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CL604 > Limitations > Flashcards

Limitations Flashcards

1
Q

Ramp weight

A

48,300lbs

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2
Q

MTOW

A

48,200lbs

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3
Q

MLW

A

38,000lbs

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4
Q

Max ZFW

A

32,000lbs

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5
Q

Min flight weight

A

26,000lbs

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6
Q

Min operating empty weight

A

22,150lbs

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7
Q

Max ambient temp approved for take off

A

ISA +35

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8
Q

Min ambient temp approved for take off

A

-40

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9
Q

Tactile check of wing leading edge required when

A

OAT 5 or less
Wing fuel temp is 0 or less
Atmospheric conditions have been conducive to frost

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10
Q

Cowl anti ice required when

A

10c or less

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11
Q

Wing anti ice required when

A

5c or less

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12
Q

Max slope

A

2% up or down

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13
Q

Max tailwind for takeoff or landing

A

10kts

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14
Q

N1 red line

A

98.6%

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15
Q

Max continuous thrust ITT

A

900degrees

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16
Q

Max continuous ITT with APR

A

928degrees

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17
Q

N2 red line

A

99.3%

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18
Q

Oil temp red line

A

163 degrees

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19
Q

Oil temp green band

A

-40 to 154 degrees

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20
Q

Oil pressure red line

A

0-25psi

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21
Q

Oil pressure green band

A

26-115psi

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22
Q

Limitation to operating above FL400

A

One pack must be operating

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23
Q

N2 split should not be greater than

A

2%

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24
Q

If the aircraft is cold soaked, the aircraft must be motored for how long

A

60 seconds

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25
Q

Continuous ignition required when

A

TO/LDG on contaminated runway
Crosswind greater than 10kts
Flight through moderate rain or turbulence
In the vicinity of TS

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26
Q

Max motoring on first engine start

A

90 seconds

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27
Q

Max motoring on 2nd and subsequent engine start

A

30 seconds

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28
Q

Time off required if engine is motored beyond limit

A

5minutes

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29
Q

Engine start: fuel to idle when ITT

A

120 on ground
90 in flight

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30
Q

Engine relight windmilling 21-10

A

IAS 300-348 N2 12 -55%

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31
Q

Engine relight windmilling 10-8

A

IAS 300-348 N2 10 -55%

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32
Q

Engine relight windmilling 8-0

A

IAS 300 N2 10 -55%

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33
Q

Engine relight starter assisted 21-15

A

IAS 200-300 N2 0 -55%

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34
Q

Engine relight starter assisted 15-0

A

IAS 140-300 N2 0 -55%

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35
Q

Fuel imbalance

A

400 taxi, take off, landing
800 in flight

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36
Q

Main tank quantity

A

9720lbs

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37
Q

Aux tank quantity

A

7168lbs

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38
Q

Tail tank quantity

A

3112lbs

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39
Q

Gravity quantity

A

15,780lbs

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40
Q

Fuel percentage reduction with gravity refuel

A

7%

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41
Q

Aux - tail ratio

A

2.65%

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42
Q

500lbs permitted in aux provided there is at least what quantity in the mains

A

1500lbs + none in the tail

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43
Q

Aux must be at least what ratio to tail quantity if the tank is equal to or greater than 1200lbs

A

2.75%

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44
Q

Aux must be at least what ratio to tail quantity if the tank is less than 1200lbs

A

2.2%

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45
Q

Fuel dump limitations

A

Zero flap, no lightening

46
Q

Max engine time without servicing oil

A

16hrs

47
Q

Oil level should be checked at what time interval after shutdown

A

15mins - 2hrs

48
Q

Max oil refill without dry motoring

A

2 q

49
Q

Flaps 20 speed

A

231kts

50
Q

Flaps 30 speed

A

197kts

51
Q

Flaps 45 speed

A

189kts

52
Q

Max landing gear operating speed

A

197kts

53
Q

Max landing gear extended speed

A

250/0.7

54
Q

Landing gear cannot be operated above what alt

A

FL200

55
Q

Tire limit speed

A

182kts

56
Q

Wet ADG limitation speed

A

250kts

57
Q

TURB penetration speed

A

280/0.75

58
Q

Load factor flaps up

A

-1 to 2.5G

59
Q

Load factor flaps down

A

0 to 2G

60
Q

Max differential pressure

A

9.2psi

61
Q

Max negative differential pressure

A

-0.5psi

62
Q

Take off, taxi and landing pressure must not exceed

A

0.2psi

63
Q

Min Autopilot height on takeoff

A

320ft

64
Q

Min Autopilot height precision approach (less than 3.5)

