab.2013-05-29; vol. 78 # 103 - Wednesday, May 29, 201378 FR 32078 - Special Conditions: Gulfstream Model G280 Airplane, Enhanced Flight Vision System (EFVS) With Head-Up Display (HUD)
typeregulations.gov FR Doc.2013-12605 RIN Docket No.FAA-2013-0406 Special Conditions No.25-493-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. The effective date of these special conditions is May 22, 2013. We must receive your comments by June 28, 2013. 14 CFR Part 25 SummaryThese special conditions are issued for the Gulfstream model G280 series airplanes. These airplanes, as modified by Gulfstream Aerospace Corporation, will have an advanced, enhanced-flight-vision system (EFVS). The EFVS is a novel or unusual design feature which consists of a head-up display (HUD) system modified to display forward-looking infrared (FLIR) imagery. 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.
2013-05-28; vol. 78 # 102 - Tuesday, May 28, 201378 FR 31835 - Special Conditions: Embraer S.A., Model EMB-550 Airplane; Landing Pitchover Condition
typeregulations.gov FR Doc.2013-12534 RIN Docket No.FAA-2013-0148 Special Conditions No.25-490-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions. Effective Date: June 27, 2013. 14 CFR Part 25 SummaryThese special conditions are issued for the Embraer S.A. Model EMB-550 airplane. This airplane will have a novel or unusual design feature associated with landing loads due to the automatic braking 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.
78 FR 31836 - Special Conditions: Embraer S.A., Model EMB-550 Airplane, Dive Speed Definition With Speed Protection System
typeregulations.gov FR Doc.2013-12535 RIN Docket No.FAA-2012-1301 Special Conditions No.25-491-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions. Effective Date: June 27, 2013. 14 CFR Part 25 SummaryThese special conditions are issued for the Embraer S.A. Model EMB-550 airplane. This airplane will have a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. These design features include a high-speed protection 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.
78 FR 31838 - Special Conditions: Embraer S.A., Model EMB-550 Airplanes; Flight Envelope Protection: General Limiting Requirements
typeregulations.gov FR Doc.2013-12536 RIN Docket No.FAA-2012-1332 Special Conditions No.25-492-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions. Effective Date: June 27, 2013. 14 CFR Part 25 SummaryThese special conditions are issued for the Embraer S.A. Model EMB-550 airplane. This airplane will have a novel or unusual design feature, specifically new control architecture and a full digital flight control system which provides flight envelope protections. 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.
2013-05-03; vol. 78 # 86 - Friday, May 3, 201378 FR 25840 - Installed Systems and Equipment for Use by the Flightcrew
typeregulations.gov FR Doc.2013-07651 RIN Docket No.FAA-2012-1215, Special Conditions No. 25-482-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; correction. The effective date of this correction is May 3, 2013. 14 CFR Part 25 SummaryThis document corrects an error that appeared in Docket No. FAA-2012-1215, Special Conditions No. 25-12-482-SC, which was published in the Federal Register on February 19, 2013 (78 FR 11562). The error was an extra number, “12,” in the number of Special Conditions. To avoid confusion, the special conditions published as Docket No. FAA-2012-1215, Special Conditions No. 25-12-482-SC, has been renamed Docket No. FAA-2012-1215, Special Conditions No. 25-482-SC. The heading of this correction also reflects the correct Special Conditions No. 25-482-SC.
2013-03-05; vol. 78 # 43 - Tuesday, March 5, 201378 FR 14155 - Special Conditions: Learjet Inc., Model LJ-200-1A10 Airplane; Use of Automatic Power Reserve (APR), an Automatic Takeoff Thrust Control System (ATTCS), for Go-Around Performance Credit
typeregulations.gov FR Doc.2013-05006 RIN Docket No.FAA-2013-0154 Special Conditions No.25-484-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. The effective date of these special conditions is February 13, 2013. We must receive your comments by April 19, 2013. 14 CFR Part 25 SummaryThese special conditions are issued for the Learjet Model LJ-200-1A10 airplane. This airplane will have novel or unusual design features associated with utilizing go-around performance credit when using an automatic takeoff thrust 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.
