Limitations Flashcards

0
Q

Max. T/O Wt.

A

85,517 lb

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1
Q

Max. Ramp Wt.

A

85,870 lb

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2
Q

Max. Lnd. Wt.

A

74,957 lb

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3
Q

Max. Zero Fuel Wt.

A

69,886

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4
Q

Max. Aft. Cargo

A

2,535 lb

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5
Q

Max. Fwd. Cargo

A

3,306 lb

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6
Q

Min. Runway Width (SW)

A

100’

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7
Q

Max. Ops. Altitude

A

41,000 ft

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8
Q

Max. T/O & Lnd.

A

8,000 ft

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9
Q

Max. Temp. T/O & Lnd.

A

ISA + 35 C (52 C)

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10
Q

Min. Temp. T/O & Lnd.

A

-40 C

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11
Q

RWY Slope

A

+/- 2%

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12
Q

Max. Tailwind

A

15 kt

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13
Q

Max. Single Pack Operations

A

31,000 ft

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14
Q

VMO SL- 8,000 ft

A

300

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15
Q

VMO 10,000 - Mach Transition.

A

320

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16
Q

MMO

A

M 0.82

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17
Q

Va

A

240

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18
Q

Vlo Ext.

A

250

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19
Q

Vle

A

250

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20
Q

Vle RET

A

250

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21
Q

V Tire

A

195

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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

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24
Q

Vb (Below 10,000 ft)

A

250

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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. (SW)

A

250

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27
Q

V Window

A

160

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28
Q

VFE 1

A

230

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29
Q

VFE 2

A

215

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30
Q

VFE 3

A

200

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31
Q

VFE 4

A

180

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32
Q

VFE 5

A

180

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33
Q

Flaps Full Speed

A

165

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34
Q

Maximum Recommended Crosswind

A

38 kt

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35
Q

Maximum Recommended Crosswind Wet Runway

A

31 kt

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36
Q

Maximum Recommended Crosswind with Compacted Snow

A

20 kt

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37
Q

Maximum Recommended Crosswind with Standing Water/Slush/Wet Snow/Dry Snow

A

18 kt

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38
Q

Maximum Recommended Crosswind with Ice

A

12 kt

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39
Q

Max. Alt. Flaps/Slats Extended

A

20,000 Ft

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40
Q

Slats/Flaps Enroute Ops.

A

Prohibited

41
Q

Slats/Flaps Cat II Approach

A

Mandatory Flaps 5

42
Q

Min. Spoiler Speed

A

180 kt

43
Q

Slats/Flaps go-Around Landing Flaps Full

A

Go-Around Flaps 4

44
Q

Slats/Flaps Go-Around Flaps 5

A

Go-Around Flaps 2

45
Q

Battery Min. Voltage

A

22.5 V

46
Q

Battery Min. Temp.

A

-20 C

47
Q

Engine Start ITT Max Temp

A

815 C

48
Q

Min Oil Temp. Start

A

-40 C

49
Q

Min. Oil Pressure Start

A

25 psi

50
Q

Starter Cranking Limits for Start 1 & 2 (Ground)

A

90 Seconds on 10 seconds off

51
Q

Starter Cranking Limits for Start 3 & 5 (Ground)

A

90 Seconds On 5 min off

52
Q

Engine Start 1 & 2 Cranking Limits (In Flight)

A

120 seconds ON 10 seconds OFF

53
Q

Engine Start 3 - 5 Cranking Limits (In Flight)

A

120 Seconds ON 5 minutes OFF

54
Q

Dry Motoring # 1 Cycle Limit

A

90 seconds ON 5 minutes OFF

55
Q

Dry Motoring #2-5 cycle limits

A

30 seconds ON 5 Minutes OFF

56
Q

Ground Start with a Tailwind Limitation.

A

If no increase in N1 before Starter Cutout (50% N2) Start must be Manually Aborted.

57
Q

Automatic Takeoff Thrust Control System (ATTCS) Limitation.

A

Takeoff with the ATTCS OFF is not authorized.

58
Q

Max. fuel capacity

A

20,935 lb

59
Q

Max. Fuel Imbalance

A

794 lb

60
Q

Min. Fuel tank temp.

