Source: https://www.law.cornell.edu/cfr/text/14/25.779
Timestamp: 2017-02-20 15:48:24
Document Index: 561010669

Matched Legal Cases: ['art 25', 'art 25', '§ 25', '§ 2473', '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', 'arts 25', 'art 25', 'art 25', 'art 25', 'art 25', '§\u200925', '§\u2009121', 'arts 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 25.779 - Motion and effect of cockpit controls. | US Law | LII / Legal Information Institute
CFR › Title 14 › Chapter I › Subchapter C › Part 25 › Subpart D › Section 25.779 14 CFR 25.779 - Motion and effect of cockpit controls.
There are 48 Updates appearing in the Federal Register for 14 CFR Part 25. View below or at eCFR (GPOAccess)
§ 25.779 Motion and effect of cockpit controls.
Cockpit controls must be designed so that they operate in accordance with the following movement and actuation: (a) Aerodynamic controls: (1)Primary.
Motion and effect
Right (clockwise) for right wing down.
Rearward for nose up.
Right pedal forward for nose right.
(2)Secondary.
Flaps (or auxiliary lift devices)
Forward for flaps up; rearward for flaps down.
Trim tabs (or equivalent)
Rotate to produce similar rotation of the airplane about an axis parallel to the axis of the control.
(b) Powerplant and auxiliary controls: (1)Powerplant.
Forward to increase forward thrust and rearward to increase rearward thrust.
Forward to increase rpm.
Forward or upward for rich.
Forward or upward for cold.
Forward or upward for low blower. For turbosuperchargers, forward, upward, or clockwise, to increase pressure.
(2)Auxiliary.
Down to extend.
[Doc. No. 5066, 29 FR 18291, Dec. 24, 1964, as amended by Amdt. 25-72, 55 FR 29778, July 20, 1990]
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 CodeU.S. Code: Title 42 - THE PUBLIC HEALTH AND WELFARE§ 2473
Title 14 published on 2015-11-17The following are ALL rules, proposed rules, and notices (chronologically) published in the Federal Register relating to 14 CFR Part 25 after this date.2017-02-08; vol. 82 # 25 - Wednesday, February 8, 201782 FR 9677 - Revisions to Operational Requirements for the Use of Enhanced Flight Vision Systems (EFVS) and to Pilot Compartment View Requirements for Vision Systems
2016-12-07; vol. 81 # 235 - Wednesday, December 7, 201681 FR 88098 - Special Conditions: Embraer S.A., Model ERJ 190-300 Series Airplanes; Landing Pitchover Condition
typeregulations.gov FR Doc.2016-29358 RIN Docket No.FAA-2016-9461 Special Conditions No.25-642-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. This action is effective on Embraer S.A. on December 7, 2016. We must receive your comments by January 23, 2017. 14 CFR Part 25 SummaryThese special conditions are issued for the Embraer S.A. Model ERJ 190-300 series airplanes. These airplanes will have a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. This design feature is an automatic braking system with a pilot-selectable function that allows earlier braking at landing without pilot pedal input. 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.
2016-12-02; vol. 81 # 232 - Friday, December 2, 201681 FR 86910 - Special Conditions: Gulfstream Aerospace Corporation Model GVII-G500 Airplanes; Electronic Flight-Control-System Mode Annunciation
typeregulations.gov FR Doc.2016-28725 RIN Docket No.FAA-2015-1495 Special Conditions No.25-641-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. This action is effective on Gulfstream on December 2, 2016. We must receive your comments by January 17, 2017. 14 CFR Part 25 SummaryThese special conditions are issued for the Gulfstream Aerospace Corporation (Gulfstream) Model GVII-G500 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. This design feature is electronic flight-control-system (EFCS) mode annunciation. 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.
2016-10-26; vol. 81 # 207 - Wednesday, October 26, 201681 FR 74347 - Special Conditions: Bombardier Inc. Models BD-700-2A12 and BD-700-2A13 Airplanes; Fuselage Post-Crash Fire Survivability
typeregulations.gov FR Doc.2016-25808 RIN Docket No.FAA-2015-2393 Notice No.25-16-07-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Notice of proposed special conditions. Send your comments on or before December 12, 2016. 14 CFR Part 25 SummaryThis action proposes special conditions for the Bombardier Inc. (Bombardier) Model BD-700-2A12 and BD-700-2A13 airplanes. 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 features are associated with an aluminum-lithium fuselage construction that may provide different levels of protection from post-crash fire threats than similar aircraft constructed from traditional aluminum structure. 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.
typeregulations.gov FR Doc.2016-25809 RIN Docket No.FAA-2016-4158 Notice No.25-16-06-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Notice of proposed special conditions. Send your comments on or before December 12, 2016. 14 CFR Part 25 SummaryThis action proposes special conditions for the Bombardier Inc. (Bombardier) Model BD-700-2A12 and BD-700-2A13 airplanes. These airplanes will have a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for transport-category airplanes. This design feature is a fuselage fabricated using aluminum-lithium materials instead of conventional aluminum. The applicable airworthiness regulations do not contain adequate or appropriate fire-safety standards for this design feature. These proposed special conditions contain the additional fire-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.2016-25810 RIN Docket No.FAA-2016-8247 Notice No.25-16-08-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Notice of proposed special conditions. Send your comments on or before December 12, 2016. 14 CFR Part 25 SummaryThis action proposes special conditions for the Boeing Model 777-200 airplane. This airplane, as modified by Aerocon Engineering Company (Aerocon), will have a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for transport-category airplanes. This design feature is an access hatch, installed between the cabin and the Class C cargo compartment, to allow in-flight access to the Class C cargo compartment. 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.
