Memory items Flashcards

1
Q

LOSS OF BRAKING

A

PF: “LOSS OF BRAKING”

REV……………………………………………….MAX BRAKE PEDALS………………………………………..RELEASE

A/SKID OFF…………………………………………….ORDER

PF: “A/SKID OFF!”

(When the flight crew sets the A/SKID & N/W STRG sw to OFF, the alternate braking mode is activated. Consequently the PF should release the brake pedals before the PM selects the A/SKID off. This action avoids brutal braking application.)

A/SKID & N/W STRG……………………OFF

BRAKE PEDALS………………………….. PRESS

MAX BRK PR………………………………. 1000 PSI

o If still no braking:

PARK BRAKE……………………………… USE

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2
Q

STALL RECOVERY

A

As soon as any stall indication (could be aural warning, buffet…) is recognized, apply the immediate actions:

“STALL, I have control”

NOSE DOWN PITCH CONTROL…APPLY

This will reduce angle of attack Note: In case of lack of pitch down authority, reducing thrust may be necessary.

BANK………………………..WINGS LEVEL

 When out of stall (no longer stall indications) : THRUST……………..INCREASE SMOOTHLY AS NEEDED

SPEEDBRAKES……………………….CHECK RETRACTED FLIGHT PATH………………………….RECOVER SMOOTHLY

 If in clean configuration and below 20 000 ft FLAP1……………………………………..SELECT

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3
Q

STALL WARNING AT LIFT OFF

A

Spurious stall warning may sound in NORMAL law, if an angle of attack probe is damaged. In this
case, apply immediately the following actions:

PF:”STALL, TOGA 15°”

THRUST………………………………………………… TOGA
At the same time:
PITCH ATTITUDE……………………………………15 °
BANK……………………………………………………….WINGS LEVEL

Note: When a safe flight path and speed are achieved and maintained, if stall warning continues, consider it as spurious.

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4
Q

UNRELIABLE SPEED INDICATION

A

PF:”UNRELIABLE SPEED”

 If the safe conduct of the flight is impacted:
AP………………………………………………………………………….. OFF
A/THR……………………………………………………………………. OFF
FD………………………………………………………………………….. OFF

PITCH/THRUST
Below THRUST RED ALT………………………………………..15° / TOGA
Above THRUST RED ALT and Below FL 100………..10° / CLB
Above THRUST RED ALT and Above FL 100………..5° / CLB

FLAPS (if CONF 0(1)(2)(3))……………… MAINTAIN CURRENT CONF
FLAPS (if CONF FULL)…………. SELECT CONF 3 AND MAINTAIN

SPEEDBRAKES………………………CHECK RETRACTED
L/G…………………………………………. UP

When at or above MSA or Circuit Altitude: Level off for troubleshooting.

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5
Q

CAUTION

“TERRAIN TERRAIN” - “TOO LOW TERRAIN” - “TERRAIN AHEAD”

 During night or IMC

A

“PULL UP TOGA”

Simultaneously:
AP………………………………………………………………..OFF
PITCH………………………………………………………….PULL UP

Pull to full backstick and maintain in that position.

THRUST LEVERS……………………………………… TOGA
SPEEDBRAKE lever………………………………….. CHECK RETRACTED
BANK………………………………………………… WINGS LEVEL or ADJUST

Aircraft achieve the best climb performance when the wings are as level as possible.
Note: For some airports, the operator may define a specific procedure.

DO NOT CHANGE CONFIGURATION (SLATS/FLAPS, GEAR) UNTIL CLEAR OF OBSTACLE.

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6
Q

CAUTION

SINK RATE

A

 Above 1 000 ft AAL in IMC or above 500 ft AAL in VMC:
FLIGHT PATH…………………………………………………….ADJUST
Adjust pitch and thrust to silence the alert.

