Boeing 787-8 - Page 299

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.13.11
ENGINE INOP
ADVISORY INFORMATION
Gear Down Landing Rate of Climb Available
Flaps 20
Flaps 30
TAT
(°C)
RATE OF CLIMB (FT/MIN)
PRESSURE ALTITUDE (FT)
-2000 0 2000 4000 6000 8000 10000
52 230 190
50 260 230 90
48 300 270 130 -10
46 340 310 170 30
44 370 340 210 70
42 410 380 240 110 -50
40 440 420 280 150 -10
38 480 460 320 180 30 -100
36 500 490 350 210 60 -70
34 510 530 390 250 100 -30 -200
32 510 550 420 280 130 0 -160
30 510 550 450 310 160 30 -130
20 520 560 480 390 290 170 10
10 540 580 490 390 300 190 70
0 550 590 500 410 300 200 70
-20 580 620 530 430 320 210 80
-40 620 660 560 450 340 230 90
Rate of climb capability shown is valid for 370000 lb, gear down at VREF20+5.
Decrease rate of climb 40 ft/min per 10000 lb greater than 370000 lb.
Increase rate of climb 60 ft/min per 10000 lb less than 370000 lb.
TAT
(°C)
RATE OF CLIMB (FT/MIN)
PRESSURE ALTITUDE (FT)
-2000 0 2000 4000 6000 8000 10000
52 50 0
50 80 40 -100
48 120 80 -60 -200
46 150 120 -20 -160
44 190 160 20 -120
42 220 190 50 -80 -240
40 260 230 90 -50 -200
38 290 260 120 -10 -170 -300
36 320 300 160 20 -130 -260
34 320 340 190 50 -100 -230 -390
32 320 360 220 80 -70 -200 -360
30 320 360 250 110 -40 -170 -330
20 330 370 270 180 80 -40 -200
10 340 380 280 190 90 -10 -140
0 350 390 290 200 90 -10 -140
-20 370 410 310 210 100 -10 -140
-40 400 440 330 220 110 0 -140
Rate of climb capability shown is valid for 370000 lb, gear down at VREF30+5.
Decrease rate of climb 40 ft/min per 10000 lb greater than 370000 lb.
Increase rate of climb 60 ft/min per 10000 lb less than 370000 lb.
February 15, 2010