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A320 > Memory Items > Flashcards

Memory Items Flashcards

1
Q

SCORNE stands for:

A 
Stop ECAM
Outstanding Checklists
OEB’s
Resets - system resets?
Navigation considerations
“Continue ECAM”
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2
Q

ADCP (failure management) stands for:

A

APU - start, off, bleed?
Destination or diversion
Communicate - ATC, cabin crew, pax, company
Paper checklist?

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3
Q

Rule of thumb for N1 during approach all engines operating

A

Current weight -10%

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4
Q

Checklist titles:

A 
Cockpit Preparation
Before Start
After Start
Taxi
Line Up
Approach
Landing
After Landing
Parking
Securing the Aircraft
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5
Q

TCAS TA

A

“TCAS. I have control”

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6
Q

TCAS RA

A 
AP off.
Both FD off.
Vertical speed monitor (within band)
Prepare to override
Respect Stall, GPWS, Windshear.
Notify ATC
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7
Q

WINDSHEAR warning during take off before V1

A

Reject the take off

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8
Q

WINDSHEAR warning during take off after V1

A

“Windshear TOGA”
Thrust Levers - TOGA
Reaching VR - rotate
SRS orders - follow
If flight director not displayed rotate to an initial pitch of 17.5’ then increase if necessary to prevent altitude loss
Pilot Monitoring will call wind variations from ND and vertical speed

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9
Q

WINDSHEAR warning airborne during initial climb or landing

A

“Windshear TOGA”
Thrust levers at TOGA - set or confirm
Autopilot - if on keep on
SRS orders - follow (May apply full back on sidestick)
If the FD is not displayed pitch to 17.5’ and increase if necessary to avoid altitude loss.
Autopilot will disengage when AofA is greater than aProt.
Do not change configuration until out of windshear.
Pilot Monitoring call wind variations from ND and V/S

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10
Q

PWS Warning during the take off roll (audio “Windshear Ahead” twice, PFD W/S AHEAD red)

A

Reject the take off

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11
Q

PWS “Windshear Ahead” Warning after V1 (audio “Windshear Ahead” x2 and PFD W/S AHEAD red)

A

Thrust levers - TOGA
Configuration can be changed as normal unless encountering windshear
Autopilot (if engaged) - keep on
SRS orders - follow (if necessary the flight crew can pull sidestick fully back)
If FD are not displayed pitch to initially 17.5’ and if necessary to avoid altitude loss increase

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12
Q

PWS warning during approach (audio “Go Around Windshear Ahead” twice, PFD W/S AHEAD red):

A

Go around - perform
Autopilot (if engaged) - keep on
Pilot may select full back sidestick.
If no FD, aim for initial 17.5 degrees pitch.

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13
Q

A Predictive Windshear Caution during take off roll (audio “Monitor Radar Display” and PFD amber W/S AHEAD):

A

Captains decision to continue or reject

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14
Q

Considerations for an approach and land if Windshear suspected

A

Consider the most appropriate runway
Flaps 3
Managed Speed (for ground speed mini)
Increase VAPP on Approach Performance FMGC page to maximum VLS+15

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15
Q

EGPWS Caution at night or IMC

A

“Pull Up TOGA”
Autopilot - off
Pitch - pitch up (pull to full back stick and maintain)
Thrust levers - TOGA
Speedbrake - check retracted
Bank - wings level or adjust
Do not change configuration until clear of obstacle.

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16
Q

EGPWS Warning

A 
“Pull Up TOGA”
Autopilot - off
Pitch - pull up (full back stick)
Thrust - select TOGA
Speed brakes lever - check retracted
Bank - wings level or adjust
Do not change configuration until clear
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17
Q

Loss of Braking

A

“Loss of Braking”
Reverse - Max
Brake Pedals - Release
“Antiskid and Nose wheel Steering - Off”
Brake Pedals - Apply
Max Brake Pressure - 1000psi
If still no braking - Park Brake Use (short successive)

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18
Q

Engine Failure in the cruise

A

Thrust to MCT
Disconnect Auto Thrust
Set a heading(off track) and pull
Determine engine out recovery altitude (MCDU)
When ready for descent set speed (.78/300) and pull
Set recovery altitude and pull for Open Descent
Review OEB’s and call for ECAM actions
Approaching OEI altitude set VS -500, set LRC speed, engage Auto Thrust

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19
Q

Emergency Descent

A 
”Emergency Descent”
Crew Oxy Masks- use
Signs - on (PM)
Emergency Descent - initiate
 [turn altitude to left and pull
   Turn heading left and pull
   Pull speed]
FMA - Announce
Speed brake - Full (monitor VLS)
Second flow tidy up altitude, heading and speed.
ECAM actions
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20
Q

Engine warm up prior to take off (if not operated within 2 hours)

