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Ele E1 > Ejet E1 - Limitations > Flashcards

Ejet E1 - Limitations Flashcards

1
Q

What’s the Maximum Landing Weight (MLW) of E-190?

A

43.000kg

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2
Q

What’s the Maximum Ramp Weight (MRW) of E-190 AR?

A

50.460 kg

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3
Q

What’s the Maximum Takeoff Weight (MTOW) of E-190 AR?

A

50.300 kg

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4
Q

What’s the Maximum Zero Fuel Weight (MZFW) of E-190 AR?

A

40.800 kg

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5
Q

The airplane may not takeoff without further maintenance inspection if it landed at what temperature?

A

-40º C

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6
Q

What’s the maximum altitude for flap extension?

A

20.000 ft

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7
Q

What’s the maximum and minumum altitude for takeoff, landing and ground start?

A

10.000 ft / -1.000 ft

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8
Q

What’s the Vlo for retration?

A

235 KIAS

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9
Q

What’s the Vlo for extension?

A

265 KIAS

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10
Q

What’s the Vle?

A

265 KIAS

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11
Q

What’s the maximum speed to open the Direct Vision Window?

A

160 KIAS

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12
Q

Maneuvers that involve angle of attack near the stall or full application of rudder, elevator, and aileron controls should be confined to speeds below ….

A

VA

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13
Q

Rapid and large alternating control inputs, especially in combination with large changes in pitch, roll or yaw (e.g. large side slip angles) may result in…

A

structural failures at any speed, even below VA

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14
Q

What’s the VFE for Flaps 1?

A

230 KIAS

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15
Q

What’s the VFE for Flaps 2?

A

215 KIAS

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16
Q

What’s the VFE for Flaps 3?

A

200 KIAS

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17
Q

What’s the VFE for Flaps 4?

A

180 KIAS

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18
Q

What’s the VFE for Flaps 5?

A

180 KIAS

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19
Q

What’s the VFE for Flaps FULL?

A

165 KIAS

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20
Q

What’s the maximum tire ground speed?

A

195 KT ( 225 mph)

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21
Q

What’s the maximum takeoff and landing tailwind component?

A

10 kt

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22
Q

What’s the maximum recommended crosswind for takeoff and landing in a DRY RUNWAY?

A

38 kt

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23
Q

What’s the maximum recommended crosswind for takeoff and landing in a WET runway?

A

31 kt

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24
Q

What’s the maximum recommended crosswind for takeoff and landing in a runway with COMPACTED SNOW?

A

20 kt

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25
Q

What’s the maximum recommended crosswind for takeoff and landing in a runway with STANDING WATER / SLUSH / WET SNOW / DRY SNOW?

A

18 kt

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26
Q

Due to …… possibility, static takeoff is not recommended with crosswind component greater than 25 kt

A

engine compressor stall

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27
Q

Due to engine compressor stall possibility, static takeoff is not recommended with crosswind component greater than …… kt

A

25 kt

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28
Q

What are the runway slope limits?

A

-2% to +2%

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29
Q

The use of predictive EGPWS functions should be manually inhibited when landing to an airport that is not ….. to avoid unwanted alerts.

A

in the airport database

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30
Q

The use of predictive EGPWS functions should be manually …….. when landing to an airport that is not in the airport database to avoid ……….

A

inhibited / unwanted alerts

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31
Q

The use of predictive EGPWS functions should be manually inhibited during ….. operations if GPS data is unavailable or inoperative.

A

QFE

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32
Q

The use of predictive EGPWS functions should be manually inhibited during QFE operations if ….. or …..

A

GPS data is unavailable / inoperative

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33
Q

What is the maximum fuel quantity (E190/E195)?

A

16.266 LT (13.192 kg )

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34
Q

What is maximum permitted imbalance between wing tanks?

A

360 kg

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35
Q

What is the minimum fuel tank temperature

A

-37º C

36
Q

The Fuel Crossfeed Selector Knob must be set ….. during takeoff and landing.

A

OFF

37
Q

What’s the lowest temperature to start the APU?

A

-54º C

38
Q

What’s the maximum altitude for APU operation?

A

33.000 ft

39
Q

What’s the maximum altitude for APU bleed?

A

15.000 ft

40
Q

What’s the maximum altitude for APU assisted engine star?

A

21.000 ft

41
Q

What’s the maximum altitude for APU eletric supply?

A

33.000 ft

42
Q

What’s the maximum altitude for APU start?

A

30.000 ft

43
Q

What’s the maximum APU RPM?

A

108%

44
Q

What’s the maximum APU start temperature?

A

1032º C

45
Q

What’s the maximum APU continous operation temperature?

A

717º C

46
Q

What are the APU starter limits?

A

1st and 2nd => 60 s OFF

3rd => 5 min OFF

47
Q

What’s the maximum N1?

