This is a list of United States Code sections, Statutes at Large, Public Laws, and Presidential Documents, which provide rulemaking authority for this CFR Part.
This list is taken from the Parallel Table of Authorities and Rules provided by GPO [Government Printing Office] .
It is not guaranteed to be accurate or up-to-date, though we do refresh the database weekly. More limitations on accuracy are described at the GPO site.
United States Code U.S. Code: Title 42 - THE PUBLIC HEALTH AND WELFARE U.S. Code: Title 49 - TRANSPORTATION
Title 14 published on 03-May-2017 03:58
The following are ALL rules, proposed rules, and notices (chronologically) published in the Federal Register relating to 14 CFR Part 25 after this date.
2017-05-23; vol. 82 # 98 - Tuesday, May 23, 2017 82 FR 23491 - Special Conditions: Garmin International, Learjet, Inc., Model 35 and 36 Airplanes; Airplane Electronic-System Security Protection From Unauthorized External Access
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. This action is effective on Garmin on May 23, 2017. We must receive your comments by July 7, 2017. 14 CFR Part 25 Summary These special conditions are issued for Garmin International (Garmin) for modifications to Learjet, Inc., (Learjet) Model 35 and 36 airplanes. These airplanes, as modified by 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. This design feature incorporates the Garmin Flight Stream 210 and GTN 6XX/7XX Navigator system into the airplanes. 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.
82 FR 23492 - Special Conditions: Garmin International, Learjet, Inc., Model 35 and 36 Airplanes; Isolation of Airplane Electronic-System Security Protection From Unauthorized Internal Access
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. This action is effective on Garmin on May 23, 2017. We must receive your comments by July 7, 2017. 14 CFR Part 25 Summary These special conditions are issued for Garmin International (Garmin) for modifications to Learjet, Inc., (Learjet) Model 35 and 36 airplanes. These airplanes, as modified by 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. This design feature incorporates the Garmin Flight Stream 210 and GTN 6XX/7XX Navigator system into the airplanes. 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.
2017-05-16; vol. 82 # 93 - Tuesday, May 16, 2017 82 FR - Special Conditions: Dassault Aviation Model Falcon 900EX Airplane; Electronic System-Security Protection From Unauthorized External Access
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions, request for comment; withdrawal. This withdrawal of special conditions is effective on Dassault on April 7, 2017. 14 CFR Part 25 Summary The FAA is withdrawing a previously published special conditions for the Dassault Aviation (Dassault) Model Falcon 900EX airplane. We are withdrawing the special conditions in response to Dassault's comments, submitted to the Federal Docket on December 5, 2014.
82 FR 22399 - Special Conditions: Airbus, Model A380-800 Series Airplanes; Non-Rechargeable Lithium Battery Installations
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comment. This action is effective on Airbus on May 16, 2017. We must receive your comments by June 30, 2017. 14 CFR Part 25 Summary These special conditions are issued for non-rechargeable lithium battery installations on the Airbus Model A380-800 series airplanes. Non-rechargeable lithium batteries are a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. 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.
82 FR 22403 - Special Conditions: The Boeing Company, Model 747-8 Series Airplanes; Non-Rechargeable Lithium Battery Installations
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comment. This action is effective on The Boeing Company on May 16, 2017. We must receive your comments by June 30, 2017. 14 CFR Part 25 Summary These special conditions are issued for non-rechargeable lithium battery installations on The Boeing Company (Boeing) Model 747-8 series airplanes. Non-rechargeable lithium batteries are a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. 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.
82 FR 22406 - Special Conditions: Textron Aviation Inc., Model 560XL Airplane; Non-Rechargeable Lithium Battery Installations
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comment. This action is effective on Textron on May 16, 2017. We must receive your comments by June 30, 2017. 14 CFR Part 25 Summary These special conditions are issued for non-rechargeable lithium battery installations on the Textron Aviation Inc. (Textron) Model 560XL airplane. Non-rechargeable lithium batteries are a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. 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.
82 FR 22409 - Special Conditions: Embraer S. A., Model EMB-135BJ Airplane; Non-Rechargeable Lithium Battery Installations
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comment. This action is effective on Embraer on May 16, 2017. We must receive your comments by June 30, 2017. 14 CFR Part 25 Summary These special conditions are issued for non-rechargeable lithium battery installations on the Embraer S. A. (Embraer) Model EMB-135BJ airplane. Non-rechargeable lithium batteries are a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. 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.