A

5 minutes to avoid thermal shock

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21
Q

Optimum engine relight speed

A

300/.78

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22
Q

Stall Recovery

A 
“Stall. I have control”
Nose down pitch control - apply
Bank - wings level
Thrust - increase smoothly as needed
Speedbrakes - check retracted
Flight path - recover smoothly
If in clean configuration and below 20000ft - flap 1 select
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23
Q

Stall warning at lift off

A

“Stall. TOGA 15”
Thrust - TOGA
Pitch attitude - 15*
Bank - wings level

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24
Q

Unusual Attitude Nose High

A 
Recognise and confirm the situation
Take over and disconnect the Auto Pilot and Auto Thrust
Apply nose down pitch order
Adjust the thrust
Adjust the roll to not exceed 60*
Recover the level flight
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25
Q

Upset Aircraft Nose Low

A

Recognise and confirm the situation
Take over and Disconnect the Auto Pilot and Auto Thrust
Recover from Stall if required
Adjust the roll in the shortest direction to wings level
Adjust the thrust and the drag
Recover to level flight

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26
Q

Unreliable Speed

A

“Unreliable Speed”
If safe conduct of flight impacted AP/ATHR/FD - Off
Pitch/Thrust - [15* TOGA/ 10* Climb/ 5* Climb]
Flaps 0/1/2/3 - Maintain Config
Flaps Config Full - Select Config 3
Speedbrakes - retract
LG - Up
When above safe altitude level off for trouble shooting

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27
Q

Above 100kts the take off should be aborted for

A

Engine fail or fire (sudden loss of engine thrust)
Malfunctions that may not be safe to fly
Red ECAM warnings
Amber ECAM cautions

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28
Q

Amber alerts possible above 100kts during take off

A 
Sidestick fault
Eng fail
Reverser fault
Reverser unlocked
Thrust lever fault
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29
Q

Captains actions during rejected take off

A

“Stop”
Thrust levers - idle
Reverse thrust - max

Once stopped:
Reverser - stowed
Parking Brake - On
Cabin Crew - Alert
ECAM actions - order
30
Q

Speeds for severe turbulence:

A

Up to FL200 - 250
FL200 to FL320 - 275
Above FL320 - M.76

31
Q

Engine idle indications after Start

A 
EPR 1.01
N1 21.4
N2 57.8
EGT 414
FF 350
32
Q

Engine start should be aborted if the N2 vibration exceeds

A

5 (indication pulses green)

33
Q

In flight the PF and PM must cross check before any action on the following controls:

A

Engine master lever
IR selector
Guarded controls
Cockpit CB’s

34
Q

Above 100kt and below V1 the amber cautions to reject a take off are:

A 
F/CTL Sidestick fault
ENG Fail
ENG Reverser fault
ENG Reverser Unlocked
ENG THR Lever Fault
35
Q

Captain actions for Rejected Take Off:

A

STOP announce
Thrust levers idle
Reverse thrust max available

Once stopped:
Reverser stow
Park brake on
Cabin crew alert
ECAM actions order
36
Q

Red LAND ASAP means:

A

Land as soon as possible at the nearest airport where a safe landing can be made

37
Q

Amber LAND ASAP means:

A

Land as soon as possible at the nearest suitable airport

38
Q

A complete IRS align must be performed in the following cases:

A

Before the first flight of the day
When there is a crew change
When the GPS is not available and the NAVAID coverage is poor along the expected route
When the GPS is not available and the expected flight time is more than 3 hours

39
Q

Do not align IRS during

A

Engine start or while the engines are running

40
Q

To perform an IRS alignment the aircraft must be:

A

Stopped on the ground. Any aircraft movement will automatically restart the IRS alignment.

41
Q

A fast IRS alignment must be performed if a:

A

Complete IRS alignment is not necessary and the difference between the IRS position and the FMGC position is at or above 5nm.

42
Q

The aircon Pack Flow selector should be set to LO if:

A

The number of occupants is below 141

43
Q

The aircon Pack Flow selector should be set to HI:

A

For abnormally hot and humid conditions.

44
Q

During the overhead panel scan the batteries should be tested by:

A

Select ECAM Elec pb
BAT 1 and 2 off then on
10 seconds after resetting the battery pb’s on check the ELEC SD page that the current charge of the battery is below 60 amps and is decreasing.

