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Airbus Flashcards

0
Q

Vlo

A

Ext 250kts

Ret 220kts

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1
Q

Vle

A

280/m.67

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2
Q

Vfe 1

A

230kt

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3
Q

Vfe 1+f

A

215kts

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4
Q

Vfe 2

A

200kts

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5
Q

Vfe 3

A

185kts

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6
Q

Vfe full

A

177kts

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7
Q

Below 1000ft above TDZE and above DH or alert height a go-around must be performed in case of:

A 
Alpha floor activation
Loss of AP (cavalry charge)
Downgrading of capability (triple click)
Amber caution (single chime) 
Engine failure
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8
Q

Automatic landings, below 200ft, go around in case of:

A

AUTOLAND warning
FLARE does not come up on FMA.

If visual landing may be done manually

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9
Q

Stable approach criteria

A 
A/C in landing config
Target final App +10/-5kts
Rate of descent less than 1200ft/min
A/C within 1 dot GS/loc (ILS)/ correct flight path
Bank angle less than 15
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10
Q

RAT supplies EMER GEN down to?

A

125kts approx

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11
Q

PTU comes on when?

A

Differential pressure > 500psi

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12
Q

RAT extension and coupling takes?

A

Approx 8 secs

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13
Q

Closed circuit config temp. Controlled by?

A

Passing air through skin heat exchanger

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14
Q

Lights available in EMER ELEC config?

A

RH dome, LH instrument panel, STBY compass/ice, torch

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15
Q

A319 min pitch for tailstrike wings level

A

13.9 degrees

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16
Q

One engine out AUTOLAND config?

A

3 or full

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17
Q

Flex corrections

A

A/ice on -5

Qnh reduction -1/2hPa

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18
Q

Emergency descent

A 
Oxygen masks and establish comms
Alt select - turn an pull
Heading - pull (maybe turn)
Speed - pull 
Mach/spd - push to select spd
Check FMA's 
Speed breaks (consider, apply slowly)

PNF
Seatbelts on
Mode select IGN
transponder 7700
Radio mayday
Pax oxy on (cab alt > 14000)

PF refine
Then “My radios EM DES xlist”
Set QNH on standby

Level off alt
Remove masks - close left door
PA SCC to FD

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19
Q

Autopilot disengage at

A

More than 25 nose up (normal law)

Pitch trim wheel beyond a certain point

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20
Q

Fire pushbutton

A

Lp fuel valve, hydraulic fire shut off valve, eng bleed valve and pack flow control valve close
Fadec power cut and IDG deactivated
CRC cancelled and squibs armed

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21
Q

To release brakes after RTO

A

Disarm spoilers

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22
Q

ALD in QRG based on

A

Spoilers operating, no reverse thrust

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23
Q

Predictive windshear alerts inhibited

A

Above 100kts up to 50ft, below 50ft

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24
Q

Normal law protections:

A

Load factor limitation
+2.5 to -1g clean
+2 to 0 other
Pitch attitude protection
+30 or +25 (Full) reducing by 5 at low speed. -15.
Bank angle protection
Positive spiral static stability above 33 degrees.
Automatically reduces to 33 degrees
Max 67 deg
AP disconnect >45 degrees
High Speed Protection
Nose up order applied VMO+6/MMO+0.01 AP disco
High Angle of Attack (has priority)
Side stick commands angle of attack to alpha max, will return automatically to alpha prot if released. AP disconnect at alpha prot+1. To deactivate protection s/stick 8 degrees forward or .5 degree for 5 seconds less than alpha max.
Alpha floor. (Autothrust) lift off to 100 ft above landing

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25
Q

Alternate law protections

A

Load factor limitation
same as normal law (+-red. prot)
No pitch att prot
No bank angle prot
High Speed Stability (with red prot, lost with 3 ADR failure)
above Vmo/Mmo nose up demand, pilot can override. Aural overspeed remains.
Low Speed Stability (lost with 2 ADR failure)
active 5-10kts above SW speed, gentle progressive nose down introduced, keeps speed above VSW. Audio stall warning remains. Aircraft can stall. No Alpha floor.