82 FR 22412 - Special Conditions: Airbus, Models A318, A319, A320, and A321 Series Airplanes; Non-Rechargeable Lithium Battery Installations
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comment. This action is effective on Airbus on May 16, 2017. We must receive your comments by June 30, 2017. 14 CFR Part 25 Summary These special conditions are issued for non-rechargeable lithium battery installations on Airbus Models A318, A319, A320, and A321 series airplanes. Non-rechargeable lithium batteries are a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. 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.
2017-05-12; vol. 82 # 91 - Friday, May 12, 2017 82 FR 22065 - Special Conditions: Bombardier Aerospace, Model BD-700-2A12 and BD-700-2A13 Airplanes; Limit Engine Torque Loads
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. This action is effective on Bombardier on May 12, 2017. Send your comments on or before June 26, 2017. 14 CFR Part 25 Summary These special conditions are issued for the Bombardier (Bombardier) Inc. Models BD-700-2A12 and BD-700-2A13 airplanes. 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 the engine torque-load limit imposed by sudden engine stoppage due to malfunction or structural failure. 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.
82 FR 22066 - Special Conditions: Bombardier Aerospace Inc., Model BD-100-1A10 Airplane; Non-Rechargeable Lithium Battery Installations
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comment. This action is effective on Bombardier on May 12, 2017. We must receive your comments by June 26, 2017. 14 CFR Part 25 Summary These special conditions are issued for non-rechargeable lithium battery installations on the Bombardier Aerospace Inc. (Bombardier) Model BD-100-1A10 airplane. Non-rechargeable lithium batteries are a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. 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.
2017-05-10; vol. 82 # 89 - Wednesday, May 10, 2017 82 FR 21679 - Special Conditions: Embraer S.A., Model ERJ 190-300 Series Airplanes; Operation Without Normal Electrical Power
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. This action is effective on Embraer S.A. on May 10, 2017. We must receive your comments by June 26, 2017. 14 CFR Part 25 Summary These special conditions are issued for the Embraer S.A. (Embraer) 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 and electronic systems that perform critical functions, the loss of which could be catastrophic to 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.
82 FR 21681 - Special Conditions: Textron Aviation Inc. Model 700 Airplane; Design Roll Maneuver Condition
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. This action is effective on Textron on May 10, 2017. We must receive your comments by June 26, 2017. 14 CFR Part 25 Summary These special conditions are issued for the Textron Aviation Inc. (Textron) Model 700 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 that provides control through pilot inputs to the flight computer. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. These special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards.
2017-05-09; vol. 82 # 88 - Tuesday, May 9, 2017 82 FR 21461 - Special Conditions: Bombardier Aerospace Inc., Model CL-600-2E25 Airplane; Non-Rechargeable Lithium Battery Installations
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comment. This action is effective on Bombardier on May 9, 2017. We must receive your comments by June 23, 2017. 14 CFR Part 25 Summary These special conditions are issued for non-rechargeable lithium battery installations on the Bombardier Aerospace Inc. (Bombardier) Model CL-600-2E25 airplane. Non-rechargeable lithium batteries are a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. 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.
82 FR 21464 - Special Conditions: Gulfstream Aerospace LP, Model Gulfstream 200 Airplane; Non-Rechargeable Lithium Battery Installations
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comment. This action is effective on Gulfstream Aerospace LP on May 9, 2017. We must receive your comments by June 23, 2017. 14 CFR Part 25 Summary These special conditions are issued for non-rechargeable lithium battery installations on the Gulfstream Aerospace LP (GALP) Model Gulfstream 200 airplane, as modified by Gulfstream Aerospace Corporation (Gulfstream). Non-rechargeable lithium batteries are a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. 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.
2017-05-08; vol. 82 # 87 - Monday, May 8, 2017 82 FR 21303 - Special Conditions: Gulfstream Aerospace LP, Model Gulfstream G280 Airplane; Non-Rechargeable Lithium Battery Installations
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comment. This action is effective on Gulfstream Aerospace LP on May 8, 2017. We must receive your comments by June 22, 2017. 14 CFR Part 25 Summary These special conditions are issued for non-rechargeable lithium battery installations on the Gulfstream Aerospace LP (GALP) Model Gulfstream G280 airplane, as modified by Gulfstream Aerospace Corporation (Gulfstream). Non-rechargeable lithium batteries are a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. 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.
