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D615Z003 Boeing Proprietary MAN.2.7
Go–Around and Missed Approach
Note: For a manual go-around:
After planned flaps set and at or
• rotate manually
• select or verify go-around thrust
• engage autopilot as needed
above flap maneuvering speed
• Select FLCH or VNAV
• Verify climb thrust
(CON thrust, 1 engine)
• Verify altitude capture
• Do the After Takeoff checklist
Above 400 feet RA
• Select roll mode
• Verify missed
approach altitude set
• Verify route tracking
Acceleration height
• Select speed for planned flap setting
• Retract flaps on schedule
Initiation
• Push TO/GA, flaps 20
(flaps 5 or 20, 1 engine)
• Verify go-around attitude
• Verify or adjust thrust as needed
• Positive rate of climb - gear up
December 15, 2006
787 Flight Crew Operations Manual
Maneuvers -
Flight Patterns
Copyright © The Boeing Company. See title page for details.
MAN.2.8 D615Z003 Boeing Proprietary
Intentionally
Blank
December 15, 2006
787 Flight Crew Operations Manual
Performance Inflight A Chapter PI
Table of Contents Section A
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary PI.TOC.A.1
PI.A Performance Inflight A-Table of Contents
Advisory Information . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PI.A10.1
Flight With Unreliable Airspeed / Turbulent Air
Penetration . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PI.A10.1
Normal Configuration Landing Distance . . . . . . . . . . . . . . PI.A10.4
Non-Normal Configuration Landing Distance . . . . . . . . . . PI.A10.7
Recommended Brake Cooling Schedule . . . . . . . . . . . . . PI.A10.11
Landing Climb Limit Weight . . . . . . . . . . . . . . . . . . . . . . PI.A10.13
Engine Inoperative . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PI.A11.1
Initial Max Continuous EPR . . . . . . . . . . . . . . . . . . . . . . . . PI.A11.1
Max Continuous EPR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PI.A11.2
Driftdown Speed/Level Off Altitude . . . . . . . . . . . . . . . . . PI.A11.5
Driftdown/LRC Cruise Range Capability . . . . . . . . . . . . . PI.A11.6
Long Range Cruise Altitude Capability . . . . . . . . . . . . . . . PI.A11.7
Long Range Cruise Control . . . . . . . . . . . . . . . . . . . . . . . . PI.A11.8
Long Range Cruise Diversion Fuel and Time . . . . . . . . . . PI.A11.9
Holding . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PI.A11.10
777-200ER TRENT892 LB FAA
Flight With Unreliable Airspeed /
Turbulent Air Penetration . . . . . . . . . . . . . . . . . . . . . . . . . . PI.A12.1
Max Climb EPR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PI.A12.1
VREF . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PI.A12.1
December 15, 2006
787 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
PI.TOC.A.2 D615Z003 Boeing Proprietary
Performance Inflight A -
Table of Contents
Intentionally
Blank
December 15, 2006
787 Flight Crew Operations Manual
Performance Inflight A Chapter PI
Advisory Information Section A10
777-200ER/TRENT892
FAA
Category A Brakes
FAST-Doc PI/PD Template 9/1/99
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary PI.A10.1
PI.A10 Performance Inflight AA-ADdVvisIoSryO IRnfYorm IaNtiFonORMATION
Advisory Information 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
PRESSURE ALTITUDE (FT)
(SPEED)
WEIGHT (1000 LB)
350 450 550 650
40000
(.82M)
PITCH ATT 4.0 3.5
V/S (FT/MIN) 1600 700
30000
(280 KIAS)
PITCH ATT 4.5 4.5 4.0 4.5
V/S (FT/MIN) 2300 1600 1000 500
20000
(270 KIAS)
PITCH ATT 7.5 6.5 6.5 6.5
V/S (FT/MIN) 3700 2700 1900 1400
10000
(270 KIAS)
PITCH ATT 10.0 8.5 8.0 8.0
V/S (FT/MIN) 4500 3300 2500 1900
SEA LEVEL
(270 KIAS)
PITCH ATT 12.5 10.5 9.5 9.0
V/S (FT/MIN) 5100 3800 3000 2300
PRESSURE ALTITUDE (FT)
(SPEED)
WEIGHT (1000 LB)
350 450 550 650
40000
(.82 M)
PITCH ATT 2.0 2.5
EPR 1.127 1.267
(Alt Mode %N1) (78.9) (84.0)
35000
(280 KIAS)
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