14 C.F.R. PART 23--AIRWORTHINESS STANDARDS: NORMAL, UTILITY, ACROBATIC, AND COMMUTER CATEGORY AIRPLANES
TITLE 14--Aeronautics and Space
CHAPTER I--FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION
SUBCHAPTER C--AIRCRAFT
PART 23--AIRWORTHINESS STANDARDS: NORMAL, UTILITY, ACROBATIC, AND COMMUTER CATEGORY AIRPLANES
Subpart A--GENERAL
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Special retroactive requirements.
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Subpart B--FLIGHT
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Load distribution limits.
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Empty weight and corresponding center of gravity.
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Propeller speed and pitch limits.
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Accelerate-stop distance.
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Takeoff distance and takeoff run.
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Climb: All engines operating.
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Takeoff climb: One-engine inoperative.
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Climb: One engine inoperative.
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Glide: Single-engine airplanes.
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Reference landing approach speed.
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Directional and lateral control.
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Elevator control force in maneuvers.
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Static longitudinal stability.
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Demonstration of static longitudinal stability.
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Static directional and lateral stability.
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Turning flight and accelerated turning stalls.
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Longitudinal stability and control.
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Directional stability and control.
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Operation on unpaved surfaces.
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High speed characteristics.
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Subpart C--STRUCTURE
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Canard or tandem wing configurations.
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Strength and deformation.
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Symmetrical flight conditions.
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Limit maneuvering load factors.
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Unsymmetrical flight conditions.
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Side load on engine mount.
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Unsymmetrical loads due to engine failure.
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Gyroscopic and aerodynamic loads.
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Loads parallel to hinge line.
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Limit control forces and torques.
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Secondary control system.
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Outboard fins or winglets.
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Ground load conditions and assumptions.
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Landing gear arrangement.
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Level landing conditions.
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Tail down landing conditions.
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One-wheel landing conditions.
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Supplementary conditions for tail wheels.
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Supplementary conditions for nose wheels.
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Supplementary conditions for skiplanes.
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Ground load; unsymmetrical loads on multiple-wheel units.
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Design weights and center of gravity positions.
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Hull and main float load factors.
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Hull and main float landing conditions.
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Hull and main float takeoff condition.
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Hull and main float bottom pressures.
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Emergency landing dynamic conditions.
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Metallic pressurized cabin structures.
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Metallic wing, empennage, and associated structures.
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Damage tolerance and fatigue evaluation of structure.
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Metallic damage tolerance and fatigue evaluation of commuter category airplanes.
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Inspections and other procedures.
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Subpart D--DESIGN AND CONSTRUCTION
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Materials and workmanship.
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Accessibility provisions.
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Material strength properties and design values.
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Stability augmentation and automatic and power-operated systems.
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Artificial stall barrier system.
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Wing flap position indicator.
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Ground load dynamic tests.
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Reserve energy absorption drop test.
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Landing gear extension and retraction system.
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Nose/tail wheel steering.
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Motion and effect of cockpit controls.
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Cockpit control knob shape.
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Seats, berths, litters, safety belts, and shoulder harnesses.
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Baggage and cargo compartments.
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Passenger information signs.
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Flightcrew emergency exits.
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Passenger and crew compartment interiors.
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Cargo and baggage compartment fire protection.
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Combustion heater fire protection.
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Flammable fluid fire protection.
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Fire protection of flight controls, engine mounts, and other flight structure.
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Electrical bonding and protection against lightning and static electricity.
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Subpart E--POWERPLANT
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Automatic power reserve system.
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Engine installation ice protection.
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Turbojet and turbofan engine thrust reverser systems tests.
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Turbopropeller-drag limiting systems.
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Powerplant operating characteristics.
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Fuel system independence.
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Fuel system lightning protection.
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Flow between interconnected tanks.
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Fuel system hot weather operation.
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Fuel tank expansion space.
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Fuel tank filler connection.
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Fuel tank vents and carburetor vapor vents.
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Pressure fueling systems.
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Fuel system lines and fittings.
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Fuel valves and controls.
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Propeller feathering system.
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Cooling test procedures for turbine engine powered airplanes.
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Cooling test procedures for reciprocating engine powered airplanes.
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Induction system icing protection.
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Carburetor deicing fluid flow rate.
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Carburetor deicing fluid system capacity.
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Carburetor deicing fluid system detail design.
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Induction air preheater design.
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Induction system screens.
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Induction system filters.
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Turbocharger bleed air system.
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Turbine engine bleed air system.
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Powerplant controls: General.
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Auxiliary power unit controls.
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Propeller speed and pitch controls.
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Propeller feathering controls.
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Turbine engine reverse thrust and propeller pitch settings below the flight regime.
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Carburetor air temperature controls.
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Designated fire zones; regions included.
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Nacelle areas behind firewalls.
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Lines, fittings, and components.
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Engine accessory compartment diaphragm.
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Fire extinguishing systems.
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Fire extinguishing agents.
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Extinguishing agent containers.
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Fire extinguishing systems materials.
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Subpart F--EQUIPMENT
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Function and installation.
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Flight and navigation instruments.
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Equipment, systems, and installations.
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Electronic display instrument systems.
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Arrangement and visibility.
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Warning, caution, and advisory lights.
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Airspeed indicating system.
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Pitot heat indication systems.
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Magnetic direction indicator.
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Instruments using a power source.
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Powerplant instruments installation.
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Storage battery design and installation.
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Circuit protective devices.
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Electrical system fire protection.
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Master switch arrangement.
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Electric cables and equipment.
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Position light system installation.
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Position light system dihedral angles.
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Position light distribution and intensities.
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Minimum intensities in the horizontal plane of position lights.
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Minimum intensities in any vertical plane of position lights.
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Maximum intensities in overlapping beams of position lights.
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Anticollision light system.
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Pneumatic de-icer boot system.
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Accessories for multiengine airplanes.
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Pressurization and pneumatic systems.
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Oxygen equipment and supply.
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Minimum mass flow of supplemental oxygen.
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Oxygen distribution system.
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Equipment standards for oxygen dispensing units.
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Means for determining use of oxygen.
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Chemical oxygen generators.
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Fire protection for oxygen equipment.
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Protection of oxygen equipment from rupture.
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Equipment containing high energy rotors.
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Subpart G--OPERATING LIMITATIONS AND INFORMATION
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Operating maneuvering speed.
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Weight and center of gravity.
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Auxiliary power unit limitations.
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Maximum passenger seating configuration.
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Maximum operating altitude.
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Instructions for continued Airworthiness.
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Instrument markings: General.
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Magnetic direction indicator.
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Powerplant and auxiliary power unit instruments.
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Miscellaneous markings and placards.
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Operating limitations placard.
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