Limitations Flashcards

1
Q

Max. Ramp Weight

A

85, 870 lb.

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2
Q

Max. Takeoff Weight

A

85, 517 lb.

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3
Q

Max. Landing Weight

A

74, 957 lb.

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4
Q

Max. Zero Fuel Weight

A

69, 886 lb.

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5
Q

Minimum Runway Width

A

100’

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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. Operational Altitude

A

41,000’

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10
Q

Max. Altitude for Takeoff or Landing

A

10,000’

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11
Q

Max. Temperature for Takeoff or Landing

A

ISA+ 35°C (52°C)

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12
Q

Minimum Temperature for Takeoff or Landing

A

-40°C

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13
Q

Runway Slope Limit

A

+/- 2%

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14
Q

Max. Tailwind

A

15 Knots

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15
Q

Max. Altitude on a Single Pack

A

31,000’

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16
Q

Vmo SL-8,000’

A

300 knots

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17
Q

Vmo 10,000’-Mach Transition

A

320 knots

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18
Q

Mmo

A

.82

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19
Q

Va

A

240 knots

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20
Q

All gear speeds

A

250 knots

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21
Q

V tire

A

195 knots

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22
Q

V Rat Deploy

A

Vmo/Mmo

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23
Q

Minimum RAT speed to provide electrical power

A

130 knots

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24
Q

Vb (turbulence)

A

Below 10,000’- 250 knots

Above 10,000’- 270 or .76 whichever is less

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25
Q

Maximum windshield wiper speed

A

250 knots

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26
Q

Max. Window Open Speed

A

160 Knots

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27
Q

Vfe Flaps 1

A

230

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28
Q

Vfe Flaps 2

A

215

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29
Q

Vfe Flaps 3

A

200

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30
Q

Vfe Flaps 4

A

180

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31
Q

Vfe Flaps 5

A

180

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32
Q

Vfe Flaps Full

A

165

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33
Q

A Static Takeoff should not be performed with more than _____ knots of crosswind

A

25 Knots

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34
Q

Takeoff Crosswind Pilot Limits

A

Dry- 38 Knots

Wet- 31 Knots

Compact Snow- 20 Knots

Dry Snow, Wet Snow, Slush, Standing Water -
18 Knots

Ice- 12 Knots

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35
Q

Should you factor in gusts when determining the crosswind component for takeoff or landing?

A

No, gusts are not required to be factored into the crosswind component.

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36
Q

Landing Crosswind Limits

A

RCC 6- 38 Knots

RCC 5- 31 Knots

RCC 4-20 knots

RCC 3- 15 Knots

RCC 2- 12 Knots

RCC 1- 8 Knots

RCC 0- Prohibited

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37
Q

Maximum Altitude to have flaps/slats extended

A

20,000’

38
Q

Flying enroute with flaps/slats is____

A

Prohibited

39
Q

Minimum Spoiler Speed

A

180 Knots

40
Q

Cat II Approach flap setting

A

Flaps 5

41
Q

Flaps full go around flap setting

A

Flaps 4

42
Q

Flaps 5 go around setting

A

Flaps 2

43
Q

Minimum Battery Voltage

A

22.5

(If battery voltage is between 21.0-22.5 follow SOPM recharging procedure)

(If Battery below 21.0 Volts, call MX and don’t depart)

44
Q

Max ITT during engine start

A

815°C

45
Q

Minimum oil pressure during start

A

25 PSI

46
Q

Engine starter cranking limits

-__-

A

On ground:
All starts regardless are 90 ON
Only differentiation on ground is 10 seconds off for attempts 1 and 2; 5 minutes off attempts 3-5.

In flight:
All starts in flight are 120 ON.
Only differentiation in air is 10 seconds off for attempts 1 and 2; 5 minutes off attempts 3-5.

47
Q

Dry motoring limits

A

Attempt 1: 90 seconds ON; 5 min OFF

Attempt 2-5: 30 seconds ON; 5 min OFF

48
Q

When no positive increase in N1 before starter cutout, ____%N2, abort the start.

A

50% N2

49
Q

All takeoffs must have ATTCS ____

A

ON

50
Q

Max. Fuel capacity

A

20, 935 lb

51
Q

Max imbalance

A

794 lb

52
Q

Min fuel tank temp

A

-37°C

53
Q

Can you takeoff or land with a FUEL IMBALANCE message?

