787 IMMEDIATE ACTION ITEMS

Question 1

Dual Eng Fail/Stall

Answer 1

1 FUEL CONTROL switches (both) . . . . . . . . . . . . . . . . CUTOFF, then RUN
Attempts to clear stall condition and allow engines to be put into start
mode.
2 RAM AIR TURBINE switch . . . . . . . . . . . . . . . Push and hold for 1 second

Question 2

Loss of All Displays

Answer 2

1 See the EFB, Documents, LOSS OF ALL DISPLAYS.

Question 3

Smoke, Fire or Fumes

Answer 3

1 Don oxygen masks, if needed.

2 Establish pilot and cabin communications.

Question 4

FD DOOR AUTO UNLOCK

Answer 4

1 FD DOOR ACCESS selector . . . . . Rotate to DENY and hold for 1 second

Question 5

CABIN ALTITUDE

Answer 5

1 Don oxygen masks.

2 Establish pilot communications.

Question 6

STABILIZER

Answer 6

1 STAB cutout switches (both) . . . . . . . . . . . . . . . . . . . . . . . . . . . . CUTOUT
2 Do not exceed the current airspeed.

Question 7

AIRSPEED UNRELIABLE

Answer 7

1 Autopilot disconnect switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Push
2 A/T ARM switches (both) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
3 F/D switches (both) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
4 Set the following gear up pitch attitude and thrust:
Flaps extended . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10° and 85% N1
Flaps up . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4° and 70% N1

Question 8

787 V1 CUT

Answer 8

ENGINE FAILURE

NLT 400,
HDG SEL, LNAV, or TRK ME TO CENTERLINE

200 ft…AUTOPILOT ON

At engine out accel altitude…
WITH VNAV….retract flaps

NO VNAV….SET CLEAN MANEUVERING SPEED, retract flaps, SET MAX CONTINUOUS THRUST

Question 9

787 SINGLE ENGINE GO-AROUND

Answer 9

GOING AROUND FLAPS 5 CHECK THRUST

POSITIVE RATE GEAR UP SET MISSED APPROACH ALTITUDE

200 ft AUTOPILOT
400ft ROLL MODE

AT 800 or accel alt
SET CLEAN MANEUVERING SPD
FINISH IN FLCH

Question 10

REJECTED TAKEOFF DUTIES

CAPTAIN

Answer 10

Calls “Reject” or “Reject, I have the
aircraft.”
Simultaneously brings both thrust levers to idle and disconnects the autothrottles.
Confirms RTO braking or initiates
maximum manual braking.
Initiates maximum reverse thrust
consistent with runway and aircraft
conditions.
Raises speed brake lever if not already up.
Calls for “Rejected Takeoff checklist.”

Question 11

REJECTED TAKEOFF DUTIES

FIRST OFFICER

Answer 11

Confirms the following actions:
• Both thrust levers idle.
• Autothrottles disengaged.
• RTO or maximum brakes applied.
• Reverse thrust.
• Speed brake lever full up. (If speed
brake lever is not up, calls “Speed
brakes.”)
• (Calls if other than both reversers
operating normally, such as “Left
reverser only.”)
Calls “80 knots.”
Notifies Tower of reject and status.
Announces “Remain seated, remain
seated” over the PA.
Reads Rejected Takeoff checklist.

Question 12

Stabilized APCH Limits

BY 1500 AGL

Answer 12

By 1500 ft AGL/RA or the FAF, whichever occurs later:
– Landing gear down
– Airspeed no greater than 180 KIAS

Question 13

Stabilized APCH Limits

BY 1000

Answer 13

Final landing configuration
– Landing Checklist complete
– Airspeed within +15 and -5 KIAS of target airspeed
– On lateral profile
– On vertical profile, or correcting with bracketing maneuvers not to exceed:
♦ ± 300 FPM
♦ Sustained vertical speed greater than 1200 FPM
♦ ± 1°
– PM shall announce deviations

Question 14

Stabilized APCH Limits

BY 500

Answer 14

At or below 500 ft:
– Except for momentary airspeed and descent rate deviations, PM announces,
“Go around” and reason (i.e., “flaps”)
Note: At 1000 ft and 500 ft stabilized approach gate altitudes:
• 787 reference altitude to TDZE

Question 15

TERRAIN WARNINGS

Answer 15

� [PF] Call “Max thrust.”
� [PF] Disconnect autopilot and autothrottles.
� [PF] Apply maximum thrust. Move throttles aggressively to forward
stops.
� [PF] Roll wings level and rotate toward 20° pitch up. Do not follow
flight director commands.
� [PM] Verify all required actions have been completed. Call out any
omissions.
� [PF] Maintain configuration. Do not change flap, gear, or trim position
until terrain separation is assured.

Question 16

UPSET RECOVERY

Answer 16

UPSET
PUSH
ROLL
THRUST
STABILIZE

Question 17

CONTACTING DISPATCH

Answer 17

TELEPHONE
ACARS
Remote dial-up interface (RDI)
RDI with Dual Tone Multi-Frequency (DTMF)
GP RADIO (General purpose) on HF
LONG DISTANCE OPERATIONAL CONTROL FACILITIES (LDOC)
HF PHONE PATCH Through GP station
SATCOM

Question 18

Contaminated Runway definition

Answer 18

is contaminated when more than 25 percent of the runway surface area (whether in isolated areas or not) within the reported length and the width being used is covered by water or slush greater than 0.125 inches (3mm), or covered by frost, ice, and any depth of snow.

Question 19

Reduced thrust takeoff

Answer 19

is not permitted when the runway is contaminated by

water, ice, slush, or snow.

Question 20

ETOPS FLIGHT Definition

Answer 20

flights whose planned routing contains a point
farther than 60 minutes flying time from an adequate airport at an approved
one-engine inoperative cruise speed under standard conditions in still air.

Question 21

CP-1, CP-2

Answer 21

The point on the intended route where the one engine inoperative diversion time at FL 100 from two depicted alternates is equal. It is not necessary for the critical point to always fall within the overlap of the AOA
circles. A strong enroute wind will affect the critical point placement.

Question 22

CRITICAL FUEL CALCULATION

Answer 22

2ENG Fuel required for decompression scenario. Based on immediate descent from cruising altitude to FL 100, and diversion to an ETOPS alternate airport on two engines in still air.
1ENG Fuel required for simultaneous failure of an engine and the pressurization system, at the most critical point, with an immediate descent to FL 100 and diversion to an ETOPS alternate airport at the approved single-engine speed
in still air.
DESCENT / CRZ FL100 / APPROACH This is the worst-casefuel burnscenario
HOLDING 15 MINS 1500FT AFE
APU BURN
ICE DRAG
ANTI-ICE
ADDL 5 PCT WIND ERROR
TOTAL FUEL REQD

Question 23

ADEQUATE AIRPORT

Answer 23

A U.S. airport meeting FAA safety standards or a foreign airport found to meet equivalent safety standards. The runway must be sufficient to accommodate the aircraft. The airport must be approved by the FAA for use in ETOPS.

Question 24

CLASS 1 NAVIGATION

Answer 24

Flight can be flown using an RNAV system, provided the aircraft’s position can be “reliably fixed” at least once each hour using airway navigation facilities. Generally, this
one hour provision is accepted to equate to not exceeding 725 NM between ground based navigation facilities. The 725 NM standard is derived from the 130
NM service volume of high altitude navigational aids plus one hour of flight time
assuming a 465 knot groundspeed (130 + 465 + 130 = 725).