Source: http://www.law.cornell.edu/cfr/text/14/25?quicktabs_7=0
Timestamp: 2013-05-19 08:45:05
Document Index: 792969410

Matched Legal Cases: ['art 25', '§ 25', '§ 25', '§ 25', '§ 25', '§ 25', '§ 25', '§ 25', '§ 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', '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', '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 - AIRWORTHINESS STANDARDS: TRANSPORT CATEGORY AIRPLANES | Title 14 - Aeronautics and Space | Code of Federal Regulations | LII / Legal Information Institute
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14 CFR 25 - AIRWORTHINESS STANDARDS: TRANSPORT CATEGORY AIRPLANES
There are 21 Updates appearing in the Federal Register for 14 CFR 25. Select the tab below to view, or View eCFR (GPOAccess)
SUBPART A — General (§§ 25.1 - 25.5)
SUBPART B — Flight (§§ 25.21 - 25.255)
SUBPART C — Structure (§§ 25.301 - 25.581)
SUBPART D — Design and Construction (§§ 25.601 - 25.899)
SUBPART E — Powerplant (§§ 25.901 - 25.1207)
SUBPART F — Equipment (§§ 25.1301 - 25.1461)
SUBPART G — Operating Limitations and Information (§§ 25.1501 - 25.1587)
SUBPART H — Electrical Wiring Interconnection Systems (EWIS) (§§ 25.1701 - 25.1733)
SUBPART I — Special Federal Aviation Regulations (§§ 25.1801 - 25.1801)
Appendix B to Part 25
Appendix C to Part 25
Appendix D to Part 25
Appendix E to Part 25
Appendix G to Part 25 - Continuous Gust Design Criteria
Appendix H to Part 25 - Instructions for Continued Airworthiness
Appendix I to Part 25 - Installation of an Automatic Takeoff Thrust Control System (ATTCS)
Appendix J to Part 25 - Emergency Evacuation
Appendix L to Part 25 - HIRF Environments and Equipment HIRF Test Levels
Appendix M to Part 25 - Fuel Tank System Flammability Reduction Means
Appendix N TO Part 25 - Fuel Tank Flammability Exposure and Reliability Analysis
Source: Docket No. 5066, 29 FR 18291, Dec. 24, 1964, unless otherwise noted.
Title 14 published on 2012-01-01The 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.2012-11-13; vol. 77 # 219 - Tuesday, November 13, 201277 FR 67557 - Special Conditions: ATR-GIE Avions de Transport Regional, Models ATR42-500 and ATR72-212A Airplanes; Aircraft Electronic System Security Protection From Unauthorized External Access
typeregulations.gov FR Doc.2012-27517 RIN Docket No.FAA-2012-0959 Special Conditions No.25-473-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. The effective date of these special conditions is November 5, 2012. We must receive your comments by December 13, 2012. 14 CFR Part 25 SummaryThese special conditions are issued for the ATR-GIE Avions de Transport Regional Models ATR42-500 and ATR72-212A airplanes. These airplanes will have novel or unusual design features associated with the architecture and connectivity capabilities of the airplanes&apos; computer systems and networks, which may allow access to or by external computer systems and networks. Connectivity to, or access by, external systems and networks may result in security vulnerabilities to the airplanes&apos; systems. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for these design features. 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.
2012-11-09; vol. 77 # 218 - Friday, November 9, 201277 FR 67251 - Special Conditions: Boeing Model 757 Series Airplanes; Seats with Non-Traditional, Large, Non-Metallic Panels
typeregulations.gov FR Doc.2012-27370 RIN Docket No.FAA-2012-1194 Special Conditions No.25-472-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special condition; request for comments. The effective date of these special conditions is November 5, 2012. We must receive your comments by December 24, 2012. 14 CFR Part 25 SummaryThese special conditions are issued for the Boeing Model 757 series airplanes. These airplanes as modified by Flight Structures, Inc. will have novel or unusual design features associated with seats that include non-traditional, large, non-metallic panels that would affect survivability during a post-crash fire event. 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.
