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SHAUN'S UPGRADE COURSE > Sop > Flashcards

Sop Flashcards

Sop

1
Q

When can you select TA only?

A
  • Engine failure
  • Flight with landing Gear down
  • At particular airports (10-10 pages) ie. closely spaced parallel rwys.

FCOM DSC-34-SURV-60-10

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2
Q

Maximum amount of contamination for landing?

A

4” dry snow
1 1/8” wet snow
1/2” slush or standing water

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3
Q

Max tire speed?

A

195kts

FCOM LIM-AG-SPD

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4
Q

Max gear speeds?

A

Max gear extension Vlo Ext 250kts
Max gear retraction Vlo Ret 220kts
Max gear extended Vle 280kts

FCOM LIM-AG-SPD

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5
Q

Max windshield wiper speed?

A

230kts

FCOM LIM-AG-SPD

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6
Q

Max cockpit window open speed?

A

200kts

FCOM LIM-AG-SPD

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7
Q

Max taxi speed in turn? (321 greater than 76T)

A

No more than 20kts taxi in turn.

FCOM LIM-AG-SPD

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8
Q

Opening ram air inlet.

A

Only open if differential pressure is less than 1psi.

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9
Q

Cabin pressure psi limitations

A
    1. 0 max psi
    • 1 max negative psi
    1. 6 safety relief valve

FCOM LIM-AIR

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10
Q

Max cabin altitudes

A

14,000ft max cabin altitude selection.
9550ft (+/-350) cabin Alt warning.
8000ft max normal cabin Alt.

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11
Q

Avionics ventilation max temps?

A

When above 49°C see limitations.

FCOM LIM-AIR

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12
Q

Autopilot altitudes?

A 
100ft min height for use on T/O.
MDA/DA for Straight-in non precision approach.
MDH-100ft for circling approach.
160ft for ILS when no cat2/3 displayed.
100ft for GA (AP or FD engagement)
500ft (900ft 321) all other phases.
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13
Q

Autopilot use while one engine out.

A

Not permitted to use AP for Non precision approach in “Final App, Nav v/s, Nav/Fpa” while single engine. Must be hand flown.

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14
Q

Maximum altitude for flap and slats?

A

20,000ft

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15
Q

Fuel Temp min temperature

A

When fuel temp reaches -34 monitor fuel temp stays above -36 (Jet A, others are ok to lower temp)

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16
Q

Hydraulic psi normal

A

3000psi (+/-200)

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17
Q

Instrument tolerances (ground check)

A

Altimeters +/-20 between Capt-FO
(+/-75 to known ground elevation)
stby no limit.
Heading ° (compass, reasonable)

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18
Q

Max brake temp for T/O?

A

300° without fans or fans not used.

150° with fans used.

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19
Q

Brake temp maintenance action required

A
  • Any brake exceeds 800° (900 for 319)
  • Fuse plug melted
  • Difference between average temps on left and right gear is greater than 200°
  • Difference between 2 brakes on the same gear is greater than 150° and and other brake is less than 60° or greater than 600°
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20
Q

How long must emergency exit lighting be charged on the first flight of the day?

A

Must be charged for 15 min with cabin lights full bright and bins closed on first flight of the day.

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21
Q

EGPWS Terr selected off when…?

A

Within 15nm of an airport not in the database or known to produce false terrain alerts.

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22
Q

Minimum flight crew O2 pressure.

A

Refer to chart when o2 pressure is amber boxed.

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23
Q

APU low oil ecam

A

Advise maintenance, can operate for up to 10 hrs.

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24
Q

APU starter limitations?

A

After 3 starter motor duty cycles must wait 60 min before attempting 3 more cycles.

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25
Q

APU load limits

A
  • Start and electrically to FL410.
  • Battery start 25,000
  • Bleed 15000 for dual pack, 20,000 (22,500) for single pack, 20,000 assist eng start.
  • APU bleed for wing anti-ice not permitted.
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26
Q

Eng thrust time limits

A

TOGA up to 5 min or 10 in case of eng failure.

MCT unlimited

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27
Q

Minimum oil temp for start and T/O?

A

-40°C for start and -10°C for take off.

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28
Q

Minimum oil qty for flt?

A

9.5 plus .5/hr.

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29
Q

Engine starter limits?

A

4 consecutive start attempts with 20s between each.
After 4th 15min cooling.

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30
Q

No Flex T/O when?

