A330 Memory Items Flashcards

1
Q

Loss of Braking

Callout: “LOSS OF BRAKING”

A
  • If no braking available:

REV………………………………………………………………………MAX

BRAKE PEDALS…………………………………………..RELEASE

Brake pedals should be released when the A/SKID & N/W STRG sw is OFF, since the pedal force or displacement produces more braking action in alternate mode than in normal mode.

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

The braking system reverts to alternate mode.

BRAKE PEDALS………………………………………………PRESS

Apply brakes with care, since initial pedal force or displacement produces more braking action in alternate mode than in normal mode.

MAX BRK PR………………………………………………..1000 PSI

  • Monitor brake pressure on the BRAKES PRESS indicator. Limit brake pressure to approximately 1 000 PSI and, at low ground speed, adjust brake pressure as required.*
  • If STILL NO BRAKING :

PARKING BRAKE…………………………………………………USE

Use short successive parking brake applications to stop the aircraft. Brake onset asymmetry may be felt at each parking brake application. If possible, delay use of the parking brake until low speed to reduce the risk of tire burst and lateral control difficulties.

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2
Q

Unreliable speed indication

Callout: ”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 FL100…………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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3
Q

Stall Recovery

Callout: “STALL, I have control”

A

As soon as any stall indication (could be aural warning, “STALL STALL” red message on PFD*, buffet…) is recognized, apply the immediate actions:

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

Note: In case of one engine inoperative, progressively compensate the thrust asymmetry with rudder.

SPEEDBRAKES……………….CHECK RETRACTED

FLIGHT PATH………………RECOVER SMOOTHLY

  • If in clean configuration and below 20 000 ft :

FLAP1……………………………. SELECT

  • Note: If a risk of ground contact exists, once clearly out of stall (no longer stall indications), establish smoothly a positive climb gradient.
  • * on DH DI & DJ*
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4
Q

Stall Warning at lift-off

Callout: “STALL, TOGA 15°”

A

Spurious stall warnings may sound and appear on PFD* in NORMAL law, if an angle of attack probe is damaged. In this case, apply immediately the following actions:

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.*
  • * on DH DI & DJ*
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5
Q

TCAS Warnings

Resolution advisory:

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

Callout: ”TCAS, I have control”

A

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.

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6
Q

TCAS warnings

Traffic advisory: “TRAFFIC” messages:

Callout: ”TCAS, I have control”

A

Do not perform a maneuver based on a TA alone.

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7
Q

EGPWS Cautions:

“DON’T SINK”

A

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

Adjust pitch and thrust to silence the alert.

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8
Q

EGPWS Cautions

“GLIDE SLOPE”

Below 1 000 ft AAL in IMC or below 500 ft AAL in VMC:

A

GO-AROUND………………………………………………………CONCIDER

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9
Q

EGPWS Cautions:

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

During night or IMC:

A

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.*
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10
Q

EGPWS Warnings

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

Callout: “PULL UP TOGA”

A

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.

If the “TERRAIN AHEAD PULL UP” or “OBSTACLE AHEAD PULL UP” aural alert triggers, a turning maneuver can be initiated if the flight crew concludes that turning is the safest action. The PULL UP maneuver must be performed before the turn towards the safe direction, as climbing increases the terrain clearance

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11
Q

EGPWS Cautions:

“TERRAIN TERRAIN” - “TOO LOW TERRAIN” - “TERRAIN AHEAD” -“OBSTACLE 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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12
Q

EGPWS Cautions:

“SINK RATE”

Above 1 000 ft AAL in IMC or above 500 ft AAL in VMC:

A

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

Adjust pitch and thrust to silence the alert.

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13
Q

EGPWS Cautions

“GLIDE SLOPE”

 Above 1 000 ft AAL in IMC or above 500 ft AAL in VMC:

A

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

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14
Q

EGPWS Cautions:

“TOO LOW GEAR” - “TOO LOW FLAPS”

A

GO-AROUND…………………………………………………..PERFORM

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15
Q

EGPWS Cautions:

“SINK RATE”

Below 1 000 ft AAL in IMC or below 500 ft AAL in VMC:

A

GO-AROUND………………………………………………..CONCIDER

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16
Q

W/S AHEAD RED

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

During landing:

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.*
    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.*
17
Q

W/S AHEAD AMBER

A

Apply precautionary measures, as indicated in FCTM Windshear Operational Recommendations

(Refer to FCTM/PR-NP-SP-10-10-3 Operational Recommendations).

18
Q

W/S AHEAD RED

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

When airborne:

A

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

If Windshear is detected, each PFD displays a red flag “WINDSHEAR” message, and an associated aural WINDSHEAR alert sounds three times.

If either the flight crew or the WX system detects WINDSHEAR, apply the following recovery technique:

AT TAKE-OFF

Callout: ”WINDSHEAR TOGA”

A
  • If before V1:

Only reject the takeoff, if significant airspeed variations occur below indicated V1, and if the flight crew determines that the runway is sufficiently long to stop the aircraft.

  • 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.*
20
Q

Windshear

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

Before takeoff:

A

Delay takeoff, or select the most favorable runway.

21
Q

Windshear

If Windshear is detected, each PFD displays a red flag “WINDSHEAR” message, and an associated aural WINDSHEAR alert sounds three times.

If either the flight crew or the WX system detects WINDSHEAR, apply the following recovery technique:

 Airborne - initial climb or landing:

Callout: ”WINDSHEAR TOGA”

A

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

W/S AHEAD RED

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

During takeoff run:

A

Reject takeoff.

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