 Below 1 000 ft AAL in IMC or below 500 ft AAL in VMC:
GO-AROUND…………………………………………………….. CONSIDER

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7
Q

WINDHSHEAR AT TAKE OFF

before V1

A

”WINDSHEAR TOGA”

 If before V1:
Only reject the takeoff, if significant airspeed variations occur below indicated V1, and if the
Captain determines that the runway is sufficiently long to stop the aircraft.

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8
Q

EMERGENCY DESCENT

A

PF: “EMERGENCY DESCENT”

CREW OXY MASKS…………………… USE SIGNS…………………………………………. ON

EMER DESCENT…………………………..INITIATE

 If A/THR not active:

THR LEVERS……………………………….. IDLE

SPD BRK……………………………………….FULL

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9
Q

“TERRAIN TERRAIN” - “TOO LOW TERRAIN” - “TERRAIN AHEAD”

 During daylight and VMC, with terrain and obstacles clearly in sight:

A

FLIGHT PATH………………………………………………………………………ADJUST
Adjust pitch, bank and thrust to silence the alert.
Note: For some airports, the operator may define a specific procedure.

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10
Q

“PULL UP” - “TERRAIN AHEAD PULL UP” - “OBSTACLE AHEAD PULL UP” - “AVOID TERRAIN” - “AVOID OBSTACLE”

WARNING

A

“PULL UP TOGA”
Simultaneously:
AP………………………………………………………………………….. OFF
PITCH……………………………………………………………………..PULL UP
Pull to full backstick and maintain in that position.

THRUST LEVERS…………………………………TOGA
SPEEDBRAKE lever……………………………CHECK RETRACTED
BANK………………………………………………….WINGS LEVEL or ADJUST

DO NOT CHANGE CONFIGURATION (SLATS/FLAPS, GEAR) UNTIL CLEAR OF OBSTACLE.

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11
Q

DON’T SINK

A

FLIGHT PATH……………………………………………………….. ADJUST

Adjust pitch and thrust to silence the alert.

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12
Q

“TOO LOW GEAR” - “TOO LOW FLAPS”

A

GO-AROUND………………………………………………………PERFORM

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13
Q

GLIDE SLOPE

A

 Above 1 000 ft AAL in IMC or above 500 ft AAL in VMC:
FLIGHT PATH…………………………………………………………ADJUST
Adjust pitch and thrust to reduce the vertical deviation from the glideslope.

 When conditions require a deliberate approach below glideslope:
G/S MODE…………………………………………………..OFF

 Below 1 000 ft AAL in IMC or below 500 ft AAL in VMC:
GO-AROUND…………………………………………………… CONSIDER

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14
Q

TCAS WARNING

TRAFFIC

A

As soon as a Traffic Advisory (TA) is triggered:

‐ If the AP/FD TCAS mode is armed : “TCAS blue”

‐ If the AP/FD TCAS mode does not arm : “TCAS, I have control”

 Traffic advisory: “TRAFFIC” messages:
Do not perform a maneuver based on a TA alone.

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15
Q

WINDHSHEAR AIRBORNE

A

”WINDSHEAR TOGA”

 Airborne - initial climb or landing:
THR LEVERS AT TOGA……………………………….. SET OR CONFIRM
AP (if engaged)…………………………………………….. KEEP ON
SRS ORDERS………………………………………………….FOLLOW

If necessary, the flight crew may pull the sidestick fully back.
Note: 1. The autopilot disengages, if the angle of attack value goes above alpha prot.
2. If the FD bars are not displayed, move toward an initial pitch attitude of 17.5 °.
Then, if necessary to prevent a loss of altitude, increase the pitch attitude.

DO NOT CHANGE CONFIGURATION (SLATS/FLAPS, GEAR) UNTIL OUT OF WINDSHEAR. CLOSELY MONITOR THE FLIGHT PATH AND THE SPEED. SMOOTHLY RECOVER TO NORMAL CLIMB OUT OF WINDSHEAR.

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16
Q

WINDSHEAR AHEAD BEFORE TAKE OFF

A

Delay takeoff, or select the most favorable runway.

