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Spirit MQF 23r5 > 0-LIMITATIONS (GENERAL) > Flashcards

0-LIMITATIONS (GENERAL) Flashcards

1
Q

KIND OF OPERATIONS

A

‐ VFR
- IFR
‐ Extended overwater flight

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2
Q

MINIMUM FLIGHT CREW

A

2 pilots

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3
Q

WINGSPANS (Traditional wing)

A

A319, A320 = 111 feet, 10 inches

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4
Q

319 - TAILSTRIKE PITCH ATTITUDE - L/G EXTENDED

A

15.5°

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5
Q

MEAN RUNWAY SLOPE

A

±2 %

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6
Q

MAX RUNWAY ALTITUDE

A

9200 ft

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7
Q

Nominal runway width

A

45 m (148 ft)

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8
Q

Minimal runway width

A

30 m (99 ft)

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9
Q

Maximum wind for passenger door operation

A

65 kt

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10
Q

Maximum wind for FWD and AFT cargo door operation

A

40 kt,
(or 50 kt, if the aircraft nose is into the wind, or if the cargo doors are on the downwind side)

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11
Q

The FWD and AFT cargo doors must be closed before the wind speed exceeds?

A

65 kt

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12
Q

Max Recommended Crosswind for RCR - Good / 5

A

38 kts

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13
Q

Max Recommended Crosswind for RCR - Good-to-Medium / 4

A

29 kts

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14
Q

Max Recommended Crosswind for RCR - Medium / 3

A

25 kts

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15
Q

Max Recommended Crosswind for RCR - Medium-to-Poor / 2

A

20 kts

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16
Q

Max Recommended Crosswind for RCR - Poor / 1

A

15 kts

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17
Q

Takeoff is not recommended on the following runway conditions:

A

‐ Water on top of Compacted Snow

‐ Dry Snow or Wet Snow over Ice

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18
Q

Takeoff is not permitted on the following runway conditions:

A

Wet ice

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19
Q

COCKPIT WINDOW OPEN MAXIMUM SPEED

A

200 kts

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20
Q

MAXIMUM FLAPS/SLATS SPEEDS
321 N

A

Lever | Display | Max Speed |Phase

   0 | 0       | VMO / MMO | CRUISE
   1 | 1       | 243 kt             | HOLDING
      | 1 + F | 225 kt             | TAKEOFF
   2 | 2       | 215 kt             | TO/APP
   3 | 3       | 195 kt             | TO/APP/LAND
   F | FULL | 186 kt             |LANDING
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21
Q

MAXIMUM FLAPS/SLATS SPEEDS
319 / 320 / 320 N

A

Lever | Display | Max Speed |Phase

   0 | 0       | VMO / MMO | CRUISE
   1 | 1       | 230 kt             | HOLDING
      | 1 + F | 215 kt             | TAKEOFF
   2 | 2       | 200 kt             | TO/APP
   3 | 3       | 185 kt             | TO/APP/LAND
   F | FULL | 177 kt             |LANDING
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22
Q

MAXIMUM FLAPS/SLATS SPEEDS
321 C

A

Lever | Display | Max Speed |Phase

   0 | 0       | VMO / MMO | CRUISE
   1 | 1       | 235 kt             | HOLDING
      | 1 + F | 225 kt             | TAKEOFF
   2 | 2       | 215 kt             | TO/APP
   3 | 3       | 195 kt             | TO/APP/LAND
   F | FULL | 190 kt             |LANDING
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23
Q

MAXIMUM OPERATING SPEED

A

VMO = 350 kt

MMO = M 0.82

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24
Q

Maximum speed with the landing gear extended (VLE)

A

280 kt /M 0.67

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25
Q

Maximum speed at which the landing gear may be extended (VLO extension)

A

250 kt /M 0.60

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26
Q

Maximum speed at which the landing gear may be retracted (VLO retraction)