A

80ft

65
Q

Min Autopilot height precision approach (3.5 - 4.5)

A

160ft

66
Q

Limitation on 10th stage if cowl/wing anti ice is required for take off

A

10th stage must be closed

67
Q

AC System loads 0-20

A

30kva

68
Q

AC System loads 20-35

A

30kva

69
Q

AC System loads 35-41

A

25kva

70
Q

AC System loads for APU 0-20

A

30kva

71
Q

Max load for TRU’s

A

100amps

72
Q

Flap use enroute limitation

A

Cannot be used

73
Q

Flap use limitation

A

Prohibited above 15,500ft

74
Q

Spoiler use limitation

A

Cannot be used below 300ft

75
Q

Spoiler limitation

A

Must not be extended in flight at air speeds below the recommended approach speed +10

76
Q

Reversers limitation

A

Below 60kts, reverse thrust must be reduced to 60% N1 or less

77
Q

FMS must be receiving suitable nav from what

A

1 x VOR/DME or
2 x DME’s or
1 x IRS or
GPS

78
Q

Airplane operation must not be predicated upon performance data ETE/ETA and fuel remaining

A

True

79
Q

Flight plans must be what to conduct an FMS approach operation

A

Identical

80
Q

FMS instrument approaches are prohibited unless approach is

A

Annunciated on the PFD

81
Q

VNAV prohibited during

A

QFE ops

82
Q

VNAV prohibited between what points of a V-MDA approach

A

FAF to missed approach point

83
Q

VFLC prohibited when using

A

MACH

84
Q

Maximum operating altitude for 100 series APU

A

20

85
Q

Maximum operating altitude for 150 series APU

A

20

86
Q

Maximum altitude and IAS for guaranteed 100 series APU start

A

15/ 141-290kts

87
Q

Maximum altitude and IAS for guaranteed 150 series APU start

A

20/ 141-290kts

88
Q

Maximum inflight bleed air extraction altitude for 100 series APU

A

14,500

89
Q

Maximum inflight bleed air extraction altitude for 150 series APU

A

15

90
Q

Start % - fuel and ignition for 100 series APU

A

10%

91
Q

Start % - fuel and ignition in for 150 series APU

A

5%

92
Q

Start % - starter cutout for 100 series APU

A

60%

93
Q

Start % - starter cutout for 150 series APU

A

35-45%

94
Q

Start % - ignition deactivated for 100 series APU

A

95%

95
Q

Start % - ignition deactivated for 150 series APU

A

99%

96
Q

Hung start for 100 series APU

A

Less than 60% in 20 seconds, or 60-95% in greater than 10 seconds

97
Q

Hung start for 150 series APU

A

Less than 30% in 60 seconds

98
Q

Is in flight use of 100/150 APU permitted?

A

100 - if IDG’s fail
150 - yes

99
Q

Overspeed auto shutdown of APU 100/150

A

100 - 110%
150 - 107%

100
Q

In flight engine start guarantee for 100/150 series APU

A

100 - 2 engine out 10,000ft
150 - 2 engine out 15,000ft

101
Q

Does the APU have dual powered ECU’s

A

100 - no
150 - yes

102
Q

Max EGT for APU use (steady ops)

A

731 degrees

103
Q

APU Start cycles using battery power on ground or normal in flight start

A

3 x 30 seconds of cranking
20 minutes off
2 further attempts each 30 seconds

104
Q

APU start cycles using ground power

A

2 x 15 seconds continuous cranking
20 minutes off
2 further attempts at 15 seconds

105
Q

If you cannot start the APU after reaching the limit of attempts, how long must you then wait

A

35 minutes

106
Q

Max APU EGT for starting

A

974 degrees

107
Q

Hydraulic accumulator pressure should be what during preflight?

A

1500psi

108
Q

Normal hydraulic pressure is?

A

3000psi

109
Q

Hydraulic pressure turns amber when pressure falls below?

A

1800psi

110
Q

OXY LO PRESS EICAS message when?

A

Less than 800psi

111
Q

OXY HP disk will rupture when pressure exceeds?

A

2800psi

112
Q

The other disk will rupture if the LP module pressure exceeds?

A

90psi

CL604 (10 decks)

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