45
Q

APU fire test:

A 
APU fire warning on ECAM
CRC
Master Warning light
APU fire PB light red
Squib and Discharge lights on
46
Q

Engine Fire test:

A 
CRC
Master Warning light
ECAM display ENG 1/2 FIRE
ENG FIRE pb red
Squib and Discharge agent pb lights on
FIRE light on engine master panel on
47
Q

Dispatch to/from narrow runways is not allowed in case of:

A

Nose wheel steering inoperative

One or more brake inoperative

48
Q

Diversion to a 45m runway (not 30m) is recommended in the case of:

A 
Rudder Jam
Rudder pedal jam
Yaw Damper system fault
Rudder Travel Limit system fault
All failures leading to the loss of the nose wheel steering
49
Q

Maximum demonstrated crosswind for take off and landing on wet runway 30m

A

33kt

50
Q

The last engine started must run for at least 2 minutes before take off initiation, to ensure that take off is not initiated before the:

A

Centre tank pumps test is completed, since take off on centre tank is prohibited

51
Q

The ice shedding procedure must be completed when conditions are at or below:

A

OAT +3^ and visible moisture

52
Q

The ice shedding procedure must be completed at intervals not exceeding —- minutes (the flight crew must include the taxi-in time from the previous flight and the taxi-out time from the current flight to determine the total taxi time).

A
  1. In addition this ice shedding procedure must also be completed just before take off, paying particular attention to normal engine parameters to ensure normal engine operation. Parking Brake must be ON for the procedure.
53
Q

During takeoff in case of a tailwind, or a crosswind greater than 20kts, the PF will

A

Apply full forward sidestick until 80kts

Apply thrust progressively to reach takeoff thrust by 40kts ground speed.

54
Q

Glideslope Interception from above:

A

With at least Flaps 2 and Gear down
Select Final Approach
Ensure GS is armed and LOC is active
FCU altitude select higher than aircraft
Vertical Speed select initial -1500 (initially. Can increase to 2000)
At GS capture (GS*) select go-around altitude

55
Q

Engine cool down time after landing, prior to shutdown:

A

3 minutes

56
Q

Below 20000ft Green Dot is calculated as — x aircraft weight (in metric tonnes) + —. Above 20000ft add —kt per —— ft.

A

2 x aircraft weight (in metric tonnes) + 80. Above 20000ft add 1kt per 1000ft.

57
Q

Speed brake automatic retraction will occur upon selection of

A

Config full

58
Q

PDC Readback

A 
Runway
SID
Transition
Transponder Code
Parking Bay
59
Q

Entry to aircraft check:

A 
Waste and Water
Flight deck door test
Gear pins on board
CB’s
Tech Log on board
60
Q

Flight Plan Check:

A 
Call sign (velocity 9337)
Submitted planned route
Route R1 page (PH Avnex Y15 Esdeg Y60 etc)
Flight Level
Trip Time and Fuel (Init B)
Track miles (flight plan page)
Waypoints
61
Q

PF actions at top of climb:

A

Radar adjust
TCAS below
ECAM systems pages
RVSM check (PFD’s 130. PFD’s and STBY ALT 445)

62
Q

Airbus lateral weather avoidance recommends at least —nm distance from the identified area of greatest threat, with an additional margin if the weather is dynamic.

A

20nm

63
Q

For flight above a convective cloud Airbus recommends applying a vertical margin of ——ft above the area of greatest threat.

A

5000ft

64
Q

Airbus Golden Rules

A

1 - Fly, Navigate, Communicate
2 - use appropriate automation at all times
3 - understand the FMA at all times
4 - take action if things do not go as expected.

65
Q

Departure Brief PM Plan:

A 
Takeoff runway (intersection)
SID designator
First cleared altitude
MSA/MORA
Extra fuel and time
66
Q

Departure Brief PF Plan:

A 
Hotspots
Stop margin
EOSID
Return/diversion considerations
Special Operation
Non standard operation
67
Q

Arrival Brief PM Plan:

A 
MORA/MSA
STAR
Type of Approach
Minimum
Go around trajectory
Extra fuel and time
68
Q

Arrival Brief PF Plan:

A 
Guidance for Approach
Landing flap setting
Stop margin
Use of reverse
Use of auto brakes
Planned runway exit
Hotspots for taxi
Special Operation
Non standard operation
69
Q 
During final approach the PM calls out deviations when:
Speed:
Pitch:
Bank Angle:
Descent Rate:
LOC/GS/XTrack/VDEV
VOR
NDB
A 
Speed less than -5 or greater than +10
Pitch lower than -2.5 or greater than +10
Bank angle greater than 7*
Descent rate greater than 1000ft/m
LOC 1/2 dot
GS 1/2 dot
XTrack >0.1nm
VDEV >1/2 dot
VOR 1/2 dot or 2.5*
NDB 5*
70
Q

Recovery of automation etc (UPRT, Stall etc):

A

“Wheels” on horizon
Set N1 - fl100-200 starting with a 6 (60-69%)
- fl200-300 7 (70-79%)
- fl300-+ 8 (80%+)
Turn FD Off then On
Push to level off
AP On
Set desired speed
Engage AT
Read FMA

A320 (19 decks)

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