2016-10-17; vol. 81 # 200 - Monday, October 17, 201681 FR 71356 - Special Conditions: Learjet Model 45 Series Airplanes; Aircraft Electronic System Security Protection From Unauthorized External Access
typeregulations.gov FR Doc.2016-25063 RIN Docket No.FAA-2013-0920 Special Conditions No.25-501-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments; correction. This correction is effective on October 17, 2016. 14 CFR Part 25 SummaryThe FAA is correcting a final special conditions; request for comments document published in the Federal Register on October 31, 2013 (78 FR 65153). In that document the special conditions number was incorrect and this document now posts the correct special conditions number. Also, a typographical error occurred in the wording of one of the headings paragraphs of the document. This document now posts the correct headings wording.
typeregulations.gov FR Doc.2016-25060 RIN Docket No.FAA-2016-9282 Special Conditions No.25-640-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. This action is effective on Embraer S.A. on October 17, 2016. We must receive your comments by December 1, 2016. 14 CFR Part 25 SummaryThese special conditions are issued for the Embraer S.A. Model ERJ 190-300 series airplanes. 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 are electrical/electronic equipment bays distributed throughout the airplane, with three of them in the pressurized area. The time it takes to determine the source of smoke in an airplane with three or more equipment bays could allow fire to spread, generating a significant quantity of smoke and damage. 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.2016-25062 RIN Docket No.FAA-2013-0919, Special Conditions No. 25-502-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments; correction. This correction is effective on October 17, 2016. 14 CFR Part 25 SummaryThe FAA is correcting a final special conditions; request for comments document published in the Federal Register on October 31, 2013 (78 FR 65155). In that document the special conditions number was incorrect and this document now posts the correct special conditions number. Also, a typographical error occurred in the wording of one of the headings paragraphs of the document. This document now posts the correct headings wording.
2016-09-30; vol. 81 # 190 - Friday, September 30, 201681 FR 67097 - Special Conditions: Embraer S.A., Model ERJ 190-300 Series Airplanes; Electronic Flight Control System: Control Surface Position Awareness, Multiple Modes of Operation
typeregulations.gov FR Doc.2016-23665 RIN Docket No.FAA-2016-9225 Special Conditions No.25-639-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. This action is effective on Embraer S.A. on September 30, 2016. We must receive your comments by November 14, 2016. 14 CFR Part 25 SummaryThese special conditions are issued for the Embraer S.A. Model ERJ 190-300 series airplanes. These airplanes will have a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. This design feature is a fly-by-wire electronic flight control system (EFCS) and no direct coupling from the flight deck controller to the control surface. As a result, the pilot is not aware of the actual control surface position. 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.
2016-09-20; vol. 81 # 182 - Tuesday, September 20, 201681 FR 64360 - Special Conditions: The Boeing Company Model 787-10 Airplane; Aeroelastic Stability Requirements, Flaps-Up Vertical Modal-Suppression System
typeregulations.gov FR Doc.2016-22547 RIN Docket No.FAA-2016-6137 Notice No.25-16-05-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Notice of proposed special conditions. Send your comments on or before November 4, 2016. 14 CFR Part 25 SummaryThis action proposes special conditions for the Boeing Company (Boeing) Model 787-10 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. This design feature is a flaps-up vertical modal-suppression 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.
2016-09-14; vol. 81 # 178 - Wednesday, September 14, 201681 FR 63051 - Special Conditions: Lufthansa Technik, AG, Boeing Model 737-700 Airplanes; Large, Non-Structural Glass in the Passenger Compartment
typeregulations.gov FR Doc.2016-22048 RIN Docket No.FAA-2016-8832 Special Conditions No.25-638-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. This action is effective on Lufthansa on September 14, 2016. We must receive your comments by October 31, 2016. 14 CFR Part 25 SummaryThese special conditions are issued for Boeing Model 737-700 airplanes. This airplane, as modified by Lufthansa Technik, AG (Lufthansa), will have a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for transport-category airplanes. This design feature is large, non-structural glass panels in the passenger compartment of Very Important Person (VIP) interiors of Model 737-700 airplanes modified by Lufthansa. 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.
