Ye Ole Limits and Mems (Updated '19CQ) Flashcards

1
Q

ENGINE ABNORMAL START

A

AFFECTED ENGINE&raquo_space;> START/STOP SELECTOR = STOP

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2
Q

CABIN ALTITUDE HI
or
SMOKE/FIRE/FUMES

A

OXYGEN MASKS&raquo_space;> DON, 100%

CREW COMMUNICATION&raquo_space;> ESTABLISH

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3
Q

SMOKE EVACUATION

A

OXYGEN MASKS»> DON, EMERG
CREW COMMUNICATION&raquo_space;> ESTABLISH
PRESSURIZATION DUMP&raquo_space;> PUSH IN

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4
Q

BATT 1 (2) OVERTEMP

A

ASSOCIATED BATTERY&raquo_space;> OFF

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5
Q

JAMMED CONTROL COLUMN - PITCH

A

ELEVATOR DISCONNECT HANDLE&raquo_space;> PULL

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6
Q

JAMMED CONTROL COLUMN - ROLL

A

AILERON DISCONNECT HANDLE&raquo_space;> PULL

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7
Q

PITCH TRIM RUNAWAY

A

A/P DISCONNECT BUTTON&raquo_space;> PRESS AND HOLD

PITCH TRIM SYS 1and2 CUTOUT BUTTONS&raquo_space;> PUSH IN

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8
Q

ROLL (YAW) TRIM RUNAWAY

A

A/P DISCONNECT BUTTON&raquo_space;> PRESS AND HOLD

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9
Q

STEERING RUNAWAY

A

STEER DISC SWITCH&raquo_space;> PRESS

Steer airplane using differential braking and rudder.

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10
Q

MTW (LR)

A

85,870 lb.

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11
Q

MTOW (LR)

A

85,517 lb.

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12
Q

MLW (LR and LL)

A

74,957 lb.

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13
Q

MZFW (LR)

A

69,886 lb.

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14
Q

Minimum Runway Width

A

100 ft (SW)

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15
Q

Wing Span

A

93 ft 11 in

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16
Q

Length

A

103 ft 11 in

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17
Q

Tail Height

A

32 ft 4 in

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18
Q

Max Ops Altitude

A

41,000 ft

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19
Q

Max Takeoff/Landing Altitude

A

8,000 ft

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20
Q

Max Temp Takeoff/Landing

A

ISA + 35C (52C)

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21
Q

Min Temp Takeoff/Landing

A

-40C

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22
Q

Runway Slope

A

+/- 2%

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23
Q

Max Tailwind

A

15 kt

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24
Q

Max Single Pack Ops

A

31,000 ft

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25
Q

MMO

A

0.82

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26
Q

VMO SL to 8,000’

A

300

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27
Q

VMO 10,000’ to Mach Transition

A

320

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28
Q

VA

A

240

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29
Q

VLOext / VLEret / VLE

A

250

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30
Q

VTIRE

A

195

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31
Q

VRAT Deploy Max

A

VMO/MMO

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32
Q

VMIN (to supply electrical power)

A

130

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33
Q

VB (<10,000’)

A

250

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34
Q

VB (>10,000’)

A

270 / .76M (whichever is lower)

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35
Q

V wiper ops max

A

250 (SW)

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36
Q

Vwindow

A

160

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37
Q

VFE 1

A

230

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38
Q

VFE 2

A

215

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39
Q

VFE 3

A

200

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40
Q

VFE 4

A

180

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41
Q

VFE 5

A

180

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42
Q

FULL flaps

A

165

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43
Q

Dry Runway Max Crosswind (Rec’d)

A

38 kt

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44
Q

Wet Runway Max Crosswind (Rec’d)

A

31 kt

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45
Q

Compact Snow Runway Max Crosswind (Rec’d)

A

20 kt

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46
Q

Standing Water/Slush/WetSnow/DrySnow Runway Max Crosswind (Rec’d)

