Boeing 787-8 - Page 207

787 Flight Crew Operations Manual
DO NOT USE FOR FLIGHT
Performance Dispatch Chapter PD
Enroute Section 11
787-8/
FAA
Category A Brakes
Copyright © The Boeing Company. See title page for details.
D615Z003-TBC PD.11.1
PD.11 Performance Dispatch-Enroute
Enroute
Long Range Cruise Maximum Operating Altitude
Max Climb Thrust
ISA + 10°C and Below
ISA + 15°C
ISA + 20°C
WEIGHT
(1000 LB)
OPTIMUM
ALT (FT)
TAT
(°C)
MARGIN TO INITIAL BUFFET 'G' (BANK ANGLE)
1.30 (39°) 1.40 (44°) 1.50 (48°)
500 35000 -11 37100 35700 34300
480 35900 -13 38000 36500 35100
460 36700 -14 38900 37400 36000
440 37700 -14 39600 38100 36700
420 38600 -14 40200 38700 37200
400 39600 -14 40700 39200 37800
380 40700 -14 41400 39900 38400
360 41800 -14 42300 40700 39200
340 43000 -14 43100 41600 40100
320 43100 -14 43100 42500 41100
300 43100 -14 43100 43100 42100
280 43100 -14 43100 43100 43100
WEIGHT
(1000 LB)
OPTIMUM
ALT (FT)
TAT
(°C)
MARGIN TO INITIAL BUFFET 'G' (BANK ANGLE)
1.30 (39°) 1.40 (44°) 1.50 (48°)
500 35000 -6 37000* 35700 34300
480 35900 -8 37800* 36500 35100
460 36700 -8 38600* 37400 36000
440 37700 -8 39400* 38100 36700
420 38600 -8 40100* 38700 37200
400 39600 -8 40700 39200 37800
380 40700 -8 41400 39900 38400
360 41800 -8 42300 40700 39200
340 43000 -8 43100 41600 40100
320 43100 -8 43100 42500 41100
300 43100 -8 43100 43100 42100
280 43100 -8 43100 43100 43100
WEIGHT
(1000 LB)
OPTIMUM
ALT (FT)
TAT
(°C)
MARGIN TO INITIAL BUFFET 'G' (BANK ANGLE)
1.30 (39°) 1.40 (44°) 1.50 (48°)
500 35000 0 36300* 35700 34300
480 35900 -2 37000* 36500 35100
460 36700 -2 37800* 37400 36000
440 37700 -2 38600* 38100 36700
420 38600 -2 39300* 38700 37200
400 39600 -2 40000* 39200 37800
380 40700 -2 40800* 39900 38400
360 41800 -2 41700* 40700 39200
340 43000 -2 42500* 41600 40100
320 43100 -2 43100 42500 41100
300 43100 -2 43100 43100 42100
280 43100 -2 43100 43100 43100
*Denotes altitude thrust limited in level flight, 300 fpm residual rate of climb.
February 15, 2010
Enroute