A

Yes, as long as the actual imbalance does not exceed 794 lb.

(The EICAS message shows up at 800, so by the time you see it you’ve exceeded the limit for takeoff or landing. However the message won’t go away until the imbalance is under 100. So you can land or takeoff with the message present)

54
Q

Crossfeed must be ____ for takeoff or landing

A

OFF

(On a single engine landing remember when the PF calls gear down, chime the FA’s and then go crossfeed off, then put the gear down.)

55
Q

Wait ____ seconds after EICAS is energized to start APU

A

30

56
Q

Do not leave aircraft unattended for more than _____ with APU running

A

5 minutes

57
Q

Simultaneous use of APU bleed and _____ is prohibited

A

HP cart

58
Q

APU start limits

A

Start attempt 1 and 2: 60 seconds off

Attempt 3: 5 minutes off

59
Q

APU starting/continuous operation Min and Max temperature limits

A

-54°c

To

ISA +35

60
Q

Maximum APU START altitude

A

30,000’

61
Q

Max APU continuous operation altitude

A

33,000’

62
Q

Max APU electrical generation altitude

A

33,000’

63
Q

Max APU bleed altitude

A

15,000’

64
Q

Max altitude for APU assisted engine start

A

21,000’

65
Q

Max differential pressure up to 37,000’

A

7.8 PSI

66
Q

Max differential pressure above 37,000’

A

8.4 PSI

67
Q

Max differential over pressure

A

8.8 PSI

68
Q

Max differential negative pressure

A

-0.5 PSI

69
Q

Max differential pressure for takeoff or landing

A

0.2 PSI

70
Q

Minimum hydraulic reservoir temperature for engine start.

A

-18°C

71
Q

Brake temp must be _____ for takeoff.

A

In the green range

72
Q

Do not attempt to go around after ____

A

Thrust reverser deployment.

73
Q

After selecting reverse thrust, wait for _______ before going back into the forward thrust range

A

REV icon to be amber or green

74
Q

Use of thrust reversers while taxiing is ____

A

Prohibited

75
Q

The use of reverse thrust to power back out of the gate (power back operations) is _______

A

Prohibited

76
Q

Takeoff dataset must be set for anti ice ENG in what conditions?

A

It must be selected to ENG when the temperature is between 5°-10°C and:

-Possibility of encountering visible moisture up to 1700 AFE

And/or

-When operating on ramps, taxiways, runways, etc where you might encounter contamination that could be ingested or freeze to engines or probes.

77
Q

Takeoff dataset must be set for anti ice ALL in what conditions?

A

It must be selected to ALL when the temperature is below 5°C and:

-Possibility of encountering visible moisture up to 1700’ AFE

And/or

-When operating on ramps, taxiways, runways, etc where you might encounter contamination that could be ingested or freeze to engines or probes.

78
Q

In case of an ice encounter where either one or both of the ice detectors have failed, what must you do?

A

Operate the anti ice system manually whenever is icing conditions

79
Q

Autopilot minimum engagement height

A

400’

80
Q

Autopilot minimum use height

A

50’

81
Q

Autopilot minimum use height for a non precision approach

A

MDA

82
Q

TAS, TAT, SAT information is only valid _________

A

Above 60 knots

83
Q

While transmitting on VHF 1, the standby magnetic compass is_____

A

Not valid

84
Q

CAT 1 approaches must use _______ minimums

A

BARO

85
Q

Navigation is not to be predicated on the use of the _______ system

A

Terrain Awareness

86
Q

When should the EGPWS be manually inhibited?

A

When landing at an airport not in the database. This is to avoid unwanted alerts

87
Q

What button do you press to inhibit the EGPWS

A

GRD PROX TERR INHIB

88
Q

Are RNAV (GPS) LP minimums authorized?

A

No

89
Q

Target N1 after both engine starts should be within ____

A

+.5% to -.1%

90
Q

When is flex takeoff prohibited?

A
  • Takeoff on contaminated runway
  • Reported or forecasted Windshear
  • When a special departure procedure specifies full thrust takeoff
91
Q

CAT 2 crosswind limit

A

12 knots