Boeing 787-8 - Page 295

787 Flight Crew Operations Manual
DO NOT USE FOR FLIGHT
Performance Inflight
Engine Inoperative
787-8/
FAA
Category A Brakes
Copyright © The Boeing Company. See title page for details.
D615Z003-TBC PI.13.7
ENGINE INOP
MAX CONTINUOUS THRUST
Long Range Cruise Altitude Capability
100 ft/min residual rate of climb
WEIGHT
(1000 LB)
PRESSURE ALTITUDE (FT)
ISA + 10°C
& BELOW
ISA + 15°C ISA + 20°C
500 16800 14200 9300
480 18300 16300 12200
460 19700 18300 14800
440 21000 19800 17500
420 22300 21000 19400
400 23700 22100 20800
380 25100 23300 21900
360 26400 24500 23200
340 27500 25900 24500
320 28600 27300 26000
300 29900 28800 27600
280 31600 30500 29300
260 33400 32400 31100
240 35200 34400 33200
220 36900 36200 35300
With anti-ice on, no altitude capability adjustment is required.
February 15, 2010