A
  • Windshear or known temp inversion below 1500ft agl.
  • Rwy is contaminated.
  • Assumed flex temp is less than actual temp.
  • Prohibited by MEL or Route Manual
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31
Q

Cold weather, single engine taxi restrictions?

A

If temp below 0°C and engines off for more than 3 hours you must start both engines to check for fuel drip. Once check is ok you can shut one down.

32
Q

Fuel drip limits?

A

If during the start of a cold engine the Ramp Lead reports a fuel leak, run thevengine at idle for at least 5 min to allow the seals to warm up.

If the leak rate decreases to less than 60 drops/minute, the aircraft can be dispatched. If the leak rate continues to exceed 60 drops/minute, shut down the affected engine and then restart.

If the leak continues in excess of 60 drops/minute after 5 more minutes, shut down the affected engine and advise Maintenance.

FCOM PRO-NOR-SOP-03-30

33
Q

What is not considered contaminants for rwy?

A

trace, less than 1/8”, wet (unless standing water), frost. Use wet rwy data

34
Q

A rwy is considered contaminated if GREATER than ________% of entire rwy is covered by greater than 1/8 “ of snow, wet snow, slush, or compacted snow/ice.

A

25

35
Q

Runway width required for a 180° turn?

A
  • 319- 99ft

- 321-105ft

36
Q

Engine to ground clearance?

A
  • 319- 21”

- 321-23”

37
Q

A/C wingspan?

A
  • 319- 111’10/34.1m

- 321-117’5”/35.8m

38
Q

Vapp in the mcdu can be modified to a maximum of Vls +_______?

A

15

39
Q

what are limits for bank and pitch and calls when on final approach?

A

7° for bank angle, call “bank bank”

7.5° (321)/ 10° (319), call “pitch pitch”

40
Q

If one reverser is inoperative (including engine failure) do you use both reversers on touchdown?

A

Yes, except if otherwise stated on ECAM.

41
Q

If engine does not shut down when selecting master switch off, what is the procedure?

A

Select engine master switch back on and then off, if engine still does not shut down push the affected engine fire pushbutton. (May take up to 2.5 min for engine to shut down)

42
Q

Below what N1 do you select beacon light off indicating engines are off?

A

10%

43
Q

IRS drift check.

A

2+2T. (2+2xnav hrs)

44
Q

Service check requirement.

A

Service (or weekly) check must have been accomplished within 72 hrs of arrival at destination. Maintenance may apply a 2 hr extension.

45
Q

Rejecting T/O below 100kts?

A

Should consider rejecting T/O for any ECAM.

46
Q

Reasons for rejecting T/O above 100kts?

A

-Fire warning, severe damage, or loss of engine thrust.
-Any reason to believe the a/c may not fly safely.
-Any Red ECAM.
–Following Amber ECAM
- - -FLT/CTL sidestick fault
- - -ENG 1(2) Fail
- - -ENG 1(2) Reverser fault
- - -ENG 1(2) Reverser unlocked
- - -ENG 1(2) Thrust lever fault
In case of tire failure between v1 -20 and v1 unless debris causes serious engine anomalies not is better to continue. BASICALLY ANY AMBER ECAM.

47
Q

When is an engine run-up required?

A

When taxiing in icing conditions and temp is +3C and below, every 30 minutes and within 5 min before T/O. Icing conditions are rain, drizzle, snow, etc… and fog with vis 1NM** or less.

48
Q

For non-precision approaches what is the acceptable differences between chart and MCDU?

A

Vertical- 0.1 degree

Horizontal 3.0 degrees.

49
Q

Which colour CB’s are monitored?

A

Green. Will get “CB tripped Ecam” if out for more than 1 min.

50
Q

Why are the wing tip brk CB’s red?

A

You cannot reset those CB.

51
Q

Fuel burn, taxi (1 and 2 Eng)

A

319,320,321
1 eng= 9kg/min
2 eng= 15kg/min

52
Q

Fuel burn (kg/min, flight)

A 
319,320 = 50kg/min
321.        = 60kg/min
53
Q

Apu burn on ground

A

130kg/hr

54
Q

Designated fuelling exits

A

319,320
L1 and L2 or R2

321
L1 and L4 or R4

55
Q

FFOD stby compass max deviation

A

Differences greater than 8 degrees from ND shall be entered into the Aircraft Defect Log.

56
Q

For flap retraction from Full or 3, does the speed have to be checked prior to retraction?

A

No, not for “Full to 3” or “3 to 2”.