2016-09-01; vol. 81 # 170 - Thursday, September 1, 201681 FR 60236 - Special Conditions: Bombardier Inc., Model BD-700-2A12 and BD-700-2A13 Airplanes; Interactions of Systems and Structures
typeregulations.gov FR Doc.2016-21122 RIN Docket No.FAA-2016-4138 Special Conditions No.25-635-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. This action is effective on Bombardier on September 1, 2016. We must receive your comments by October 17, 2016. 14 CFR Part 25 SummaryThese special conditions are issued for the Bombardier Inc. (Bombardier) Model BD-700-2A12 and BD-700-2A13 airplanes. These airplanes will have novel or unusual features when compared to the state of technology envisioned in the airworthiness standards for transport-category airplanes. These design features include 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.
81 FR 60240 - Special Conditions: Bombardier Aerospace Inc. Model BD-700-2A12 and BD-700-2A13 Airplanes; Sidestick Controllers
typeregulations.gov FR Doc.2016-21123 RIN Docket No.FAA-2016-4135 Special Conditions No.25-636-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. This action is effective on Bombardier on September 1, 2016. We must receive your comments by October 17, 2016. 14 CFR Part 25 SummaryThese special conditions are issued for the Bombardier Aerospace Inc. (Bombardier) Model BD-700-2A12 and BD-700-2A13 airplanes. These airplanes will have a novel or unusual feature when compared to the state of technology envisioned in the airworthiness standards for transport-category airplanes. This design feature is a sidestick controller, designed to be operated with only one hand, in lieu of the conventional wheel or stick controls. 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.
81 FR 60241 - Special Conditions: Bombardier Inc. Model BD-700-2A12 and BD-700-2A13 Airplanes; Hydrophobic Coatings in Lieu of Windshield Wipers
typeregulations.gov FR Doc.2016-21079 RIN Docket No.FAA-2015-6363 Special Conditions No.25-637-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. This action is effective on Bombardier on September 1, 2016. We must receive your comments by October 17, 2016. 14 CFR Part 25 SummaryThese special conditions are issued for the Bombardier Inc. (Bombardier) Model BD-700-2A12 and BD-700-2A13 airplanes. These airplanes will have a novel or unusual feature when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. This design feature is hydrophobic coatings in lieu of windshield wipers. 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.
2016-08-24; vol. 81 # 164 - Wednesday, August 24, 201681 FR 57758 - Special Conditions: The Boeing Company, Boeing Model 767-2C Airplane; Non-Rechargeable Lithium Battery Installations
typeregulations.gov FR Doc.2016-19991 RIN Docket No.FAA-2015-5391 Special Conditions No.25-630-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions. Effective April 22, 2017. 14 CFR Part 25 SummaryThese special conditions are issued for the Boeing Model 767-2C 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. This design feature is associated with non-rechargeable lithium battery installations. 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.
2016-08-22; vol. 81 # 162 - Monday, August 22, 201681 FR 56472 - Special Conditions: Bombardier Aerospace Inc. Model BD-700-2A12 and BD-700-2A13 Airplanes; Automatic Speed Protection for Design Dive Speed
typeregulations.gov FR Doc.2016-19993 RIN Docket No.FAA-2016-4137 Special Conditions No.25-631-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. This action is effective on Bombardier on August 22, 2016. We must receive your comments by October 6, 2016. 14 CFR Part 25 SummaryThese special conditions are issued for the Bombardier Aerospace Inc. (Bombardier) Model BD-700-2A12 and BD-700-2A13 airplanes. These airplanes will have a novel or unusual feature when compared to the state of technology envisioned in the airworthiness standards for transport-category airplanes. This design feature is associated with a reduced margin between design cruising speed, V C /M C, and design diving speed, V D /M D, based on the incorporation of a high-speed-protection system that limits nose-down pilot authority at speeds above V D /M D . 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.
81 FR 56474 - Special Conditions: Bombardier Inc. Model BD-700-2A12 and BD-700-2A13 Airplanes; Airplane Electronic-System Security Protection From Authorized Internal Access
typeregulations.gov FR Doc.2016-19994 RIN Docket No.FAA-2015-6359 Special Conditions No.25-633-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. This action is effective on Bombardier on August 22, 2016. We must receive your comments by October 6, 2016. 14 CFR Part 25 SummaryThese special conditions are issued for the Bombardier Inc. (Bombardier) Model BD-700-2A12 and BD-700-2A13 airplanes. These airplanes will have novel or unusual design features, specifically, digital systems architecture composed of several connected data networks that will have the capability to allow 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 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.
81 FR 56475 - Special Conditions: Garmin International, Beechcraft Corporation Model 400A Airplanes; Airplane Electronic-System Security Protection From Unauthorized External Access
typeregulations.gov FR Doc.2016-20000 RIN Docket No.FAA-2016-8029 Special Conditions No.25-634-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. This action is effective on Garmin on August 22, 2016. We must receive your comments by October 6, 2016. 14 CFR Part 25 SummaryThese special conditions are issued for the Beechcraft Corporation (Beechcraft) Model 400A airplane. This airplane, as modified by Garmin International (Garmin), 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 airplanes will have a digital-systems network architecture composed of several connected networks that may allow access to or by external computer systems and networks, and may otherwise result in airplane electronic-system security vulnerabilities without appropriate protection. 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.
