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From Flashcardlet > SkyWest ERJ-175 Limitations > Flashcards

SkyWest ERJ-175 Limitations Flashcards

0
Q

Max. T/O Wt. lb

A

85517

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1
Q

Max. Ramp Wt. lb

A

85870

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2
Q

Max. Lnd. Wt. lb

A

74957

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3
Q

Max. Zero Fuel Wt. lb

A

69886

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4
Q

Max AFT Cargo lb

A

2535

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5
Q

Max. FWD Cargo lb

A

3306

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6
Q

Min. Runway Width ft (SW)

A

100

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7
Q

Wing Span tip-to-tip ft/in

A

93/11

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8
Q

Aircraft Length ft/in

A

103/11

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9
Q

Tail Height ft/in

A

32/3

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10
Q

Max. Ops. Alt. ft

A

41000

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11
Q

Max. T/O & Lnd ft

A

8000

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12
Q

Max. Temp. T/O Lnd ISA +__°C

A

35

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13
Q

Min. Temp. T/O Lnd °C

A

-40

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14
Q

RWY Slope +/-__%

A

2

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15
Q

Max. Tailwind kt

A

15

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16
Q

Max. Single Pack Operations ft

A

31000

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17
Q

VMO SL-8,000’ kt

A

300

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18
Q

VMO 10,000 - Mach Transition kt

A

320

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19
Q

MMO

A

.82

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20
Q

VA kt

A

240

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21
Q

VLO EXT kt

A

250

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22
Q

VLE RET kt

A

250

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23
Q

VLE kt

A

250

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24
Q

V Tire kt

A

195

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25
Q

V RAT DEPLOY MAX

A

Vmo/Mmo

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26
Q

VMIN (to provide electrical power) kt

A

130

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27
Q

VB (below 10,000 ft) kt

A

250

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28
Q

VB (10,000 ft and above) kt/M (whichever is lower)

A

270/.76

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29
Q

V wiper ops max (SW) kt

A

250

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30
Q

Vwindow kt

A

160

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31
Q

VFE 1 kt

A

230

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32
Q

VFE 2 kt

A

215

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33
Q

VFE 3 kt

A

200

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34
Q

VFE 4 kt

A

180

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35
Q

VFE 5 kt

A

180

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36
Q

FULL [FLAP] kt

A

165

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37
Q

Max recommended xwind, Dry Rwy kt

A

38

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38
Q

Max recommended xwind, Wet Rwy kt

A

31

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39
Q

Max recommended xwind, Compacted Snow kt

A

20

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40
Q

Max recommended xwind, Standing Water/Slush/Wet Snow/Dry Snow kt

A

18

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41
Q

Max recommended xwind, Runway with Ice kt

A

12

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42
Q

Due to engine compressor stall possibility, static takeoff is not recommended with crosswind component greater than ____ kt (updated)

A

30

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43
Q

Max. Alt. Flaps/Slats Extended ft

A

20000

44
Q

Enroute Ops [slats/flaps] _________

A

Prohibited

45
Q

Min. Spoiler Speed kt

A

180

46
Q

CAT II Approach, Mandatory flaps __

A

5

47
Q

Landing Flaps Full, go around flaps __

A

4

48
Q

Landing Flaps 5, go around flaps __

A

2

49
Q

Min. Batt. voltage V

A

22.5

50
Q

Min. Batt. temp °C

A

-20

51
Q

Engine start Max °C

A

815

52
Q

Engine start Oil temp., min. °C

A

-40

53
Q

Engine start Oil pressure, min. psi

A

25

54
Q

Engine Start (Ground), Start attempt#:
1 & 2: [ ]Sec. ON; [ ]Sec. OFF
3-5: [ ]Sec ON; [ ]Min. OFF
Answer format: __/__;__/__

A

90/10;90/5

55
Q

Engine Start (In Flight), Start attempt#:
1 & 2: [ ]Sec. ON; [ ]Sec. OFF
3-5: [ ]Sec ON; [ ]Min. OFF
Answer format: __/__;__/__

A

120/10;90/5

56
Q

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

A

90

57
Q

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

A

120

58
Q

Dry Motoring, event#:
1: [ ] Sec. ON; [ ] Min. OFF
2-5: [ ] Sec. ON; [ ] Min. OFF
Answer format: __/__;__/__

A

90/5;30/5

59
Q

After ___ sequential motoring cycles, the process may be repeated following a ___ minute cool down period. __/__

A

5/15

60
Q

If it is necessary to perform an engine start with tailwind, monitor ___ indication. If there is no positive increase of ___ indication before starter cutout __%N2, the engine start must be manually aborted. Format: __/__/__

A

N1/N1/50

61
Q

Takeoff with the Automatic Takeoff Thrust Control System (ATTCS) ___ is not authorized.

