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Memory Items & Procedures 787 > Memory Items, Maneuvers & Scan Flows > Flashcards

Memory Items, Maneuvers & Scan Flows Flashcards

1
Q

[] CABIN ALTITUDE

A

1 Don the oxygen masks.

2 Establish crew communications.

3 Check the cabin altitude and rate.

4 If the cabin altitude is uncontrollable:

PASS OXYGEN switchPush to ON and

hold for 1 second

Without delay, descend to the lowest safe altitude or 14,000 feet (10,000 feet if fuel endurance is not critical), whichever is higher.

To descend:

Move the thrust levers to idle

Extend the speedbrakes

If structural integrity is in doubt, limit airspeed and avoid high maneuvering loads

Descend at Vmo/Mmo

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2
Q

Aborted Engine Start L, R

A

1 FUEL CONTROL switch (affected side)…CUTOFF

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3
Q

Dual Eng Fail/Stall

A

1 FUEL CONTROL switches (both)…CUTOFF, then RUN

2 RAM AIR TURBINE switch…Push and hold

for 1 second

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4
Q

[] ENG AUTOSTART L, R

A

1 FUEL CONTROL switch (affected side)…Confirm…CUTOFF

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5
Q

[] ENG LIMIT EXCEED L, R

A

1 A/T ARM switch (affected side)Confirm. . . . .OFF

2 Thrust lever (affected side)Confirm. . . . .Retard until

ENG LIMIT EXCEED

message blanks or

the thrust lever is at idle

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6
Q

[] ENG SURGE L, R

A

1 A/T ARM switch (affected side)…Confirm. . . . .OFF

2 Thrust lever (affected side)…Confirm. . . . .Retard until

the ENG SURGE

message blanks or

the thrust lever is at idle

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7
Q

Eng Svr Damage/Sep L, R

A

1 A/T ARM switch (affected side)…Confirm. . . . .OFF

2 Thrust lever (affected side)…Confirm. . . . .Idle

3 FUEL CONTROL switch (affected side)…Confirm. . . . .CUTOFF

4 Engine fire switch (affected side)…Confirm. . . . .Pull

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8
Q

[] FIRE ENG L, R

A

1 A/T ARM switch (affected side)…Confirm. . . . .OFF

2 Thrust lever (affected side)…Confirm. . . . .Idle

3 FUEL CONTROL switch (affected side)…Confirm. . . . .CUTOFF

4 Engine fire switch (affected side)…Confirm. . . . .Pull

5 If the FIRE ENG message stays shown:

Engine fire switch (affected side)…Rotate to the stop

and hold for 1 second

If after 30 seconds, the FIRE ENG message stays shown:

Engine fire switch (affected side)…Rotate to the

other stop and hold for 1 second

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9
Q

[] STABILIZER

A

1 STAB cutout switches (both)…CUTOUT

2 Do not exceed the current airspeed.

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10
Q

Stall Recovery

A

1. Apply nose down elevator (unload the wing)

2. Roll wings level, apply thrust as needed, retract speedbrakes (select flap 1 on rotation)

3. Check airspeed and adjust thrust as needed. Establish pitch attitude

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11
Q

RTO (You as PF)

A

1. Close the thrust levers

2. Disengage the autothrottles

3. Apply maximum manual wheel brakes or verify operation of RTO autobrake.

4. Verify the speedbrake lever UP.

5. 60kts call “REVERSE IDLE”

6. Taxi Speed “FORWARD IDLE”

7. Set the parking brake

8.ACAS

9. Ask

  • Is the Parking Brake Set?
  • Is Reverse Cancelled?
  • Whats Your Diagnosis?

10. Agree a checklist for FO to do unmonitored

11. Declare PAN/MAYDAY/Speak to tower/ other aircraft for any signs of flames/smoke

12. Situation Contained = “Passengers and Crew remain seated and await further instructions” Consult QRH RTO Section

13. Not Contained = EVACUATION CHECKLIST

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12
Q

PM RTO

A

1. Apply reverse thrust up to the maximum amount consistent with conditions ( <60kts Reverse Idle)

2. Call

  • “SPEEDBRAKE UP / SPEEDBRAKE NOT UP”
  • “REVERSERS NORMAL / NO REVERSER LEFT/RIGHT ENGINE / NO REVERSERS”

3. Call 60kts

4. Reverse Idle / Forward Idle

5. When Parking Brake Set “I Have Control”

6. Rest as PF duties

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13
Q

“PULL UP”, “OBSTACLE PULL UP” or “TERRAIN TERRAIN PULL UP”

A

Call “PULL UP, GO-AROUND”

Disconnect autopilot

Disconnect autothrottle(s)

Aggressively apply maximum* thrust

Simultaneously roll wings level and rotate to an initial pitch attitude of 20°

Verify the speedbrakes are retracted

If terrain remains a threat, continue rotation up to the pitch limit indicator or stick shaker or initial buffet

Do not change gear or flap configuration until terrain separation is assured​

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14
Q

CAUTION OBSTACLE

CAUTION TERRAIN

SINK RATE

TERRAIN

DON’T SINK

TOO LOW FLAPS

TOO LOW GEAR

TOO LOW TERRAIN

GLIDESLOPE

BANK ANGLE

A

Correct the flight path or the airplane configuration. Confirm MOA/MSA.

