787 Memory Recall Limitations & Immediate Action Items

Front 1

Maximum operating pressure altitude

Back 1

-8, -9, 43,100 feet

-10, 41,100 feet

Front 2

Maximum takeoff & landing tailwind component

Back 2

15 knots

Front 3

Turbulent air penetration speed

Back 3

Severe turbulence at and above 25,000 feet: 310 knots/.84 Mach (whichever is lower)

Below 25,000 feet: 290 KIAS

Front 4

Takeoff crosswind guidelines, CG =20% MAC, all weights, dry runway

Back 4

40 knots

Front 5

Landing crosswind guidelines, dry runway

Back 5

40 knots

Front 6

Icing conditions definition

Back 6

Icing conditions exist when OAT (ground) or TAT (flight) is 10°C or below.

Front 7

Do not engage the autopilot below a minimum engagement altitude of

Back 7

200 feet AGL after takeoff.

Front 8

Autoland capability may only be used for operations to runways

Back 8

at or below 8400 feet airport field elevation.

Front 9

Without LAND 2 or LAND 3 annunciated, the autopilot must

Back 9

be disengaged below 135 feet AGL.

Front 10

With LAND 2 or LAND 3 annunciated and glideslope angles greater than 3.25°,

Back 10

The autopilot must be disengaged below 100 feet AGL.

Front 11

Do not use FLCH on final approach below

Back 11

1000 feet AFE.

Front 12

Low visibility HUD takeoff (RVR <500) maximum wind components

Back 12

Headwind 25 knots

Tailwind 15 knots

Crosswind 15 knots

Front 13

ILS automatic landing maximum wind component speeds:

Back 13

Headwind 25 knots

Tailwind 15 knots (10 knots for CAT II/III)

Crosswind 25 knots (15 knots for CAT II/III)

Front 14

Maximum glideslope angle

Back 14

3.25°

Front 15

Minimum glideslope angle

Back 15

2.50°

Front 16

Do not operate HF radio

Back 16

during fueling operations.

Front 17

Minimum engine oil quantity prior to start

Back 17

18 quarts

Front 18

For engine start, oil temperature must be

Back 18

greater than -40°C.

Front 19

Intentional selection of reverse thrust in flight

Back 19

is prohibited.

Front 20

Backing the aircraft with use of reverse thrust

Back 20

is prohibited.

Front 21

Control inputs

Back 21

Avoid rapid and large alternating control inputs, especially in combination with large changes in pitch, roll, or yaw (e.g., large side slip angles) as they may result in structural failure at any speed, including below VA.

Front 22

IMMEDIATE ACTION

AIRSPEED UNRELIABLE

Back 22

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

Front 23

IMMEDIATE ACTION

CABIN ALTITUDE

Back 23

1. Don oxygen masks.

2. Establish pilot communications.

Front 24

IMMEDIATE ACTION

Dual Eng Fail/Stall u

Back 24

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

Front 25

IMMEDIATE ACTION

FD DOOR AUTO UNLOCK

Back 25

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

Front 26

IMMEDIATE ACTION

Loss of All Displays u

Back 26

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

Front 27

IMMEDIATE ACTION

Smoke, Fire or Fumes u

Back 27

1. Don oxygen masks, if needed.

2. Establish pilot and cabin communications.

Front 28

IMMEDIATE ACTION

STABILIZER

Back 28

1. STAB cutout switches (both) - CUTOUT

2. Do not exceed the current airspeed.