A

100%

48
Q

What’s the minimum and maximum N2?

A

59,27% / 100%

49
Q

What’s the maximum ITT for ground start?

A

740º C

50
Q

What’s the maximum ITT for inflight start?

A

875º C

51
Q

What’s the maximum ITT for normal takeoff and go around?

A

945º C limited to 5 min

52
Q

What’s the maximum ITT for maximum takeoff and go around?

A

983º C limited to 5 min

53
Q

When the maximum takeoff and go around is automatically engaged?

A
  • one engine inoperative
  • windshear conditions
54
Q

During starts with oil temperature below -22°C the minimum oil pressure is … psi, time limited to… min.

A

5 psi / 2 min

55
Q

During starts with oil temperature below … °C the minimum oil pressure is 5 psi, time limited to 2 min.

A

-22º C

56
Q

What’s the minimum oil pressure?

A

25 psi

57
Q

What’s maximum oil temperature for continous operation?

A

155º C

58
Q

What are the engine dry motoring duty cycle limits?

A
  • 1st = 90 s + 5 min cool- time
  • 2nd to 5th = 30 sec + 5 min cool-down
  • 15min cool-down after five sequential motorings
59
Q

After five sequential motorings, engine start cycle may be repeated following a …. minute cool-down period.

A

15 minutes

60
Q

For ground starts, the maximum cumulative starter run time per start attempt is ….. seconds (motoring plus start time).

A

90 sec

61
Q

For in-flight starts, the maximum cumulative starter run time per start attempt is …. seconds (motoring plus start time).

A

120 sec

62
Q

After applying thrust reverser, do not move thrust levers back to the forward thrust range, unless ….

A

the REV icon on EICAS is shown amber or green

63
Q

Reduced takeoff thrust based on the assumed temperature must not exceed … % of the full takeoff thrust.

A

25%

64
Q

What’s the maximum differential pressure?

A

8.4 psi

65
Q

What’s the maximum differential overpressure?

A

8.8 psi

66
Q

What’s the maximum differential negative pressure?

A

-0.5 psi

67
Q

What’s the maximum differential pressure for Takeoff and Landing?

A

0.2 psi

68
Q

What’s the temperature limitation for anti-icing system automatic operation?

A

There is no limitation!

69
Q

The TO DATASET MENU on the MCDU must be set to ENG when OAT is between 5°C and 10°C and:

A
  • if there is any possibility of encountering visible moisture up to 1700 ft AFE
  • when operating on ramps, taxiways, or runways where surface snow, ice, standing water, or slush may be ingested by the engines, or freeze on engines, nacelles, or engine sensor probes.
70
Q

The TO DATASET MENU on the MCDU must be set to ENG when OAT is between …°C and …°C and if there is any possibility of encountering visible moisture up to ….. ft AFE

A

5°C / 10°C / 1700 ft

71
Q

If either one or both ice detectors are failed, the crew must set the mode selector to …. when icing conditions exist or are anticipated below .. °C TAT with…..

A

ON / 10º C / visible moisture

72
Q

Icing conditions may exist whenever the OAT on the ground or for T/O or TAT in flight is igual or bellow ….°C and visible moisture in any form is present (such as clouds, fog with visibility of one mile or less, rain, snow, sleet, and ice crystals)

A

10 ºC

73
Q

What’s the maximum airspeed for windshield wiper operation?

A

253 KIAS

74
Q

Delaying the use of ….. until ice buid-up is visible from the cockpit may result in ice ingestion and possible engine damage or flameout

A

the anti-icing system

75
Q

Delaying the use of the anti-icing system until ice buid-up is visible from the cockpit may result in ice ingestion and possible …. or …..

A

engine damage / flameout

76
Q

What’s the minimum autopiloto use height?

A

50 ft

77
Q

TAS, TAT and SAT information are only valid above … KIAS.

A

60 KIAS

78
Q

While transmitting in …. the standby magnetic compass indication is not valid.

A

VHF1

79
Q

While transmitting in VHF1 the ….. indication is not valid

A

standby magnetic compass

80
Q

Back course approaches using IESS are …..

A

prohibited

81
Q

Back course approaches using …. are prohibited.

A

IESS

82
Q

Baro altimeter minimums must be used for all …. approaches.

A

CAT I

83
Q

The airplanes may be operated within the North and South magnetic polar cut-out regions, but ….. and …… will not be available.

A

IRS magnetic heading / track angle magnetic data

84
Q

Whenever operating within North or South magnetic polar cut-out regions, current airplane heading must be referenced to …. heading, if not already selected. Otherwise, the…. flag will be displayed.

A

true / Heading Failure Indication

85
Q

What’s the maximum latitude for stationary alignment?

A

78.25° Northern and Southern

Ele E1 (5 decks)

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