A320-1 Must Know Flashcards

Essential Knowledge

1
Q

MEMORY ITEM

LOSS OF BRAKING

A
  • Announce, “Loss of Braking”
  • Max Reverse
  • Release brake pedals
  • A/Skid & N/W Steering OFF
  • Reapply pressure on brake pedals
  • Max brake pressure 1000psi
  • If a still no braking, short and successive applications of the park brake
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2
Q

MEMORY ITEM

UNRELIABLE SPEED / ADR CHECK PROCEDURE
- MEMORY ITEM
- GPS ALT
- INITIAL LEVEL OFF 
     Ball park Pitch & Thrust
A
  • Announce “UNRELIABLE SPEED”
  • If the safe conduct of the flight is impacted:
    AP and FD OFF
    A/THR OFF
    Set target pitch and thrust
    - Below THR RED ALT 15 deg/TOGA
    - Otherwise 10 deg /CLB
    - Above 10,000’ 5 deg /CLB
    Check Speed brakes retracted
    Leave Flaps in current Config
    - if flaps at FULL - Flaps to 3
    GEAR UP
    When at or above MSA or Circuit Altitude
    Level off for troubleshooting

GPS ALT: On MCDU

INITIAL LEVEL OFF
-Circuit Level Off: 7 deg / 58%
- < FL200:  4 deg / 60%
- > FL200:  3 deg / 70%
- >FL320: 2.5 deg / 80%
Note: 4+6=10, 3+7=10, 2+8=10
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3
Q

MEMORY ITEM

EGPWS ALERTS

WARNING
- “PULL UP”

CAUTION

  • “TERRAIN”
  • “SINK RATE” & “DON’T SINK”
  • “TO LOW GEAR” / “TOO LOW FLAPS”
  • “GLIDE SLOPE”
A

⚠️”PULL UP” WARNING
- Announce “Pull Up, TOGA”
- AP OFF
- Pitch full up
- TOGA thrust
- Check speed brakes retracted
- Wings level or adjust bank as required
- When at a safe altitude and the warning stops
lower the pitch altitude and accelerate
- With a positive rate of climb above VLS
clean up the aircraft as required

“TERRAIN” CAUTION
- Adjust V/S, stop descent, Turn, or GA

“SINK RATE” - “DON’T SINK” CAUTION
Adjust pitch attitude and thrust to silence alert

⚠️”TO LOW GEAR” - “TOO LOW FLAPS”
Go-Around

“GLIDE SLOPE”

  • Position back onto the Glide slope, or
  • Turn the G/S MODE pb OFF if intentional
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4
Q

MEMORY ITEM

TCAS

TRAFFIC ADVISORY
- “Traffic”

RESOLUTION ADVISORY

  • “Climb”,
  • “Descend”,
  • “Maintain Vertical Speed”
  • “Adjust Vertical Speed”

ATC RADIO CALLS

A

TRAFFIC ADVISORY

  • Announce “TCAS, I have control”
  • Don’t manoeuvre on a TA alone”
RESOLUTION ADVISORY
- AP OFF
- FD's OFF
- keep the vertical speed within the green area
- Use between V(alpha)Max and VMAX
- Respect stall, GPWS and windshear warnings
- Notify ATC
- In final approach config must GA for RA CLIMB
     inhibited below 900'
- When "Clear of Conflict" announced 
     Resume ATC clearance
     AP/FD can be re-engaged

ATC RADIO CALLS

  • TCAS RA
  • Clear of Conflict, Returning to [ALT/FL]
  • Clear of Conflict, [ALT/FL] Resumed
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5
Q

MEMORY ITEM

EMERGENCY DESCENT

  • MEMORY ITEM
  • ATC RADIO CALLS
  • PA - PRAM U/S
  • PA TO CABIN CREW at safe altitude
A
INITIAL ACTIONS
- Announce "Attention Cabin Crew Emergency Descent"
- Crew oxygen masks ON
- PA "Emergency Decent"
- Signs ON
- Initiate the emergency descent
     Turn Alt and Pull
     Turn HDG and Pull
     - Initiate diversion, avoid traffic or terrain,
     Pull Speed if structural damage suspected
- Check FMA
- If A/THR OFF, Thrust levers idle
- FULL SPD BRK
ESTABLISHED ON DESCENT
- Set higher of 10,000 or LSALT
- Speed Max/Appropriate
     If structural damage suspected 
     use flight controls and speed with care
- Eng Mode Selector IGN
- ATC Notify
- Transponder 7700
- If Cabin ALT >14,000' Pax Oxy ON

