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E175 Limitations > E175 Limitations > Flashcards

E175 Limitations Flashcards

1
Q

Max. Ramp Wt.

A

85,870

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2
Q

Max. T/O Wt.

A

85,517

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3
Q

Max. Lnd. Wt.

A

74,957

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4
Q

Max. Zero Fuel Wt.

A

69,886

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5
Q

Max. Aft. Cargo

A

2,535

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6
Q

Max. Fwd. Cargo

A

3,306

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7
Q

Min. Runway Width

A

100’ (SW)

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8
Q

Wing Span

A

93’ 11”

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9
Q

Aircraft Length

A

103’ 11”

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10
Q

Tail Height

A

32’ 4”

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11
Q

Battery Min Voltage

A

22.5

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12
Q

Engine Start Max. Temp

A

815°C

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13
Q

Min. Oil Temp Start

A

-40°C

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14
Q

Min. Oil Pressure Start

A

25 psi

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15
Q

Engine Start Cranking Limits (Ground) 1&2

A

90 Sec Max Cumulative On 10 Sec Off

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16
Q

Engine Start Cranking Limits (Ground) 3-5

A

90 Sec Max Cumulative On 5 Min Off

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17
Q

Engine Start Cranking Limits (Flight) 1&2

A

120 Sec Max Cumulative On 10 Sec Off

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18
Q

Engine Start Cranking Limits (Flight) 3-5

A

120 Sec Max Cumulative On 5 Min Off

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19
Q

Engine Dry Motoring Limits Attempt 1

A

90 Sec On 5 Min Off

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20
Q

Engine Dry Motoring Limits Attempt 2-5

A

30 Sec On 5 Min Off

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21
Q

Engine Dry Motoring After 5 Attempts

A

The process may be repeated following a 15 minute cool down period.

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22
Q

When it is necessary to perform an engine start with tailwind, monitor N1 indication.

A

When there is no positive increase of N1 indication before starter cutout (50% N2), the engine start must be manually aborted.

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23
Q

Takeoff with the Automatic Takeoff Thrust Control System (ATTCS) OFF

A

Not authorized.

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24
Q

Max. Fuel Capacity

A

20,935 lb

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25
Q

Max. Fuel Imbalance

A

794 lb

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26
Q

Min. Fuel Tank Temp.

A

-40°C

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27
Q

Fuel crossfeed must be selected

A

OFF during takeoff and landing.

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28
Q

APU Start, after the EICAS is energized.

A

Wait 30 seconds to start the APU.

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29
Q

Max. aircraft unattended with APU running.

A

5 Min.

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30
Q

APU Start Limit 1&2

A

60 Sec. off

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31
Q

APU Start Limit 3

A

5 Min.

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32
Q

APU Min./Max. Start Temp.

A

-54°C/ ISA +35°C

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33
Q

APU Min./Max. Continuous Operation Temp.

A

-54°C/ ISA +35°C

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34
Q

Max Alt. APU Start

A

30,000 ft.

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35
Q

Max. Alt. APU Operation

A

33,000 ft.

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36
Q

Max. Alt APU Gen. Use

A

33,000 ft.

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37
Q

Max. Alt APU Bleed Use

A

15,000 ft.

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38
Q

Max. Alt APU Engine Start

A

21,000 ft.

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39
Q

Max. Diff. Press. Up to 37,000 ft.

A

7.8 psi

40
Q

Max Diff. Press. Above 37,000 ft.

A

8.34 psi

41
Q

Max Diff. Over Press.

A

8.77 psi

42
Q

Max Diff Press. T/O & Lnd

A

0.2 psi

43
Q

Min. Hydraulic Reservoir Temp For Eng. Start

A

-18°C

44
Q

Brake temperature indication for takeoff.

A

Must be in the green range.

45
Q

Do not attempt a go-around maneuver.

A

After deployment of the thrust reversers.

46
Q

After selecting reverse thrust, do not move the thrust levers into the forward thrust range.

