SOP Flashcards

1
Q

Max. Lnd. Wt.

A

74,957 lb

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2
Q

Max. Zero Fuel Wt.

A

69,886 lb

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3
Q

Max. AFT Cargo

A

2,535 lb

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4
Q

Max. FWD Cargo

A

3,306 lb

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5
Q

Min. Runway Width

A

100’ (SW)

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6
Q

Wing Span

A

93 ft 11 in.

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7
Q

Aircraft Length

A

103 ft 11 in.

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8
Q

Tail Height

A

32 ft 4 in.

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9
Q

Max. T/O & Landing Temp; Max Lnd Altitude

A

8,000 ft

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10
Q

Max. Temp. T/O Lnd

A

ISA + 35°C (52˚C)

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11
Q

Min. Temp. T/O Lnd

A

-40°C

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12
Q

Max RWY Slope

A

+/- 2%

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13
Q

Max. Tailwind

A

15 kt

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14
Q

Max. Single Pack Operations

A

FL310

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15
Q

VMO 10,000- Mach Transition

A

320 kts

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16
Q

MMO

A

0.82

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17
Q

VA

A

240 kts

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18
Q

VLO EXT

A

250 kts

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19
Q

VLE RET

A

250 kts

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20
Q

VLE

A

250 kts

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21
Q

V Tire

A

195 kts

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22
Q

V RAT DEPLOY MAX

A

Vmo/Mmo

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23
Q

VMIN (to provide electrical power)

A

130 kts

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24
Q

VB (below 10,000 ft)

A

250 kts

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25
Q

VB (10,000 ft and above)

A

270/.76M (whichever is lower)

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26
Q

V wiper ops max

A

250 kts (SW)

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27
Q

Vwindow

A

160 kts

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28
Q

VFE 1

A

230 kts

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29
Q

VFE 2

A

215 kts

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30
Q

VFE 3

A

200 kts

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31
Q

VFE 4

A

180 kts

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32
Q

VFE 5

A

180 kts

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33
Q

Flaps Full Speed

A

165 kts

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34
Q

MAXIMUM RECOMMENDED CROSSWIND

DryRunway

A

38kts

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35
Q

MAXIMUM RECOMMENDED CROSSWIND

WetRunway

A

31kts

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36
Q

MAXIMUM RECOMMENDED CROSSWIND

RunwaywithStandingWater/Slush/WetSnow/DrySnow

A

18kts

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37
Q

MAXIMUM RECOMMENDED CROSSWIND

Runway with Ice

A

12kts

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38
Q

FLIGHT CONTROLS
SLATS / FLAPS
Max. Alt. Flaps/SlatsExtended

A

FL200

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39
Q

DRY MOTORING CYCLE LIMITS
DRY MOTORING DUTY CYCLE LIMITS
Motoring #2-5

A

30 Seconds ON 5 Minutes OFF

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

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40
Q

FUEL GENERAL FUEL JET A - JET A1

Max. Fuel Capacity

A

20,935 lbs

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41
Q

APU OPERATIONAL LIMITS
CONTINUOUS OPERATION
Temperature

A

-54°C ISA +35 (52°C)

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42
Q

When must predictive EGPWS functions must be manually inhibited?

A

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

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43
Q

AUXILIARY POWER UNIT (APU)

Battery switch position for APU start?

A

BATT 1 must be ON and BATT 2 must be in AUTO for the APU to start.

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44
Q

OPERATION IN ICING CONDITIONS

What is temperature limitation for anti-icing system?

A

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

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45
Q

OPERATION IN ICING CONDITIONS
On ground
Under what conditions do use The TO DATASET MENU on the MCDU must be set to ENG ?

A

1: When OAT is between 5°C and 10°C
2: When there is any possibility of encountering visible moisture up to 1,700 ft AFE.
3: 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.

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46
Q

Max. Ramp Wt.