A

Off

62
Q

Max. Fuel Capacity lb

A

20935

63
Q

Max. Imbalance lb

A

794

64
Q

Min. Fuel Tank Temp. °C

A

-40

65
Q

Fuel crossfeed must be selected ___ during takeoff and landing.

A

Off

66
Q

Wait ___ seconds after the EICAS is energized to start the APU.

A

30

67
Q

Do not leave the aircraft unattended more than ___ minutes with the APU running (SW).

A

5

68
Q

Simultaneous use of the APU bleed and the HP cart is ___.

A

Prohibited

69
Q

Time between APU Start Attempt 1 & 2 __ seconds off

A

60

70
Q

Third before APU Start Attempt __ minutes off

A

5

71
Q

APU Start Temperature, min. °C

A

-54

72
Q

APU Start Temperature, max. ISA + °C

A

35

73
Q

APU Start Altitude, max. Ft

A

30000

74
Q

APU temp. min. °C

A

-54

75
Q

APU temp. max. ISA+__°C

A

35

76
Q

APU alt. max. Ft

A

33000

77
Q

APU electrical generator use, max. alt. ft

A

33000

78
Q

APU bleed use, max. Ft

A

15000

79
Q

APU engine start, max. alt. Ft

A

21000

80
Q

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

A

7.8

81
Q

Max. Diff. Press., Above 37,000 ft __psi

A

8.34

82
Q

Max. Diff. Over Pressure psi

A

8.77

83
Q

Max. Diff. Neg. Press psi

A

-0.5

84
Q

Max. Diff. Press T/O Lnd psi

A

0.2

85
Q

Min. Hyd. Res. Temp. for ENG Start °C

A

-18

86
Q

Brake temperature indication must be in the ___ range for takeoff.

A

Green

87
Q

Do not attempt a ___ after deployment of the thrust reversers.

A

Go around

88
Q

After selecting reverse thrust, do not move the thrust levers into the ___ until the REV icon on the EICAS is shown in amber or green.

A

Forward thrust range

89
Q

The use of ___ during normal taxi operations is prohibited.

A

Thrust reverse

90
Q

The use of ___ for power back operations is prohibited.

A

Thrust reverse

91
Q

There is ___ temperature limitation for anti-icing automatic operation.

A

No

92
Q

On ground:

• The TO DATASET MENU on the MCDU must be set to ENG in the following cases when OAT is between 5ºC and 10ºC and:

A
  • If there is any possibility of encountering visible moisture up to 1,700 feet 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
93
Q

On ground:

• The TO DATASET MENU on the MCDU must be set to ALL in the following cases when OAT is below 5ºC and:

A
  • If there is any possibility of encountering visible moisture up to 1,700 feet 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
94
Q

In Flight:
• The engine and wing anti-ice systems operate automatically, in case of ice encounter when the ice protection mode selector is in the AUTO position. If either one or both ice detectors are failed, the crew must set the mode selector to ON when icing conditions exist or are anticipated below ___°C TAT with visible moisture.

A

10

95
Q

Icing conditions may exist whenever the Outside Air Temperature (OAT) on the ground or for takeoff, or Total Air Temperature (TAT) in flight, is ___°C or below 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

96
Q

Icing conditions may also exist when the OAT on the ground and for takeoff is ___ °C or below 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.

A

10

97
Q

[Autopilot] Min. Engagement Height ft

A

400

98
Q

[Autopilot] Min. Use Height ft

A

50

99
Q

[Autopilot] Min. Use Height - Non-precision Approach

A

MDA

100
Q

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

A

60

101
Q

While transmitting in ___, standby magnetic compass indication is not valid.

A

VHF1

102
Q

______ altimeter minimums must be used for all CAT I approaches.

A

Barometric

103
Q

_______ approaches using IESS are prohibited.

A

Back course

104
Q

___ is not to be predicated on the use of the Terrain Awareness System.

A

Navigation

105
Q

The use of ___ functions should be manually inhibited when landing at an airport that is not in the database to avoid unwanted alerts.

A

Predictive EGPWS

106
Q

The use of ___ functions should be manually inhibited during QFE operations, if GPS data is unavailable or inoperative.

A

Predictive EGPWS

107
Q

___ instrument approaches are not authorized (SW).

A

RNP

108
Q

The use of FMS Speed Mode is prohibited in the event of an _________.

A

Engine failure

From Flashcardlet (6 decks)

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