2016-08-19; vol. 81 # 161 - Friday, August 19, 201681 FR 55351 - Special Conditions: The Boeing Company, Boeing Model 737-8 Airplane; Non-Rechargeable Lithium Battery Installations
typeregulations.gov FR Doc.2016-19856 RIN Docket No.FAA-2015-5758 Special Conditions No.25-632-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions. Effective April 22, 2017. 14 CFR Part 25 SummaryThese special conditions are issued for the Boeing Company (Boeing) Model 737-8 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. This design feature is associated with non-rechargeable lithium battery installations. 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.
2016-08-03; vol. 81 # 149 - Wednesday, August 3, 201681 FR 51081 - Special Conditions: The Boeing Company Model 787-9 Series Airplane; Dynamic Test Requirements for Single-Occupant Oblique (Side-Facing) Seats With Inflatable and 3-Point Restraint Systems
typeregulations.gov FR Doc.2016-18449 RIN Docket No.FAA-2016-5909 Special Conditions No.25-626-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. This action is effective on Boeing on August 3, 2016. We must receive your comments by September 19, 2016. 14 CFR Part 25 SummaryThese special conditions are issued for The Boeing Company (Boeing) Model 787-9 series airplane. This airplane, as modified by Boeing, 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 are single-occupant oblique (side-facing) seats with inflatable and 3-point restraint systems requiring dynamic testing. 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.
81 FR 51084 - Special Conditions: The Boeing Company Model 777-300ER Airplanes; Dynamic Test Requirements for Single-Occupant Oblique (Side-Facing) Seats with Inflatable Restraints
typeregulations.gov FR Doc.2016-18323 RIN Docket No.FAA-2016-4136 Special Conditions No.25-621-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. This action is effective on Boeing on August 3, 2016. We must receive your comments by September 19, 2016. 14 CFR Part 25 SummaryThese special conditions are issued to The Boeing Company (Boeing) for their Model 777-300ER airplane. This airplane has novel or unusual design features associated with single-occupant oblique (side-facing) seats equipped with inflatable restraints. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for occupants of seats installed at an angle of greater than 18 degrees, but substantially less than 90 degrees, to the vertical plane containing the centerline of the airplane, nor for inflatable restraints or related airbag devices. 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.
81 FR 51086 - Special Conditions: Gulfstream Aerospace Corporation Model GVII-G500 Airplanes; Interaction of Systems and Structures Through a Three-Axis Fly-by-Wire System
typeregulations.gov FR Doc.2016-18448 RIN Docket No.FAA-2015-7294 Special Conditions No.25-628-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. This action is effective on Gulfstream on August 3, 2016. We must receive your comments by September 19, 2016. 14 CFR Part 25 SummaryThese special conditions are issued for the Gulfstream Aerospace Corporation (Gulfstream) Model GVII-G500 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. This design feature is a fly-by-wire flight-control system that governs the pitch, yaw, and roll axes of the airplane. 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.
81 FR 51090 - Special Conditions: Embraer S.A. Model EMB-545 and EMB-550 airplanes, Synthetic Vision System and Enhanced Flight Vision System on Head-Up Display
typeregulations.gov FR Doc.2016-18447 RIN Docket No.FAA-2016-3872 Special Conditions No.25-629-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. This action is effective on Embraer S.A. on August 3, 2016. We must receive your comments by September 19, 2016. 14 CFR Part 25 SummaryThese special conditions are issued for the Embraer S.A. (Embraer) Model EMB-545 and EMB-550 airplanes. These airplanes will have a novel or unusual design feature associated with a vision system that displays video imagery on the head-up display. 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.
81 FR 51093 - Special Conditions: FedEx Express Corporation, Boeing Model 767-300F; Enhanced Flight Vision System
typeregulations.gov FR Doc.2016-18445 RIN Docket No.FAA-2016-4116 Special Conditions No.25-627-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. This action is effective on FedEx on August 3, 2016. We must receive your comments by September 19, 2016. 14 CFR Part 25 SummaryThese special conditions are issued for the Boeing Model 767-300F airplane. This airplane, as modified by the FedEx Express Corporation (FedEx), 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.
81 FR 51095 - Special Conditions: Associated Air Center, Boeing Model 747-8 Airplane; Installation of an Airbag System To Limit the Axial Rotation of the Upper Leg on Single-Place Side-Facing Seats
typeregulations.gov FR Doc.2016-18398 RIN Docket No.FAA-2016-7851 Special Conditions No.25-625-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. This action is effective on Associated Air Center on August 3, 2016. We must receive your comments by September 19, 2016. 14 CFR Part 25 SummaryThese special conditions are issued for the Boeing Model 747-8 airplane. This airplane, as modified by Associated Air Center, will have a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for transport-category airplanes. This design feature is an airbag system to limit axial rotation of the upper leg, due to leg flail, of occupants in single-place side-facing seats. 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.
