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CFM International LEAP: Revision history


For any version listed below, click on its date to view it. For more help, see Help:Page history and Help:Edit summary. (cur) = difference from current version, (prev) = difference from preceding version, m = minor edit, → = section edit, ← = automatic edit summary

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  • curprev 14:1014:10, 7 June 2023 Marlonwood45 talk contribs 46,201 bytes +28 Source document mentions differing numbers for max. continuous thrust and max. take-off thrust within each family - before edit, only highest number was mentioned. For example the -1A29 has max. continuous thrust of 118.68 kN, whereas the table before claimed max. continuous thrust was 140.96 kN for the entire engine series. The most practical way, in my opinion, to show this variation would be to include a range within the table. undo Tag: Reverted

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