{"id":668284,"date":"2024-11-06T03:21:15","date_gmt":"2024-11-06T03:21:15","guid":{"rendered":"https:\/\/pdfstandards.shop\/product\/uncategorized\/sae-air-1678b2011\/"},"modified":"2024-11-06T03:21:15","modified_gmt":"2024-11-06T03:21:15","slug":"sae-air-1678b2011","status":"publish","type":"product","link":"https:\/\/pdfstandards.shop\/product\/publishers\/sae\/sae-air-1678b2011\/","title":{"rendered":"SAE AIR 1678B:2011"},"content":{"rendered":"
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This document defines and illustrates the process for determination of uncertainty of turbofan and turbojet engine in-flight thrust and other measured in-flight performance parameters. The reasons for requiring this information, as specified in the E-33 Charter, are:<\/div>\n