A

220 kt /M 0.54

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27
Q

Maximum TIRE ground speed

A

195 kt

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28
Q

MINIMUM CONTROL SPEED FOR LANDING (VMCL) - 321N

A

115 kt

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29
Q

MINIMUM CONTROL SPEED FOR LANDING (VMCL) - 319

A

109 kt

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30
Q

MINIMUM CONTROL SPEED FOR LANDING (VMCL) - 320C

A

109 kt

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31
Q

MINIMUM CONTROL SPEED FOR LANDING (VMCL) - 320N

A

116 kt

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32
Q

MINIMUM CONTROL SPEED FOR LANDING (VMCL) - 321C

A

114 kt

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33
Q

MINIMUM CONTROL SPEED ON NARROW RUNWAYS

A

WIDTH | +VMCG
98 ft | +2.5 kt
114 ft | +1.5 kt
131 ft | +0 kt

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34
Q

When is an immediate landing at weight above maximum landing weight is permitted, provided the pilot follows the overweight landing procedure.

A

In exceptional cases of in-flight turn back or diversion.

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35
Q

With passengers on board, it is not recommended to exceed _____ without air conditioning supply. The lack of fresh air supply will significantly reduce the cabin’s air quality.

A

20 min

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36
Q

AVIONICS VENTILATION

During ground operations and depending on the Outside Air Temperature (OAT), the flight crew must limit the time that the aircraft electric power supply is used, in normal avionics ventilation system configuration, as follows:

A

OAT | Limitation
up to ≤ 49 °C | None
up to ≤ 55 °C | 2 h
up to ≤ 60 °C | 1 h
up to ≤ 64 °C | 0.5 h

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37
Q

CABIN Maximum positive differential pressure

A

9.0 PSI

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38
Q

CABIN Maximum negative differential pressure

A

-1.0 PSI

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39
Q

CABIN Safety relief valve setting

A

8.6 PSI

40
Q

The ram air inlet must only be opened when the cabin differential pressure is less than

A

+1 PSI (70 hPa).

41
Q

FMGS lateral and vertical navigation is certified for:

A

‐ After takeoff, en route, and terminal area operations

‐ Navigation within RNAV/RNP airspace

  • Instrument approach procedures (except ILS & FLS finals)

‐ Missed approach procedures.

42
Q

If GPS PRIMARY LOST is displayed on the ND and MCDU, the navigation accuracy remains sufficient for RNP operations provided that. . .

A

. . . the RNP value is checked or entered on the MCDU and HIGH ACCURACY is displayed.

43
Q

If one engine is inoperative, it is not permitted to use the autopilot to perform NPAs in the following modes:

A

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

44
Q

Min Decision Height ILS CAT 2

A

100 ft AGL, with at least one autopilot engaged and CAT 2, CAT 3 SINGLE or CAT 3 DUAL must be displayed on the FMA.

For manual landing, AP should be disconnected no later than 80 ft AGL.

45
Q

Min Decision Height SA CAT 2

A

100 ft AGL, with at least one autopilot engaged and CAT 2, CAT 3 SINGLE or CAT 3 DUAL must be displayed on the FMA.

46
Q

Min Decision Height ILS CAT 3 SINGLE
(PASSIVE)

A

50 ft AGL, with at least one autopilot & A/THR engaged and CAT 3 SINGLE or CAT 3 DUAL must be displayed on the FMA.

47
Q

Min Decision Height ILS CAT 3 DUAL
(OPERATIONAL)

A

0 ft AGL (NODA). Alert height of “100 ft” AGL, with at least one autopilot & A/THR engaged and CAT 3 DUAL must be displayed on the FMA.

48
Q

Minimum Runway Visual Range for CAT III without DH:

A

300 RVR

49
Q

320C CAT II and CAT III fail passive auto-land are approved in CONFIG _____

A

CONFIG FULL only

50
Q

319 / 320N / 321 / 321N CAT II and CAT III fail passive auto-land are approved in CONFIG ____

A

CONFIG 3 and FULL

51
Q

During refuel/defuel procedures, APU starts or shutdown are. . .