17
Q

WINDSHEAR AHEAD DURING TAKE OFF RUN

A

Reject takeoff.
Note: The predictive windshear alerts are inhibited above 100 kt, until 50 ft

18
Q

WINDSHEAR AHEAD AIRBORNE

A

”WINDSHEAR TOGA”

THR LEVERS…………………………………………………………TOGA
As usual, the slat/flap configuration can be changed, provided the windshear is not entered.
AP (if engaged)…………………………………………………….KEEP ON
SRS ORDERS………………………………………………………. FOLLOW
If necessary, the flight crew may pull the sidestick fully back.

Note: 1. The autopilot disengages, if the angle of attack value goes above alpha prot.

  1. If the FD bars are not displayed, move toward an initial pitch attitude of 17.5 °. Then, if necessary to prevent a loss of altitude, increase the pitch attitude.
19
Q

WINDSHEAR AHEAD LANDING

Associated with a synthetic aural voice: “GO AROUND, WINDSHEAR AHEAD”.

A

GO AROUND……………………………………………………..PERFORM
AP (if engaged)………………………………………………… KEEP ON
If necessary, the flight crew may pull the sidestick fully back.
Note: 1. The autopilot disengages, if the angle of attack value goes above alpha prot.
2. If the FD bars are not displayed, move toward an initial pitch attitude of 17.5 °.
Then, if necessary to prevent a loss of altitude, increase the pitch attitude.

20
Q

WINDHSHEAR AT TAKE OFF

After V1

A

”WINDSHEAR TOGA”

 If after V1:
THR LEVERS…………………………………………………………….TOGA
REACHING VR………………………………………………………….ROTATE
SRS ORDERS…………………………………………………………… FOLLOW
If necessary, the flight crew may pull the sidestick fully back.
Note: If the FD bars are not displayed, move toward an initial pitch attitude of 17.5 °.
Then, if necessary to prevent a loss of altitude, increase the pitch attitude.

21
Q

WINDHSHEAR AT TAKE OFF

Airborne - initial climb or landing:

A

 Airborne - initial climb or landing:
THR LEVERS AT TOGA……………………………….. SET OR CONFIRM
AP (if engaged)…………………………………………….. KEEP ON
SRS ORDERS………………………………………………….FOLLOW
If necessary, the flight crew may pull the sidestick fully back.
Note: 1. The autopilot disengages, if the angle of attack value goes above alpha prot.
2. If the FD bars are not displayed, move toward an initial pitch attitude of 17.5 °.
Then, if necessary to prevent a loss of altitude, increase the pitch attitude.
DO NOT CHANGE CONFIGURATION (SLATS/FLAPS, GEAR) UNTIL OUT OF
WINDSHEAR.
CLOSELY MONITOR THE FLIGHT PATH AND THE SPEED.
SMOOTHLY RECOVER TO NORMAL CLIMB OUT OF WINDSHEAR.

22
Q

TCAS WARNING

RESOLUTION

A

 Resolution advisory: All “CLIMB” and “DESCEND” or “MAINTAIN VERTICAL SPEED MAINTAIN” or “LEVEL OFF, LEVEL OFF” or “MONITOR VERTICAL SPEED” type messages:

AP (if engaged)……………………………………………………OFF
BOTH FDs………………………………………………………….. OFF
Respond promptly and smoothly to a RA by adjusting or maintaining the pitch, as required, to
reach the green area and/or avoid the red area of the vertical speed scale.
Note: Avoid excessive maneuvers while aiming to keep the vertical speed just outside the
red area of the VSI, and within the green area. If necessary, use the full speed range
between Vαmax and VMAX.
Respect stall, GPWS, or windshear warning.
Notify ATC.

 The GO AROUND procedure must be performed, when a RA “CLIMB” or “INCREASE
CLIMB” is triggered on final approach:

Note: Resolution Advisories (RA) are inhibited below 900 ft.

 When “CLEAR OF CONFLICT” is announced:
Resume normal navigation in accordance with ATC clearance.
AP/FD can be reengaged as desired.