14 CFR 23, Subpart B - Flight
- — General
- § 23.21 — Proof of compliance.
- § 23.23 — Load distribution limits.
- § 23.25 — Weight limits.
- § 23.29 — Empty weight and corresponding center of gravity.
- § 23.31 — Removable ballast.
- § 23.33 — Propeller speed and pitch limits.
- — Performance
- § 23.45 — General.
- § 23.49 — Stalling period.
- § 23.51 — Takeoff speeds.
- § 23.53 — Takeoff performance.
- § 23.55 — Accelerate-stop distance.
- § 23.57 — Takeoff path.
- § 23.59 — Takeoff distance and takeoff run.
- § 23.61 — Takeoff flight path.
- § 23.63 — Climb: General.
- § 23.65 — Climb: All engines operating.
- § 23.66 — Takeoff climb: One-engine inoperative.
- § 23.67 — Climb: One engine inoperative.
- § 23.69 — Enroute climb/descent.
- § 23.71 — Glide: Single-engine airplanes.
- § 23.73 — Reference landing approach speed.
- § 23.75 — Landing distance.
- § 23.77 — Balked landing.
- — Flight Characteristics
- § 23.141 — General.
- — Controllability and Maneuverability
- § 23.143 — General.
- § 23.145 — Longitudinal control.
- § 23.147 — Directional and lateral control.
- § 23.149 — Minimum control speed.
- § 23.151 — Acrobatic maneuvers.
- § 23.153 — Control during landings.
- § 23.155 — Elevator control force in maneuvers.
- § 23.157 — Rate of roll.
- — Trim
- § 23.161 — Trim.
- — Stability
- § 23.171 — General.
- § 23.173 — Static longitudinal stability.
- § 23.175 — Demonstration of static longitudinal stability.
- § 23.177 — Static directional and lateral stability.
- § 23.181 — Dynamic stability.
- — Stalls
- § 23.201 — Wings level stall.
- § 23.203 — Turning flight and accelerated turning stalls.
- § 23.207 — Stall warning.
- — Spinning
- § 23.221 — Spinning.
- — Ground and Water Handling Characteristics
- § 23.231 — Longitudinal stability and control.
- § 23.233 — Directional stability and control.
- § 23.235 — Operation on unpaved surfaces.
- § 23.237 — Operation on water.
- § 23.239 — Spray characteristics.
- — Miscellaneous Flight Requirements
- § 23.251 — Vibration and buffeting.
- § 23.253 — High speed characteristics.
Title 14 published on 2013-01-01
The following are only the Rules published in the Federal Register after the published date of Title 14.
For a complete list of all Rules, Proposed Rules, and Notices view the Rulemaking tab.
GPO FDSys XML | Text type regulations.gov FR Doc. 2013-03296 RIN Docket No. FAA-2012-0485 Special Conditions No. 23-258A-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Amended final special conditions; request for comments. This final rule is effective February 13, 2013, and is applicable beginning February 6, 2013. Comments must be received by March 15, 2013. 14 CFR Part 23 This action amends special conditions No. 23-258-SC, issued on July 13, 2012, for the Tamarack Aerospace Group's modification to the Cirrus Model SR22 airplane. This amendment clarifies the intent of two requirements: The requirement for reporting of load alleviation system failures (see paragraph (c) under Loads, Probability of Failure of Load Alleviation System) and the requirement for consideration of limit loads with an unannunciated load alleviation system failure (see paragraph (b) under Factor of Safety, Load Alleviation Systems). This airplane as modified by Tamarack will have a novel or unusual design feature(s) associated with Tamarack Aerospace Group's modification. The design change will install winglets and an Active Technology Load Alleviation System (ATLAS). The addition of the ATLAS mitigates the negative effects of the winglets by effectively aerodynamically turning off the winglet under limit gust and maneuver loads. This is accomplished by measuring the aircraft loading and moving a small aileron-like device called a Tamarack Active Control Surface (TACS). The TACS movement reduces lift at the tip of the wing, resulting in the wing center of pressure moving inboard, thus reducing bending stresses along the wing span. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. These final 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. Additionally, this amendment corrects the issue date of special condition No. 23-258-SC to July 13, 2012.
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.
§ 106 - Federal Aviation Administration
§ 40113 - Administrative
§ 44701 - General requirements
§ 44702 - Issuance of certificates
§ 44704 - Type certificates, production certificates, airworthiness certificates, and design organization certificates
Title 14 published on 2013-01-01
The following are ALL rules, proposed rules, and notices (chronologically) published in the Federal Register relating to 14 CFR 23 after this date.
GPO FDSys XML | Text type regulations.gov FR Doc. 2013-11731 RIN Docket No. FAA-2013-0413 Special Conditions No. 23-259-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. The effective date of these special conditions is May 8, 2013. We must receive your comments by June 17, 2013. 14 CFR Part 23 These special conditions are issued for the Cessna Aircraft Company (Cessna) Model J182T airplane. This airplane will have a novel or unusual design feature(s) associated with the installation of an aircraft diesel engine (ADE). 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.
GPO FDSys XML | Text type regulations.gov FR Doc. 2013-03296 RIN Docket No. FAA-2012-0485 Special Conditions No. 23-258A-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Amended final special conditions; request for comments. This final rule is effective February 13, 2013, and is applicable beginning February 6, 2013. Comments must be received by March 15, 2013. 14 CFR Part 23 This action amends special conditions No. 23-258-SC, issued on July 13, 2012, for the Tamarack Aerospace Group's modification to the Cirrus Model SR22 airplane. This amendment clarifies the intent of two requirements: The requirement for reporting of load alleviation system failures (see paragraph (c) under Loads, Probability of Failure of Load Alleviation System) and the requirement for consideration of limit loads with an unannunciated load alleviation system failure (see paragraph (b) under Factor of Safety, Load Alleviation Systems). This airplane as modified by Tamarack will have a novel or unusual design feature(s) associated with Tamarack Aerospace Group's modification. The design change will install winglets and an Active Technology Load Alleviation System (ATLAS). The addition of the ATLAS mitigates the negative effects of the winglets by effectively aerodynamically turning off the winglet under limit gust and maneuver loads. This is accomplished by measuring the aircraft loading and moving a small aileron-like device called a Tamarack Active Control Surface (TACS). The TACS movement reduces lift at the tip of the wing, resulting in the wing center of pressure moving inboard, thus reducing bending stresses along the wing span. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. These final 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. Additionally, this amendment corrects the issue date of special condition No. 23-258-SC to July 13, 2012.