787 MEMORY ITEMS Flashcards
ABORTED ENGINE START L,R
1) FUEL CONTROL SWITCH (AFFECTED SIDE)….. CUTOFF
ENG AUTOSTART L,R
FUEL CONTROL SWITCH (affected side)……. CONFIRM……CUTOFF
DUAL ENG FAIL/STALL
FUEL CONTROL SWITCHES (BOTH) ….. CUTOFF THEN RUN
RAM AIR TURBINE SWITCH …. PUSH AND HOLD FOR 1 SEC
ENG LIMIT EXCEEDED, SURGE, OR STALL L,R
1) AT ARM SWITCH … CONFIRM AND OFF
2) THRUST LEVER … CONFIRM AND RETARD UNTIL EXCEED MESSAGE IS BLANK
OR THRUST LEVER IDLE
SMOKE OR FIRE FROM LITHIUM BATTERY
1) TRANSFER CONTROL IF NEEDED TO CREW OPPOSITE TO FIRE
2) PA BACKUP TO THE FLIGHT DECK x2
SMOKE FIRE FUMES
1) OXYGEN AND SMOKE MASK….ON 100%
2) CREW AND CABIN COMMS…. ESTABLISH
STABILIZER
1) STAB CUTOUT SWITCHES (Both)… CUTOUT
2) DO NOT EXCEED CURRENT SPEED
AIRSPEED UNRELIABLE
1) AUTOPILOT…. DISCONNECT
2) AT ARM SWITCHES (Both)…. OFF
3) F/D SWITCHES (Both)…..OFF
FLAPS EXTENDED - 10 degrees 85%N1
FLAPS RETRACTED - 4 degrees 70%N1
OCEANIC DIVERSION - ALL ENGINE
1) INITIATE APPLICABLE DRILLS AND TIME CRITICAL CHECKLISTS
2) DECLARE EMERGENCY AND REQUEST CLEARANCE
IF CLEARANCE OBTAINED - PROCEED PER CLEARANCE
IF CLEARANCE UNAVAILABLE
TURN ATLEAST AND OFFSET
OCA 30 RIGHT OR LEFT 5NM
CHINA 30 RIGHT 5NM
RUSSIA 30 RIGHT 16.2NM
WHEN ESTABLISHED, +- 500FT
OCEANIC DIVERSION - ENGINE OUT
1) INITIATE APPLICABLE DRILLS AND TIME CRITICAL CHECKLISTS
2) DECLARE EMERGENCY AND REQUEST CLEARANCE
IF CLEARANCE OBTAINED - PROCEED PER CLEARANCE
IF CLEARANCE UNAVAILABLE
TURN ATLEAST AND OFFSET
OCA 30 RIGHT OR LEFT 5NM
CHINA 30 RIGHT 5NM
RUSSIA 30 RIGHT 16.2NM
WHEN ESTABLISHED, DESCEND BELOW FL290 AND MAINTAIN +/- 500FT
FIRE ON GROUND
FIRE ON GROUND CHECKLIST
PASSENGER EVACUATION
PASSENGER EVACUATION CHECKLIST
MAX LANDING WEIGHTS 787-8/787-9
787-8 - 172 365
787-9 - 192 776
WINDSHEAR MANUAL FLIGHT
1) Call “WINDSHEAR TOGA” and disconnect
autopilot.
2) Push either TO/GA switch.
3) Aggressively apply maximum* thrust.
4) Disconnect autothrottle(s).
5) Simultaneously roll wings level and rotate toward an
initial pitch attitude of 15°.
6) Retract speedbrakes.
7) Follow flight director TO/GA guidance (if available)
Do not change gear or flap configuration.
Maintain wings level to maximize climb gradient. Unless turn required
Monitor vertical speed and altitude
Do not attempt to regain lost airspeed
WINDSHEAR AUTOMATIC FLIGHT
Call “WINDSHEAR TOGA”
Push either TO/GA switch.*
Verify TO/GA mode annunciation.
Verify thrust advances to GA* power.
Retract speedbrakes.
Monitor system performance**
Do not change gear or flap configuration.
Maintain wings level to maximize climb gradient. Unless turn required
Monitor vertical speed and altitude
Do not attempt to regain lost airspeed