A

18 kt

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47
Q

Icy Runway Max Crosswind (Rec’d)

A

12 kt

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48
Q

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

A

30 kt

49
Q

Max Altitude Flaps/Slats Extended

A

20,000 ft

50
Q

Flaps/Slats Enroute Operations

A

Prohibited

51
Q

Minimum Spoiler Speed

A

180

52
Q

CAT II Approach Flap Setting

A

Mandatory Flaps 5

53
Q

Landing Flaps Full, G/A Flaps =

A

Flaps 4

54
Q

Landing Flaps 5, G/A Flaps =

A

Flaps 2

55
Q

Battery Min Voltage

A

22.5 V

56
Q

Engine Start Max Temp Max

A

815C

57
Q

Engine Start Oil Temp Min

A

-40C

58
Q

Engine Start Oil Pressure Min

A

25 psi

59
Q

Engine Start Ground, First and Second Attempt

A

90 seconds ON, 10 seconds OFF

60
Q

Engine Start Ground, Third, Fourth, Fifth Attempts

A

90 seconds ON, 5 minutes OFF

61
Q

Engine Start Flight, First and Second Attempt

A

120 seconds ON, 10 seconds OFF

62
Q

Engine Start Flight, Third, Fourth, Fifth Attempts

A

120 seconds ON, 5 minutes OFF

63
Q

Ground start max cumulative starter run time (motoring plus start time)

A

90 seconds

64
Q

Flight start max cumulative starter run time (motoring plus start time)

A

120 seconds

65
Q

Dry motor first attempt

A

90 seconds ON, 5 minutes OFF

66
Q

Dry motor attempts 2 thru 5

A

30 seconds ON, 5 minutes OFF

67
Q

Dry motor after 5th attempt?

A

You can try #6 after you wait 15 minutes.

68
Q

Tailwind start

A

No positive increase in N1 before starter cutout (50% N2) then the engine start must be manually aborted.

69
Q

Can you takeoff with Automatic Takeoff Thrust Control System OFF?

A

No.

70
Q

Max Fuel Capacity (JET A / A1)

A

20,935 lb

71
Q

Max Fuel Imbalance

A

794 lb

72
Q

Mun Fuel Tank Temp

A

-40C

73
Q

Fuel crossfeed must be selected _____ during takeoff and landing.

A

OFF

74
Q

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

A

30 seconds

75
Q

Do not leave the airplane unattended more than ____ minutes with the APU running. (SW)

A

5 minutes

76
Q

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

A

PROHIBITED

77
Q

APU Start Attempt 1 & 2.

A

60 seconds

78
Q

APU Start Attempt #3…

A

5 minutes OFF

79
Q

APU Min Start Temp

A

-54C

80
Q

APU Max Start Temp / Continuous Ops

A

ISA +35C (52C)

81
Q

APU Max Start Altitude / Continuous Ops

A

30,000 ft

82
Q

APU Max Altitude Use / Electrical Gen Use

A

33,000 ft

83
Q

APU Max Altitude Engine Start

A

21,000 ft

84
Q

APU Max Bleed Altitude Use

A

15,000 ft

85
Q

Max DeltaP <37,000 ft

A

7.8 psi

86
Q

Max DeltaP >37,000 ft

A

8.4 psi

87
Q

Max DeltaP Over Pressure

A

8.8 psi

88
Q

Max DeltaP Negative Pressure

A

-0.5 psi

89
Q

Max Pressure Differential Takeoff/Landing

A

0.2 psi

90
Q

Min Hydraulic Reservoir Temp for Engine Start

A

-18C

91
Q

Brake temp indication must in the ____ range for takeoff.

A

GREEN

92
Q

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

A

…REV icon on EICAS is shown in amber or green.