2013-03-04; vol. 78 # 42 - Monday, March 4, 201378 FR 14005 - Special Conditions: Embraer S.A., Model EMB-550 Airplanes; Flight Envelope Protection: Pitch and Roll Limiting Functions
typeregulations.gov FR Doc.2013-04855 RIN Docket No.FAA-2012-1211 Special Conditions No.25-486-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions. Effective Date: April 3, 2013. 14 CFR Part 25 SummaryThese special conditions are issued for the Embraer S.A. Model EMB-550 airplane. This airplane will have a novel or unusual design feature associated with pitch and roll limiting functions, specifically an electronic flight control system which contains fly-by-wire control laws, including envelope protections. 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.
78 FR 14007 - Special Conditions: Embraer S.A., Model EMB-550 Airplanes; Electrical/Electronic Equipment Bay Fire Detection and Smoke Penetration
typeregulations.gov FR Doc.2013-04854 RIN Docket No.FAA-2012-1292 Special Conditions No.25-485-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions. Effective April 3, 2013. 14 CFR Part 25 SummaryThese special conditions are issued for the Embraer S.A. Model EMB-550 airplane. This airplane will have novel or unusual design features, specifically distributed electrical and electronic equipment bays in pressurized areas of the airplane. Older transport category airplane electrical/electronic equipment bay installations are located in the lower lobe where the flight crew could determine the origin of smoke or fire by a straightforward airplane flight manual procedure. In distributed electrical/electronic bay installations it is not as straightforward. The FAA has no requirement for smoke and/or fire detection in the electrical/electronic equipment bays. To ensure effective mitigation of fires, the FAA proposes these special conditions. 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.
2013-02-19; vol. 78 # 33 - Tuesday, February 19, 201378 FR 11553 - Special Conditions: Embraer S.A., Model EMB-550 Airplane; Electronic Flight Control System: Control Surface Awareness and Mode Annunciation
typeregulations.gov FR Doc.2013-03656 RIN Docket No.FAA-2012-0978 Special Conditions No.25-478-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions. Effective Date: March 21, 2013. 14 CFR Part 25 SummaryThese special conditions are issued for the Embraer S.A. Model EMB-550 airplane. This airplane will have a novel or unusual design feature(s) associated with the control surface awareness and mode annunciation of the electronic flight 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.
typeregulations.gov FR Doc.2013-03657 RIN Docket No.FAA-2012-1216 Special Conditions No.25-479-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions. Effective Date: March 21, 2013. 14 CFR Part 25 SummaryThese special conditions for the Embraer S.A. Model EMB-550 airplane. This airplane will have a novel or unusual design feature, specifically sidestick controllers designed to be operated with only one hand. 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.
78 FR 11555 - Special Conditions: Embraer S.A., Model EMB-550 Airplane; Design Roll Maneuver for Electronic Flight Controls
typeregulations.gov FR Doc.2013-03658 RIN Docket No.FAA-2012-1241 Special Conditions No.25-480-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions. Effective Date: March 21, 2013. 14 CFR Part 25 SummaryThese special conditions are issued for the Embraer S.A. Model EMB-550 airplane. This airplane will have a novel or unusual design feature(s) associated with the design roll maneuver for electronic flight controls, specifically an electronic flight control system that provides control of the aircraft through pilot inputs to the flight computer. 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.
78 FR 11556 - Special Conditions: Embraer S.A., Model EMB-550 Airplane; Interaction of Systems and Structures
typeregulations.gov FR Doc.2013-03678 RIN Docket No.FAA-2012-1246 Special Conditions No.25-481-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions. Effective date: March 21, 2013. 14 CFR Part 25 SummaryThese special conditions are issued for the Embraer S.A. Model EMB-550 airplane. This airplane will have a novel or unusual design feature(s) associated with the interaction of systems and structures. 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.