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15
Q

TCAS TA

A

Its Amber.

Look for traffic using traffic display as a guide. Call out any conflicting traffic.

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16
Q

TCAS RA

A

Its Red.

If maneuvering is required, disengage the autopilot and autothrottle. Smoothly adjust pitch and thrust to satisfy the RA command. Follow the planned lateral flight path unless visual contact with the conflicting traffic requires other action.

17
Q

Upset Recovery Nose High

A

i.e.25 degrees nose up, 10 degrees nose down, 45 degrees, airspeed inappropriate for the conditions

Initially:

  • Disengage autopilot & autothrottle
  • Nose down elevator (trim if required)
  • Reduce thrust
  • Roll to get nose down pitch rate

Then:

  • When approaching the horizon, roll to wings level
  • Check airspeed and adjust thrust
  • Establish pitch attitude.
18
Q

Upset Recovery Nose Low Recovery

A

Disconnect autopilot/ autothrottle

Recover:

  • Recover from stall, if needed
  • Roll in the shortest direction to wings level. If bank angle is more than 90 degrees, unload and roll*

Complete the recovery:

  • Apply nose up elevator
  • Apply nose up trim, if needed*
  • Adjust thrust and drag, if needed.
19
Q

“MONITOR RADAR DISPLAY”

A

Maneuver as required to avoid the windshear

20
Q

“WINDSHEAR AHEAD, WINDSHEAR AHEAD”

A
  • prior to V1, reject takeoff
  • after V1, perform the Windshear Escape Maneuver
21
Q

“GO-AROUND, WINDSHEAR AHEAD”

A

perform Windshear Escape Maneuver or, at pilot’s discretion, perform a normal go-around

22
Q

“WINDSHEAR,WINDSHEAR,WINDSHEAR” MANUAL FLIGHT

A

W/S defined as:

15 knots indicated airspeed, 500 FPM vertical speed, 5 degrees pitch attitude, 1 dot displacement from the glideslope, unusual thrust lever position for a significant period of time

  • Call “WINDSHEAR, GO-AROUND”
  • Disconnect autopilot
  • Push either TO/GA switch
  • Aggressively apply maximum* thrust
  • Disconnect autothrottle(s)
  • Simultaneously roll wings level and rotate toward an initial pitch attitude of 15°
  • Verify the speedbrakes are retracted
  • Follow flight director TO/GA guidance (if available)**
23
Q

“WINDSHEAR,WINDSHEAR,WINDSHEAR” AUTOMATIC FLIGHT

A
24
Q

P2 BEFORE START PROCEDURE

A

HYDRAULICS AUTO (right to left)

FUEL

BEACON

RECALL x2

XPDR

TRIM

25
Q

P2 BEFORE TAXI PROCEDURE

A

APU

ENGINE ANTI ICE

FLAPS

ENG DISPLAY

RECALL

26
Q

P2 AFTER LANDING PROCEDURE

A

I L(ove) RAFT

ENGINE ANTI ICE

LIGHT

WXR RADARS

AUTOBRAKE

FLAPS

XPDR

27
Q

P2 SHUTDOWN PROCEDURE

A

Check BALD

Anti Ice

FUEL CONTROL SWITCHES

BELTS

HYDRAULICS

DOOR PWR

FWD CARGO AC

FUEL

BEACON

FDs

2000/STBY

28
Q

PF EFATO ACTIONS

A
  • RUDDER TO KEEP STRAIGHT
  • LOCK LEG
  • SLIGHT BACK PRESSURE
  • ROTATE TO TOGA REF LINE
  • THEN PITCH TO MAINTAIN SPEED REF V2
  • 200’ ENGAGE A/P
  • RESTATE FAILURE
  • 400’ FNC
  • DIAGNOSE
  • CALL MEMORY ITEMS
29
Q

PM EFATO ACTIONS

A

STATE NATURE OF FAILURE “ENG FIRE/FAILURE”

ROTATE

MONITOR

200’ RESTATE

400’ DIAGNOSE CORRECTLY

30
Q
A

Memory Items & Procedures 787 (1 decks)

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