82 FR 21306 - Special Conditions: Gulfstream Aerospace Corporation, Model GV-SP Airplane; Non-Rechargeable Lithium Battery Installations
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comment. This action is effective on Gulfstream Aerospace Corporation on May 8, 2017. We must receive your comments by June 22, 2017. 14 CFR Part 25 Summary These special conditions are issued for non-rechargeable lithium battery installations on the Gulfstream Aerospace Corporation (Gulfstream) Model GV-SP airplane. Non-rechargeable lithium batteries are a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. 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.
2017-05-05; vol. 82 # 86 - Friday, May 5, 2017 82 FR 21110 - Special Conditions: AMAC Aerospace Switzerland AG, Boeing Model 737-700 Airplane; Installation of a Therapeutic Oxygen System for Medical Use
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. This action is effective on AMAC Aerospace Switzerland AG on May 5, 2017. We must receive your comments by June 19, 2017. 14 CFR Part 25 Summary These special conditions are issued for the Boeing Model 737-700 airplane, as modified by AMAC Aerospace Switzerland AG (AMAC). 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 the installation of a therapeutic oxygen system for medical use. 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.
2017-05-01; vol. 82 # 82 - Monday, May 1, 2017 82 FR 20241 - Special Conditions: Gulfstream Aerospace LP, Model Gulfstream G150 Airplane; Non-Rechargeable Lithium Battery Installations
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comment. This action is effective on Gulfstream Aerospace LP on May 1, 2017. We must receive your comments by June 15, 2017. 14 CFR Part 25 Summary These special conditions are issued for non-rechargeable lithium battery installations on the Gulfstream Aerospace LP (GALP) Model Gulfstream G150 airplane, as modified by Gulfstream Aerospace Corporation (Gulfstream). Non-rechargeable lithium batteries are a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. 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.
82 FR 20244 - Special Conditions: Bombardier Aerospace Inc., Model DHC-8-400 Series Airplanes; Non-Rechargeable Lithium Battery Installations
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comment. This action is effective on Bombardier on May 1, 2017. We must receive your comments by June 15, 2017. 14 CFR Part 25 Summary These special conditions are issued for non-rechargeable lithium battery installations on the Bombardier Aerospace Inc. (Bombardier) Model DHC-8-400 series airplanes. Non-rechargeable lithium batteries are a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. 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.
82 FR 20247 - Special Conditions: Gulfstream Aerospace Corporation, Model GVII-G500 Airplane; Non-Rechargeable Lithium Battery Installations
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comment. This action is effective on Gulfstream Aerospace Corporation on May 1, 2017. We must receive your comments by June 15, 2017. 14 CFR Part 25 Summary These special conditions are issued for non-rechargeable lithium battery installations on the Gulfstream Aerospace Corporation (Gulfstream) Model GVII-G500 airplane. Non-rechargeable lithium batteries are a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. 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.
82 FR 20250 - Special Conditions: Bombardier Aerospace Inc., Model BD-500-1A10 Airplane; Non-Rechargeable Lithium Battery Installations
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comment. This action is effective on Bombardier on May 1, 2017. We must receive your comments by June 15, 2017. 14 CFR Part 25 Summary These special conditions are issued for non-rechargeable lithium battery installations on the Bombardier Aerospace Inc. (Bombardier) Model BD-500-1A10 airplane. Non-rechargeable lithium batteries are a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. 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.
82 FR 20253 - Special Conditions: Bombardier Aerospace Inc., Model BD-700-1A11 Airplane; Non-Rechargeable Lithium Battery Installations
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comment. This action is effective on Bombardier on May 1, 2017. We must receive your comments by June 15, 2017. 14 CFR Part 25 Summary These special conditions are issued for non-rechargeable lithium battery installations on the Bombardier Aerospace Inc. (Bombardier) Model BD-700-1A11 airplane. Non-rechargeable lithium batteries are a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. 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.
2017-04-12; vol. 82 # 69 - Wednesday, April 12, 2017 82 FR 17531 - Special Conditions: Bombardier Inc. Model BD-700-2A12 and BD-700-2A13 Airplanes; Fuselage In-Flight Fire Safety and Flammability Resistance of Aluminum-Lithium Material
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions. Effective May 12, 2017. 14 CFR Part 25 Summary These 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 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 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.
2017-04-10; vol. 82 # 67 - Monday, April 10, 2017 82 FR 17101 - Special Conditions: Embraer S.A. Model ERJ 190-300 Airplane; Flight Envelope Protection, General Limiting Requirements
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. This action is effective on Embraer on April 10, 2017. We must receive your comments by May 25, 2017. 14 CFR Part 25 Summary These special conditions are issued for the Embraer S.A. (Embraer) Model ERJ 190-300 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 new control architecture and a full digital flight-control system, both of which provide flight-envelope protections. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. These special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards.
