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Ejet E179 > Limitations > Flashcards

Limitations Flashcards

1
Q

E1

Max Taxi​ &​ Ramp

Weight

A

50,950 kg

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2
Q

E2

Max Taxi​ &​ Ramp

Weight

A

61,700 kg

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3
Q

E1

Max​ Takeoff

Weight

A

50,790 kg

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4
Q

E2

Max​ Takeoff

Weight

A

61,200 kg

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5
Q

E2

Max​ Landing

Weight

A

54,000 kg

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6
Q

E1

Max​ Landing

Weight

A

45,000 kg

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7
Q

E1

Max​ Zero Fuel

Weight

A

42,500 kg

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8
Q

E2

Max​ Zero Fuel

Weight

A

51,850 kg

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9
Q

E1/E2

Max Headwind (for CAT II and LVO)

Operational Limits

A

25 kts

AOM Vol 1 - Limitations

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10
Q

E1/E2

Max 90 degree crosswind (including gusts) for CAT II and LVO

Operational Limits

A

15 kts (AD)

AOM Vol 1 - Limitations

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11
Q

E1/E2

Max 90 degree crosswind component (STEADY)
Takeoff - DRY

Operational Limits

A

25 kts

AOM Vol 1 - Limitations

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12
Q

E1/E2

Max 90 degree crosswind component (STEADY)
Landing - DRY

Operational Limits

A

25 kts

AOM Vol 1 - Limitations

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13
Q

E1/E2

Max 90 degree crosswind component (STEADY)
Takeoff - WET

Operational Limits

A

20 kts

AOM Vol 1 - Limitations

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14
Q

E1/E2

Max 90 degree crosswind component (STEADY)
Landing - WET

Operational Limits

A

15 kts

AOM Vol 1 - Limitations

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15
Q

E1/E2

Max 90 degree crosswind component (STEADY)

Landing - DRY​ RWY​ or TAXIWAYS (1700m X40m or​ less)

Operational Limits

A

15 kts

AOM Vol 1 - Limitations

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16
Q

E1/E2

Max 90 degree crosswind component (STEADY)

Takeoff - DRY​ RWY​ or TAXIWAYS (1700m X40m or​ less)

Operational Limits

A

15 kts

AOM Vol 1 - Limitations

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17
Q

E1/E2

Max 90 degree crosswind component (STEADY)

Takeoff - WET​ RWY​ or TAXIWAYS (1700m X40m or​ less)

Operational Limits

A

05 kts

AOM Vol 1 - Limitations

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18
Q

E1/E2

Max 90 degree crosswind component (STEADY)

Landing - WET​ RWY​ or TAXIWAYS (1700m X40m or​ less)

Operational Limits

A

05 kts

AOM Vol 1 - Limitations

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19
Q

E1/E2

Max 90 degree crosswind component (STEADY)
Takeoff and Landing
STANDING WATER
GROOVED​ RWY

Operational Limits

A

10 kts

AOM Vol 1 - Limitations

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20
Q

E1/E2

Max 90 degree crosswind component (STEADY)
Takeoff and Landing
STANDING WATER
NON-GROOVED​ RWY

Operational Limits

A

05 kts

AOM Vol 1 - Limitations

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21
Q

E1/E2

Max takeoff and landing tailwind component

Operational Limits

A

10 kts (AD)

AOM Vol 1 - Limitations

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22
Q

E1/E2

Max takeoff tailwind component for LVO

Operational Limits

A

05 kts (AD)

AOM Vol 1 - Limitations

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23
Q

E1/E2

Maximum wind for passenger door operation

Operational Limits

A

40 kts

AOM Vol 1 - Limitations

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24
Q

E1/E2

Maximum wind for cargo door opening

Operational Limits

A

40 kts

AOM Vol 1 - Limitations

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25
Q

E1/E2

Max Runway Slope (up hill, down hill)

Runway Slope

A

+/- 2.0%

AOM Vol 1 - Limitations

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26
Q

E1/E2

Min fuel temperature

Fuel

A

- 37 °C

AOM Vol 1 - Limitations

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27
Q

E1/E2

Max fuel imbalance

Fuel

A

360 kg

AOM Vol 1 - Limitations

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28
Q

E1/E2

How the CROSSFEED switch must be for takeoff and landing?

Fuel

XFEED Switch must be set to ____ for takeoff and landing

A

OFF

AOM Vol 1 - Limitations

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29
Q

E1/E2

Max operating airspeed

Speeds

A

Vmo

AOM Vol 1 - Limitations

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30
Q

E1/E2

Max operating mach​ number

Speeds

A

.82 (Mmo)