A

. . . permitted unless:

‐ If the APU failed to start or following an automatic APU shutdown, do not start the APU

‐ If a fuel spill occurs, perform a normal APU shutdown.

52
Q

APU BLEED
Max altitude to assist engine start

A

20,000 ft

53
Q

APU BLEED
Max altitude for single pack operation

A

20,000 ft

54
Q

APU BLEED
Max altitude for dual pack operation

A

15,000 ft

55
Q

APU BLEED
Use of APU bleed air for wing anti-ice. . .

A

. . . is not permitted.

56
Q

The use of Wi-Fi devices within the flight compartment (cockpit) is. . .

A

is prohibited when engines are operating for the purpose of flight unless the following condition is met:
* Additional FAA certification of the wireless devices to be used on the flight deck is obtained.

57
Q

ENGINE EGT LIMITS - 320N / 321N
Starting, Takeoff & Go-Around

A

1083 °C

58
Q

ENGINE EGT LIMITS - 319 / 320
Starting, Takeoff & Go-Around

A

635 °C

59
Q

ENGINE EGT LIMITS - 321
Starting

A

635 °C

60
Q

ENGINE EGT LIMITS - 320N / 321N
Maximum Continuous Thrust (MCT)

A

1043 °C

61
Q

ENGINE EGT LIMITS - 321
Takeoff & Go-Around

A

650 °C

62
Q

ENGINE EGT LIMITS - 319 / 320 / 321
Maximum Continuous Thrust (MCT)

A

610 °C

63
Q

ENGINE OIL TEMP - 319 / 320 / 321
Max continuous temp

A

155 °C
165 °C transient (15 min)

64
Q

ENGINE OIL TEMP - 319 / 320 / 321
Min before takeoff

A

50 °C

65
Q

ENGINE OIL QUANTITY - 319 / 320 / 321
Min Oil Quantity

A

11 qt + 0.3 qt/hr

66
Q

ENGINE OIL PRESSURE - 319 / 320 / 321
Min Oil Pressure

A

60 PSI

67
Q

ENGINE OIL PRESS - 320N / 321N
Min Oil Pressure

A

65 PSI

68
Q

ENGINE OIL TEMP - 320N / 321N
Min Starting

A

-40 °C

69
Q

ENGINE OIL QUANTITY 320N / 321N
Min Oil Quantity

A

14 qt when OAT => -30 °C

16.5 qt when OAT < -30 °C

70
Q

ENGINE OIL PRESSURE - 320N / 321N
Min Oil Pressure

A

65 PSI

71
Q

ENGINE OIL PRESSURE - 320N / 321N
Max Oil Pressure

A

270 PSI

72
Q

ENGINE STARTER CYCLE - 320N / 321N

A

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

‐ For ground starts (automatic or manual), a 35 s pause is required between successive cycles

‐ A 15 min cooling period is required, subsequent to three failed cycles, or 15 min of continuous or cumulated crank

‐ The starter must not be run when N2 is above 20 %.

73
Q

ENGINE STARTER CYCLE - 319 / 320 / 321
IAE2500

A

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

‐ For ground starts (automatic or manual), a 15 s pause is required between successive cycles

‐ A 30 min cooling period is required, subsequent to three failed cycles, or 4 min of continuous crank, or 5 min cumulated crank

‐ For manual start, do not exceed the two-minute maximum cycle time

‐ The starter must not be run when N2 is above 10 % on-ground and 18 % in-flight.

74
Q

USE OF REVERSE THRUST

A

Selection of the reverse thrust is prohibited in flight.

Backing the aircraft with reverse thrust is not permitted.

75
Q

The use of GA SOFT mode is ___________ with one engine inoperative.

A

The use of GA SOFT mode is PROHIBITED with one engine inoperative.