57
Q

For flap retraction from Flap 2 or Flap 1 does the speed have to be checked?

A

Yes, speed checked above F speed prior to selecting flap 1 and above S speed for flap 0.

58
Q

When retracting flaps from flap 3, what is the next flap setting selected and when?

A

From Flap 3 you select flap 1 at F speed

59
Q

Engine Secure definitions:
Engine Failure-
Engine Failure with damage-
Engine Fire-

A

Engine Failure- Engine master “off”
Eng Fail with damage- Agent 1 discharge
Eng Fire- Fire Extinguished or Agent 2 discharge

60
Q

Definition: LAND ASAP Red

A

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

61
Q

Definition: LAND ASAP Amber

A

Land at the nearest suitable airport (suitable as judged by the Capt.)

62
Q

User-defined waypoints confirmation

A

Confirm lat/long and track +/-3°, distance +/-2NM. Confirm at waypoint before and just prior to user-defined.

63
Q

If LDG DIST PROC APPLY is displayed on the ECAM, what must be done?

A

The crew must enter the calculated Vapp (WAT or ACPT) into the PERF APP page.

“If an ECAM alert/QRH procedure affects landing performance, the ECAM/QRH procedure requests LDG DIST PROC… APPLY. In this case the flight crew must verify the landing performance”

FCOM-EFB-LDG-50

64
Q

What is the maximum wiper speed?

A

230 knots

65
Q

What is maximum wind speed for passenger door operation? What about the cargo doors?

A

65 knots for passenger door
40 knot for cargo door (or 50 if the nose is into the wind, or doors are on leeward side)

66
Q

What is the maximum speed for the RAT during flight testing?

A

In the case of RAT deployment during testing, limit the speed from 250 knot from RAT deployment to landing.

67
Q

When does the engine anti ice need to be on?

A

The engine anti ice must be on during all ground and flight operations when icing conditions exist or are anticipated, except during climb and cruise when the temperature is below -40°C SAT.

The engine anti ice must be on prior to and during descent in icing conditions, including temperatures below -40°C SAT.

68
Q

At what point is the option of a Go-around eliminated?

A

When you apply reverse-thrust

69
Q

During the overhead panel check, when would you select PACK FLOW to LO on an A319/20? What about ECON FLOW on A321?

A

PACK FLOW goes to LO if less than 85 pax
ECON FLOW for less than 140 pax

70
Q

What are the maximum differences allowed on the Captain / FO panel check?

A

±20 feet between both PFD’s

Depending on aircraft configuration
±100 between ISIS and PFD’s
±300 between mechanical sby altimeter and PFD’s

For RVSM operation the maximum allowable difference between Captain’s and FO’s altitude display and field elevation is 75 feet.

71
Q

When should you modify the secondary flight plan before departure?

A

Special engine failure departure procedures.

Wx below landing minima at the departure airfield - secondary flight plan should be programmed for a diversion to take-off alternate.

Anticipated change in rwy/SID.

72
Q

Maximum taxi speeds?

A

30 kt straight line, 10 kt for a sharp turn

73
Q

When should CONF 3 be considered for the approach?

A

When windshear or severe turbulence is considered possible on approach.

FCOM PRO-NOR-SOP-09-20

74
Q

When should PACKS OFF data be used when generating a takeoff WAT?

A

Confirm PACKS OFF data is used if planning takeoff from a contaminated runway.

Confirm PACKS OFF data is used for the first takeoff after an Engine Wash.

Confirm PACKS OFF data is used if planning takeoff with PACKS ON APU BLEED

FCOM PRO-NOR-SOP-02-50

75
Q

In flight, the PF and PM must crosscheck by confirming these following controls before any action is taken…

A

‐ ENG MASTER lever
‐ IR MODE selector
‐ All guarded controls
‐ Cockpit C/Bs.

FCOM PRO-ABN-30-20

76
Q

In flight, the PF and PM must crosscheck before any action on the following controls:

A

‐ ENG MASTER lever
‐ IR MODE selector
‐ All guarded controls
‐ Cockpit C/Bs.

FCOM PRO-ABN-30-20

77
Q

Timing for engine shutdown on the taxi-in

The following cooling periods must be applied before engine shutdown

A

If only idle reverse was used: 1 min

If only idle reverse was used* : 2 min

If more than idle reverse was used: 3 min

* Below 50% N1 is acceptable

SHAUN'S UPGRADE COURSE (4 decks)

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