2016-07-29; vol. 81 # 146 - Friday, July 29, 201681 FR 49869 - Special Conditions: Embraer S.A. Model EMB-545 and EMB-550 Airplanes; Installation of an Airbag System To Limit the Axial Rotation of the Upper Leg on Single- and Multiple-Place Side-Facing Seats
typeregulations.gov FR Doc.2016-17845 RIN Docket No.FAA-2016-6925 Special Conditions No.25-623-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. This action is effective on Embraer on July 29, 2016. We must receive your comments by September 12, 2016. 14 CFR Part 25 SummaryThese special conditions are issued for the Embraer S.A. (Embraer) Model EMB-545 and EMB-550 series airplanes. These airplanes will have a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for transport-category airplanes. This feature is an airbag system designed to limit the axial rotation of the upper leg on single-place and multiple-place side-facing seats. 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.
81 FR 49871 - Special Conditions: ATR Model ATR-42-200/-300/-320/-500 and ATR-72-102/-202/-212/-212A Airplanes; Seats With Non-Traditional, Large, Non-Metallic Panels
typeregulations.gov FR Doc.2016-17846 RIN Docket No.FAA-2016-8246 Special Conditions No.25-624-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. This action is effective on ATR on July 29, 2016. We must receive your comments by September 12, 2016. 14 CFR Part 25 SummaryThese special conditions are issued for ATR Model ATR-42-200/-300/-320/-500 and ATR-72-102/-202/-212/-212A airplanes. These airplanes will have a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for transport-category airplanes. This design feature is seats with non-traditional, large, non-metallic panels. 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.
2016-07-26; vol. 81 # 143 - Tuesday, July 26, 201681 FR 48693 - Fuel Tank Vent Fire Protection; Correction
typeregulations.gov FR Doc.2016-17590 RIN2120-AK30 Docket No.FAA-2014-0500 Amdt. Nos.25-143, 121-375, and 129-52 DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final rule; correction. This correction is effective on July 26, 2016. 14 CFR Parts 25, 121, and 129 SummaryThe FAA is correcting a final rule published in the Federal Register on June 24, 2016 (81 FR 41200). In that final rule, the FAA amended certain airworthiness regulations for transport category airplanes to require fuel tank designs that prevent a fuel tank explosion caused by the propagation of flames, from external fires, through the fuel tank vents. The final rule requires a delay of two minutes and thirty seconds between exposure of external fuel tank vents to ignition sources and explosions caused by propagation of flames into the fuel tank, thus increasing the time available for passenger evacuation and emergency response. The amendments apply to applications for new type certificates and certain applications for amended or supplemental type certificates. The amendments also require certain airplanes produced in the future and operated by air carriers to meet the new standards. However, in that document, the amendment numbers for the final rules were incorrect, and an airplane model number in a footnote was incorrect. This document now posts the correct amendment numbers and airplane model number in the footnote.
2016-07-25; vol. 81 # 142 - Monday, July 25, 201681 FR 48319 - Special Conditions: Avmax Aviation Services Inc., Bombardier Model DHC-8-100/-200/-300 Series Airplanes; Installed Rechargeable Lithium Batteries and Battery Systems
typeregulations.gov FR Doc.2016-17428 RIN Docket No.FAA-2015-1087 Special Conditions No.25-622-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. This action is effective on Avmax July 25, 2016. We must receive your comments by September 8, 2016. 14 CFR Part 25 SummaryThese special conditions are issued for the Bombardier Model DHC-8-100/-200/-300 series airplanes. These airplanes, as modified by Avmax Aviation Services Inc. (Avmax), will have a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for transport-category airplanes. This design feature is rechargeable lithium batteries to replace the existing nickel-cadmium and lead-acid rechargeable batteries. 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.
2016-07-15; vol. 81 # 136 - Friday, July 15, 201681 FR 45968 - Special Conditions: Gulfstream Aerospace Corporation Model GVII-G500 Airplanes; Isolation or Protection of Airplane Electrical-System Security From Unauthorized Internal Access
typeregulations.gov FR Doc.2016-16638 RIN Docket No.FAA-2016-4237 Special Conditions No.25-619-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. This action is effective on Gulfstream on July 15, 2016. We must receive your comments by August 29, 2016. 14 CFR Part 25 SummaryThese special conditions are issued for the Gulfstream Aerospace Corporation (Gulfstream) Model GVII-G500 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. This design feature is a digital systems architecture requiring isolation or protection from unauthorized internal access. 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.
