![]() ![]() ![]() During the endurance test the engine power and the crankshaft rotational speed must be kept within ☓ percent of the rated values. The runs must be made in the order found appropriate by the Administrator for the particular engine being tested. Each engine must be subjected to an endurance test that includes a total of 150 hours of operation (except as provided in paragraph (e)(1)(iii) of this section) and, depending upon the type and contemplated use of the engine, consists of one of the series of runs specified in paragraphs (b) through (e) of this section, as applicable. Mixed Phase and Ice Crystal Icing Envelope (Deep Convective Clouds) Special Requirements: Turbine Aircraft Enginesĭesign and test requirements for Early ETOPS eligibility.Ĭertification Standard Atmospheric Concentrations of Rain and Hail Turbine, compressor, fan, and turbosupercharger rotor overspeed.ĭesign and Construction Reciprocating Aircraft Enginesīlock Tests Reciprocating Aircraft Enginesĭesign and Construction Turbine Aircraft Enginesīlade containment and rotor unbalance tests.Įngine tests in auxiliary power unit (APU) mode. Selection of engine power and thrust ratings.Įngine mounting attachments and structure. Instruction manual for installing and operating the engine.Įngine ratings and operating limitations. Instructions for Continued Airworthiness. Airworthiness Standards: Aircraft Engines ![]()
0 Comments
Leave a Reply. |
AuthorWrite something about yourself. No need to be fancy, just an overview. ArchivesCategories |