2017-04-07; vol. 82 # 66 - Friday, April 7, 2017 82 FR 16891 - Special Conditions: Bombardier Inc. Models BD-700-2A12 and BD-700-2A13 airplanes; Operation Without Normal Electrical Power.
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. This action is effective on Bombardier on April 7, 2017. We must receive your comments by May 22, 2017. 14 CFR Part 25 Summary These special conditions are issued for the Bombardier Inc. (Bombardier) Models 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 design features are electrical and electronic systems that perform critical functions, the loss of which could be catastrophic to 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.
82 FR 16893 - Special Conditions: VT DRB Aviation Consultants, Boeing Model 777-200 Airplanes; Installation of an Airbag System in Shoulder Belts
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. This action is effective on VT DRB Aviation Consultants on April 7, 2017. We must receive your comments by May 22, 2017. 14 CFR Part 25 Summary These special conditions are issued for the Boeing Model 777-200 airplane. This airplane, as modified by VT DRB Aviation Consultants (VT DRB), 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 installed in shoulder belts. 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.
2017-03-17; vol. 82 # 51 - Friday, March 17, 2017 82 FR 14111 - Special Conditions: L-3 Communications Integrated Systems; Boeing Model 747-8 Series Airplanes, Large Non-Structural Glass in the Passenger Compartment
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions. Effective April 17, 2017. 14 CFR Part 25 Summary These special conditions are issued for the Boeing Model 747-8 airplane. This airplane, as modified by L-3 Communications Integrated Systems (L-3 Communications), 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 the installation of large, non-structural glass panels in the cabin area of an executive interior occupied by passengers and crew. 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.
82 FR 14113 - Special Conditions: Textron Aviation Inc. Model 700 Airplane; Isolation of Airplane Electronic System Security Protection From Unauthorized Internal Access
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. This action is effective on Textron on March 17, 2017. We must receive your comments by May 1, 2017. 14 CFR Part 25 Summary These special conditions are issued for the Textron Aviation Inc. (Textron) Model 700 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 airplane electronic systems and networks that allow access, from aircraft internal sources ( e.g., wireless devices, Internet connectivity), to the airplane's previously isolated, internal, electronic components. 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.
82 FR 14115 - Special Conditions: The Boeing Company Model 787-10 Airplane; Aeroelastic Stability Requirements, Flaps-Up Vertical Modal-Suppression System
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions. Effective April 17, 2017. 14 CFR Part 25 Summary These special conditions are issued 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, which is in lieu of traditional methods of improving airplane flutter characteristics. 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.
82 FR 14117 - Definition with High-Speed-Protection System
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. This action is effective on Embraer on March 17, 2017. We must receive your comments by May 1, 2017. 14 CFR Part 25 Summary These special conditions are issued for the Embraer, S.A., (Embraer) Model ERJ 190-300 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 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.
82 FR 14119 - Special Conditions: Avionics Design Services Ltd., Textron Model 550/S550/560/560XL Airplanes; Rechargeable Lithium Batteries and Battery Systems
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. This action is effective on Textron on March 17, 2017. We must receive your comments by May 1, 2017. 14 CFR Part 25 Summary These special conditions are issued for the Textron Model 550/S550/560/560XL airplanes. These airplanes, as modified by Avionics Design Services Ltd., 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 and battery systems installed in the airplanes. 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.
82 FR 14122 - Special Conditions: Aerocon Engineering Company, Boeing Model 777-200 Airplane; Access Hatch Installed Between the Cabin and the Class C Cargo Compartment To Allow In-Flight Access to the Cargo Compartment
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions. Effective April 17, 2017. 14 CFR Part 25 Summary These special conditions are issued 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 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.
82 FR 14122 - Special Conditions: Embraer S.A. Model ERJ-170 Airplanes; Seats With Large, Non-Traditional, Non-Metallic Panels
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments; correction. The effective date of this correction is March 17, 2017 14 CFR Part 25 Summary This document corrects an error that appeared in Federal Docket no. FAA-2014-0078, Special Conditions no. 25-543-SC, which was published in the Federal Register on March 3, 2014 (79 FR 11679). The error is in the type-certificate number referenced in the Background and Type Certification Basis sections of the special conditions. It is being corrected herein.
