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Volaris > Limitaciones > Flashcards

Limitaciones Flashcards

1
Q

-Engine-

Reverse thrust

A

Selection of the reverse thrust is prohibited in flight.

Backing the aircraft with reverse thrust is not permitted.

Maximum reverse should not be used below 70kt. Idle reverse is permitted down to aircraft stop.

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2
Q

-Ángulo de banqueo (PEO)-

Ángulo máximo de banqueo

A

30º

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3
Q

-Shaft speeds-

Maximum N1 in normal operation

Maximum N1 permitted (NEO)

Maximum N2 in normal operation

Maximum N2 permitted (NEO)

A

100%

105%

100%

105%

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4
Q

-Thrust setting/ EGT limits (CEO)-

Take off and Go-around (all engines 5 minutes, one engine 10 minutes)

Maximum continuous thrust (MCT)

Starting (on-ground or in-flight)

A

635°C (319, 320) - 650°C (321)

610°C

635°C

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5
Q

-APU-

APU start

Rotor speed maximum N speed

A

After 3 consecutive APU start attempts, the flight crew must wait 60 min before a new start attempt.

107%

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6
Q

-Maximum allowed fuel imbalance (A321, 321N)-

Fuel imbalance in flight and landing

A

Full — 1,320 kg
4,000 kg — 1,450 kg
2,350 kg — 2,350 kg

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7
Q

-Weights (A320)-

Maximum Takeoff Weight (MTOWBR)

Maximum Landing Weight (MLW)

A

77,000 kg

66,000 kg

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8
Q

-APU bleed-

Max altitude to assist engine start

Max altitude for AC and pressurization (single pack operation)

Max altitude for AC and pressurization (dual pack operation)

Use of APU bleed air for wing anti-ice

A

20,000 ft

22,500 ft

15,000 ft

Is not permitted

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9
Q

-Oil quantity (NEO)-

Minimum oil quantity

A

OAT at or above -30°C = 14 qt

OAT below -30°C = 16.5 qt

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10
Q

-Weights (A319)-

Maximum Takeoff Weight (MTOWBR)

Maximum Landing Weight (MLW)

A

75,500 kg

62,500 kg

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11
Q

-Fuel-

Minimum fuel quantity for takeoff

A

1,500 kg

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12
Q

-Oil (CEO)-

Maximum continuous temperature

Maximum transient temperature (15 min)

Minimum starting temperature

Minimum temperature before IDLE is exceeded

Minimum temperature before takeoff

A

155°C

165°C

-40°C

-10°C

50°C

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13
Q

-Thrust setting/ EGT limits (NEO)-

Take off and Go-around (all engines 5 minutes, one engine 10 minutes)

Maximum continuous thrust (MCT)

Starting (on-ground or in-flight)

A

1,083°C

1,043°C

1,083°C

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14
Q

-Maximum flaps/slats speed A321 NEO-

1

1+F

2

3

FULL

A

238 kt

225 kt

215 kt

195 kt

186 kt

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15
Q

-Oil pressure (NEO)-

Minimum oil pressure

Maximum oil pressure

A

65 PSI

270 PSI

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16
Q

-Weights (A321)-

Maximum Takeoff Weight (MTOWBR)

Maximum Landing Weight (MLW)

A

93,000 kg

77,800 kg

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17
Q

-Autopilot function-

Engage at takeoff

Disengage in approach with F-G/S

Disengage in approach with final APP, V/S, or FPA mode

Disengage in circling approach

Disengage in ILS/MLS approach when CAT I is displayed on the FMA

Disengage in GLS approach when AUTOLAND is not displayed on the FMA

A

100 ft AGL and at least 5s after liftoff

200 ft AGL

250 ft AGL

500 ft AGL for aircraft category C

160 ft AGL

160 ft AGL

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18
Q

-Maximum allowed fuel imbalance at takeoff (A319, A320, A320N)-

Inner tanks (outer tanks balanced)

Outer tanks (inner tanks balanced)

