Proficiency Items Flashcards

1
Q

Crew Incapacitation

Reference: COM 3.80 - “Crew Incapacitation” procedure.

A

Condition: Cockpit Crew Member becomes incapacitated.

C—Call FA
S—Secure or Remove Crew Member 
A—Attendant Stays if Crew Member Unmovable 
Dr—On Board Aircraft
P—Pilot typed from our company onboard
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2
Q

One Engine Inoperative - Obstacle Strategy

Reference: COM 3.10.18 - “One Engine Inoperative (Obstacle Strategy)” procedure.

A

Condition: One engine inoperative with obstacle consideration.

IN CRUISE (DO NOT DECEL BELOW GREEN DOT)
M—MCT all Thrust Levers
A—A/THR: OFF
H—HDG Set and Pull as Appropriate
D—Determine Drift Down Altitude (PERF-CRZ PAGE)
N—Notify ATC
S—Start ECAM/OEB Actions When Appropriate

DESCENT (DRIFT DOWN)
S—SPD on FCU: Set Green DOT and PULL
A—ALT on FCU: Selected Cruise FL and PULL

WHEN CLEAR OF OBSTACLES:
Return to STANDARD STRATEGY

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3
Q

Severe Turbulence

Reference: 3.80.35- “Severe Turbulence” procedure.

A
  1. Signs ….. ON
  2. Speed and Thrust ….. ADJUST
    (Reference “Speed and Thrust Setting for Recommended Turbulence Speed” tables in COM Book 2 3.80.36)
    Note: Only change thrust in case of an extreme variation in airspeed, and do not chase your Mach or airspeed.
  3. Autopilot ….. KEEP ON
  4. A/THR (if thrust changes become excs) ….. OFF
  5. ALTITUDE ….. DO NOT CHASE
    Note: for altitude:
    If the Flight Crew flies the aircraft manually:
    - The Flight Crew may expect large variations in altitude, but should not chase altitude.
  6. DESCENT TO OR BELOW OPT FL ….. CONSIDER
    - In order to increase buffet margin.
  7. For approach:
    A/THR ….. ON (managed speed USE)
  8. For landing:
    Configuration ….. FULL, or 3
    CONF FULL provides better handling capability in turbulent conditions, however, CONF 3 provides more energy and less drag.
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4
Q

Stall Recovery

Reference: COM 3.10 - “Stall Recovery” procedure.

A

Condition: Stall indication recognized.

"STALL I HAVE CONTROL”
1. NOSE DOWN PITCH CONTROL ..... APPLY
2. BANK ..... WINGS LEVEL
When out of stall:
3. THRUST ..... INCREASE SMOOTHLY AS NEEDED
4. SPEEDBRAKES ..... CHECK RETRACTED
5. FLIGHT PATH ..... RECOVER SMOOTHLY
If in clean config and below 20,000 ft:
6. FLAP 1 ..... SELECT
  1. NOSE DOWN PITCH CONTROL ….. APPLY
    Note: In case of lack of pitch down authority, reducing thrust may be
    necessary.
  2. BANK ….. WINGS LEVEL

When out of stall:
3. THRUST ….. INCREASE SMOOTHLY AS NEEDED
Note: In case of one engine inoperative, progressively compensate the thrust asymmetry with rudder.

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

If in clean config and below 20,000 ft:
6. FLAP 1 ….. SELECT
Note: If a risk of ground contact exists, once clearly out of stall (no longer stall indication), smoothly establish a positive climb gradient.

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5
Q

Stall Warning at Lift-Off

Reference: COM 3.10.28 - “Stall Recovery at Lift-Off” procedure.

A

“STALL, TOGA 15°”

THRUST ……………….TOGA 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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6
Q

Windshear

Before V1
After V1
Airborne, Initial Climb, Landing

Reference: COM 3.80.44 - “Windshear Warning - Reactive Windshear” procedure.

A

Condition: Windshear advisory annunciated or windshear is detected.
Both PFDs display a WINDSHEAR message with a red flag. An associated aural WINDSHEAR alert sounds three times.

AT TAKEOFF:
Before V1 ….. CONSIDER REJECT

After V1:
“WINDSHEAR TOGA”

  1. THR LEVERS ….. TOGA
  2. REACHING VR ….. ROTATE
  3. SRS ORDERS ….. FOLLOW
    - **If necessary the Flight Crew may pull the side stick fully back.
    - Autopilot disengages if the angle of attack value goes above α prot.
    - If the FD bars are not displayed, move toward an initial pitch attitude of 17.5°. Then, if necessary, to prevent a loss in altitude, increase the pitch attitude.

Airborne, initial climb or landing:

  1. THR LEVERS AT TOGA ….. SET OR CONFIRM
  2. AP (if engaged) ….. KEEP ON
  3. SRS ORDERS ….. FOLLOW -
    * *Same Note from Above
  • DO NOT CHANGE CONFIG TILL OUT OF WINDSHEAR
  • CLOSELY MONITOR FLIGHT PATH AND SPEED
  • RECOVER SMOOTHLY TO NORMAL CLIMB
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7
Q

Windshear Ahead Red

  • Before Takeoff
  • During Takeoff
  • When airborne
  • Landing

Reference: COM 3.80.46 - “Windshear Warning - Predictive Windshear” procedure.

A

Condition: Predictive windshear “W/S AHEAD” or “GO AROUND WINDSHEAR AHEAD” alert triggered.

Note: Associated with an aural synthetic voice “WINDSHEAR AHEAD, WINDSHEAR AHEAD”.
Before takeoff ….. Delay Takeoff or change runway
During Takeoff ….. REJECT TAKEOFF
Note: Predictive windshear alerts are inhibited above 100 knots until 50 feet.

When Airborne:
1. THR LEVERS ….. TOGA
Note: As usual, the slat/flap configuration can be changed, provided the windshear is not entered.
2. AP (if engaged) ….. KEEP ON
3. SRS ORDERS ….. FOLLOW
- **If necessary the Flight Crew may pull the side stick fully back.
- Autopilot disengages if the angle of attack value goes above α prot.
- If the FD bars are not displayed, move toward an initial pitch attitude of 17.5°. Then, if necessary, to prevent a loss in altitude, increase the pitch attitude.

LANDING:
Note: Associated with an aural synthetic voice "GO AROUND, WINDSHEAR AHEAD".
1. GO AROUND ..... PERFORM 
2. AP (IF ENGAGED) ..... KEEP ON
- **Same Note as above
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8
Q

Windshear Ahead Amber

Reference: COM 3.80.47 - “Windshear Warning - Predictive Windshear” procedure.

A

BEFORE TAKEOFF:

  1. Delay takeoff until conditions improve.
  2. Evaluate takeoff conditions:
    - Using observations and experience.
    - Checking weather conditions.
  3. Select the most favorable runway (considering location of the likely windshear).
  4. Use the weather radar or the predictive windshear system before commencing takeoff to ensure that the flight path clears any potential problem areas.
  5. Select TOGA thrust.
  6. Monitor closely airspeed and airspeed trend during the takeoff run for early signs of windshear
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