Memory Items Flashcards

1
Q

Loss of braking

A

Rev … idle
Brake pedals … release
Anti skid …. Order
Anti skid & NWS … off
Brake pedals … apply
Max brake pressure … 1000psi

If still no braking
Lake brake … use

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2
Q

Emergency descent

A

Oxygen … use
Signs … on
Descent … initiate

If not autothrust
Thrust … idle
Speed brake … use

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3
Q

Stall

A

NOSE DOWN PITCH CONTROL APPLY
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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4
Q

Unreliable speed

A

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

EGPWS Warning

A

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

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 obtain the best climb performance when the wings are as level as possible. The flight crew can adjust bank while climbing, provided that turning is the safest action.

L1 DO NOT CHANGE CONFIGURATION (SLATS/FLAPS, GEAR) UNTIL CLEAR OF OBSTACLE.

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6
Q

TCAS

A

All RA, except any CLIMB RA during approach in CONF 3 or FULL:
AP (if engaged) OFF
FDs OFF
Respond promptly and smoothly.
VERTICAL SPEED ADJUST or MAINTAIN

Any CLIMB RA during approach in CONF 3 or FULL:
GO-AROUND PERFORM
Follow the SRS GA mode.
VERTICAL SPEED MONITOR

ATC NOTIFY

When the “CLEAR OF CONFLICT” aural alert sounds:
ATC NOTIFY
LATERAL AND VERTICAL GUIDANCE ADJUST
Adjust the lateral and vertical guidance to resume normal navigation, in accordance with ATC clearance.
AP/FD AS RQRD

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7
Q

Wind shear airborne

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: The autopilot disengages, if the angle of attack value goes above alpha prot.
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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8
Q

Engine failure in the cruise

A

X

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