76
Q

FUEL IMBALANCE AT TAKEOFF - 319 / 320 / 320N
Inner Tanks (outer balanced)

A

Heavier | Max
Tank | Asymmetry
————+—————-
6613 | 2314
3196 | 3196

77
Q

FUEL IMBALANCE AT TAKEOFF - 319 / 320 / 320N
Inner Tanks (outer balanced)

A

Heavier | Max
Tank | Asymmetry
————+—————-
6613 | 2314
3196 | 3196

78
Q

FUEL IMBALANCE AT TAKEOFF - 321 / 321N

A

Heavier | Max
Tank | Asymmetry
————+—————-
6614 | 882
1543 | 1543

79
Q

FUEL IMBALANCE INFLIGHT & LANDING - 319 / 320 / 320N
Inner Tanks (outer balanced)

A

Heavier | Max
Tank | Asymmetry
————+—————-
FULL | 3306
9479 | 3527
4960 | 4960

80
Q

FUEL IMBALANCE INFLIGHT & LANDING - 321 / 321N

A

Heavier | Max
Tank | Asymmetry
————+—————-
FULL | 2910
8818 | 3196
5180 | 5180

81
Q

MINIMUM FUEL QUANTITY FOR TAKEOFF

A

3307 lbs

  • The ECAM alerts that are related to fuel low level in the wing tanks (FUEL WING TK LO LVL, etc.) must not appear for takeoff.
82
Q

DEFINITION OF ICING CONDITIONS

A

‐ Icing conditions exist when the OAT (on ground or after takeoff) or the TAT (in flight) is at or below 10 °C and visible moisture in any form is present (such as clouds, fog with visibility of 1 sm or less, rain, snow, sleet or ice crystals).

‐ Icing conditions also exist when the OAT on the ground and for takeoff is at or below 10 °C and operating on ramps, taxiways or runways where surface snow, standing water or slush may be ingested by the engines, or freeze on engines, nacelles or engine sensor probes.

83
Q

DEFINITION OF SEVERE ICE ACCRETION

A

Ice accretion is considered severe when the ice accumulation on the airframe reaches approximately 5 mm (0.2 in) thick or more.

84
Q

DEFINITION OF THIN HOARFROST

A

Thin hoarfrost is typically a white crystalline deposit which usually develops uniformly on exposed surfaces on cold and cloudless nights. It is so thin that surface features (lines or markings) can be distinguished beneath it.

85
Q

The flight crew should _____ use the rain repellent in the case of moderate to heavy rain.

A

The flight crew should ONLY use the rain repellent in the case of moderate to heavy rain.

86
Q

The braking system _____ designed to hold the aircraft in a stationary position when a high thrust level is applied on at least one engine.

A

The braking system IS NOT designed to hold the aircraft in a stationary position when a high thrust level is applied on at least one engine.

During ground procedures that require a thrust increase with braking, the flight crew must ensure that the aircraft remains stationary, and must be ready to immediately retard the thrust levers to
IDLE.

87
Q

320 - TAILSTRIKE PITCH ATTITUDE - L/G EXTENDED

A

13.5°

88
Q

320N - TAILSTRIKE PITCH ATTITUDE - L/G EXTENDED

A

13.7°

89
Q

321 - TAILSTRIKE PITCH ATTITUDE - L/G EXTENDED

A

11.2°

90
Q

MANEUVERING LOAD ACCELERATION LIMITS - CLEAN

A

-1 g to +2.5 g

91
Q

MANEUVERING LOAD ACCELERATION LIMITS - OTHER

A

0 g to +2 g

92
Q

FLS function is certified for …

A

RNAV, RNAV (GNSS), GPS, VOR to LNAV/VNAV or LNAV only minima

93
Q

SLS function is certified for …

A

RNAV (GNSS) to LPV or LP minima

94
Q

MAX HEADWIND FOR ILS CAT 2 or CAT 3

A

30 kt

95
Q

MAX TAILWIND FOR ILS CAT 2 or CAT 3

A

10 kt

96
Q

MAX CROSSWIND FOR ILS CAT 2 or CAT 3

A

15 kt

Spirit MQF 23r5 (49 decks)

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