Instruction manual for installing and operating the engine.

CFR · 2024-01-01 · US · Title 14

Each applicant must prepare and make available to the Administrator (a) (2) The location and description of engine connections to be attached to accessories, pipes, wires, cables, ducts, and cowling. (3) An outline drawing of the engine including overall dimensions. (4) A definition of the physical and functional interfaces with the aircraft and aircraft equipment, including the propeller when applicable. (5) Where an engine system relies on components that are not part of the engine type design, the interface conditions and reliability requirements for those components upon which engine type certification is based must be specified in the engine installation instructions directly or by reference to appropriate documentation. (6) A list of the instruments necessary for control of the engine, including the overall limits of accuracy and transient response required of such instruments for control of the operation of the engine, must also be stated so that the suitability of the instruments as installed may be assessed. (b) (2) The power or thrust ratings and procedures for correcting for nonstandard atmosphere. (3) The recommended procedures, under normal and extreme ambient conditions for— (i) Starting; (ii) Operating on the ground; and (iii) Operating during flight. (4) For rotorcraft engines having one or more OEI ratings, applicants must provide data on engine performance characteristics and variability to enable the aircraft manufacturer to establish aircraft power assuran

official document · source cfr-2024 · id 14:§ 33.5