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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]]