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Spirit Airbus A320 Training - 8/21 > Limitations 2021 > Flashcards

Limitations 2021 Flashcards

1
Q

Wingspans A319, A320

A

111 feet, 10 inches

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2
Q

Wingspan A320 Sharklet and A321 Sharklet

A

117 Feet, 5 inches

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3
Q

Tailstrike A319 Strut Compressed

A

13.9 degrees

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4
Q

Tailstrike A320,A320 NEO Strut Compressed

A

11.7 degrees

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5
Q

Tailstrike A321 Strut Compressed

A

9.7 degrees

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6
Q

Maximum certified altitude

A

FL398

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7
Q

Runway slope (mean)

A

+/- 2%

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8
Q

Runway Altitude

A

9,200 feet

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9
Q

Normal runway width

A

45m (148 feet)

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10
Q

Maximum demonstrated crosswind (takeoff and landing)

A

38 knots (guest included)

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11
Q

Maximum tailwind for takeoff

A

15 knots

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12
Q

Maximum tailwind for landing

A

10 knots

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13
Q

Maximum wind for passenger door operation

A

65 knots

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14
Q

Cockpit window open max speed

A

200 knots

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15
Q

Maximum speed with landing gear extended (VLE)

A

280 knots / M.67

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16
Q

Maximum speed landing gear extension (VLO)

A

250 Knots / M.60

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17
Q

Maximum speed landing gear retraction (VLO retract)

A

220 Knots / M.54

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18
Q

Maximum altitude landing gear may be extended

A

25,000 feet

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19
Q

Maximum tire speed (ground speed)

A

195 knots

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20
Q

When the taxi weight is higher than 167,550 pounds (76,000kg) taxi speed should not exceed during a turn

A

20 knots

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21
Q

Wipers maximum operating speed

A

230 knots

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22
Q

Maximum landing weight A320 NEO

A

148,591 pounds

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23
Q

Maximum landing weight A320

A

145,505 pounds

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24
Q

Maximum landing weight A319

A

137,788 pounds

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25
Q

Maximum landing weight A321

A

171,519 pounds

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26
Q

APU bleed use with air start unit

A

APU bleed should not be used at the same time when using a HP air start unit.

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27
Q

Maximum cabin pressure positive differential pressure

A

9.0 PSI

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28
Q

Maximum cabin pressure negative differential pressure

A

-1.0 PSI

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29
Q

Cabin pressure safety relief valve pressure setting is

A

8.6 PSI

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30
Q

Pack use with LP air conditioning unit

A

The flight crew must not use conditioned air from the packs and from the LP air conditioning unit at the same time, to prevent any adverse effect on the air conditioning system.

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31
Q

Minimum height Auto Pilot usage at takeoff with SRS

A

100 feet AGL (or 5 seconds after liftoff)

32
Q

Minimum height Auto Pilot usage Straight-in non-precision approach

A

Applicable minimums

33
Q

Minimum height Auto Pilot usage Circling Approach

A

Applicable circling minimums

-100 feet

34
Q

Minimum height Auto Pilot usage ILS approach with CAT 2 or 3 is NOT displayed on the FMA

A

160 Feet AGL

35
Q

Minimum height Auto Pilot usage at Go-Around (AP or FD engagement)

A

100 feet AGL

36
Q

Minimum height Auto Pilot usage All other phases of flight

A

500 feet AGL (A319,A320)

900 feet AGL (A321)

37
Q

Use of the AP or FD in open DES or DES mode is not permitted in approach, unless the FCU altitude is set at or above.

A

Highest of:
Minimum or 500 feet (A319,A320)
900 feet (A321)

38
Q

NAV mode maybe used in the terminal area provided that

A
  • GPS primary is available
  • The appropriate RNP is checked or entered on the MCDU, and high accuracy is displayed or
  • FMS navigation is cross checked with nav aid raw data
39
Q

If one engine is inoperative, it is NOT permitted to use the autopilot to perform non-precision approaches in the following modes

A

FINAL APP, NAV, V/S, NAV, FPA only FD use is permitted

40
Q

APU Maximum altitude assisted engine start

A

20,000 feet

41
Q

Hamilton APU maximum altitude air conditioning and pressurization single pack

A

20,000 feet

42
Q

Hamilton APU maximum altitude air conditioning and pressurization dual pack

A

15,000

43
Q

Is APU bleed air able to be used for wing anti ice?

