Memo Items Flashcards

0
Q

What are the Memory Items?

A
CREW INCAPACITATION 
EGPWS
EMER DESCENT
UNRELIABLE SPEED INDICATION
LOSS OF BRAKING
STALL RECOVERY
STALL WARNING AT LIFT-OFF
TCAS
WINDSHEAR
WINDSHEAR AHEAD
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1
Q

Where can you find the Memory Items?

A

FCOM Procedures Abnomal and Emercency

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3
Q

What is the procedure for Crew Incapacitaton ?

A

CREW INCAPACITATION:

request assistance from the cabin crew, by means of the passenger address system: “ATTENTION, PURSER TO COCKPIT PLEASE”

The cabin attendant must then: Tighten and manually lock the shoulder harness of the incapacitated crew member; Push the seat completely aft; Recline the seat back.

Request assistance from any medically qualified passenger. Check if a type qualified company pilot is on board to replace the incapacitated crew member.

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4
Q

What is the procedure for EGPWS?

A

EGPWS:

“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 LEVER…………………………………………………………………….TOGA
SPEED BRAKES lever……………………….CHECK RETRACTED BANK……………………………………..WINGS LEVEL or ADJUST

Best climb performance is obtained when close to wings level.
Then, for “TERRAIN AHEAD PULL UP” or for “OBSTACLE AHEAD PULL UP”, and if the crew concludes that turning is the safest way of action, a turning maneuver can be initiated.

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5
Q

What is the procedure for Emergency Descent?

A

EMER DESCENT, IMMEDIATE ACTIONS CREW :

OXY MASKS…………………………………………………………………ON
EMER DESCENT………………………………………ANNOUNCE (PA)
SIGNS…………………………………………………………………………..ON

‐ Turn and pull ALT
‐ Turn and pull HDG
‐ Pull SPD

THR LEVERS (if A/THR not engaged)……………………..IDLE

‐ If autothrust is engaged, check that THR IDLE is displayed on the FMA.
‐ If not engaged, retard the thrust levers

SPD BRK…………………………………………………………………….FULL

Extension of the speedbrakes will significantly increase Vls. To avoid autopilot disconnection and automatic retraction of the speedbrakes, due to possible activation of the angle of attack protection, allow the speed to increase before starting to use the speed brakes.

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6
Q

What is the procedure for Unreliable Speed Indication?

A

UNRELIABLE SPEED:

AP/FD…………………………………………………………………………..OFF A/THR………………………………………………………………………….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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7
Q

What is the procedure for Stall Recovery?

A

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

NOSE DOWN PITCH CONTROL…………………………….APPLY
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 assymetry with rudder.

SPEED BRAKES…………………………….CHECK RETRACTED FLIGHT PATH…………………………………RECOVER SMOOTHLY

If in clean configuration and below 20 000 ft:
FLAPS 1 …………………………………………………………….SELECT

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8
Q

What is the procedure for Loss of Braking?

A

LOSS OF BRAKING:

IF NO BRAKING AVAILABLE: REV………………………………………………………………….MAX BRAKE PEDALS…………………………………………………………….RELEASE

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

A/SKID & N/W STRG……………………………………………OFF
Braking system reverts to alternate mode.

BRAKE PEDALS………………………………………………PRESS
Apply brake 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 or 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………………..SHORT AND SUCCESSIVE APPLICATIONS

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9
Q

What is the procedures for 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:

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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10
Q

What is the procedures for TCAS?

A

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

Resolution advisory: All “CLIMB” and “DESCEND” or “MAINTAIN VERTICAL SPEED MAINTAIN” or “ADJUST VERTICAL SPEED ADJUST” or “MONITOR VERTICAL SPEED” type messages:

AP (if engaged)…………………………………………………………………OFF
BOTH FDs……………………………………………………………………….OFF

Respect stall, GPWS, or windshear warning.
Notify ATC.

GO AROUND procedure must be performed when an 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 re-engaged as desired.

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11
Q

What is the procedures for Windshear?

A

 At Takeoff:

If before V1:
The takeoff should be rejected only if significant airspeed variations occur below indicated V1 and the pilot decides that there is sufficient runway remaining to stop the airplane.

If after V1:
THR LEVERS………………………………………………………………….TOGA
REACHING VR………………………………………,……………………… ROTATE
SRS ORDERS……………………………………………………………….. FOLLOW

 Airborne, initial climb or landing:

THR LEVERS AT TOGA………………………………. SET OR CONFIRM
AP (if engaged)………………………………………………………….KEEP ON
SRS ORDERS……………………………………………………………FOLLOW

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

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12
Q

What is the procedures for Windshear Ahead?

A

Before takeoff:
Delay takeoff, or select the most favorable runway.

During the takeoff run:
Reject takeoff.

Note: Predictive windshear alerts are inhibited above 100 kt until 50 ft.

When airborne:
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

Landing:

WINDSHEAR AHEAD”.
GO-AROUND……………………………………………………………PERFORM
AP (if engaged)………………………………………………………….KEEP ON

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