787 Flight Crew Operations Manual
DO NOT USE FOR FLIGHT
Performance Inflight
General
787-8/
FAA
Category A Brakes
Copyright © The Boeing Company. See title page for details.
D615Z003-TBC PI.10.21
Flight With Unreliable Airspeed / Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
Climb
Flaps Up, Set Max Climb Thrust
Cruise
Flaps Up, Set Thrust for Level Flight
Descent
Flaps Up, Set Idle Thrust
PRESSURE ALTITUDE (FT)
(SPEED)
WEIGHT (1000 LB)
300 350 400 450 500
40000
(.85M)
PITCH ATT 3.5 3.5 3.5 3.5
V/S (FT/MIN) 1300 1000 600 100
30000
(310 KIAS)
PITCH ATT 3.5 3.5 3.5 3.5 3.5
V/S (FT/MIN) 2000 1700 1300 1100 900
20000
(290 KIAS)
PITCH ATT 6.5 6.0 6.0 6.0 6.0
V/S (FT/MIN) 3500 2900 2400 2000 1700
10000
(290 KIAS)
PITCH ATT 9.0 8.5 8.0 7.5 7.5
V/S (FT/MIN) 4600 3900 3300 2900 2500
SEA LEVEL
(290 KIAS)
PITCH ATT 11.5 10.5 9.5 9.0 9.0
V/S (FT/MIN) 5400 4500 3900 3400 3000
PRESSURE ALTITUDE (FT)
(SPEED)
WEIGHT (1000 LB)
300 350 400 450 500
40000
(.85M)
PITCH ATT 1.5 1.5 2.0
TPR 64.8 69.0 77.0
35000
(310 KIAS)
PITCH ATT 1.0 1.0 1.5 2.0 2.0
TPR 58.8 62.0 64.9 68.5 74.0
30000
(310 KIAS)
PITCH ATT 0.5 1.0 1.5 1.5 2.0
TPR 54.1 56.0 58.5 61.1 63.9
25000
(310 KIAS)
PITCH ATT 0.5 1.0 1.5 1.5 2.0
TPR 47.7 48.9 50.7 52.8 55.1
20000
(290 KIAS)
PITCH ATT 1.0 1.5 2.0 2.5 2.5
TPR 39.4 40.9 42.6 44.7 47.1
15000
(290 KIAS)
PITCH ATT 1.0 1.5 2.0 2.5 3.0
TPR 35.1 36.3 37.6 39.3 41.1
PRESSURE ALTITUDE (FT)
(SPEED)
WEIGHT (1000 LB)
300 350 400 450 500
40000
(.85M)
PITCH ATT -2.0 -1.0 -1.0 -0.5 0.0
V/S (FT/MIN) -2700 -2500 -2500 -2600 -2900
30000
(310 KIAS)
PITCH ATT -2.5 -2.0 -1.5 -1.0 -0.5
V/S (FT/MIN) -2600 -2300 -2100 -2000 -1900
20000
(290 KIAS)
PITCH ATT -2.0 -1.5 -0.5 0.0 0.5
V/S (FT/MIN) -2100 -1900 -1800 -1700 -1600
10000
(290 KIAS)
PITCH ATT -2.5 -1.5 -1.0 -0.5 0.5
V/S (FT/MIN) -2000 -1800 -1600 -1500 -1500
SEA LEVEL
(290 KIAS)
PITCH ATT -2.5 -1.5 -1.0 -0.5 0.0
V/S (FT/MIN) -1800 -1600 -1500 -1400 -1300
February 15, 2010
General