ADDITIONAL

  • Lights ON
  • EAI ON

ATC RADIO CALLS
- “MAYDAY (x3), EMERGENCY DESCENT”

PA - PRAM U/S
- “Fasten Seatbelts and breathe oxygen from the masks provided until further notice”

PA TO CABIN CREW at safe altitude
- “Cabin Crew Carry out Follow UP Duties”

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6
Q

OVERSPEED RECOVERY

A
  • Keep the AP ON
  • Full Speed Brake
  • Monitor the thrust reduction
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7
Q

MEMORY ITEM

STALL RECOVERY
- MEMORY ITEM

A
  • Announce; “Stall, I have control”
  • Upon first indication of a stall
    (aural warning, buffet…)
    Apply nose down pitch control
    (thrust reduction may be necessary)
    Level the wings
  • When there are no longer any stall indications
  • Smoothly increase the thrust as required
  • Check Speed brakes retracted
  • Smoothly recover the flightpath
  • If in the clean config below 20,000’,select Flaps 1
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8
Q

MEMORY ITEM

STALL WARNING AFTER LIFTOFF
- MEMORY ITEM

A
  • Announce, “Stall, TOGA 15”
  • Apply TOGA thrust
  • Pitch to 15 deg nose up
  • Level the wings
  • When a safe flightpath and speed are maintained,
    consider warning spurious
    • angle of Attack probe damaged in Normal Law
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9
Q

MEMORY ITEM

PREDICTIVE WINDSHEAR AHEAD

W/S AHEAD RED (Warning)
    1. Before Takeoff
    2. During Takeoff Run
    3. Airborne
    4. Landing
W/S AHEAD AMBER (Caution)
    1. Before Takeoff
    2. During Approach
     - In case of strong or gusty conditions

When Is it Active

A

W/S AHEAD RED (Warning)

  1. BEFORE TAKEOFF
    - Delay, evaluate
    select most favourable runway and TOGA thrust
  2. DURING TAKEOFF RUN
    - Reject (inhibited 100kts until 50’)
  3. AIRBORNE
    - TOGA thrust and follow SRS
  4. LANDING
    - Go-Around
W/S AHEAD AMBER (Caution)
BEFORE TAKEOFF
- Delay, evaluate 
   select most favourable runway
   TOGA thrust
DURING APPROACH     
- Delay and evaluate, 
   use most favourable runway
   Flap 3, 
   AP and FD's for early recognition 
   Managed speed
   - In case of strong or gust conditions
     greater than 20 kts Vapp+5 up to +15

Below 2300’

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10
Q

MEMORY ITEM

REACTIVE ‘WINDSHEAR’

  • AT TAKEOFF
  • AFTER V1
  • AIRBORNE

CALL TO ATC
- “Windshear Escape”

SUPPORT CALLS

WHEN IS W/S DETECTION ACTIVE

  • Takeoff
  • Landing

W/S WARNING INDICATIONS

PILOT DETECTED W/S

  • Prior to V1
  • Airborne
A

If Windshear warning received or the pilot detects Windshear

Announce, “Windshear TOGA”

AT TAKEOFFF:
- Below V1 reject if sufficient runway available

AFTER V1:

  • TOGA Thrust
  • At VR, Rotate
  • Follow SRS (or 17.5 deg if no pitch bars)

AIRBORN:

  • TOGA Thrust
  • Keep AP ON if engaged
  • Follow the SRS orders
  • Do not change gear or flap
  • Closely monitor flight path and speed
  • Recover smoothly to normal climb out of the shear

CALL TO ATC
- “Windshear Escape”

SUPPORT CALLS
- Radio Altitude and Vertical Speed

WHEN IS W/S DETECTION ACTIVE

  • Takeoff: 3 sec after liftoff until 1300’
  • Landing: 1300’ until 50’

W/S WARNING INDICATIONS

  • Red “Windshear” displayed on PFD
  • Aural”Windshear”

PILOT DETECTED W/S
- If significant airspeed variations during TO:
- Conduct RTO prior to V1 if sufficient runway remains.
- Below 1000’ on Approach
- Change from normal steady flight of:
>15 kts
>500 fpm V/S
>5 deg Pitch Att
>1 dot Glideslope