A

Full — 500 kg
3,000 kg — 1,050 kg
1,450 kg — 1,450 kg

Maximum asymmetry 370 kg

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19
Q

-Maximum speed with the landing gear extended-

Maximum speed with the landing gear extended (VLE)

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

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

Maximum tire speed (Maximum ground speed)

Minimum control speed for landing (VMCL)

A

280 kt/M0.67

250 kt/M0.60

220 kt/M0.54

195 kt

109 kt (A319) 114 kt (A320, 321) 116 kt (NEO)

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20
Q

-Engine-

IDLE parameters (A320N, A321N)

A

N1 — 19%

N2 — 59%

EGT — 550ºC

FF — 270 kg/h

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21
Q

-Autopilot functions-

Disengage in ILS/MLS approach when CAT2 or CAT3 is displayed on the FMA

Disengage in PAR approach

Engage after a manual go-around

Engage in all other fases (319, 320, 320N)

Engage in all other cases (321, 321N)

A

0 ft AGL if autoland

250 ft AGL

100 ft AGL

500 ft AGL

900 ft AGL

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22
Q

-APU bleed-

Bleed air and electric power

Electric power only

APU ground operation

APU battery restart limit (Elec Emer Config)

A

-2,000 ft to 22,500 ft

22,500 ft to 41,000 ft

-2,000 ft to 14,500 ft

25,000 ft

23
Q

-Engine-

IDLE parameters (A319, A320, A321)

A

EPR — 1.01%

N1 — 21.4%

N2 — 57.8%

EGT — 414°C

FF — 350 kg/h

24
Q

-Velocidades de rodaje (PEO)-

Sobre pista

Salida de pista en calle de alta velocidad

En calles de rodaje en línea recta

Área de movimiento en plataforma (alleyways)

Virajes de 90º o más

Recta final a posición de estacionamiento

A

No hay limitación

50 kts

30 kts

15 kts

10 kts

7 kts

25
Q

-Flight controls-

Maximum operating altitude with slats and/or flaps

Use of flight controls

A

20,000 ft

Rapid an large alternating control inputs, especially in combination with large changes in pitch, roll or yaw (e.g. large side slip angles) may result in structural failures at any speed

26
Q

-Wind limitations-

Maximum demonstrated crosswind

Maximum tailwind for takeoff-landing

Maximum wind for passenger door operation

Maximum wind for FWR and AFT cargo doors

A

38 kt (gust included) por PEO 30 kt y con menos de 400m de visibilidad será de 10 kt

15 kt

65 kt

40 kt (50 kt, if the aircraft nose into the wind)

27
Q

-Maximum recommended crosswind on wet and contaminated runways-

Good (5)

Good to medium (4)

Medium (3)

Medium to poor (2)

Poor (1)

A

38 kt

29 kt

25 kt

20 kt

15 kt

28
Q

-Maximum allowed fuel imbalance (A321, A321N)-

Fuel imbalance at takeoff

A

Full — 400 kg
3,000 kg — 400 kg
1,450 kg — 700 kg

29
Q

-Speeds-

Cockpit window open maximum speed

Wipers maximum operating speed

A

200 kt

230 kt

30
Q

-Weights (A320 NEO)-

Maximum Takeoff Weight (MTOWBR)

Maximum Landing Weight (MLW)

A

79,000 kg

67,400 kg

31
Q

-Autopilot functions-

The AP or FD in OP DES or DES mode can be used in approach

A

Is only permitted if the FCU selected altitude is set to, or above, the higher of the two:
- MDA/MDH
Or
- 500 ft AGL (319, 320, 32N)
- 900 ft AGL (321, 321N)

32
Q

-Oil quantity (CEO)-

Minimum oil quiantity

A

11 qt + consumo (0.3 qt/h)

33
Q

-APU EGT-

Maximum EGT for APU start (below 35,000 ft)

Maximum EGT for APU start (above 35,000 ft)

Maximum EGT for APU running

A

1,090°C

1,120°C

675°C

34
Q

-Maximum allowed fuel imbalance in flight and at landing (A319, A320, A32N)-

Inner tanks (outer tanks balanced)

