Memory Items Flashcards

1
Q

LOSS OF BRAKING

A

“LOSS OF BRAKING”

  • If no braking:
    REV……………………………………………………………………………………………………………………… MAX
    (If needed, the flight crew may keep maximum reverse thrust until full aircraft stop.)
    BRAKE PEDALS…………………………………………………………………………………………….RELEASE
    A/SKID OFF………………………………………………………………………………………………………ORDER
    (The PF orders the PM to set the A/SKID & N/W STRG sw to OFF.)
    A/SKID & N/W STRG………………………………………………………………………………………………OFF
    BRAKE PEDALS……………………………………………………………………………………………….. PRESS
    MAX BRK PR…………………………………………………………………………………………………. 1000 PSI
    (Limit brake pressure to approximately 1 000 PSI. Monitor brake pressure on the BRAKES
    PRESS indicator.)
  • If still no braking:
    PARK BRAKE……………………………………………………………………………………………………….. USE
    (Use short successive parking brake applications to stop the aircraft)
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2
Q

EMER DESCENT

A

“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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3
Q

STALL RECOVERY

A

“STALL, MY CONTROLS”

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

STALL WARNING AT LIFTOFF

A

“STALL, TOGA 15”

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

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5
Q

UNRELIABLE SPEED INDICATION

A

“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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6
Q

EGPWS CAUTIONS
“TERRAIN TERRAIN” - “TOO LOW TERRAIN” - “CAUTION TERRAIN”

A

“PULL UP TOGA”

*During night or IMC:
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.

*During daylight and VMC, with terrain and obstacles clearly in sight:
FLIGHT PATH…………………………………………………………………………………………….ADJUST

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7
Q

EGPWS CAUTIONS
SINKRATE

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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8
Q

EGPWS CAUTIONS

“DON’T SINK”

A

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

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9
Q

EGPWS CAUTIONS

“TOO LOW GEAR” - “TOO LOW FLAPS”

A

GO-AROUND………………………………………………………………………………………………..PERFORM

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10
Q

EGPWS CAUTIONS

“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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11
Q

EGPWS WARNINGS

“PULL UP” - “TERRAIN TERRAIN PULL UP”

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

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12
Q

TCAS WARNING RA

A

“TCAS, MY CONTROLS”

*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
(Adjust or maintain the vertical speed as required, depending on the green area, and/or to avoid
the red area of the vertical speed scale.)
(Note: Avoid excessive maneuvers while attempting to maintain the vertical speed just
outside the red area of the vertical speed scale, and within the green area. If
necessary, use the full speed range between Vαmax and VMAX.)

*Any CLIMB RA during approach in CONF 3 or FULL:
GO-AROUND………………………………………………………………………………………………..PERFORM
(Follow the SRS GA mode.)
VERTICAL SPEED………………………………………………………………………………………… MONITOR
(Check that the vertical speed remains out of the red area of the vertical speed scale and take
over if necessary.)
(Respect stall, GPWS, or windshear warnings.)
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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13
Q

WINDSHEAR WARNING - REACTIVE WINDSHEAR

A

“WINDSHEAR TOGA”

*Takeoff:
-If before V1:
(If there are significant variations in airspeed, and in airspeed trend below the indicated V1,
reject the takeoff.
If windshear occurs during the takeoff roll, the aircraft may reach V1 later (or sooner) than
expected. The flight crew should ensure that there is sufficient runway remaining to stop
the aircraft, if necessary.)

*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.)

*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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14
Q

Predictive Windshear warning or caution during T/O

A

Warning: -Reject T/O

Caution: -continue with TOGA, or
-Reject T/O

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