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EFD: RUNWAY 9000' T38 WT=12.5kL6 TEMP 90 Degrees > assume FLAPS= 60% WIND 0 RCR=23 ALT SL TAKE-OFF FACTOR = 3.05 TAKE-OFF DISTANCE = 3450' CRITICAL FIELD LENGTH = 6200' (CFL < 17/35) CRITICAL ENGINE FAILURE SPEED = 130K Acceleration check speed = 125K (@ 1500') SETO = 168K refusal speed = 152K decision speed = ~0 => at EFD, could make a single engine takeoff from brake release [[diagram]] [[right margin]] any place after here arcraft can lose an engine and takeoff [where do you find Runway length?] [[/right margin]]