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11
Q

OEI AT OR AFTER V1

A
  • Keep aircraft straight with rudder
  • At VR rotate to 12.5 degrees and
    then pitch to V2
  • Performance;
    MAN TOGA
    Positive rate - Gear UP
    OCP - pull HDG/NAV
  • Trim then AP ON
  • PAN Call
  • ECAM Actions
  • Once Engine secure
    Above EO Aa
    Wings level
  • Push To Level Off
    (Flaps 1 for immediate visual return)
  • GAM/nE ▶️ Twr Debris, APP WX! details & TRK
  • SCORnE
  • ECAM Actions Complete
  • ADCLP
    A - APU
    D - Dest Decision* Wx, Fuel, Ldg - FORDEC
    C - Comms* CM, ATC/COY, PAX
    L - Load FMS* (silent review of STATUS and any Summary procedures)
    P - Paper procedures, e.g. LD and Overweight, Etc
  • BAC.RA
    B - Brief app, Summary [APP, LDG, GA]
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12
Q

LIMITATIONS

MAX WEIGHT
- ZFW
- LDG
- TO
- Taxi
MIN WEIGHT
- Weight
A
MAX WEIGHTS
- ZFW 62,500 kg
- LDG: 66,000 kg
- T/O:  77,000 kg
- Taxi:  77,400 kg
MIN WEIGHTS
- Weight: 37,230 kg
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13
Q

IMMEDIATE RETURN TO LAND - AEO

A
  • Flap 1 - Activate Approach Phase
  • After T/O Checklist
  • Activate Secondary FLT PLN but
    don’t delete PPOS
    DOWNWIND
  • Brief visual approach back onto runway ##
  • Clear PPOS
  • Approach Checklist
    ABEAM
  • Start timing
  • FLAPS 2
  • AP OFF, FD’s OFF…..
  • BIRD ON, Set RWY TRK
    BASE TURN
  • GEAR DN, F 3, F FULL
  • LDG C/L
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14
Q

ENGINE FAILURE IN THE CRUISE

- main actions to level off

A
  • Set Thrust Levers to MCT
  • Disconnect the A/THR
  • MCP Left to Right
    • Pull Speed
      Standard strategy (.78 / 300)
    • Pull HDG
      to alternate, avoid traffic or terrain
    • Set lower altitude for EO
      and PULL ALT (OP DESC)
  • PAN Call first, then,
  • ECAM Actions
  • When descending at 500’/min or less
    pull ‘V/S -500’
    A/THR ON
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15
Q

PRM CLIMB BREAKOUT

PRM DESCEND BREAKOUT

A

PRM CLIMB BREAKOUT

PF:

  • AP OFF
  • MAN TOGA
  • Announce HDG & ALT
PNF:
- Don't read back
- Set FCU
     HDG Turn & Pull (HDG)
     ALT   Turn & Pull (OP CLB)
PF:
- AP ON 
- FMA's
- THR CLB
- +'ve Climb / Gear UP
- PULL SPD & increase
   Accelerate / retract flaps
- Activate approach phase
- After TO CLB C/L

PRM DESCEND BREAKOUT

PF:
- AP OFF
maintain descent rate and turn
- Announce HDG & ALT

PNF: 
- Don't read back
- Set FCU
      HDG Turn & Pull (HDG)
      ALT   Turn & Pull (OP DESC)
      If V/S >1000 ft/min 
      V/S Pull & Turn -1000
PF: 
- AP ON
When cleared:
- Set ALT
- MAN TOGA 
- FMA's
- THR CLB
- Now set HDG
- +'ve Climb / Gear UP
- Set SPEED (OP CLB)
   Accelerate / Flap retraction
- At desired flap, Activate Approach Phase
- After TO CLB C/L
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16
Q

LIMITATIONS

MAX ALT

CROSSWIND
- 45m Runway
    TO    Dry/Wet
     LDG Dry/Wet
- 30m Runway 
     TO   Dry/Wet
     LDG Dry/Wet
- Low Visibility Operations
- Runway Visual Range

TAILWIND

  • TO
  • LDG
  • Sharklet Difference
  • Autoland (Automatic Rollout)
A
MAX ALT: 39,800 ft
CROSSWIND
- 45m Runway
    TO    Dry/Wet: 38 kts 
     LDG Dry/Wet: 38 kts
- 30m Runway 
     TO   Dry/Wet: 38 kts &amp; 33 kts
     LDG Dry/Wet: 30 kts &amp; 20 kts
- LVO: 15 kts
- RVR
17
Q

