Limitations Flashcards

1
Q

Maximum Ramp Weight

A

85,870 LBS

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2
Q

Maximum Takeoff Weight

A

85,517 LBS

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3
Q

Maximum Landing Weight

A

74,957 LBS

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4
Q

Maximum Zero Fuel Weight

A

69,886

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5
Q

FWD Cargo Max Weight?

A

3,306 lbs (110 bags)

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6
Q

AFT Cargo Max Weight?

A

2,535 lbs (84 bags)

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7
Q

Taxi single engine what has to be on?

A

(Eng#2) Hydraulic 1B On

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8
Q

How long before engine shutdown?

A

2 min cool down before shutdown.

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9
Q

Wing span?

A

85’ 4” (94’ 2” with new winglet)

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10
Q

Aircraft length?

A

103’ 11”

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11
Q

Tail height?

A

32’ 3”

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12
Q

Max Ops. Alt?

A

41,000 ft

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13
Q

Max T/O & Land Alt?

A

8,000 ft

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14
Q

MAX temp T/O & land?

A

ISA +35ºC (52ºC)

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15
Q

Minimum temp T/O & land?

A

-40ºC

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16
Q

Runway slope?

A

+/- 2%

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17
Q

Max tailwind?

A

15 Kts

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18
Q

Max single pack alt?

A

31,000 ft

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19
Q

VMO (SL to 8,000 ft)?

A

300

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20
Q

VMO (10,000 ft to Mach transition)?

A

320

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21
Q

MMO?

A

0.82M

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22
Q

VA?

A

240

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23
Q

VLE RET?

A

250

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24
Q

VLE?

A

250

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25
Q

VLE EXT?

A

250

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26
Q

V tire?

A

195

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27
Q

V RAT deploy max?

A

250

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28
Q

VMIN(RAT) (to provide electrical power)?

A

130

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29
Q

VB (below 10,000)?

A

250

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30
Q

VB (10,000 and above)?

A

270 / 0.76M (whichever is lower)

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31
Q

V wiper ops max(SW)?

A

250

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32
Q

V window?

A

160

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33
Q

VX (flaps retracted/all weights)?

A

VFS

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34
Q

VY (flaps retracted/all weights)?

A

VFS+50 kts

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35
Q

VFE 1?

A

230

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36
Q

VFE 2?

A

215

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37
Q

VFE 3?

A

200

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38
Q

VFE 4?

A

180

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39
Q

VFE 5?

A

180

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40
Q

FULL?

A

165

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41
Q

Flaps 5 go around flaps

A

Flaps 2

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42
Q

Flaps FULL go around flaps?

A

Flaps 4

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43
Q

Maximum recommended crosswinds!

Dry runway?

A

38 kts

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44
Q

Maximum recommended crosswinds Wet runway?

A

31 kts

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45
Q

Maximum recommended crosswinds Runway with compacted snow?

A

20 kts

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46
Q

Runway with standing water/slush/wet snow/ dry snow?

A

18 kts

47
Q

Runway with ice?

A

12 kts

48
Q

Crosswind limit (recommended) for static takeoff?

A

25 kts

49
Q

Bank angle at which engine nacelle will strike the ground (landing gear struts
compressed)?

A

16°

50
Q

Bank angle at which engine nacelle will strike the ground (landing gear struts not
compressed)?

A

18°

51
Q

Max alt for slats/flaps extended?

A

20,000 ft

52
Q

Slat/flap enroute use limit?

A

Prohibited

53
Q

Min spoiler speed?

A

180 kts

54
Q

Speed at which AFCS retracts spoilers?

A

180 KIAS

55
Q

Flap setting at which AFCS retracts spoilers?

A

Flap 2, and above

56
Q

Cat II flap setting (mandatory)?

A

Flap 5

57
Q

Go around flap setting for a full flap landing?

A

Go-Around Flaps 4

58
Q

Go around flap setting for a flap 5 landing?

A

Go-Around Flaps 2

59
Q

Minimum battery voltage?

A

22.5V

60
Q

Minimum battery (#2) temp for APU start?

A

-20°C

61
Q

Engine max temp, start?

A

815ºC (redline)

62
Q

Engine min oil temp, start?

A

-40ºC

63
Q

Engine min oil pressure, start?

A

25 psi

64
Q

Engine starter/cranking limits, ground?

A

1&2, 90sec ON / 10sec OFF }{ 3-5, 90sec ON / 5 min OFF

65
Q

Engine starter/cranking limits, in flight?