A

85,870 lb

47
Q

MINIMUM / EMERGENCY FUEL TABLE

MINIMUM FUEL

A

2250lbs

48
Q

MINIMUM / EMERGENCY FUEL TABLE

EMERGENCY FUEL

A

1500lbs

49
Q

ENGINE ABNORMAL START

A

AFFECTED ENGINE: START/STOP SELECTOR ………….STOP

50
Q

SMOKE EVACUATION

A

OXYGEN MASKS …………………DON EMER

CREW COMMUNICATION ………ESTABLISH PRESSURIZATION DUMP ………..PUSH IN

51
Q

SMOKE/FIRE/FUMES

A

OXYGEN MASKS …………………DON, 100 % CREW COMMUNICATION ……………….ESTABLISH

52
Q

BATT 1 (2) OVERTEMP

A

ASSOCIATED

BATTERY…………..OFF

53
Q

AMMED CONTROL COLUMN - PITCH

A

ELEVATOR DISCONNECT

HANDLE ……………PULL

54
Q

AMMED CONTROL WHEEL - ROLL

A

AILERON DISCONNECT

HANDLE………………PULL

55
Q

PITCH TRIM RUNAWAY

A

A/P DISC BUTTON ………………PRESS AND HOLD PITCH TRIM SYS 1 and 2 CUTOUT BUTTONS ………… PUSH IN

56
Q

ROLL (YAW) TRIM RUNAWAY

A

A/P DISC BUTTON ……………PRESS AND HOLD

57
Q

STEERING RUNAWAY

A

STEER DISC SWITCH……….PRESS Steer the airplane us ing differential braking and rudder.

58
Q

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

A

not authorized.

59
Q

Brake temperature indication range for take-off?

A

In the green

60
Q

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

A

60kts

61
Q

While transmitting in VHF1what indication is not valid?

A

the standby magnetic compass indication

62
Q

The use of FMS Speed Mode is

A

prohibited in the event of an engine failure

63
Q

How long does the IESS initialization take?

A

IESS initialization occurs within 90 seconds after power-up.

64
Q

Durning power up which displays are available?

A

When more than displays 2 and 3 are available, the airplane must not be dispatched.

65
Q

What can you do if battery voltage is between 21.0 and 22.5 volts?

A

Recharge the batteries prior to takeoff, through any AC source (including engines during taxi) for:

– Battery Temp >= 0°C – 30 min

– BatteryTemp>=-5°Cand= -10°C and

66
Q

Battery voltage is showing below 21.0 volts what do can you do?

A

Report irregularity as outlined in Flight Operations Manual (FOM) SP3100 Chapter 5 Mechanical Irregularities

• DO NOT depart

67
Q

When performing a FIRE EXTINGUISHER PANEL CHECK what are you looking for?

A

First verify there are no fire protection fail messages displayed on the EICAS after power up.
Then Press and hold the TEST button and observe the following EICAS messages, lights, and warnings:

– Aural warning

– Fire handles illuminated

– CARGO SMOKE FWD / AFT buttons illuminated

– APU button illuminated

– Upper half of the APU Emergency Stop Button illuminated

– WARNING lights flashing

– “CARGO FWD (AFT) SMOKE” EICAS message

– “APU FIRE” EICAS message.

– “ENG 1 (2) FIRE” EICAS message

– “FIRE” warning annunciation displayed inside ITT indicators

68
Q

The electrical PBIT is automatically performed during power up after the airplane is powered by any AC source and takes about how long?

A

3 minutes

69
Q

The electrical PBIT test is interrupted when?

A
  • Any hydraulic pump is running
  • The Flight Control Mode Panel switches are cycled
  • The AC power supply is interrupted
70
Q

The the hydraulic PBIT is performed when?

A

All three hydraulic systems are pressurized for at least one minute and the reservoir temperature is greater than +10ºC.

71
Q

A FLT CTRL BIT EXPIRED EICAS message is displayed when?

A

The last successful PBIT was more then 50 hours old while the aircraft is on the ground and the EICAS messages are no longer inhibited.

72
Q

How long will A FLT CTRL BIT EXPIRED EICAS message be displayed?

A

The message continues being displayed on the EICAS until a new Electrical or Hydraulic PBIT is successfully completed.

73
Q

On the first flight of the day, with temperatures below -18°C (0°F), or when the smart probes are frozen accomplish the following procedure after AC power is established on the aircraft

A

ADSP Heater Switch…….ON

74
Q

How much frost layer is permitted on the underwing surfaces of the wing?

A

A 3 mm (1/8 in.) frost layer is permitted on the underwing surfaces of the wing.

75
Q

What is SkyWest min speeds in icing conditions?

A

maximum endurance speed or 210kts whichever is higher

76
Q

What are the 4 things you get back when the RAT powers the AC ESS BUS?

A

AC fuel pump 2 
ACMP hyd pump 3A 
1 channel of slats 
1 channel of flaps

77
Q

How long does the evacuation slide light battery last?

A

10 minutes

78
Q

With an inop APU, why do we start the #2 engine first?

A

The ground connections for the ext power and high pressure air, are on the left side of the plane.

