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CL-650S > Limitations > Flashcards

Limitations Flashcards

1
Q

TAXI/ RAMP WEIGHT

A

48,300

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2
Q

TAKEOFF WEIGHT

A

48,200

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3
Q

LANDING WEIGHT

A

38,000

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4
Q

Zero Fuel Weight

A

32,000

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5
Q

Minimum Flight Weight

A

26,000

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6
Q

Maximum Airport Pressure Altitude for T/O and LDG

A

10,000’

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7
Q

Maximum Operating Altitude

A

41,000’

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8
Q

Maximum OAT for T/O and LDG

A

ISA +35C

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9
Q

Minimum OAT for T/O

A

-40C

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10
Q

Maximum Runway Slope

A

+/- 2%

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11
Q

Maximum Tailwind

A

10 kts

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12
Q

Maximum Crosswind to use reverse thrust

A

24 kts

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13
Q

Flaps UP load factor

A

-1.0 G to 2.5 G

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14
Q

Flaps DOWN load factor

A

0.0 G to 2.0 G

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15
Q

Maximum G/P angle < 1500’ TDZE

A

4.49 degrees

(See Supplement 11 Chapter 7 of AFM for G/P angles above 3.5 degrees)

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16
Q

Above FL250, at least 1 pilot…

A

Must wear a safety harness

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17
Q

Enroute use of flaps or flight with flaps extended is prohibited above what altitude?

A

15,500’

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18
Q

VLo

A

197 kts / M .6

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19
Q

VLe

A

250 kts / M .7

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20
Q

Maximum altitude with gear down

A

20,000’

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21
Q

Tire speed limit

A

182 kts

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22
Q

Turbulent air penetration speed

A

280 kts / M .75

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23
Q

Maximum RVSM cruise speed

A

M .83

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24
Q

Maximum N2 split on ground at idle.

A

2%

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25
Q

VFe 20 degrees

A

231 kts

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26
Q

VFe 30 degrees

A

197 kts

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27
Q

VFe 45 degrees

A

189 kts

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28
Q

Wing fuel capacity

A

4,860# each

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29
Q

Auxiliary fuel tank capacity

A

7,168#

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30
Q

Tail tank fuel capacity

A

3,112#

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31
Q

Total fuel capacity

A

20,000#

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32
Q

Maximum wing fuel imbalance for taxi, takeoff, and landing

A

400#

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33
Q

Maximum wing fuel imbalance for cruise flight

A

800#

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34
Q

T/O with < 500# fuel in Aux tank permitted provided how much fuel is in each wing tank?

A

1,500# in each wing tank and tail tank must contain 0.

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35
Q

If Aux tank has > 500# fuel, takeoff is permitted when each wing tank is fueled according to the Wing Tank Schedule. What is minimum amount in each wing for a gross weight of up to 42,400?

A

1,500# in each wing.

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36
Q

Minimum fuel for go-around

A

500# per wing with maximum 10 degrees nose-up pitch attitude.

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37
Q

Fuel transfer must be in what position for takeoff?

A

OFF

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38
Q

Can tail tank be used as a C.G. device?

A

No. Must remain in AUTO mode.

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39
Q

2 conditions must be met for jettisoning fuel. What are they?

A

Flaps 0 degrees and no lightning conditions.

40
Q

Minimum engine fuel temp for takeoff?

41
Q

Minimum altitude to engage autopilot after takeoff

A

320’ AGL

42
Q

Minimum altitude for autopilot use during visual/non-precision approach

A

320’ AGL

43
Q

Minimum altitude for autopilot use on precision approach (glide path < or = 3.5 degrees)

44
Q

Minimum altitude for autopilot use during precision approach (glide path > 3.5 and < 4.5 degrees)

A

160’ AGL

45
Q

Maximum relief differential pressure

46
Q

Maximum negative differential pressure

47
Q

Maximum differential pressure during taxi, takeoff, and landing

A

0.2 PSI

Aircraft must be depressurized prior to opening doors.

48
Q

If engine cowl and/or wing anti/ice is selected to ON for takeoff or landing, bleed air 10th stage valves must be in what position?

49
Q

Above 40,000’, what must be selected ON for each engine?

A

1 ACU

or

COWL A/ICE for each engine

50
Q

Maximum engine-driven generator load 0-35,000’?

51
Q

Maximum engine-driven generator load > 35,000’?

52
Q

Maximum APU generator load 0-20,000’?

53
Q

Maximum load on TRU’s?