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28
Q

Max flaps/slats alt

A

20000ft

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29
Q

All electric generators output power

A

90kVa

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30
Q

Landing gear

A

Green hydraulics
LGCIU switch over at end of retraction cycle or failure
Can reset after man gear ext if training and green Hyd available

31
Q

AP available

A

After 100ft and 5s

32
Q

AUTOLAND wind limits

A

HW 30kts
TW 10kts
XW 20kts

33
Q

AUTOLAND warning (below 200ft)

A

Both AP’s trip off
Excessive beam deviation
Loc or GS transmitter or receiver fail
RA discrepancy of at least 15ft

34
Q

Engine failure target speed

A

V2 or current speed if higher up to V2+15

35
Q

How many fire loops?

A

2 each per engine and APU
(Gas detection loops)
3 sensing elements engine, 1 sensing element APU

36
Q

Eng 1 thrust reverser hydraulic system

37
Q

To enable alternate

A

Lateral revision at the to waypoint

38
Q

To activate Go Around

A

Thrust levers to TOGA as long as at least flap 1 selected

39
Q

When the APU is supplying bleed air the pack provides

A

High flow at all times

40
Q

Window heating is on when

A

1 engine on, in-flight or manually

41
Q

APU can be started

A

Throughout flight envelope

42
Q

Wing anti ice on the ground

A

30s test only

43
Q

Wing tip brakes on flaps, are slats still operative?

A

Yes. Can still use the other system

44
Q

Can select slats below:

45
Q

Vmo/Mmo

46
Q

No autobrake below? Why?

A

72kts, ground spoilers do not activate

47
Q

Why select flap 1 if slats/flaps locked and unselectable?

A

Means you have go around mode and SRS available.

48
Q

APU fuel burn?

49
Q

Taxi fuel burn?

50
Q

Eng a. Ice in cruise fuel penalty?

A

1kg/min

2kg/min in hold

51
Q

Stall recovery

A

Nose down pitch
Wings level
Once out of stall smoothly increase thrust as required
Check speedbrakes retracted

If clean below 20000ft select flap 1

52
Q

APU fuel burn per min

53
Q

Taxi fuel burn

A

Two engine: 10kg/min

OETD: 7kg/min

54
Q

RNAV approach, call outs and GA

A

Call >.1nm XTK, 1/2 dot 50ft

GA >.3nm XTK, 3/4 dot 75ft

55
Q

To dispatch with no destination alternate

A

Flight time

56
Q

IFR A/C in class C?

A

Separated from IFR, VFR, SVFR

57
Q

MORA terrain clearance?

A

1000ft above reference point below 5000 ft

2000ft above reference point above 5000ft

58
Q

Required RFFS category

A

Dept/dest 6 (sometimes 5 if low volume), downgrade to 4 temporarily (if notified and fewer than 72 hrs.
Alternates UK 5 other 4

59
Q

EASA RVSM?

A

Part - SPA (special approvals)

60
Q

Stall warning at lift off

A

Thrust toga
Pitch 15 degrees
Wings level

62
Q

Engine failure in cruise actions

A

All thrust levers MCT
Disconnect A/THR
Select speed (300/.78 or green dot)
Select heading (away from airway and/or towards alternate)
Select altitude (from PROG or obstacle strat from PERF CRZ)
ECAM actions

63
Q

What are the four NOTECH’s

A

SA
WLM
DM
Co-op

64
Q

Flight parameters, SPEED

A

Vapp -5 or +10

65
Q

Flight parameters, SINK RATE

A

V/S greater than 1200ft/min

66
Q

Flight parameters, BANK

A

Bank angle greater than 7 degrees

67
Q

Flight parameters,
LOC/GLIDE
CROSSTRACK/VDEV
COURSE

A

1/2 dot LOC/GS
.1nm deviation inbound track/ 1/2 dot in FINAL APP
1/2 dot in VOR or 5 degrees ADF

68
Q

REC MAX level from PROG page provides?

A

FCOM auto flight - flight management

0.3g buffet margin, min rate of climb at MAX CL THR and level flight at MAX CRZ thrust

69
Q

SRS target speed on GA is?

A

Current speed or Vapp whichever is higher. Limited to VLS plus 25kts (2 eng) or plus 15kts (1 eng).

70
Q

What do you lose with EIU failure?

A

Engine fail ECAM

71
Q

Can you dispatch with anti skid inoperative?

72
Q

Which system runs the normal brakes?

73
Q

Above what ground speed is antiskid available?

Flying (19 decks)

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