LIMITATIONS

SPEEDS
- Max Speed 
- Flaps
     Config 1
     Config 1+F
     Config 2
     Config 3
     Config F
- Landing Gear
     VLE Extended
     VLO extension
     VLO retraction
     Max altitude
- Max Tyre Speed
- Windshield Wipers
- Cockpit Window
- Taxi Speed
A
  • Max Speed: 350 kts / M.82
  • Flaps
    Config 1: 230
    Config 1+F: 215
    Config 2: 200
    Config 3: 185
    Config F: 177
  • Landing Gear
    VLE Extended: 280 kts /M.67
    VLO extension: 250 kts
    VLO retraction: 220 kts
    Max altitude: 25,000’
  • Max Tyre Speed: 195 kts
  • Windshield Wipers: 230 kts
  • Cockpit Window: 200 kts
  • Taxi Speed: When above 76t, max 20 kts in a turn
18
Q

LIMITATIONS

VMCA
Minimum Control Speeds (SL)
- 1+F
- Config 2
- Config 3
A
  • 1+F: 112 kts
  • Config 2: 109 kts
  • Config 3: 108 kts
19
Q

RECOVERY TECHNIQUE

REENGAGE A/THR, FD’s & AP

A
  • A/THR ARM pb ON
  • THR CLB
  • FD’s ON
  • Pull Speed
  • HDG or Manage NAV
  • AP 1
  • Set ALT and PULL
20
Q

LIMITATIONS

LOAD ACCELERATION LIMITS

  • Clean
  • Slats or Flaps
A
  • Clean -1 to +2.5 g

- Slats or Flaps Extended 0 to +2 g

21
Q

LIMITATIONS

MAX ALTITUDE WITH FLAPS/SLATS EXTENDED

A
  • 20,000 feet
22
Q

OEB 38

ERRONEOUS RADIO ALTIMETER HT INDICATION

  • WHEN CAN THIS OCCUR
  • WHAT HAPPENS
  • RECOVERY OPTIONS
  • THREATS
    Main Threat
    Threat if Automatic GA
    How is this fault overcome:
A

CAN OCCUR
- During ILS with AP engaged (Autoland function)

WHAT HAPPENS
- Unexpected early THR IDLE and FLARE mode engagement

OPTIONS
1.  Automatic GA
2.  AP &amp; FD's OFF
- Continue Raw Data Approach (min VIS 1200m), or
- Visual Approach
- Manual GA
    expect significant sidestick inputs

THREATS
- AoA increases to the stall
- GA with RA still frozen at low altitude
- SRS and GA TRK modes engage
NAV, HDG or TRK cannot be selected
LVR CLB will not be displayed on FMA at Aa
ALT* and ALT will not engage
- To correct above; AP OFF, RESET FD’S
This will engage basic modes HDG & V/S

23
Q

OEB 36

EPR MODE FAULT
NO SRS ENGAGEMENT DURING GA

  • GA PROCEDURE
  • FMS
    Phase during GA
    Explain A/THR threat
A
GA PROCEDURE
- AP OFF
- FD OFF
- Conduct Go Around
    "GO AROUND FLAP" /  TOGA
     Pitch to 15 deg NU
     Positive CLB /Gear UP
- FD's ON
- PULL ALT (OP CLB)
- AP ON
- At Aa - THR CLB*

FMS

  • Remains in Approach phase
  • THR CLB FMA will not indicate
24
Q

MNEUMONICS

  • GAM/nE
  • SCORnE
  • ADCLP
  • FROWNS
  • FORDEC
  • BAC.RA
  • BALD
  • PPC.BDC
A
G - G/DOT
A - Pull ALT
M - THR MCT
/.  - TWR debris, APP Wx
N - Consider navigation
E - Continue ECAM
S - Status/Stop ECAM
C - Checklists
O - OEB's
R - Reset's / Relights
n - (Navigation)
E - Continue ECAM
A - APU
D - Destination/Decision - FORDEC
C* - Communications (CM, ATC/COY, ATIS PA)
L* - Load FMS
P - Paper Procedures, Overweight, LDG
F - Fuel
R - Runway
O - Overweight
W - Weather
N - Notams
S - Services

B - Brief
AC - Approach C/L
R - Ready

F - Facts, --- inc. Wx, Fuel, Landing
O - Options
R - Risks
D - Decision
E - Execution
C - Crosscheck
25
Q

OEB 41

ERRONEOUS ALTN FUEL PREDICTIONS
OF A COY RTE IN ALTN F-PLN

  • What occurs to the fuel predictions
  • How is this rectified
  • When can’t this be rectified
A
  • When a CO RTE is used in the ALT F-PLN the ALTN fuel mat indicate ‘0’.
  • Enter a waypoint in the enroute F-PLN to commence a new ALTN fuel calculation
  • During the departure or arrival phase this recalculation will not be able to be accomplished this may include the active leg of a STAR
26
Q