79
Q

Do you need to reference the QRH for a crossbleed start?

A

No, it is an SOP procedure

80
Q

Who arms the autothrottles and when?

A

The captain will after runway verification and lined up on the runway

81
Q

What should be on your FMA before Takeoff?

A

White (To) Autothrottles 
Green Roll in later mode 
Green TO in Vnav

82
Q

What color is ATTCS before Takeoff?

A

White

83
Q

When does ATTCS turn Green?

A

When the thrust levers reach TOGA

84
Q

When will ATTCS command RSV?

A

Thrust levers at TOGA and one of following


Difference between both engine N1 value is greater than 15%, one engine failure during takeoff or go around, Windshear detection

85
Q

Describe “HOLD” mode

A

it deactivates the autothrottle servos between 60 kts and 400’. this is to “lock” in the takeoff thrust setting and also to prevent the autothottles from increasing thrust during a rejected takeoff

86
Q

What are the recommended climb, cruise and descent speeds?

A

250 kts below 10,000’ 
290 to .74 above 10,000 
cruise .74 or .78 per dispatch 
descent .78 to 290 to 250 below 10,000’

These numbers are still changing but this is the latest

87
Q

Why are we disarming the auto throttles on a driftdown procedure?

A

We are getting the thrust to CON (max continuous) we disconnect them to allow us to descend in FLCH in Speed on Elevator and maintaining green dot 
i.e. a slow descent rate at max power, stay as high as possible for as long as possible

88
Q

Will the low rate cargo bottle discharge automatically on the ground?

A

No, you must push the button again

89
Q

When do we adjust for icing speeds?

A

When Advisory msg Ice conditions is announced. or Stall prot ice speeds found in QRH or Acars

90
Q

How many batteries for the emergency lights 
how long will they last?

A

4 batteries, 10 minutes

91
Q

What is max rated thrust of engine?

A

14,200lbs

92
Q

Which areas of plane have fire protection?

A

LAV 
APU 
CARGO COMPS 
ENGINES

93
Q

How many fire detection loops in Apu and Engines?

A

2

94
Q

How long does it take the RAT to deploy and what powers plane during this time?

A

8 seconds, batteries during this 8 secs

95
Q

How long will batteries last if they are the only source of power in flight?

A

10 minutes

96
Q

Where is the O2 blow out disc?

A

just forward of the fwd cargo pit

97
Q

You find a 3” puddle of oil in the engine exhaust, what do you do?

A

Nothing up to 4” is considered within normal limits

98
Q

Will nav lights switch automatically if one burns out?

A

no, there is a switch in the cockpit and it is a mx function

99
Q

How many static dischargers on wing?

A

6 on winglet 3 on aileron

100
Q

What does a green Oxy indication mean? 
Cyan? 
Amber?

A

Green, good for 3 crewmembers 
Cyan, good for 2 crewmembers (sorry Adam and Aaron) 
Amber, call mx

101
Q

How long will ice pro remain on after ice is detected?

A

5 minutes

102
Q

Is the DV window heated?

A

No

103
Q

When does ACMP 3B turn on?

A

When ACMP 3A fails

104
Q

What is max X-wind for a Cat 2?

A

15 kts

105
Q

Which airports in Canada can we shoot a Cat 2?

A

Winnipeg 
Montreal 
Toronto 
Vancouver

106
Q

Can you LAHSO a) on a wet runway 
without vert or visual guidance b) 
with windshear in last 20 mins c) 
with a tail wind

A

No, no, no

107
Q

What are the LAHSO wx mins?

A

ceiling no less than 1500’ 
no less than 5 miles visibility

1000’ and 3 miles with a PAPI or VASI

108
Q

What is the lowest Cat 1 mins?

A

1800’ RVR, must use flight director, 
15 kt xwind NO LONGER APPLIES

109
Q

Takeoff 
1000,1000,1000 
what do you need?

A

CL lights or HIRL and RCLM

110
Q

When will RSV POWER BE ACTIVATED?

A

ATTCS must be engaged 
And if one of the following occurs

N1 difference greater than 15% 
One engine fails during takeoff 
One engine fails during go around 
Windshear detected

Max thrust commanded by thrust levers

111
Q

What is minimum flex thrust for takeoff?

A

75% of Max rated takeoff thrust or 
Climb -2 + .5 %n1 whichever is higher

112
Q

If FADEC aborts the start due to a high ITT what do you need to do?

A

Close the SCV by putting the start stop switch to stop

113
Q

How many fire extinguishing bottles are there?

A
  1. A and B