2012-10-18; vol. 77 # 202 - Thursday, October 18, 201277 FR 64023 - Special Conditions: Airbus Model A318, A319, A320, and A321 Series Airplanes; Design Roll Maneuver Conditions
typeregulations.gov FR Doc.2012-25606 RIN Docket No.FAA-2012-1120 Special Conditions No.25-471-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. The effective date of these special conditions is October 11, 2012. We must receive your comments by December 3, 2012. 14 CFR Part 25 SummaryThese special conditions are issued for the Airbus Model A318, A319, and A320 series airplanes with modification 160500 and Model A321 series airplanes with modification 160023 (Sharklet). These airplanes will have novel or unusual design features when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. These design features include electronic flight controls that affect maneuvering. 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.
77 FR 64025 - Special Conditions: Airbus Model A318, A319, A320, and A321 Series Airplanes; Interaction of Systems and Structures
typeregulations.gov FR Doc.2012-25604 RIN Docket No.FAA-2012-1118 Special Conditions No.25-469-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. The effective date of these special conditions is October 11, 2012. We must receive your comments by December 3, 2012. 14 CFR Part 25 SummaryThese special conditions are issued for the Airbus Model A318, A319, and A320 series airplanes with modification 160500 and Model A321 series airplanes with modification 160023 (Sharklet). These airplanes will have novel or unusual design features when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. The design features are associated with the systems that affect the structural performance of the airplane. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for these design features. 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.2012-25605 RIN Docket No.FAA-2012-1119 Special Conditions No.25-470-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. The effective date of these special conditions is October 11, 2012. We must receive your comments by December 3, 2012. 14 CFR Part 25 SummaryThese special conditions are issued for the Airbus Model A318, A319, and A320 series airplanes with modification 160500 and Model A321 series airplanes with modification 160023 (Sharklet). These airplanes will have novel or unusual design features 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.
2012-09-18; vol. 77 # 181 - Tuesday, September 18, 201277 FR 57481 - Special Conditions: Embraer S.A., Models EMB-135 and EMB-145 Series; Airplane Seats with Non-Traditional, Large, Non-Metallic Panels
typeregulations.gov FR Doc.2012-22831 RIN Docket No.FAA-2012-0984 Special Conditions No.25-468-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. The effective date of these special conditions is September 11, 2012. We must receive your comments by November 2, 2012. 14 CFR Part 25 SummaryThese special conditions are issued for the Embraer S.A. Models EMB-135 and EMB-145 series airplanes. These airplanes will have a novel or unusual design feature associated with the airplane seats that have non-traditional, large, non-metallic panels that would affect survivability during a post-crash fire event. 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.
2012-09-13; vol. 77 # 178 - Thursday, September 13, 201277 FR 56525 - Special Conditions: Bombardier, Model CL-600-2B16 Airplane (CL-601-3A, CL-601-3R, and CL-604 Variants); Enhanced Flight Vision System
typeregulations.gov FR Doc.2012-22468 RIN Docket No.FAA-2012-0968 Special Conditions No.25-467-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. The effective date of these special conditions is September 6, 2012. We must receive your comments by October 29, 2012. 14 CFR Part 25 SummaryThese special conditions are issued for the Bombardier Model CL-600-2B16 airplanes, including variants CL-601-3A, CL-601-3R and CL-604. This airplane, as modified by Atlantic Aero, Inc., will have a novel or unusual design feature associated with an advanced, enhanced flight vision system (EFVS). The EFVS 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.
2012-07-09; vol. 77 # 131 - Monday, July 9, 201277 FR 40255 - Special Conditions: Boeing, Model 737-800; Large Non-Structural Glass in the Passenger Compartment
typeregulations.gov FR Doc.2012-16720 RIN Docket No.FAA-2012-0499 Special Conditions No.25-466-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions. Effective Date: June 25, 2012. 14 CFR Part 25 SummaryThese special conditions are issued for the Boeing Model 737-800 airplane. This airplane as modified by Lufthansa Technik will have a novel or unusual design feature associated with the installation of large non-structural glass items in the cabin area of an executive interior occupied by passengers and crew. The installation of these items in a passenger compartment, which can be occupied during taxi, takeoff, and landing, is a novel or unusual design feature with respect to the material used. 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.
