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10) 5 sec. allowed for A/B light on takeoff. 16) S/E G/A @ VCV 〜1000# Rem.; T= [[strikethrough]]50, 70[[/strikethrough]]60 [[strikethrough]]10- 20°C[[/strikethrough]] 15°C decrease thrust available 〜10% for 3000' Altitude @ 1000# => 12,5000 - 3,800 + 1,000 = 9,700# A/C Normal T/O = 139 KIAS = SETO TOF 3.1-3.4 TD A/S = 130 KIAS Reconstruct => touchdown S/E @ 〜140 KIAS, roll + slow to 〜130K, add MIL thrust good eng. accel to 〜135-140 + take off. 9700# 140 KIAS - thrust required ≅ 2300+ lbs. 135 KIAS ≅ 2500 lbs [[right margin, circled]]FA7-3[[/right margin]] [[right margin, circled]]A7-5[[/right margin]] thrust available [[3 column table]] |(SL)|MIL|MAX| |140K|[[strikethrough]]2000.2100 10-20°C[[/strikethrough]] 2050|3030| |135K|2050|3020| @3000' PA [[6 column table]] |---|THRUST REQ|THRUST AVAIL MIL|THRUST AVAIL MAX|MARGIN MIL|MARGIN MAX| |140K|2300|1850|2730|-450|+430| |140K|2500|1850|2720|-650|+220| |140K|2000|1850|2740|-150|+740| [[arrow pointing to -150]]
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