78 FR 11560 - Special Conditions: Embraer S.A., Model EMB-550 Airplane; Electronic Flight Control System: Lateral-Directional and Longitudinal Stability and Low Energy Awareness
typeregulations.gov FR Doc.2013-03677 RIN Docket No.FAA-2012-1218 Special Conditions No.25-483-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions. Effective date: March 21, 2013. 14 CFR Part 25 SummaryThese special conditions are issued for the Embraer S.A. Model EMB-550 airplane. This airplane will have a novel or unusual design feature(s) associated with an electronic flight control system with respect to lateral-directional and longitudinal stability and low energy awareness. 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.
78 FR 11562 - Special Conditions: Embraer S.A., Model EMB-550 Airplanes; Flight Envelope Protection: High Speed Limiting
typeregulations.gov FR Doc.2013-03676 RIN Docket No.FAA-2012-1215 Special Conditions No.25-12-482-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions. Effective date: March 21, 2013. 14 CFR Part 25 SummaryThese special conditions are issued for the Embraer S.A. Model EMB-550 airplane. This airplane will have a novel or unusual design feature, specifically an electronic flight control system which contains fly-by-wire control laws, including envelope protections, for the overspeed protection and roll limiting function. 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.
2013-02-15; vol. 78 # 32 - Friday, February 15, 201378 FR 11089 - Special Conditions: Bombardier Aerospace, Model BD-500-1A10 and BD-500-1A11 Airplanes; Sidestick Controllers
typeregulations.gov FR Doc.2013-03590 RIN Docket No.FAA-2012-1236 Special Conditions No.25-477-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions. Effective Date: March 18, 2013. 14 CFR Part 25 SummaryThese special conditions are issued for the Bombardier Aerospace Model BD-500-1A10 and BD-500-1A11 airplanes. These airplanes will have a novel or unusual design feature, specifically sidestick controllers designed to be operated with only one hand. 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.
2013-02-07; vol. 78 # 26 - Thursday, February 7, 201378 FR 8961 - Special Conditions: Embraer S.A., Model EMB-550 Airplane; Hydrophobic Coatings in Lieu of Windshield Wipers
typeregulations.gov FR Doc.2013-02740 RIN Docket No.FAA-2012-1200 Special Conditions No.25-475-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions. Effective Date: March 11, 2013. 14 CFR Part 25 SummaryThese special conditions are issued for the Embraer S.A., Model EMB-550 airplane. This airplane will have a novel or unusual design feature(s) associated with hydrophobic coatings. 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.
2013-01-30; vol. 78 # 20 - Wednesday, January 30, 201378 FR 6195 - Special Conditions: Embraer S.A., Model EMB-550 Airplanes; Flight Envelope Protection: Performance Credit for Automatic Takeoff Thrust Control System (ATTCS) During Go-Around
typeregulations.gov FR Doc.2013-01928 RIN Docket No.FAA-2012-1199 Special Conditions No.25-476-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions. Effective Date: March 1, 2013. 14 CFR Part 25 SummaryThese special conditions are issued for the Embraer S.A. Model EMB-550 airplane. This airplane will have a novel or unusual design feature associated with the use of an Automatic Takeoff Thrust Control System (ATTCS) during go-around. 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.
typeregulations.gov FR Doc.2013-01939 RIN Docket No.FAA-2012-0699 Special Conditions No.25-474-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions. Effective Date: January 24, 2013. 14 CFR Part 25 SummaryThese special conditions are issued for the Airbus Model A318-112 airplane, serial number (S/N) 3238. This airplane, as modified by Fokker Services B.V., will have a novel or unusual design feature associated with a cooktop installation. 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.