2012-06-28; vol. 77 # 125 - Thursday, June 28, 201277 FR 38467 - Special Conditions: Gulfstream Aerospace LP (GALP), Model Gulfstream G280 Airplane; Isolation or Aircraft Electronic System Security Protection From Unauthorized Internal Access
typeregulations.gov FR Doc.2012-15913 RIN Docket No.FAA-2012-0624 Special Conditions No.25-464-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. The effective date of these special conditions is June 7, 2012. We must receive your comments by August 13, 2012. 14 CFR Part 25 SummaryThese special conditions are issued for the Gulfstream Aerospace LP, Model Gulfstream G280 airplane. This airplane will have novel or unusual design features associated with connectivity of the passenger service computer systems to the airplane critical systems and data networks. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for these design features. 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.
2012-06-18; vol. 77 # 117 - Monday, June 18, 201277 FR 36123 - Special Conditions: Gulfstream Aerospace LP (GALP), Model Gulfstream G280 Airplane; Aircraft Electronic System Security Protection From Unauthorized External Access
typeregulations.gov FR Doc.2012-14787 RIN Docket No.FAA-2012-0625 Special Conditions No.25-465-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. The effective date of these special conditions is June 7, 2012. We must receive your comments by August 2, 2012. 14 CFR Part 25 SummaryThese special conditions are issued for the Gulfstream Aerospace LP, Model Gulfstream G280 airplane. This airplane will have novel or unusual design features associated with the architecture and connectivity capabilities of the airplane&apos;s computer systems and networks, which may allow access to or by external computer systems and networks. Connectivity to, or access by, external systems and networks may result in security vulnerabilities to the airplane&apos;s systems. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for these design features. 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.
2012-05-31; vol. 77 # 105 - Thursday, May 31, 201277 FR 32006 - Special Conditions: Gulfstream Model GVI Airplane; High Incidence Protection
typeregulations.gov FR Doc.2012-13213 RIN Docket No.NM438 Special Conditions No. 25-423-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; correction. Effective May 31, 2012. 14 CFR Part 25 SummaryThis document corrects an error that appeared in Docket No. NM438, Special Conditions No. 25-423-SC, which were published in the Federal Register on March 28, 2011. The error resulted in the omission of two paragraphs of text in The Special Conditions section.
2012-04-12; vol. 77 # 71 - Thursday, April 12, 201277 FR 21861 - Special Conditions: Boeing, Model 777F; Enhanced Flight Vision System
typeregulations.gov FR Doc.2012-8739 RIN Docket No.FAA-2012-0352 Special Conditions No.25-462-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. The effective date of these special conditions is March 22, 2012. We must receive your comments by May 14, 2012. 14 CFR Part 25 SummaryThese special conditions are issued for the Boeing Model 777F airplane. This airplane, as modified by the FedEx Express Corporation, will have a novel or unusual design feature associated with an advanced, enhanced flight vision system (EFVS). The EFVS 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.
2012-03-27; vol. 77 # 59 - Tuesday, March 27, 201277 FR 18099 - Special Conditions: Dassault Aviation, Model Falcon 7X Airplanes; Seats With Inflatable Shoulder Straps
typeregulations.gov FR Doc.2012-7280 RIN Docket No.FAA-2012-0344 Special Conditions No.25-461-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. The effective date of these special conditions is March 19, 2012. We must receive your comments by May 11, 2012. 14 CFR Part 25 SummaryThese special conditions are issued for the Dassault Aviation Model Falcon 7X airplane. This airplane will have a novel or unusual design feature associated with seats with inflatable shoulder straps. 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.