A

Until the REV icon on the EICAS is shown in amber or green.

47
Q

The use of thrust reversers during normal taxi operations is:

A

Prohibited.

48
Q

The use of thrust reversers for power back operations is:

A

Prohibited.

49
Q

The TO DATASET MENU on the MCDU must be set to ENG in the following cases:

A

When OAT is between 5°C and 10°C and: – When there is any possibility of encountering visible moisture up to 1,700 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.

50
Q

The TO DATASET MENU on the MCDU must be set to ALL in the following cases:

A

when OAT is below 5°C and: – When there is any possibility of encountering visible moisture up to 1,700 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.

51
Q

When either one or both ice detectors are failed:

A

The crew must set the mode selector to ON when icing conditions exist or are anticipated below 10°C TAT with visible moisture.

52
Q

Auto Pilot Min. Engagement Alt. T/O.

A

400 ft. AGL

53
Q

Auto Pilot Min. Use Alt.

A

50 Ft. AGL

54
Q

Auto Pilot Min. Use Alt. Non-Precision Approach

A

MDA

55
Q

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

A

60 kt.

56
Q

While transmitting in VHF1, the standby magnetic compass indication is:

A

Not valid.

57
Q

Barometric altimeter minimums must be used for all:

A

CAT I approaches.

58
Q

Back course approaches using IESS are:

A

Prohibited.

59
Q

Navigation is not to be predicated on the use of:

A

The Terrain Awareness System.

60
Q

The use of predictive EGPWS functions should be manually inhibited when:

A

Landing at an airport that is not in the database to avoid unwanted alerts.

61
Q

The use of predictive EGPWS functions must be manually inhibited during:

A

QFE operations, when GPS data is unavailable or inoperative. Press in the GRD PROX TERR INHIB button to inhibit predictive EGPWS functions.

62
Q

RNP instrument approaches are:

A

Not authorized (SW).

63
Q

The use of FMS Speed Mode in the event of an engine failure.

A

Is prohibited.

64
Q

Max. Ops. Alt.

A

41,000

65
Q

Max Alt. T/O And Land

A

8000

66
Q

Max. RWY Slope

A

+/- 2%

67
Q

Max Tail Wind

A

15 kts

68
Q

Max Single Pack ops.

A

31,000

69
Q

VMO SL-8,000

A

300

70
Q

VMO 10,000-Mach Transition

A

320

71
Q

MMO

A

0.82

72
Q

VA

A

240

73
Q

VLO EXT, RET & VLE

A

250

74
Q

V Tire

A

195

75
Q

V RAT Deploy Max.

A

VMO/MMO

76
Q

V Min to provide RAT Power

A

130

77
Q

VB (Below 10,000’)

A

250

78
Q

VB (10,000 & Above)

A

270/.76M (Whichever is lower)

79
Q

V Wiper Ops. Max.

A

250 (SW)

80
Q

V Window

A

160

81
Q

VFE 1

A

230

82
Q

VFE 2

A

215

83
Q

VFE 3

A

200

84
Q

VFE 4

A

180

85
Q

VFE 5

A

180

86
Q

VFE Full

A

165

87
Q

Max. Xwind Dry RWY.

A

38 KTS.

88
Q

Max. Xwind Wet RWY.

A

31 KTS.

89
Q

Max. Xwind Compacted Snow

A

20 KTS.

90
Q

Max. Xwind Standing Water / Wet & Dry Snow

A

18 KTS.

91
Q

Max. Xwind Ice

A

12 KTS.

92
Q

Max Alt. Flaps / Slats Extended

A

20,000

93
Q

Flap / Slats Enroute Ops.

A

Prohibited

94
Q

Min Spoiler Speed

A

180 KTS.

95
Q

CAT II Approach Mandatory Flaps:

A

5

96
Q

Landing Flaps Full, Go-Around Flaps:

A

4

97
Q

Landing Flaps 5, Go-Around Flaps:

A

2

E175 Limitations (1 decks)

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