![]() ![]() (4 ) Other general procedural instructions including procedures for system testing during ground running, symmetry checks, weighing and determining the center of gravity, lifting and shoring, and storage limitations. (3 ) Information describing the order and method of removing and replacing products and parts with any necessary precautions to be taken. (2 ) Troubleshooting information describing probable malfunctions, how to recognize those malfunctions, and the remedial action for those malfunctions. ![]() In addition, the applicant must include an inspection program that includes the frequency and extent of the inspections necessary to provide for the continued airworthiness of the airplane. ![]() The recommended overhaul periods and necessary cross reference to the Airworthiness Limitations section of the manual must also be included. However, the applicant may refer to an accessory, instrument, or equipment manufacturer as the source of this information if the applicant shows that the item has an exceptionally high degree of complexity requiring specialized maintenance techniques, test equipment, or expertise. (1 ) Scheduling information for each part of the airplane and its engines, auxiliary power units, propellers, accessories, instruments, and equipment that provides the recommended periods at which they should be cleaned, inspected, adjusted, tested, and lubricated, and the degree of inspection, the applicable wear tolerances, and work recommended at these periods. (4 ) Servicing information that covers details regarding servicing points, capacities of tanks, reservoirs, types of fluids to be used, pressures applicable to the various systems, location of access panels for inspection and servicing, locations of lubrication points, lubricants to be used, equipment required for servicing, tow instructions and limitations, mooring, jacking, and leveling information. (3 ) Basic control and operation information describing how the airplane components and systems are controlled and how they operate, including any special procedures and limitations that apply. (2 ) A description of the airplane and its systems and installations including its engines, propellers, and appliances. (1 ) Introduction information that includes an explanation of the airplane's features and data to the extent necessary for maintenance or preventive maintenance. (a ) Airplane maintenance manual or section. The Instructions for Continued Airworthiness must contain the following manuals or sections and information: The contents of the manual or manuals must be prepared in the English language. (b ) The format of the manual or manuals must provide for a practical arrangement. (a ) The Instructions for Continued Airworthiness must be in the form of a manual or manuals as appropriate for the quantity of data to be provided. (c ) The applicant must submit to the FAA a program to show how changes to the Instructions for Continued Airworthiness made by the applicant or by the manufacturers of products and appliances installed in the airplane will be distributed. If Instructions for Continued Airworthiness are not supplied by the manufacturer of an appliance or product installed in the airplane, the Instructions for Continued Airworthiness for the airplane must include the information essential to the continued airworthiness of the airplane. (b ) The Instructions for Continued Airworthiness for each airplane must include the Instructions for Continued Airworthiness for each engine and propeller (hereinafter designated “products”), for each appliance required by this chapter, and any required information relating to the interface of those appliances and products with the airplane. (a ) This appendix specifies requirements for the preparation of Instructions for Continued Airworthiness as required by this part. Instrument markings, control markings, and placards.įlight, navigation, and powerplant instruments.Īppendix A to Part 23-Instructions for Continued Airworthiness System power generation, storage, and distribution.įlightcrew Interface and Other Information High-intensity Radiated Fields (HIRF) protection. Powerplant induction and exhaust systems.Įlectrical and electronic system lightning protection. Powerplant installation hazard assessment. Performance and flight characteristics requirements for flight in icing conditions.įire protection in designated fire zones and adjacent areas.Īutomatic power or thrust control systems. Vibration, buffeting, and high-speed characteristics. Ground and water handling characteristics. Stall characteristics, stall warning, and spins. Instructions for continued airworthiness.Ĭertification of normal category airplanes. Airworthiness Standards: Normal Category Airplanes
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