2012-03-26; vol. 77 # 58 - Monday, March 26, 201277 FR 17325 - Special Conditions: Airbus, A350-900 Series Airplane; Passenger Seats With Non-Traditional, Large, Non-Metallic Panels
typeregulations.gov FR Doc.2012-7235 RIN Docket No.FAA-2012-0325 Notice No.25-459-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions, request for comments. The effective date of these special conditions is March 14, 2012. We must receive your comments by May 10, 2012. 14 CFR Part 25 SummaryThese special conditions are issued for the Airbus A350-900 series airplane. These airplanes will have a novel or unusual design feature(s) associated with seats that include non-traditional, large, non-metallic panels that would affect survivability during a post-crash fire event. 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.
2012-03-23; vol. 77 # 57 - Friday, March 23, 201277 FR 16910 - Special Conditions: Boeing Model 787 Series Airplanes; Single-place Side-facing Seats With Inflatable Lapbelts
typeregulations.gov FR Doc.2012-6957 RIN Docket No.FAA-2012-0311 Special Conditions No.25-458-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. The effective date of these special conditions is March 12, 2012. We must receive your comments by April 23, 2012. 14 CFR Part 25 SummaryThese special conditions are issued for the Boeing Model 787 series airplanes. These airplanes have a novel or unusual design feature associated with single-place side-facing seats with inflatable lapbelts. 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.
2012-02-10; vol. 77 # 28 - Friday, February 10, 201277 FR 6945 - Special Conditions: Learjet Inc., Learjet Model LJ-200-1A10; Interaction of Systems and Structures
typeregulations.gov FR Doc.2012-3077 RIN Docket No.FAA-2012-0154 Special Conditions No.25-457-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. The effective date of these special conditions is February 3, 2012. We must receive your comments by March 26, 2012. 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 systems that, directly or as a result of failure or malfunction, affect structural performance. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for these design features. 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.
2012-02-07; vol. 77 # 25 - Tuesday, February 7, 201277 FR 5990 - Special Conditions: Learjet Inc., Model LJ-200-1A10 Airplane, Pilot-Compartment View Through Hydrophobic Windshield Coatings in Lieu of Windshield Wipers
typeregulations.gov FR Doc.2012-2672 RIN Docket No.FAA-2011-1108 Special Conditions No.25-456-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions. Effective Date: March 8, 2012. 14 CFR Part 25 SummaryThese special conditions are issued for the Learjet Model LJ-200-1A10 airplane. This airplane will have a novel or unusual design feature associated with hydrophobic windshield coatings in lieu of windshield wipers. 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.
2012-01-18; vol. 77 # 11 - Wednesday, January 18, 201277 FR 2437 - Special Conditions: Gulfstream Aerospace Corporation, Model GVI Airplane; Rechargeable Lithium Batteries and Rechargeable Lithium-Battery Systems
typeregulations.gov FR Doc.2012-798 RIN Docket No.FAA-2012-0015 Special Conditions No.25-455-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. The effective date of these special conditions is January 9, 2012. We must receive your comments by March 5, 2012. 14 CFR Part 25 SummaryThese special conditions are issued for the Gulfstream Aerospace Corporation (GAC) Model GVI airplane. This airplane will have a novel or unusual design feature associated with the installation of rechargeable lithium batteries and rechargeable lithium-battery systems. 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.
2012-01-11; vol. 77 # 7 - Wednesday, January 11, 201277 FR 1614 - Harmonization of Airworthiness Standards for Transport Category Airplanes—Landing Gear Retracting Mechanisms and Pilot Compartment View
typeregulations.gov FR Doc.2012-360 RIN2120-AJ80 Docket No.FAA-2010-1193 Amdt. No.25-136 DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final rule. Effective March 12, 2012. 14 CFR Part 25 SummaryThe Federal Aviation Administration amends the airworthiness standards for transport category airplanes on landing gear retracting mechanisms and the pilot compartment view. For the landing gear retracting mechanism, this rulemaking adopts the 1-g stall speed as a reference stall speed instead of the minimum speed obtained in a stalling maneuver and adds an additional requirement to keep the landing gear and doors in the correct retracted position in flight. For the pilot compartment view, this rulemaking revises the requirements for pilot compartment view in precipitation conditions. This action eliminates regulatory differences between the airworthiness standards of the U.S. and the European Aviation Safety Agency (EASA), without affecting current industry design practices.