93
Q

TO DATASET MENU on MCDU must be set to ENG when OAT is…

A

5C-10C, when there is any possibility of contacting visble moisture up to 1,700’ AFE. When operating on ramps, taxiways, runways, etc where snow, ice, standing water, slush, may be ingested by the engines, or freeze on the engines, nacelles, or engine sensor probes.

94
Q

TO DATASET MENU on MCDU must be set to ALL when OAT is…

A

<5C, when there is any possibility of contacting visble moisture up to 1,700’ AFE. When operating on ramps, taxiways, runways, etc where snow, ice, standing water, slush, may be ingested by the engines, or freeze on the engines, nacelles, or engine sensor probes.

95
Q

When either or both ice detectors are failed, the crew must set the mode selector to ON when…

A

…icing conditions exist or below 10C TAT with visible moisture.

96
Q

A/P min engagement height

A

400 ft

97
Q

A/P min use height

A

50 ft

98
Q

A/P min use height non-precision approach

A

MDA

99
Q

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

A

60 kt

100
Q

While transmitting in VHF1, the standby mag compass indication is…

A

…not valid.

101
Q

RNAV LP minima are…

A

Not Authorized.

102
Q

Manual engine start abort:

A

NNoTM*/HHN

  1. No +Oil press w/in 10 sec after N2 increase.*
  2. No N1 increase at starter cutout (~50% N2) when starting with Tailwind.*
  3. No ITT w/in 30 sec of start. (no light off).
  4. ITT exceeds 815C (hot start).
  5. Oil press stabilizes not in green range.*
  6. N1 or N2 fail to accelerate to stable (hung start).
  7. Intermittent elec or pneu or starter Malfunction before starter cutout.*
103
Q

Cold WX Preflt

A
  1. OAT 5C or less.
  2. Wing fuel temp 0C or less.
  3. Atmospheric conds conducive to icing exist.
  4. Overnight contamination.
  5. Through flight residual.
  6. Cold Soak ice.
104
Q

Is underwing frost allowed?

A

Up to 1/8” frost layer underwing surfaces.

105
Q

Defacto Emergency Descent Memory Items (think SOPM).

A

At least one MFD with terrain.

Once Cabin Altitude reaches 14,500, PASSENGER OXYGEN to OVRD.

106
Q

Engine Dry Motoring Duty Cycle Limits

A
#1 = 90 seconds ON, 5 minutes OFF.
#2-5 = 30 seconds ON, 5 minutes OFF.

After five sequential motoring cycles, the process may be repeated following a 15 min cool down period.

107
Q

APU Starter Duty Cycle

A

Start Attempt #1 & 2 = 60 seconds OFF.

Start Attempt #3 = 5 minutes OFF.

108
Q

MTW (LL)

A

LR MTW - 420#

109
Q

MTOW (LL)

A

LR MTOW - 419#

110
Q

MZFW (LL)

A

LR MZFW - 419#

111
Q

When an auto abort occurs or engine start is manually aborted due to abnormal indications… can you try again?

A

…its cause must be investigated and corrected before further attempts to start the engines.

112
Q

In case of an automatic abort due to an engine hot start and with no ENGINE EXCEEDANCE EICAS message…

A

…two additional engine starts are allowed. (but you should probably investigate why / call mx).

113
Q

No Flex Thrust Takeoffs?

A
  1. Contaminated Runway.
  2. Reported or forecasted Windshear.
  3. Special departure (ex: Reno).
114
Q

Max Angle Climb Speed?

A

VFS.

115
Q

Max Rate of Climb Speed?

A

~VFS+50

116
Q

SkyWest min hold speed?

A

<=6000 ft = 200 KIAS (FAA…)

>6000 ft = 210 KIAS

117
Q

Minimum Fuel?

A

2,250 lbs, 45 min, 1,500 ft AFE green dot clean.

118
Q

Emergency Fuel?

A

1,500 lbs, 30 min, 1,500 ft AFE green dot clean.

119
Q

Which checklist do you do first?

A
MEAN
Memory/QRC
Emergency
Abnormal
Normal