82 FR 14125 - Special Conditions: Textron Aviation Inc. Model 700 Airplane; Airplane Electronic-System Security Protection From Unauthorized External Access
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. This action is effective on Textron on March 17, 2017. We must receive your comments by May 1, 2017. 14 CFR Part 25 Summary These special conditions are issued for the Textron Aviation Inc. (Textron) Model 700 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 airplane electronic systems and networks that allow access from external sources ( e.g., wireless devices, Internet connectivity) to the airplane's internal electronic components. 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.
82 FR 14126 - Special Conditions: Bombardier Inc., Model BD-700-2A12 and BD-700-2A13 Series Airplanes, Electronic Flight Control System: Lateral-Directional and Longitudinal Stability, and Low-Energy Awareness
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. This action is effective on Bombardier on March 17, 2017. We must receive your comments by May 1, 2017. 14 CFR Part 25 Summary These special conditions are issued for the Bombardier Inc. (Bombardier) Model BD-700-2A12 and BD-700-2A13 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 lateral-directional and longitudinal stability, and low-energy awareness, provided through an electronic flight-control system (EFCS). 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.
82 FR 14128 - Special Conditions: Lufthansa Technik AG; Boeing Model 747-8 Series Airplanes, Large Non-Structural Glass in the Passenger Compartment
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions. Effective April 17, 2017. 14 CFR Part 25 Summary These special conditions are issued for the Boeing Model 747-8 airplane. 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 the installation of large, non-structural glass panels in the cabin area of an executive interior occupied by passengers and crew. 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.
82 FR 14164 - Special Conditions: AmSafe; Non-Rechargeable Lithium Battery Installations
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Notice of proposed special conditions. Send your comments on or before April 17, 2017. 14 CFR Part 25 Summary This action proposes special conditions for a supplemental type certificate for installing an inflatable restraint system with non-rechargeable lithium batteries on seats in certain transport category airplanes. These airplanes, as modified by AmSafe, 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 non-rechargeable lithium battery. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. These proposed special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards.
2017-03-16; vol. 82 # 50 - Thursday, March 16, 2017 82 FR 13961 - Special Conditions: Embraer S.A., Model ERJ 190-300 Series Airplanes; Flight Envelope Protection: Pitch, Roll, and High-Speed Limiting Functions
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. This action is effective on Embraer S.A. on March 16, 2017. We must receive your comments by May 1, 2017. 14 CFR Part 25 Summary These 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 electronic flight control system that contains fly-by-wire control laws, including flight envelope protection functions that impose pitch-angle, bank-angle, and high-speed limits during normal operation. 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.
2017-02-08; vol. 82 # 25 - Wednesday, February 8, 2017 82 FR 9677 - Revisions to Operational Requirements for the Use of Enhanced Flight Vision Systems (EFVS) and to Pilot Compartment View Requirements for Vision Systems
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final rule; delay of effective date. The effective date of the rule amending 14 CFR parts 1, 23, 25, 27, 29, 61, 91, 121, 125, and 135 published at 81 FR 90126, December 13, 2016, is delayed until March 21, 2017, except for the amendments to §§ 61.66 (amendatory instruction no. 15), 91.175 (amendatory instruction no. 18), 91.1039 (amendatory instruction no. 23), 121.651 (amendatory instruction no. 27), 125.325 (amendatory instruction no. 33), 125.381 (amendatory instruction no. 35), and 135.225 (amendatory instruction no. 38), which are effective March 13, 2018. 14 CFR Parts 1, 23, 25, 27, 29, 61, 91, 121, 125, and 135 Summary On December 13, 2016, the Federal Aviation Administration (FAA) published a final rule to permit operators to use an enhanced flight vision system in lieu of natural vision to continue descending from 100 feet above the touchdown zone elevation to the runway and to land on certain straight-in instrument approach procedures under instrument flight rules. The FAA is delaying the effective date of this final rule.