77 FR 1618 - Special Conditions: The Boeing Company, Model 767-300; Seats With Inflatable Lapbelts
typeregulations.gov FR Doc.2012-350 RIN Docket No.FAA-2012-0009 Special Conditions No.25-454-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. The effective date of these special conditions is January 5, 2012. We must receive your comments by February 27, 2012. 14 CFR Part 25 SummaryThese special conditions are issued for the Boeing Model 767-300 series airplanes. These airplanes will have a novel or unusual design feature associated with seats with inflatable lapbelts. 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 2012-01-01The following are ALL rules, proposed rules, and notices (chronologically) published in the Federal Register relating to 14 CFR 25 after this date.2013-01-24; 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
typeregulations.gov FR Doc.2013-01457 RIN Docket No.FAA-2012-1301 Notice No.25-12-18-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Notice of proposed special conditions. Send your comments on or before March 11, 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 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 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.
78 FR 5148 - Special Conditions: Embraer S.A., Model EMB-550 Airplanes; Flight Envelope Protection: General Limiting Requirements
typeregulations.gov FR Doc.2013-01379 RIN Docket No.FAA-2012-1332 Notice No.25-12-19-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Notice of proposed special conditions. Send your comments on or before March 11, 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), 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 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.
2013-01-09; vol. 78 # 6 - Wednesday, January 9, 201378 FR 1765 - Requirements for Chemical Oxygen Generators Installed on Transport Category Airplanes
typeregulations.gov FR Doc.2013-00238 RIN2120-AK14 Docket No.FAA-2012-0812 Notice No.13-01 DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Notice of proposed rulemaking (NPRM). Send comments on or before March 11, 2013. 14 CFR Part 25 SummaryThis rulemaking would amend the type certification requirements for chemical oxygen generators installed on transport category airplanes so the generators are secure and not subject to misuse. The intended effect of this action would be to increase the level of security for future transport category airplane designs. This proposal does not directly affect the existing fleet.
2012-12-19; vol. 77 # 244 - Wednesday, December 19, 201277 FR 75066 - Special Conditions: Airbus, A350-900 Series Airplane; Flight Envelope Protection (Icing and Non-Icing Conditions); High Incidence Protection and Alpha-Floor Systems
typeregulations.gov FR Doc.2012-30441 RIN Docket No.FAA-2012-1207 Notice No.25-12-09-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Notice of proposed special conditions. Send your comments on or before February 4, 2013. 14 CFR Part 25 SummaryThis action proposes special conditions for Airbus A350-900 series airplanes. These airplanes will have novel or unusual design features associated with flight envelope protection in icing and non-icing conditions that use low speed incidence protection and an alpha-floor function that automatically advances throttles whenever the airplane angle of attack reaches a predetermined value. 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.
77 FR 75071 - Special Conditions: Embraer S.A., Model EMB-550 Airplanes; Electrical/Electronic Equipment Bay Fire Detection and Smoke Penetration
typeregulations.gov FR Doc.2012-30493 RIN Docket No.FAA-2012-1292 Notice No.25-12-17-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Notice of proposed special conditions. Send your comments on or before February 4, 2013. 14 CFR Part 25 SummaryThis action proposes special conditions 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 flightcrew 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 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.
2012-11-28; vol. 77 # 229 - Wednesday, November 28, 201277 FR 70941 - Special Conditions: Embraer S.A., Model EMB-550 Airplane; Interaction of Systems and Structures
typeregulations.gov FR Doc.2012-28768 RIN Docket No.FAA-2012-1246 Notice No.25-12-16-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Notice of proposed special conditions. Send your comments on or before January 14, 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 the interaction of systems and structures. 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.