Title 14 published on 2013-01-01The following are ALL rules, proposed rules, and notices (chronologically) published in the Federal Register relating to 14 CFR 25 after this date.2013-05-29; vol. 78 # 103 - Wednesday, May 29, 201378 FR 32078 - Special Conditions: Gulfstream Model G280 Airplane, Enhanced Flight Vision System (EFVS) With Head-Up Display (HUD)
78 FR 31851 - Harmonization of Airworthiness Standards—Gust and Maneuver Load Requirements
typeregulations.gov FR Doc.2013-12445 RIN2120-AK12 Docket No.FAA-2013-0142 Notice No.25-139 DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Notice of proposed rulemaking (NPRM). Send comments on or before August 26, 2013. 14 CFR Part 25 SummaryThe FAA proposes to amend certain airworthiness regulations for transport category airplanes based on recommendations from the Aviation Rulemaking Advisory Committee (ARAC). Adopting this proposal would eliminate certain regulatory differences between the airworthiness standards of the FAA and European Aviation Safety Agency (EASA) without affecting current industry design practices. This action would revise the pitch maneuver design loads criteria; revise the gust and turbulence design loads criteria; revise the application of gust loads to engine mounts, high lift devices, and other control surfaces; add a “round-the-clock” discrete gust criterion and a multi-axis discrete gust criterion for airplanes equipped with wing-mounted engines; revise the engine torque loads criteria; add an engine failure dynamic load condition; revise the ground gust design loads criteria; revise the criteria used to establish the rough air design speed, and require the establishment of a rough air Mach number.
2013-05-06; vol. 78 # 87 - Monday, May 6, 201378 FR 26280 - Special Conditions: Embraer, S.A., Model EMB-550 Airplane; Side-Facing Seats; Installation of Airbag Systems in Shoulder Belts
typeregulations.gov FR Doc.2013-10581 RIN Docket No.FAA-2013-0384 Notice No.25-13-02-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Notice of proposed special conditions. Send your comments on or before June 20, 2013. 14 CFR Part 25 SummaryThis action proposes special conditions for the Embraer S.A. Model EMB-550 airplane. This airplane will have a novel or unusual design feature(s) associated with multiple place and single place side-facing seats and installation of airbag systems in the shoulder belts. 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.
2013-03-01; vol. 78 # 41 - Friday, March 1, 201378 FR 13835 - Harmonization of Airworthiness Standards—Miscellaneous Structures Requirements
typeregulations.gov FR Doc.2013-04812 RIN2120-AK13 Docket No.FAA-2013-0109 Notice No.25-137 DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Notice of proposed rulemaking (NPRM). Send comments on or before May 30, 2013. 14 CFR Part 25 SummaryThe FAA proposes to amend certain airworthiness regulations for transport category airplanes, based on recommendations from the Aviation Rulemaking Advisory Committee (ARAC). Adopting this proposal would eliminate regulatory differences between the airworthiness standards of the FAA and European Aviation Safety Agency (EASA). This proposal would not add new requirements beyond what manufacturers currently meet for EASA certification and would not affect current industry design practices. This proposal would revise the structural test requirements necessary when analysis has not been found reliable; clarify the quality control, inspection, and testing requirements for critical and non-critical castings; add control system requirements that consider structural deflection and vibration loads; expand the fuel tank structural and system requirements regarding emergency landing conditions and landing gear failure conditions; add a requirement that engine mount failure due to overload must not cause hazardous fuel spillage; and revise the inertial forces requirements for cargo compartments by removing the exclusion of compartments located below or forward of all occupants in the airplane.
typeregulations.gov FR Doc.2013-03679 RIN Docket No.FAA-2013-0148 Notice No.25-13-01-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Notice of proposed special conditions. Send your comments on or before April 5, 2013. 14 CFR Part 25 SummaryThis action proposes special conditions for the Embraer S.A. Model EMB-550 airplane. This airplane will have a novel or unusual design feature(s) associated with landing loads due to the automatic braking 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.
2013-01-24; vol. 78 # 16 - Thursday, January 24, 201378 FR 5146 - Special Conditions: Embraer S.A., Model EMB-550 Airplane, Dive Speed Definition With Speed Protection System