2016-07-14; vol. 81 # 135 - Thursday, July 14, 201681 FR 45405 - Special Conditions: American Airlines, Boeing 777-200 Series Airplanes; Dynamic Test Requirements for Single-Occupant Oblique (Side-Facing) Seats Equipped With Inflatable Lapbelts
typeregulations.gov FR Doc.2016-16639 RIN Docket No.FAA-2016-6136 Special Conditions No.25-620-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. This action is effective on American Airlines on July 14, 2016. We must receive your comments by August 29, 2016. 14 CFR Part 25 SummaryThese special conditions are issued for the Boeing 777-200 series airplane. This airplane, as modified by American Airlines, will have novel or unusual design features when compared to the state of technology envisioned in the airworthiness standards for transport-category airplanes. These airplanes will include single-occupant oblique seats with inflatable lapbelts requiring dynamic testing. 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.
2016-07-05; vol. 81 # 128 - Tuesday, July 5, 201681 FR 43471 - Special Conditions: JAMCO America, Inc., Boeing Model 777-300ER, Dynamic Test Requirements for Single-Occupant Oblique (Side-Facing) Seats With Inflatable Restraints
typeregulations.gov FR Doc.2016-15784 RIN Docket No.FAA-2015-8298 Special Conditions No.25-611-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special condition; request for comments; corrections. This action is effective on JAMCO America, Inc., on July 5, 2016. We must receive your comments August 19, 2016. 14 CFR Part 25 SummaryThis document corrects omissions in docket no. FAA-2015-8298, special conditions no. 25-611-SC, which was published in the Federal Register on March 16, 2016 (81 FR 13969). The special conditions in the published document are incomplete. This correction replaces the entire special conditions section from that which appeared in the original Federal Register publication.
2016-06-24; vol. 81 # 122 - Friday, June 24, 201681 FR 41200 - Fuel Tank Vent Fire Protection
typeregulations.gov FR Doc.2016-14454 RIN2120-AK30 Docket No.FAA-2014-0500 Amdt. Nos.25-142, 21-376, and 129-53 DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final rule. Effective August 23, 2016. The compliance date for the requirements in § 25.975 is August 23, 2016. The compliance date for the requirements in §§ 121.1119 and 129.119 is August 23, 2018. 14 CFR Parts 25, 121, and 129 SummaryThe FAA is amending certain airworthiness regulations for transport category airplanes to require fuel tank designs that prevent a fuel tank explosion caused by the propagation of flames, from external fires, through the fuel tank vents. This final rule requires a delay of two minutes and thirty seconds between exposure of external fuel tank vents to ignition sources and explosions caused by propagation of flames into the fuel tank, thus increasing the time available for passenger evacuation and emergency response. These amendments apply to applications for new type certificates and certain applications for amended or supplemental type certificates. The amendments also require certain airplanes produced in the future and operated by air carriers to meet the new standards.
2016-05-04; vol. 81 # 86 - Wednesday, May 4, 201681 FR 26668 - Special Conditions: Gulfstream Aerospace Corporation Model GVII-G500 Airplane, Technical Criteria for Approving Side-Facing Seats
typeregulations.gov FR Doc.2016-10440 RIN Docket No.FAA-2016-1085 Special Conditions No.25-618-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. The effective date of these special conditions is May 4, 2016. We must receive your comments by June 20, 2016. 14 CFR Part 25 SummaryThese special conditions are issued for the Gulfstream Aerospace Corporation (Gulfstream) Model GVII-G500 airplane. This airplane will have a novel or unusual design feature associated with side-facing seats. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. These special conditions contain the additional safety standards the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards.
2016-04-22; vol. 81 # 78 - Friday, April 22, 201681 FR 23566 - Special Conditions: Dassault Aviation Model Falcon 5X Airplane; Use of Automatic Power Reserve (APR), an Automatic Takeoff Thrust Control System (ATTCS) for Go-Around Performance Credit
typeregulations.gov FR Doc.2016-09333 RIN Docket No.FAA-2014-1078 Special Conditions No.25-616-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. This action is effective on Dassault Aviation on April 22, 2016. We must receive your comments by June 6, 2016. 14 CFR Part 25 SummaryThese special conditions are issued for the Dassault Aviation (Dassault) Model Falcon 5X airplane. This airplane will have a novel or unusual design feature associated with 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.
81 FR 23570 - Special Conditions: Gulfstream Aerospace Corporation Model GVII-G500 Airplanes, Pilot Compartment View Requirements With an Enhanced Flight Vision System
typeregulations.gov FR Doc.2016-09334 RIN Docket No.FAA-2015-7301 Special Conditions No.25-614-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. This action is effective on Gulfstream Aerospace Corporation on April 22, 2016. We must receive your comments by June 6, 2016. 14 CFR Part 25 SummaryThese special conditions are issued for the Gulfstream Aerospace Corporation (Gulfstream) Model GVII-G500 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. This design feature is an enhanced flight vision system (EFVS) that includes a head-up display (HUD) capable of displaying forward-looking infrared (FLIR) imagery, intended to be used for instrument approaches under provisions of Title 14, Code of Federal Regulations (14 CFR) 91.175(l) and (m). 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.