CHANGE OF RUNWAY

- DEPARTURE

A
DEPARTURE
P - Plan
P - Performance
C - Configuration
.
B - Brief
D - Data Check
C - Checklist
27
Q

REJECTED TAKEOFF BRIEF

- note

A
  • Prior to 100 kts I’ll stop for almost all ECAM Cautions and Warnings, unusual noise, vibration or predictive windshear
  • Above 100 kts and prior to V1 I’ll stop for
    any ECAM Caution or Warning
    Loss of thrust on an engine
    any Fire
    pilot detected Windshear with sufficient runway remaining
    Or if aircraft is unable or unsafe to fly
  • Upon electing to stop I will call “STOP” simultaneously close both thrust levers apply maximum available reverse and ensure RTO autobrakes are operating or apply maximum manual braking
  • I will maintain this until assured of being able to stop on the runway
  • I expect you to monitor my actions and call any omissions, Reverse Green or No reverse as appropriate, DECEL, and at an appropriate time advise the tower “stopping on the runway”.
  • I’ll set the park brake, make an alert PA and then call for ECAM actions.

Note: If reject prior to 72 kts spoilers will not deploy, thus the Autobrakes will not activate.

28
Q

SEVERE TURBULENCE

GENERAL

  • Avoidance
  • Speed
  • Cruise Altitude
  • Noise Abatement

LANDING

  • Config
  • A/THR

TAKE OFF / GO AROUND
- Flap Retraction: TBA

POST FLIGHT
- Requirement:

A
GENERAL
- Whenever possible 
   avoid known or forecast severe turbulence 
- 250 kts to FL200 then 275 / M.76
- Descend to 4000' below REC MAX ALT 
- Do not conduct in conditions of 
   significant turbulence or windshear

LANDING
- Use Config FULL or 3
but 3 provides more energy and less drag
- A/THR ON in Managed speed

TAKE OFF / GO AROUND
- Flap Retraction:

POST FLIGHT
- Log Book entry required

29
Q

GO AROUND

SEQUENCE

  • Whats the last thing to do during a Go-around
  • What threat should be briefed for Config 3 LDG
  • What are the FMAs

CLB THR

  • Lowest altitude
  • Company standard altitude
  • Do crew have to wait for FMA
  • If retard early will there be an FMS reminder
A
SEQUENCE
- Go-Around Flaps
- * Flaps # (up one stage only)
- FMA
- * Checked, Positive Climb
- Gear UP
- * Gear UP
- Call the tower
- GA Flap setting of 1 stage Flap (Config 2)
- MAN TOGA / SRS / HDG or NAV, 
   A/THR (blue)

CLB THR

  • 800’ HAA
  • 1500’ HAA
  • No
30
Q

SAFETY PA’s

IMPACT ALERT

  • PA
  • By whom and when should it be made
  • How is it given if the PA is unserviceable

BRACE ORDER

  • PA
  • By whom and when should it be made
  • How is it given if the PA is unserviceable

DITCHING

  • PA
  • When should it be made
A
IMPACT ALERT
- "Attention cabin crew, 
   resume your seats immediately"
- Made by FO aprox 2000' 
   or 2 mins prior to impact
- If PA u/s cycle No Smoking sign twice 
   (4 chimes)
BRACE ORDER
- "Brace, Brace, Brace"
- Made by FO at aprox 500' 
   or 30 sec prior to impact
- If PA u/s cycle No Smoking sign once 
   (2 chimes)

DITCHING
- “ATTENTION This is a ditching.
Follow your crew members instructions”
- Made after impact with the water

31
Q

SAFETY PA’s

ANTICIPATED SEVERE TURBULENCE

  • PA
  • when would this be made
  • What call back is expected from the cabin
  • When should this be expected

UNANTICIPATED SEVERE TURBULENCE
- PA

A
ANTICIPATED SEVERE TURBULENCE
 - "All passengers and crew be seated 
     and fasten seat belts"
 - any time turbulence is anticipate
 - "All passengers and crew are secure"
 - No specific time frame specified

UNANTICIPATED SEVERE TURBULENCE
- “All passengers and crew be seated
and fasten seat belts immediately.”

32
Q

ENGINE FIRE IN THE CRUISE

A
ECAM Actions
(When thrust lever Idle, THR MCT will annunciation on MCP - A/THR OFF)
Advise ATC when indicated on ECAM
SQ7700
MCP left to right 
- Speed Select GD+5
- HDG avoid traffic or Adequate or leave
- Altitude initially FL180, Pull ALT
Clean up altitude and speed as go through ADCLP