2012-11-26; vol. 77 # 227 - Monday, November 26, 201277 FR 70384 - Special Conditions: Embraer S.A., Model EMB-550 Airplane; Design Roll Maneuver for Electronic Flight Controls
typeregulations.gov FR Doc.2012-28386 RIN Docket No.FAA-2012-1241 Notice No.25-12-15-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Notice of proposed special conditions. Send your comments on or before January 10, 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 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 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.
2012-11-20; vol. 77 # 224 - Tuesday, November 20, 201277 FR 69568 - Special Conditions: Bombardier Aerospace, Model BD-500-1A10 and BD-500-1A11 Airplanes; Sidestick Controllers
typeregulations.gov FR Doc.2012-28131 RIN Docket No.FAA-2012-1236 Notice No.25-12-14-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Notice of proposed special conditions. Send your comments on or before January 4, 2013. 14 CFR Part 25 SummaryThis action proposes special conditions 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 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.
77 FR 69569 - Special Conditions: Embraer S.A., Model EMB-550 Airplanes; Flight Envelope Protection: Pitch and Roll Limiting Functions
typeregulations.gov FR Doc.2012-28133 RIN Docket No.FAA-2012-1211 Notice No.25-12-10-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Notice of proposed special conditions. Send your comments on or before January 4, 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 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 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.
77 FR 69571 - Special Conditions: Embraer S.A., Model EMB-550 Airplane, Limit Pilot Forces for Sidestick Control
typeregulations.gov FR Doc.2012-28113 RIN Docket No.FAA-2012-1216 Notice No.25-12-13-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Notice of proposed special conditions. Send your comments on or before January 4, 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, 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 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.
77 FR 69572 - Special Conditions: Embraer S.A., Model EMB-550 Airplanes; Flight Envelope Protection: High Speed Limiting
typeregulations.gov FR Doc.2012-28132 RIN Docket No.FAA-2012-1215 Notice No.25-12-12-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Notice of proposed special conditions. Send your comments on or before January 4, 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, 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 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.
77 FR 69573 - 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.2012-28115 RIN Docket No.FAA-2012-1218 Notice No.25-12-11-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Notice of proposed special conditions. Send your comments on or before January 4, 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 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 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.
2012-11-13; vol. 77 # 219 - Tuesday, November 13, 201277 FR 67557 - Special Conditions: ATR-GIE Avions de Transport Regional, Models ATR42-500 and ATR72-212A Airplanes; Aircraft Electronic System Security Protection From Unauthorized External Access
77 FR 67308 - Special Conditions: Embraer S.A., Model EMB-550 Airplane; Hydrophobic Coatings in Lieu of Windshield Wipers
typeregulations.gov FR Doc.2012-27373 RIN Docket No.FAA-2012-1200 Notice No.25-12-07-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Notice of proposed special conditions. Send your comments on or before December 24, 2012. 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 hydrophobic coatings. 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.
77 FR 67309 - 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.2012-27372 RIN Docket No.FAA-2012-1199 Notice No.25-12-06-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Notice of proposed special conditions. Send your comments on or before December 24, 2012. 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 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 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.
2012-09-25; vol. 77 # 186 - Tuesday, September 25, 201277 FR 58970 - Special Conditions: Embraer S.A. Model EMB-550 Airplanes, Sudden Engine Stoppage
typeregulations.gov FR Doc.2012-23536 RIN Docket No.FAA-2012-0260 Notice No.25-12-05-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Notice of proposed special conditions. Submit your comments on or before October 26, 2012. 14 CFR Part 25 SummaryThis action proposes special conditions for the Embraer Model EMB-550 airplane. This airplane will have a novel or unusual design feature associated with the effects of sudden engine stoppage upon the airframe. 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.