81 FR 23573 - Special Conditions: Gulfstream Aerospace Corporation, Gulfstream GVI Airplane; Non-Rechargeable Lithium Battery Installations
typeregulations.gov FR Doc.2016-09311 RIN Docket No.FAA-2015-4279 Special Conditions No.25-612-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions. Effective April 22, 2017. 14 CFR Part 25 SummaryThese special conditions are issued for the Gulfstream Aerospace Corporation (Gulfstream) GVI 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. This design feature is non-rechargeable lithium 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.
81 FR 23578 - Special Conditions: Bombardier Inc. Model BD-700-2A12 and BD-700-2A13 Airplanes; Airplane Electronic System Security Protection From Unauthorized External Access
typeregulations.gov FR Doc.2016-09336 RIN Docket No.FAA-2016-4819 Special Conditions No.25-615-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. This action is effective on Bombardier Inc. on April 22, 2016. We must receive your comments by June 6, 2016. 14 CFR Part 25 SummaryThese special conditions are issued for the Bombardier Inc. Model BD-700-2A12 and BD-700-2A13 airplanes. These airplanes will have a digital-systems network architecture composed of several connected networks that may allow access to or by external computer systems and networks, and may result in airplane systems-security vulnerabilities. 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.
81 FR 23579 - Special Conditions: Gulfstream Aerospace Corporation Model GVII-G500 Airplanes; Airplane Electronic System Security Protection From Unauthorized External Access
typeregulations.gov FR Doc.2016-09335 RIN Docket No.FAA-2016-4238 Special Conditions No.25-613-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. This action is effective on Gulfstream Aerospace Corporation on April 22, 2016. We must receive your comments by June 6, 2016. 14 CFR Part 25 SummaryThese special conditions are issued for the Gulfstream Aerospace Corporation (Gulfstream) Model GVII-G500 airplane. These airplanes will have a digital-systems network architecture composed of several connected networks that may allow access to or by external computer systems and networks, and may result in airplane electronic system-security vulnerabilities. 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.
2016-04-21; vol. 81 # 77 - Thursday, April 21, 201681 FR 23421 - Special Conditions: Gulfstream Aerospace Corporation Model GVII-G500 Airplanes, Design Roll Maneuver Requirement
typeregulations.gov FR Doc.2016-09326 RIN Docket No.FAA-2015-1484 Special Conditions No.25-617-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. This action is effective on Gulfstream Aerospace Corporation on April 21, 2016. We must receive your comments by June 6, 2016. 14 CFR Part 25 SummaryThese special conditions are issued for the Gulfstream Aerospace Corporation (Gulfstream) Model GVII-G500 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. This design feature is 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.
2016-03-16; vol. 81 # 51 - Wednesday, March 16, 201681 FR 13969 - Special Conditions: JAMCO America, Inc., Boeing Model 777-300ER, Dynamic Test Requirements for Single-Occupant Oblique (Side-Facing) Seats With Inflatable Restraints
typeregulations.gov FR Doc.2016-05995 RIN Docket No.FAA-2015-8298 Special Conditions No.25-611-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special condition; request for comments. This action is effective on March 16, 2016. We must receive your comments by May 2, 2016. 14 CFR Part 25 SummaryThese special conditions are issued for the Boeing Model 777-300ER airplane. This airplane, as modified by JAMCO America, Inc. (JAMCO), will have a novel or unusual design feature associated with side-facing, oblique seats equipped with inflatable restraints. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for occupants of seats installed at an angle of greater than 18 degrees, but substantially less than 90 degrees, to the centerline of the airplane, nor for airbag devices. 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.
2016-03-02; vol. 81 # 41 - Wednesday, March 2, 201681 FR 10761 - Harmonization of Airworthiness Standards—Fire Extinguishers and Class B and F Cargo Compartments; Correction
typeregulations.gov FR Doc.2016-04508 RIN2120-AK29 Docket No.FAA-2014-0001 Amdt. No.25-142 DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final rule; correction. This correction is effective on March 2, 2016. 14 CFR Part 25 SummaryThe FAA is correcting a final rule published on February 16, 2016. In that rule, the FAA amended certain airworthiness regulations for transport category airplanes by upgrading fire safety standards for Class B cargo compartments; establishing fire safety standards for a new type of cargo compartment, Class F; and updating related standards for fire extinguishers. This amendment eliminated certain regulatory differences between the airworthiness standards of the FAA and the European Aviation Safety Agency (EASA), without affecting current industry design practices. However, in that document, the amendment number for the final rule was incorrect, and this document now posts the correct amendment number.
2016-02-25; vol. 81 # 37 - Thursday, February 25, 201681 FR 9363 - Special Conditions: Lufthansa Technik AG; Boeing Model 747-8 Series Airplanes, Large Non-Structural Glass in the Passenger Compartment
typeregulations.gov FR Doc.2016-03997 RIN Docket No.FAA-2015-7689 Notice No.25-16-03-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Notice of proposed special conditions. Send your comments on or before March 16, 2016. 14 CFR Part 25 SummaryThis action proposes special conditions for the Boeing Model 747-8 airplane. This airplane, as modified by Lufthansa Technik AG, will have a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for transport-category airplanes. This design feature is large, non-structural glass panels in the passenger compartment. 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.
