Limitations Flashcards

1
Q

What is the maximum ramp weight for EMBRAER 195 LR?

A

50950 kg

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2
Q

What is the maximum landing weight (MLW) for EMBRAER 195 LR?

A

42500 kg

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3
Q

What is the maximum zero fuel weight for EMBRAER 195 LR?

A

45000 kg

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4
Q

What is the maximum takeoff weight (MTOW) for EMBRAER 195 LR?

A

50790 kg

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5
Q

What is the maximum altitude for flap extended?

A

20000 ft

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6
Q

Vlo retraction speed

A

235

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7
Q

Vlo for extension

A

265 KIAS.

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8
Q

Vle speed

A

265 kias

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9
Q

Maximum flap extended speed for Flaps 1

A

230 KIAS

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10
Q

Maximum flap extended speed for Flaps 2

A

215 KIAS

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11
Q

Maximum flap extended speed for Flaps 3

A

200 KIAS

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12
Q

Maximum flap extended speed for Flaps 4

A

180 KIAS

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13
Q

Maximum flap extended speed for Flaps 5

A

180 kias

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14
Q

Maximum flap extended speed for Flaps full

A

165 kias

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15
Q

Maximum Takeoff and Landing Tailwind Component

A

10 kt

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16
Q

Maximum Landing Speed

A

165 KIAS

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17
Q

Maximum tire Ground Speed:

A

195 kt

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18
Q

What is the crosswind component limit(not recommended) for static takeoff?

A

The crosswind component limit for static takeoff is 30 kt.

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19
Q

What is the load factor limit for flaps up?

A

2.5 g

Negative limit is -1.00 g.

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20
Q

What is the load factor limit for flaps down? Flaps 1,2,3,4,5 and full

A

Positive 2g
Negative 0 g

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21
Q

What is the maximum usable quantity per wing tank:

A

6550 kg / 8076,3 L

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22
Q

What is the unusable quantity per wing tank?

A

56.7 l (46 kg)

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23
Q

What is the maximum permitted imbalance between wing tanks?

A

360 kg

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24
Q

What is the maximum fuel capacity?

A

16266 l (13192 kg)

Note: The weights above have been determined for an adopted fuel density of 0.811 kg/l.

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25
Q

APU max start alt:

A

30000ft

26
Q

APU max operation alt:

A

33000 ft

27
Q

APU to assist engine strats alt:

A

21000ft

28
Q

APU electrical Gen alt:

A

33000ft

29
Q

APU bleed altitude:

A

15000ft

30
Q

APU starter limits first and second attempt

A

60s off

31
Q

APU starter limits third attempt

A

5 min off

32
Q

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

A

There is no temperature limitation for anti-icing system automatic operation.

33
Q

When do icing conditions exist?

A

Icing conditions may exist when the Outside Air Temperature (OAT) is 10°C or below and visible moisture is present.

34
Q

What forms of visible moisture can indicate icing conditions?

A

Visible moisture can include clouds, fog with visibility of one mile or less, rain, snow, sleet, and ice crystals.

35
Q

What additional conditions may indicate icing on the ground?

A

Icing conditions may exist when the OAT is 10°C or below on ramps, taxiways, or runways with surface snow, ice, standing water, or slush.

36
Q

What caution should be taken regarding the anti-icing system on the ground?

A

Do not rely on visual icing evidence or ice detector actuation to turn on the anti-icing system.

37
Q

What criteria should be used to activate the anti-icing system?

A

Use the temperature and visual moisture criteria as specified.

38
Q

What could happen if the anti-icing system is activated too late?

A

Delaying the use of the anti-icing system may result in ice ingestion and possible engine damage or flameout.

39
Q

What is required during ground operations of more than 30 minutes in icing conditions?

A

A static engine run-up is required before takeoff.

40
Q

What is the maximum airspeed for windshield wiper operation?

A

The maximum airspeed for windshield wiper operation is 253 KIAS.

41
Q

Max Vmo

A

0.82

42
Q

Autopilot: What is the minimum use height for cruise/descent?

A

1000ft

43
Q

Autopilot: What is the minimum use height for approach?

A

50 ft

44
Q

Autopilot: what is the minimum engagement height?

A

400 ft

45
Q

Doors max operating Gust wind open and close

A

40 kts

46
Q

Doors max wind fully open in kts

A

65 kts

47
Q

Max diff pressure below 37000ft.

A

7.8 psi

48
Q

Max diff pressure above 37000ft.

A

8.4 psi

49
Q

Max diff overpressure psi

A

8.8 psi

50
Q

Max diff. Press for t/i + ldn psi

A

0.2 psi

51
Q

Max negative diff. Pressure psi

A

-0.5 psi

52
Q

Positive pressure relief opens psi

A

8.6 psi

53
Q

Max celing ft

A

41.000ft

54
Q

Min takeoff altitude

A
  • 1000ft
55
Q

Max takeoff altitude

A

10.000ft

56
Q

Min. Temp. For TO + LDN

A
  • 40°
57
Q

Max itt eng start air/ground

A

875/740

58
Q

Max itt Cont

A

960°

59
Q

Max itt toga AEO

A

983°

60
Q

Max itt toga OEI

A

983°

61
Q

Max oil temp cont

A

155°