ERJ 175 Limitations Flashcards

1
Q

Max Ramp Weight

A

85,870 lbs

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2
Q

Max Take Off Weight

A

85,517 lbs

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3
Q

Max Landing Weight

A

74,957 lbs

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4
Q

Max Zero Fuel Weight

A

69,886 lbs

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5
Q

Max Aft Cargo Weight

A

2535 lbs

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6
Q

Max Fwd Cargo Weight

A

3306 lbs

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7
Q

Min Runway Width

A

100 ft (SW)

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8
Q

Wing Span

A

93 ft 11 in

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9
Q

Aircraft Length

A

103 ft 11 in

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10
Q

Tail Height

A

32 ft 4 in

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11
Q

Distance between main landing gear tires

A

17 ft 1 inch

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12
Q

Height to the top of winglets

A

15 ft 12 in

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13
Q

Max Ops Altitude

A

41,000 ft

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14
Q

Max Take Off and Land Airport Elevation

A

8000 ft

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15
Q

Max Temp Take Off and Land

A

ISA + 35 deg C (52 deg C)

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16
Q

Min Temp Take Off and Land

A

-40 deg C

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17
Q

Max RWY Slope

A

+/- 2%

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18
Q

Max Tail Wind

A

15 Kt

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19
Q

Max Single Pack Ops

A

31,000 ft

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20
Q

Vmo Sea Level - 8000 ft

A

300 KIAS

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21
Q

Vmo 10,000 - Mach Transition

A

320 KIAS

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22
Q

Mmo

A

.82 Mach

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23
Q

Va

A

240 KIAS

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24
Q

Vlo Ext

A

250 KIAS

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25
Q

Vle

A

250 KIAS

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26
Q

Vle Retract

A

250 KIAS

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27
Q

V Tire

A

195 KIAS

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28
Q

V Rat Deploy Max

A

Vmo / Mmo

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29
Q

Vmin ( to provide electrical power )

A

130 KIAS

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30
Q

Vb below 10,000 ft

A

250 KIAS

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31
Q

Vb 10,000 ft and above

A

270 KIAS / .76 Mach (whichever is lower)

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32
Q

V wiper ops max

A

250 (SW)

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33
Q

V window

A

160 KIAS

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34
Q

Vfe 1

A

230 KIAS

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35
Q

Vfe 2

A

215 KIAS

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36
Q

Vfe 3

A

200 KIAS

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37
Q

Vfe 4

A

180 KIAS

38
Q

Vfe 5

A

180 KIAS

39
Q

V f - Full

A

165 KIAS

40
Q

Max Recommended Crosswind - Dry Runway

A

38 Kts

41
Q

Max Rec Crosswind - Wet Runway

A

32 Kts

42
Q

Max Rec Crosswind - Compacted Snow

A

28 KTS

43
Q

Max Rec Crosswind - Standing Water / Slush / Wet Snow / Dry Snow

A

18 Kts

44
Q

Max Rec Crosswind - Ice

A

12 Kts

45
Q

Static Take Off not recommended with XW of

A

30 Kts

46
Q

Max Altitude Flaps / Slats Extended

A

20,000 ft

47
Q

Max Enroute Ops Flaps / Slats Extended

A

Prohibited

48
Q

Min Spoiler Speed

A

180 KIAS

49
Q

CAT II Approach Flap Setting

A

Mandatory Flaps 5

50
Q

Landing Flaps Full

A

Go Around Flaps 4

51
Q

Landing Flaps 5

A

Go Around Flaps 2

52
Q

Min Battery Voltage

A

22.5 Volts

53
Q

Max ITT Engine Start

A

815 degs C

54
Q

Min Oil Temp

A

-40 degrees C

55
Q

Min Oil Pressure

A

25 psi

56
Q

Engine Starts 1 and 2 limits on Ground

A

90 Seconds ON - 10 Seconds Off

57
Q

Engine Starts 3 through 5 on Ground

A

90 Seconds ON - 5 Minutes OFF

58
Q

Engine Starts 1 and 2 in Flight

A

120 Seconds ON - 10 Seconds OFF

59
Q

Engine Starts 3 through 5 in Flight

A

120 Seconds ON - 5 Min OFF

60
Q

Max Cumulative Starter Run Time per start on the ground

A

90 Seconds

61
Q

Max Cumulative Starter Run Time in Flight

A

120 Seconds

62
Q

Max Cumulative Starter Run Time on the Ground

A

90 Seconds ( Motoring plus start time)

63
Q

Dry Motoring Limits

A

First Start 90 Seconds ON - 5 Minutes OFF
Starts 2 - 5 30 Seconds ON - 5 Minutes OFF

64
Q

Engine Start Tail Wind Limitation

A

When there is no positive N1 indication prior to starter cutout, the start must be aborted.

65
Q

Take Off with ATTCS OFF

A

is not authorized

66
Q

Max Fuel Capacity

A

20,935 lbs

67
Q

Max Fuel Imbalance

A

794 lbs

68
Q

Min Fuel Tank Temp

A

-40 degs C

69
Q

Take Off with FUEL IMBALANCE message

A

permissible as long as imbalance does not exceed 794 lbs.

70
Q

Wait _______ Seconds after EICAS is energized to start APU

A

30 Seconds

71
Q

Simultaneous use of the APU bleed and HP cart

A

Prohibited

72
Q

APU Start Limits

A

Start 1 and 2 - 60 seconds OFF

Third attempt - 5 minutes OFF

73
Q

Max Altitude for APU Start

A

30,000 ft

74
Q

Max Temperature for APU Start

A

ISA + 35 C

75
Q

Min Temperature for APU Start

A

-54 C

76
Q

Max Altitude for APU Electrical Generator Use

A

33,000 ft

77
Q

Max Altitude for APU Bleed Use

A

15,000 ft

78
Q

Max Altitude for APU assisted Engine Start

A

21,000 ft

79
Q

Max Differential Pressure Up to 37,000 ft

A

7.8 psi

80
Q

Max Differential Pressure above 37,000 ft

A

8.34 psi

81
Q

Max Differential Over Pressure

A

8.77 psi

82
Q

Max Differential Negative Pressure

A
  • 0.5 psi
83
Q

Max Differential Pressure for Takeoff and Landing

A

0.2 psi

84
Q

Min Reservoir Temp for Engine Start

A

-18 deg C

85
Q

Auto Pilot Min Engagement Height

A

400 ft

86
Q

Auto Pilot Min Use Height

A

50 ft

87
Q

Can you use the auto pilot below the MDA on a non precision approach?

A

NO

88
Q

Can you fly a LOC Back Course using the IESS

A

NO - Prohibited

89
Q

The DATASET MENU must be set to ENG when OAT is between ___ deg C and ____ deg C and: when there is a possibility of visible moisture up to ______ ft AFE

A

5 deg C
10 deg C
1700 AFE
And when operating on contaminated ramps or taxi ways.

90
Q

The DATASET MENU must be set to ALL when OAT is below ____ deg C and: when there is a possibility of visible moisture up to ______ ft AFE

A

5 deg C

1700 AFE