A

-40 C

61
Q

Fuel Crossfeed for Takeoff and Landing Limitation.

A

Fuel crossfeed must be OFF during take off and landing

62
Q

EICAS Must be Energized for ( ___ ) Before Starting the APU.

A

30 seconds

63
Q

Simultaneous use of HP air cart and APU bleeds limitation

A

Not authorized

64
Q

APU Starter Duty Cycle Limit For Start Attempt 1 & 2

A

60 seconds off

65
Q

APU Starter Duty Cycle Limit For Start Attempt 3

A

5 minutes OFF

66
Q

APU START Min. And Max. Temperatures.

A

-54 C and ISA +35 C

67
Q

APU Max. START Altitude Limit

A

30,000 ft

68
Q

APU Max. Operational Altitude

A

33,000 ft

69
Q

APU Max. Operational Altitude for Bleed Use.

A

15,000 ft

70
Q

APU Max. Operational Altitude for Electrical Generator Use

A

33,000 ft

71
Q

APU Max. Operational Altitude for Engine Start Use

A

21,000 ft

72
Q

Max. Differential Pressure Up To 37,000

A

7.8 psi

73
Q

Max. Differential Pressure Above 37,000 ft

A

8.34 psi

74
Q

Max Differential Over Pressure

A

8.77 psi

75
Q

Max. Differential Neg. Pressure

A

-0.5 psi

76
Q

Max. Differential Pressure T/O and Land

A

0.2 psi

77
Q

Min. Hydraulic Temp. For Engine Start.

A

-18 C

78
Q

Thrust Reverser Limit for Go-Around Maneuver.

A

Do not attempt.

79
Q

Reverse Thrust Stowage Movement Limitation.

A

No not move the thrust levers into the forward range until the REV icon on the EICAS is shown in AMBER or GREEN

80
Q

Operation in Icing Conditions ON THE GROUND when the Temp. Is Between 5 C and 10 C

A

The TO DATASET MENU on the MCDU must be set to ENG.
When:
Any chance of encountering visible moisture below 1,700 ft. OR contaminated ramp or taxi ways.

81
Q

Operation in Icing Conditions ON THE GROUND when the OAT Is Less Than 5 C

A

The TO DATASET MENU on the MCDU must be set to ALL if any possibility of visible moisture may be encountered up to 1,700 ft. Or with contaminated ramp, taxi ways or runways.

82
Q

Autopilot Min. Engagement Height

A

400 ft

83
Q

Min. Auto Pilot Use Height

A

50 ft

84
Q

Min. Use height - Non-Precision Approach

A

MDA

85
Q

TAS, TAT, and SAT information limitation

A

Only valid above 60 kt

86
Q

While transmitting on VHF 1 the Standby Magnetic Compass limitation.

A

Compass information not valid

87
Q

Altimeter limitations for CAT I approaches

A

Barometric altimeter settings must be used

88
Q

Back Course Approach limitations

A

B/C approaches using IESS are prohibited.

89
Q

EGPWS limitations (3)

A
  1. Do not navigate using the EGPWS.
  2. Predictive EGPWS needs to be disabled for approaches to airports not yet in the database.
  3. Predictive EGPWS needs to be manually inhibited for QFE operations if the GPS data is unavailable or inoperative.
90
Q

FMS limitations (2)

A
  1. RNP approaches Not Authorized. (SW)

2. Use of speed mode prohibited in the event of an Engine Failure.

91
Q

APU Continuous Operational Min. And Max. Temperature.

A

Min. -54 C and Max. ISA +35 C (52 C)

92
Q

Wing Span (old wing)

A

85’ 4”

93
Q

Aircraft Length

A

103’ 11”

94
Q

Tail Height

A

32’ 3”

95
Q

Main Landing Gear Width Center to Center

A

17’

96
Q

In the event of landing below -40 C

A

Must have a maintenance inspection performed.

97
Q

Crosswind component greater than 25

A

Static takeoff not recommended

98
Q

After five sequential motoring cycles

A

Must wait 15 minutes for a cool down period.

99
Q

BTMS limit for takeoff

A

Must be in the green