Outer tanks

A

Full — 1,500 kg
4,300 kg — 1,600 kg
2,250 kg — 2,250 kg

Maximum asymmetry — 690 kg

35
Q

-Maximum flaps/slats speed A321 NEO NX-

1

1+F

2

3

FULL

A

243 kt

225 kt

215 kt

195 kt

186 kt

36
Q

-Air bleed/cond/press/vent-

General air conditioning

A

It is not recommended to exceed 20min without air conditioning (reduce the cabin’s air quality)

37
Q

-APU during refueling/defueling-

APU start/shutdown during refueling/defueling

A

During refuel/defuel procedures, APU starts or shutdown are permitted with the following restrictions:
- 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

38
Q

-Ice and rain protection-

Rain repellent

A

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

39
Q

-Airport operations-

Runway slope

Runway altitude

Nominal runway width

Minimal runway width

A

+-2°

9,200 ft (A319) 14,100 ft

45m

30m

40
Q

-Oil pressure (CEO)-

Minimum oil pressure

A

60 PSI

41
Q

-Aircraft general-

Maximum operating speed VMO/MMO

A

350 kt/M 0.82

42
Q

-Taxi with deflated or damaged tires-

If maximum one tire per gear is deflated (consider 3 gears): Maximum taxi speed during turn

If 2 tires are deflated in the same main gear (maximum one main gear): Maximum taxi speed

For the NWS angle: Maximum NWS angle

A

7 kt

3 kt

30°

43
Q

-Engine-

Crosswind operation on ground

Soft go-around

A

The engine is not able to start in crosswind up to 35 kt

The use of GA SOFT mode is prohibited with one a fine inoperative

44
Q

-Weights (A321 NEO)-

Maximum Takeoff Weight (MTOWBR)

Maximum Landing Weight (MLW)

A

93,500 kg

79,200 kg

45
Q

-Air bleed/cond/press/vent Avionics ventilation-

OAT menor o igual a 49°C

OAT de 49°C a 55°C

OAT de 55°C a 60°C

OAT de 60°C a 64°C

A

No limitation

2 hrs

1 hrs

0.5 hrs

46
Q

-Landing gear-

Maximum brake temperature for takeoff (brake fans off)

Maximum NWS angle

A

300°C

+-85°

47
Q

-Maximum flaps/slats speed A321-

1

1+F

2

3

FULL

A

235 kt

225 kt

215 kt

195 kt

190 kt

48
Q

-Engine-

Starter (A32N, A321N)

A
  • Up to 2 start attempts = 1 cycle
  • For ground starts, a 35s pause is required
  • 15min cooling period is required is required, subsequent to 3 failed cycles, or 15min of continuous or accumulated crank
  • The starter must not be run when N2 is above 20%
49
Q

-Air bleed/cond/press/vent Cabin pressure-

Maximum positive differential pressure

Maximum negative differential pressure

Safety relief valve setting

A

9.0 PSI

-1.0 PSI

8.6 PSI

50
Q

-Maximum flaps/slats speed (A319, A320, 320NEO)-

1

1+F

2

3

FULL

A

230 kt

215 kt

200 kt

185 kt

177 kt

51
Q

-Oil (NEO)-

Maximum temperature

Minimum starting temperature

Minimum temperature before takeoff

A

151°C

-40°C

52°C

52
Q

-Flight maneuvering load acceleration limits-

Clean configuration

Other configuration

A

-1g to +2.5g

-0g to +2g

53
Q

-Engine-

Starter (A319, 320, 321)

A
  • 1 start attempt = 1 cycle
  • For ground starts 15s pause is required between successive cycles
  • 30min cooling period is required, subsequent to 3 failed cycles or 5min of continuous crank
  • For manual starts, observe a two-minute maximum cycle time
  • For crank, observe a 5min maximum cycle time
  • The start must no be run when N2 is above 10% on-ground and 18% in-flight
54
Q

-Environmental Envelope-

Takeoff and Landing

Maximum cruising altitude

A

-1,000 ft to 14,100 ft

39,800 ft

Volaris (6 decks)

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