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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
Normal law protections:
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
25
Alternate law protections
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.
28
Max flaps/slats alt
20000ft
29
All electric generators output power
90kVa
30
Landing gear
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
AP available
After 100ft and 5s
32
AUTOLAND wind limits
HW 30kts TW 10kts XW 20kts
33
AUTOLAND warning (below 200ft)
Both AP's trip off Excessive beam deviation Loc or GS transmitter or receiver fail RA discrepancy of at least 15ft
34
Engine failure target speed
V2 or current speed if higher up to V2+15
35
How many fire loops?
2 each per engine and APU (Gas detection loops) 3 sensing elements engine, 1 sensing element APU
36
Eng 1 thrust reverser hydraulic system
Green
37
To enable alternate
Lateral revision at the to waypoint
38
To activate Go Around
Thrust levers to TOGA as long as at least flap 1 selected
39
When the APU is supplying bleed air the pack provides
High flow at all times
40
Window heating is on when
1 engine on, in-flight or manually
41
APU can be started
Throughout flight envelope
42
Wing anti ice on the ground
30s test only
43
Wing tip brakes on flaps, are slats still operative?
Yes. Can still use the other system
44
Can select slats below:
20000ft
45
Vmo/Mmo
350/.82
46
No autobrake below? Why?
72kts, ground spoilers do not activate
47
Why select flap 1 if slats/flaps locked and unselectable?
Means you have go around mode and SRS available.
48
APU fuel burn?
2kg/min
49
Taxi fuel burn?
10kgs/min
50
Eng a. Ice in cruise fuel penalty?
1kg/min | 2kg/min in hold
51
Stall recovery
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
APU fuel burn per min
2kg/min
53
Taxi fuel burn
Two engine: 10kg/min | OETD: 7kg/min
54
RNAV approach, call outs and GA
Call >.1nm XTK, 1/2 dot 50ft | GA >.3nm XTK, 3/4 dot 75ft
55
To dispatch with no destination alternate
Flight time
56
IFR A/C in class C?
Separated from IFR, VFR, SVFR
57
MORA terrain clearance?
1000ft above reference point below 5000 ft | 2000ft above reference point above 5000ft
58
Required RFFS category
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
EASA RVSM?
Part - SPA (special approvals)
60
Stall warning at lift off
Thrust toga Pitch 15 degrees Wings level
62
Engine failure in cruise actions
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
What are the four NOTECH's
SA WLM DM Co-op
64
Flight parameters, SPEED
Vapp -5 or +10
65
Flight parameters, SINK RATE
V/S greater than 1200ft/min
66
Flight parameters, BANK
Bank angle greater than 7 degrees
67
Flight parameters, LOC/GLIDE CROSSTRACK/VDEV COURSE
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
REC MAX level from PROG page provides?
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
SRS target speed on GA is?
Current speed or Vapp whichever is higher. Limited to VLS plus 25kts (2 eng) or plus 15kts (1 eng).
70
What do you lose with EIU failure?
Engine fail ECAM
71
Can you dispatch with anti skid inoperative?
No
72
Which system runs the normal brakes?
Green
73
Above what ground speed is antiskid available?
20kts

Flying (19 decks)

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