A

1&2, 120sec ON / 10sec OFF }{ 3-5, 120sec

ON / 5 min OFF

66
Q

Engine dry motor limits?

A

1, 90sec ON / 5 min OFF }{ 2-5, 30sec ON / 5 min OFF

67
Q

How many sequential dry motorings can be accomplished before a 15 min cool down is
required?

A

Five

68
Q

When must the flight crew monitor N1 and accomplish a manual engine start abort?

A

Engine starts with a tailwind must be monitored. If there is no positive N1 increase
before starter cutout, the engine start must be manually aborted

69
Q

What is the ATTCS limitation for takeoff (SW)?

A

It must be ON, takeoff with the ATTCS off is prohibited

70
Q

Max fuel capacity?

A

20,935 Lbs

71
Q

Max fuel imbalance?

A

794

72
Q

Min fuel tank temp?

A

-40ºC

73
Q

Minimum fuel level?

A

2250 lbs

74
Q

Emergency fuel level?

A

1500 lbs

75
Q

What is the fuel crossfeed limitation for T/O & landing?

A

Selected OFF

76
Q

How long must the flight crew wait, after aircraft power up, to start the APU?

A

30 seconds after EICAS is energized

77
Q

How log can the aircraft be left unattended with the APU running (SW)?

A

5 minutes

78
Q

What limitation is involved with simultaneous use of the APU and HP cart?

A

Simultaneous use of the APU bleed and HP cart is prohibited

79
Q

APU start limit, attempts 1 & 2?

A

60 sec OFF

80
Q

APU start limit, attempt 3?

A

5 minutes OFF

81
Q

APU max OAT, start?

A

ISA +35ºC

82
Q

APU min OAT, start?

A

-40ºC

83
Q

APU max altitude, start?

A

30,000 ft

84
Q

APU min OAT, continuous use?

A

ISA +35ºC (52ºC)

85
Q

APU max OAT, continuous use?

A

-54ºC

86
Q

APU max altitude?

A

33,000 ft

87
Q

APU max altitude, generator use?

A

33,000 ft

88
Q

APU max altitude, bleed air use?

A

15,000 ft

89
Q

APU max altitude, engine start?

A

21,000 ft

90
Q

Max pressure differential, up to 37,000 ft?

A

7.8 psi

91
Q

Max pressure differential, above 37,000 ft?

A

8.34 psi

92
Q

Max diff. over pressure?

A

8.77 psi

93
Q

Max diff. negative pressure?

A

-0.5 psi

94
Q

Max diff. pressure T/O & land?

A

0.2 psi

95
Q

Minimum hydraulic reserve temp for engine start?

A

-18ºC

96
Q

What is the brake temperature indication limit for takeoff?

A

GREEN

97
Q

What is the go-around limitation in relation to thrust reverser deployment?

A

Do not

attempt go-around after thrust reverser deployment

98
Q

After selecting reverse thrust, when can the thrust levers be moved into the forward
thrust range?

A

Do not move the trust levers forward until a GREEN or AMBER REV icon
is shown on EICAS

99
Q

Reverse thrust during taxi is?

A

prohibited

100
Q

Powerback (using reverse thrust) operations are?

A

prohibited

101
Q

Temperature limitation for automatic operation of anti-icing system?

A

None

102
Q

When must the TO DATASET menu on the MCDU be set to ENG?

A

OAT between 10º
and 5ºC and there is any possibility of encountering visible moisture up to 1,700 ft AGL
and/or operating on contaminated surfaces

103
Q

When must the TO DATASET menu on the MCDU be set to ALL?

A

OAT is BELOW 5ºC
and there is any possibility of encountering visible moisture up to 1,700 ft AGL and/or
operating on contaminated surfaces

104
Q

Minimum height for autopilot engagement?

A

400 ft

105
Q

Minimum height for autopilot use?

A

50 ft

106
Q

Minimum height for autopilot use, non-precision approaches?

A

MDA

107
Q

When are TAS, TAT and SAT valid?

A

Above 60 KIAS

108
Q

When is the magnetic compass unreliable?

A

While transmitting on VHF1

109
Q

What setting must be used for CAT I ILS?

A

(BARO)metric minimums (altimeter setting)

110
Q

Back course approaches using the IESS are?

A

prohibited

111
Q

Is SKW authorized to conduct RNP approaches?

A

No

112
Q

What FMS mode is prohibited from use during single engine (OEI) operations?

A

FMS

Speed Mode

113
Q

Which FA is the primary contact for the flight deck?

A

Forward