2017-01-09; vol. 82 # 5 - Monday, January 9, 2017 82 FR - Revisions to Operational Requirements for the Use of Enhanced Flight Vision Systems (EFVS) and to Pilot Compartment View Requirements for Vision Systems
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration 14 CFR Parts 1, 23, 25, 27, 29, 61, 91, 121, 125, and 135 Summary
2016-12-13; vol. 81 # 239 - Tuesday, December 13, 2016 81 FR 90126 - Revisions to Operational Requirements for the Use of Enhanced Flight Vision Systems (EFVS) and to Pilot Compartment View Requirements for Vision Systems
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final rule. The final rule is effective March 13, 2017, except for the amendments to §§ 61.66 (amendatory instruction no. 15), 91.175 (amendatory instruction no. 18), 91.1039 (amendatory instruction no. 23), 121.651 (amendatory instruction no. 27), 125.325 (amendatory instruction no. 33), 125.381 (amendatory instruction no. 35), and 135.225 (amendatory instruction no. 38), which are effective March 13, 2018. 14 CFR Parts 1, 23, 25, 27, 29, 61, 91, 121, 125, and 135 Summary Prior to this final rule, persons could only use an Enhanced Flight Vision System (EFVS) in lieu of natural vision to descend below the decision altitude, decision height, or minimum descent altitude (DA/DH or MDA) down to 100 feet above the touchdown zone elevation (TDZE) using certain straight-in landing instrument approach procedures (IAPs). This final rule permits operators to use an EFVS in lieu of natural vision to continue descending from 100 feet above the TDZE to the runway and to land on certain straight-in IAPs under instrument flight rules (IFR). This final rule also revises and relocates the regulations that permit operators to use an EFVS in lieu of natural vision to descend to 100 feet above the TDZE using certain straight-in IAPs. Additionally, this final rule addresses provisions that permit operators who conduct EFVS operations under parts 121, 125, or 135 to use EFVS-equipped aircraft to dispatch, release, or takeoff under IFR, and revises the regulations for those operators to initiate and continue an approach, when the destination airport weather is below authorized visibility minimums for the runway of intended landing. This final rule establishes pilot training and recent flight experience requirements for operators who use EFVS in lieu of natural vision to descend below the DA/DH or MDA. EFVS-equipped aircraft conducting operations to touchdown and rollout are required to meet additional airworthiness requirements. This final rule also revises pilot compartment view certification requirements for vision systems using a transparent display surface located in the pilot's outside field of view. The final rule takes advantage of advanced vision capabilities, thereby achieving the Next Generation Air Transportation System (NextGen) goals of increasing access, efficiency, and throughput at many airports when low visibility is the limiting factor. Additionally, it enables EFVS operations in reduced visibilities on a greater number of approach procedure types while maintaining an equivalent level of safety.
2016-12-07; vol. 81 # 235 - Wednesday, December 7, 2016 81 FR 88098 - Special Conditions: Embraer S.A., Model ERJ 190-300 Series Airplanes; Landing Pitchover Condition
GPO FDSys XML | Text Additional Documents 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 Summary These 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, 2016 81 FR 86910 - Special Conditions: Gulfstream Aerospace Corporation Model GVII-G500 Airplanes; Electronic Flight-Control-System Mode Annunciation
GPO FDSys XML | Text Additional Documents 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 Summary These 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, 2016 81 FR 74347 - Special Conditions: Bombardier Inc. Models BD-700-2A12 and BD-700-2A13 Airplanes; Fuselage Post-Crash Fire Survivability
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Notice of proposed special conditions. Send your comments on or before December 12, 2016. 14 CFR Part 25 Summary This 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.
81 FR 74348 - Special Conditions: Bombardier Inc. Model BD-700-2A12 and BD-700-2A13 Airplanes; Fuselage In-Flight Fire Safety and Flammability Resistance of Aluminum-Lithium Material
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Notice of proposed special conditions. Send your comments on or before December 12, 2016. 14 CFR Part 25 Summary This 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.
81 FR 74350 - Special Conditions: Aerocon Engineering Company, Boeing Model 777-200 Airplane; Access Hatch Installed Between the Cabin and the Class C Cargo Compartment To Allow In-Flight Access to the Cargo Compartment
GPO FDSys XML | Text Additional Documents DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Notice of proposed special conditions. Send your comments on or before December 12, 2016. 14 CFR Part 25 Summary This 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, 2016 81 FR 71356 - Special Conditions: Learjet Model 45 Series Airplanes; Aircraft Electronic System Security Protection From Unauthorized External Access
GPO FDSys XML | Text Additional Documents 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 Summary The 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.
81 FR 71357 - Special Conditions: Embraer S.A., Model ERJ 190-300 Series Airplanes; Electrical/Electronic Equipment Bay Fire Detection and Smoke Penetration
GPO FDSys XML | Text Additional Documents 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 Summary These 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.
81 FR 71357 - Special Conditions: Learjet Model 45 Series Airplanes; Isolation or Security Protection of the Aircraft Control Domain and the Airline Information Services Domain From the Passenger Services Domain
GPO FDSys XML | Text Additional Documents 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 Summary The 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, 2016 81 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
GPO FDSys XML | Text Additional Documents 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 Summary These 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.
Pages