81 FR 9365 - Special Conditions: L-3 Communications Integrated Systems; Boeing Model 747-8 Series Airplanes, Large Non-Structural Glass in the Passenger Compartment
typeregulations.gov FR Doc.2016-03996 RIN Docket No.FAA-2015-3324 Notice No.25-16-04-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Notice of proposed special conditions. Send your comments on or before March 28, 2016. 14 CFR Part 25 SummaryThis action proposes special conditions for the Boeing Model 747-8 airplane. This airplane, as modified by L-3 Communications Integrated Systems, will have a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for transport-category airplanes. This design feature is large, non-structural glass panels in the passenger compartment. 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.
2016-02-17; vol. 81 # 31 - Wednesday, February 17, 201681 FR 7965 - Special Conditions: Dassault Aviation Model Falcon 5X Airplane, Design Roll Maneuver Condition
typeregulations.gov FR Doc.2016-03212 RIN Docket No.FAA-2014-1077 Special Conditions No.25-609-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. This action is effective on Dassault Aviation on February 17, 2016. We must receive your comments by April 4, 2016. 14 CFR Part 25 SummaryThese special conditions are issued for the Dassault Aviation Model Falcon 5X airplane. This airplane will have novel or unusual design features when compared to the state of technology envisioned in the airworthiness standards for transport-category airplanes. This design feature is 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.
2016-02-16; vol. 81 # 30 - Tuesday, February 16, 201681 FR 7698 - Harmonization of Airworthiness Standards—Fire Extinguishers and Class B and F Cargo Compartments
typeregulations.gov FR Doc.2016-03000 RIN2120-AK29 Docket No.FAA-2014-0001 Amdt. No.25-141 DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final rule. Effective April 18, 2016. 14 CFR Part 25 SummaryThe FAA is amending certain airworthiness regulations for transport category airplanes by upgrading fire safety standards for Class B cargo compartments; establishing fire safety standards for a new type of cargo compartment, Class F; and updating related standards for fire extinguishers. This amendment is based on recommendations from the Aviation Rulemaking Advisory Committee (ARAC) and the National Transportation Safety Board (NTSB), and the changes address designs for which airworthiness directives (ADs) have been issued by both the FAA and the French civil aviation authority, Direction Générale de l&apos;Aviation Civile (DGAC). This amendment eliminates certain regulatory differences between the airworthiness standards of the FAA and the European Aviation Safety Agency (EASA), without affecting current industry design practices. These changes ensure an acceptable level of safety for these types of cargo compartments by standardizing certain requirements and procedures.
2016-02-11; vol. 81 # 28 - Thursday, February 11, 201681 FR 7198 - Special Conditions: The Boeing Company, Model 737-8 Airplanes; Design Roll-Maneuver Requirements
typeregulations.gov FR Doc.2016-02762 RIN Docket No.FAA-2015-5877 Special Conditions No.25-610-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. This action is effective on the Boeing Company on February 11, 2016. We must receive your comments by March 28, 2016. 14 CFR Part 25 SummaryThese special conditions are issued for Boeing Model 737-8 airplanes. These airplanes will have a novel or unusual design feature associated with an electronic flight-control system that provides roll control of the airplane through pilot inputs to the flight computers. 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.
14 CFR 25.771 — Pilot Compartment.
14 CFR 25.777 — Cockpit Controls.
2016-01-27; vol. 81 # 17 - Wednesday, January 27, 201681 FR 4577 - Special Conditions: Dassault Aviation, Model Falcon 2000EX Airplanes, Head-Up Display (HUD) With Vision-System Video
typeregulations.gov FR Doc.2016-01583 RIN Docket No.FAA-2015-5878 Special Conditions No.25-608-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. This action is effective on Dassault Aviation on January 27, 2016. We must receive your comments by March 14, 2016. 14 CFR Part 25 SummaryThese special conditions are issued for Dassault Aviation Model Falcon 2000EX airplanes. This airplane will have a novel or unusual design feature associated with a vision system that displays video imagery on the head-up display (HUD). 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.
81 FR 4579 - Special Conditions: Dassault Aviation Model Falcon 5X, Limit Pilot Forces
typeregulations.gov FR Doc.2016-01581 RIN Docket No.FAA-2014-1076 Special Conditions No.25-607-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. This action is effective on Dassault Aviation on January 27, 2016. We must receive your comments by March 14, 2016. 14 CFR Part 25 SummaryThese special conditions are issued for the Dassault Aviation Model Falcon 5X 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. This design feature is an electronic flight-control system with pilot controls through a side stick instead of a conventional control stick. 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.
2015-11-20; vol. 80 # 224 - Friday, November 20, 201580 FR 72555 - Special Conditions: Associated Air Center, Boeing Model 747-8 Airplane; Shoulder-Belt Airbags for Side-Facing Seats