A

NO

44
Q

Honeywell APU maximum altitude air conditioning and pressurization single pack

A

22,500 feet

45
Q

Honeywell APU maximum altitude air conditioning and pressurization dual pack

A

15,000

46
Q

Power plant EGT limits for (502-656,690-694)

A319, A320

A

Takeoff go around All engines 5 min, EGT 635
Takeoff go around One engine 10 min, EGT 635
Takeoff go around MCT No limit EGT 610
Starting on ground 635
Starting in air 635

47
Q

Power plant EGT limits for (657-687) A321

A

Takeoff go around All engines 5 min, EGT 650
Takeoff go around One engine 10 min, EGT 650
Takeoff go around MCT No limit, EGT 610
Start on the ground 635
Start in flight 635

48
Q

Power plant EGT limits for (901-928) A320 NEO

A

Takeoff go around all engines 5 min, EGT 1083
Takeoff go around one engine 10 min, EGT 1083
Takeoff go around MCT no limit EGT 1043
Start on the ground 1083
Start in the air 1083

49
Q

Minimum oil temperature starting (N502NK-N698NK) (901-928)

A

-40 c

50
Q

Minimum oil temperature before IDLE (N502NK-N698NK)

A

-10 c

51
Q

Minimum oil temperature before takeoff (N502NK-N698NK)

A

50 c

52
Q

Maximum oil pressure (502-698)

A

60 PSI

53
Q

Minimum oil temperature before takeoff (901-928)

A

52 c

54
Q

Minimum oil pressure (901-928)

A

65 PSI

55
Q

What is considered a engine start cycle for (502-698)

A

A standard automatic start that includes only one start attempt, is considered one cycle

56
Q

Starter limits (502-698)

A
  • For ground starts (automatic or manual), a 15 second pause is required between successive cycles
  • A 30 minute cooling period is required, subsequent to 3 failed cycles or 5 minutes of continuous crank
  • For manual start, observe a 2 minute maximum cycle time
  • For crank, observe a 5 minute maximum cycle time
  • The starter must not be run when N2 is above 10% on the ground and 18% inflight
57
Q

What is considered a engine start cycle for (901-928)

A

A standard automatic start that includes up to 2 start attempts, is considered one cycle

58
Q

Starter limits (901-928)

A
  • For ground start (automatic or manual) a 35 second pause is required between successive cycles
  • A 15 minute cooling period is required, subsequent to 3 failed cycles, or 15 minute of continuous or cumulative crank
  • Starter must not be run when N2 is above 20%
59
Q

When should max reverse thrust not be used

A

Below 70 knots, Idle reverse is permitted down to aircraft stop.

60
Q

Maximum altitude flaps/slats extended

A

20,000 feet

61
Q

Maximum fuel imbalance INFLIGHT and at LANDING Inner tanks (outer tanks balanced) Tank fuel quantity (heavier tank) (502-536 / 601-656 / 690-698 / 901-928)

A

3,306 pounds

62
Q

Maximum fuel imbalance at TAKEOFF Wing Tanks (657-687)

A

882 pounds

63
Q

Maximum brake temperature for takeoff

A

300 c

64
Q

Flight Maneuvering Load Acceleration Limits

A

Clean configuration……………..-1.0g to +2.5g

Other configuration……………..0g to +2.0g

65
Q

Takeoff is NOT permitted on which runway conditions

A

Wet Ice

66
Q

Maximum Operating speed Vmo/Mmo

A

Vmo…………350kt

Mom…………M0.82

67
Q

Can the APU be started and operated even if the LOW OIL LEVEL ECAM advisory is displayed

A

Yes, maintenance action is required within the next 10 hours of APU operation

68
Q

How many start attempts on the APU

A

After three consecutive APU start attempts, the Flight Crew must wait 60 min before a new start attempt.

69
Q

Engine Start crosswind max speed

A

Engine is able to start in crosswind up to 35kt

70
Q

Maximum operating altitude with slats and/or flaps extended

A

20,000ft

71
Q

Fuel Imbalance at TAKEOFF: Inner Tanks (Outer Tanks Balanced) (502-536 / 601-656 / 690-698 / 901-928)

A

Maximum Asymmetry 1,102 LB

72
Q

Fuel Temperature

A

For JET A only, if TAT reaches -34 c, monitor on FUEL SD page that fuel temperature remains higher than -36 C

73
Q

Nosewheel steering (NWS) Maximum NWS angle?

A

+/- 75 degrees

74
Q

ENG oil quantity check (V2500)?

A

(V2500): Check that the oil quantity is at or above 11 qt. +
estimated consumption (average estimated consumption
~ 0.3 qt./h).

75
Q

ENG oil quantity check for (PW1100G):

A

Above 14 quarts, if OTS -30 Check that the oil quantity is at, or above 16.5 quarts

76
Q

Hydraulic system normal operating pressure?

A

3,000 PSI

77
Q

Max altitude for APU start (on A/C power) and operations?

A

FL410

Spirit Airbus A320 Training - 8/21 (50 decks)

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