2012-09-17; vol. 77 # 180 - Monday, September 17, 201277 FR 57039 - Special Conditions: Embraer S.A., Model EMB-550 Airplane; Electronic Flight Control System: Control Surface Awareness and Mode Annunciation
typeregulations.gov FR Doc.2012-22777 RIN Docket No.FAA-2012-0978 Notice No.25-12-03-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Notice of proposed special conditions. Send your comments on or before November 1, 2012. 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 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 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.
2012-08-28; vol. 77 # 167 - Tuesday, August 28, 201277 FR 51944 - Special Conditions: Airbus, Model A318-112 Airplane (S/N 3238); Certification of Cooktops
typeregulations.gov FR Doc.2012-21100 RIN Docket No.FAA-2012-0699 Notice No.25-12-02-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Notice of proposed special conditions. Send your comments on or before October 12, 2012. 14 CFR Part 25 SummaryThis action proposes special conditions for the Airbus Model A318-112 airplane. 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 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.
2012-07-17; vol. 77 # 137 - Tuesday, July 17, 201277 FR 41930 - Bleed Air Cleaning and Monitoring Equipment and Technology
typeregulations.gov FR Doc.2012-17368 RIN Docket No.FAA-2012-0714 DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Notice; request for information. Written comments must be received on or before September 17, 2012. 14 CFR Part 25 SummaryThe FAA seeks information from industry developers, manufacturers, and the public related to effective air cleaning technology and sensor technology for the engine and auxiliary power unit bleed air supplied to the passenger cabin and flight deck of a pressurized aircraft. The information obtained will inform the agency of potential research and development plans.
2012-05-15; vol. 77 # 94 - Tuesday, May 15, 201277 FR 28533 - Special Conditions: Boeing, Model 737-800; Large Non-Structural Glass in the Passenger Compartment
typeregulations.gov FR Doc.2012-11697 RIN Docket No.FAA-2012-0499 Notice No.25-12-01-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Notice of proposed special conditions. Send your comments on or before June 4, 2012. 14 CFR Part 25 SummaryThis action proposes special conditions for the Boeing Model 737-800 airplane. This airplane as modified by Lufthansa Technik will have a novel or unusual design feature associated with the installation of large non-structural glass items in the cabin area of an executive interior occupied by passengers and crew. The installation of these items in a passenger compartment, which can be occupied during taxi, takeoff, and landing, is a novel or unusual design feature with respect to the material used. 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.
2012-03-30; vol. 77 # 62 - Friday, March 30, 201277 FR 19148 - Special Conditions: Airbus, A350-900 Series Airplane; Crew Rest Compartments
typeregulations.gov FR Doc.2012-7732 RIN Docket No.FAA-2012-0343 Notice No.25-460-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Notice of proposed special conditions. We must receive your comments by May 14, 2012. 14 CFR Part 25 SummaryThis action proposes special conditions for Airbus A350-900 series airplanes. These airplanes will have novel or unusual design features associated with two separate Crew Rest Compartments: a Flight Crew Rest Compartment (FCRC) intended to be occupied by flight crew members only, and a Cabin Crew Rest Compartment (CCRC) intended to be occupied by cabin crew members. Both types of Crew Rest Compartments (CRC) are installed in the overhead area with access from the main deck. 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.
Appendix A to Part 25Appendix B to Part 25Appendix C to Part 25Appendix D to Part 25Appendix E to Part 25Appendix F to Part 25Appendix G to Part 25 - Continuous Gust Design CriteriaAppendix H to Part 25 - Instructions for Continued AirworthinessAppendix I to Part 25 - Installation of an Automatic Takeoff Thrust Control System (ATTCS)Appendix J to Part 25 - Emergency EvacuationAppendix K to Part 25 - Extended Operations (ETOPS)Appendix L to Part 25 - HIRF Environments and Equipment HIRF Test LevelsAppendix M to Part 25 - Fuel Tank System Flammability Reduction MeansAppendix N TO Part 25 - Fuel Tank Flammability Exposure and Reliability Analysis CFR Toolbox