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31
Q

E1/E2

Max airspeed​ for RAT​ operation

Speeds

A

Vmo or Mmo

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32
Q

E1/E2

Max Turbulent airspeed below 10,000​ ft

Speeds

A

250 kts

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33
Q

E1/E2

Max Turbulent airspeed at or above 10,000​ ft

Speeds

A

270 kts or M.76

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34
Q

E1/E2

Tire limit ground speed

Speeds

A

195 kts

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35
Q

E1/E2

Max​ speed​ with​ windshield wiper​ failed​ in non-parked position​

Speeds

A

320 kts

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36
Q

E1/E2

Max windshield wiper operation speed

Speeds

37
Q

E1/E2

Max speed Flap 1

Speeds

38
Q

E1/E2

Max speed Flap 2

Speeds

39
Q

E1/E2

Max speed Flap 3

Speeds

40
Q

E1/E2

Max speed Flap 4

Speeds

41
Q

E1/E2

Max speed Flap 5

Speeds

42
Q

E1/E2

Max speed Flap FULL

Speeds

43
Q

E1/E2

Design maneuvering speed

Speeds

44
Q

E1/E2

Max​ operating altitude

Altitudes

A

41,000 fts

45
Q

E1/E2

Max​ takeoff​ and landing altitude

Altitudes

A

10,000 fts

46
Q

E1/E2

Max​ flap extension altitude

Altitudes

A

20,000 fts

47
Q

E1/E2

Max​ ambient temperature for​ takeoff and landing

Temperatures

48
Q

E1/E2

Min​ ambient temperature approved​ for takeoff

Temperatures

49
Q

E1/E2

Max​ altitude​ for single pack operation

Pneumatics

50
Q

E1/E2

Max​ differencial pressure

Pneumatics

51
Q

E1/E2

Max​ negative differential pressure​

Pneumatics

52
Q

E1

Max gear retraction speed VLO

Speeds

53
Q

E1/E2

Max differential pressure for takeoff & landing​

Pneumatics

54
Q

E1

Max gear extension speed VLO

Speeds

55
Q

E1

Max​ gear extended speed​ V​LE

Speeds

56
Q

E1

Min altitude​ for​ autopilot​ use precision approach

Autoflight

A

50 ft below DH/DA

57
Q

E1/E2

Min altitude​ for​ autopilot​ use nonprecision approach

Autoflight

58
Q

E1

Min altitude​ for​ autopilot​ use enroute

Autoflight

A

500 ft AGL

59
Q

E1

Min altitude​ for​ autopilot​ use Visual​ Approach​ not​ backed up by instrument procedure

Autoflight

A

500 ft AGL

60
Q

E1/E2

Min Engagement Height Takeoff

Autoflight

A

Acceleration Altitude

61
Q

E1/E2

Min Engagement Height other than Takeoff

Autoflight

A

400 ft AGL

62
Q

E1/E2

Limit Maneuvering Load Factors
Flaps Up

Autoflight

A

- 1.0G to + 2.5G

63
Q

E1/E2

Limit Maneuvering Load Factors
Flaps​ down (1, 2, 3, 4, 5 and​ full)

Autoflight

A

0.0G to + 2.0G

64
Q

E1/E2

Max N1

Engine

65
Q

E1/E2

Max N2

Engine

66
Q

E1

Max ITT​ During engine start (on ground)

Engine

67
Q

E1

Max ITT​ During engine start (in flight)

Engine

68
Q

E1

Max ITT​ Takeoff and Go-Around​

Engine

69
Q

E1

Max Continuous ITT

Engine

70
Q

E1

Min Oil Pressure

Engine

71
Q

E1

Max Oil Temperature​

Engine

72
Q

E1

Min temperature for operations

APU

73
Q

E1

Max​ altitude for​ Start

APU

74
Q

E1/E2

Max​ temperature for operations

APU

A

ISA + 35 °C

75
Q

E1

Max​ altitude for​ electrical​ supply

APU

76
Q

E1

Max​ altitude to assist​ engine start​

APU

77
Q

E1

Max​ EGT​ Continuous

APU

78
Q

E1/E2

Max​ altitude for​ bleed​ supply

APU

79
Q

E1/E2

Max​ rotor speed

APU

80
Q

E1/E2

Max​ EGT​ start

APU

81
Q

E1/E2

The T/O DATASET MENU on the MCDU​ must be set to EN​G in the following cases

Anti-Ice System

A
  • when​ OAT is between 5ºC and 10ºC and;
  • if​​ there is any possibility of encountering visible moisture​ up to 1700 ft AFE.
82
Q

E1/E2

The T/O DATASET MENU on the MCDU​ must be set to ALL in the following cases

Anti-Ice System

A
  • when​ OAT is below 5ºC and;
  • if​​ there is any possibility of encountering visible moisture​ up to 1700 ft AFE.
83
Q

E1/E2

Do​ not hold ________ with slats/flaps​ extended.

Anti-Ice System

A

in icing conditions

84
Q

E1

Maximum fuel capacity

Fuel

A

13,192​ kg

85
Q

E2

Maximum fuel capacity

Fuel

86
Q

E1/E2

Do not attempt a go-around​ maneuver after ____

Thrust Reversers

A

deployment of the thrust ​reversers

87
Q

E1

Maximum value​ for​ Last Minute Change

LMC

88
Q

E1

Engine Warm-up

Engine

A

two​ (2) minutes

89
Q

E1

Engine Shutdown

Engine

A

two​ (2) minutes

Ejet E179 (2 decks)

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