54
Q

During ground operations at ambient temperatures > 40C (104F), operation of electrical/avionics equipment must be limited to how long?

A

30 minutes

UNLESS: at least 1 air conditioning pack is operating and the passenger door is closed

55
Q

Inflight extension of flight spoilers prohibited below what altitude and below what airspeed?

A

< 300’ AGL

< approach speed plus 10 kts

56
Q

Continuous engine ignition is required when?

A

T/O and LDG on contaminated runway

T/O and LDG with high crosswind component

Flight through moderate or heavier intensity rain

Flight through moderate or heavier intensity turbulence

Flight in vicinity of thunderstorms

57
Q

Maximum contaminant depths for takeoff?

A

Standing water 0.25 in

Slush 0.25 in

Wet snow 0.5 in

Dry snow 1.2 in

58
Q

Maximum contaminant depths for landing?

A

Standing water 0.5 in

Slush 0.5 in

Wet Snow 1.0 in

Dry snow 2.4 in

59
Q

Taxi lights must be selected OFF when the aircraft is?

A

Stationary

60
Q

Left and right landing lights must be selected OFF when the aircraft is?

A

Stationary

The left and right landing lights must not be used on the ground, except for the takeoff roll and landing

61
Q

APU max EGT (start)

62
Q

APU max continuous EGT

63
Q

APU max RPM

A

110% (auto shutdown at 107%)

64
Q

APU minimum temp for start

65
Q

APU max altitude for start

66
Q

Maximum indicated airspeed for inflight APU start and operation

67
Q

APU max altitude for bleed air usage

68
Q

Max altitude to use APU for inflight engine start (double-engine failure only)

69
Q

If both engines started with APU, what is the maximum N2 for the operating engine?

70
Q

Selection of the APU PWR FUEL switch/light activates:

A

APU ECU is powered, and after 3-second BITE test, the APU EGT and RPM are displayed on the EICAS page

APU fuel pump energizes

Opens APU fuel shutoff valve

Opens negative-G shut off valve

71
Q

APU Battery rating

A

24V / 43 ampere-hour

72
Q

Minimum APU battery voltage for APU start

73
Q

APU start cycles using aircraft batteries

A

Attempt 1, 2, 3
Max time 30 seconds ON
Followed by 20 minutes cooling

Attempt 4, 5
Max time 30 seconds ON
Followed by 35 minutes cooling

*3 attempts in 1 hour (AOM 12.8.1)

74
Q

APU start cycles using ground power

A

Attempt 1, 2
Max time 15 seconds ON
Followed by 20 minutes OFF

Attempt 3, 4
Max time 15 seconds ON
Followed by 35 minutes OFF

*3 attempts in 1 hour (AOM 12.8.1)

75
Q

APU hung start

A

Not greater than 30% RPM within 60 seconds

76
Q

Normal takeoff maximum ITT and time limits

A

884 for 5 minutes

900 2 minutes out of 5 total transient

77
Q

Maximum takeoff (APR operating) ITT and time limits

A

899 for 5 minutes

928 for 2 minutes out of 5 total transient

78
Q

Minimum engine oil pressure for takeoff

79
Q

Maximum transient engine oil pressure after cold start

A

156 psi

(130 psi at idle, 10 minutes max)

80
Q

Normal engine starter cycle

A

3 consecutive start attempts of 60 seconds each. 5 minutes cooling required prior to additional start attempts.

81
Q

Engine dry motoring limits

A

First dry motor 90 seconds followed by 5 minutes cooling.

Second and subsequent dry motors 30 seconds followed by 5 minutes cooling.

82
Q

Continuous engine ignition required

A

Takeoff/landing on contaminated runway

Takeoff in high crosswind

Moderate or heavier intensity rain

Moderate or heavier intensity turbulence

In vicinity of thunderstorms

83
Q

Maximum crosswind dry or wet runway?

84
Q

Maximum crosswind contaminated runway fair/medium braking action?

85
Q

Maximum crosswind contaminated runway braking action poor?

86
Q

45-minute IFR Reserve Fuel

87
Q

Minimum Release Fuel

88
Q

Hot Spare Fuel

89
Q

Emergency Release Fuel

90
Q

Minimum Dry Runway Length

91
Q

Minimum Runway Width

92
Q

Baggage Compartment Max Weight

93
Q

Minimum Altitude for use of Flight Spoilers

A

300’ AGL

94
Q

Minimum Pavement Width for 180-degree turn

95
Q

Maximum fuel imbalance between left & right main tanks during gravity refueling

96
Q

When is the use of KA SAT GND TX/KA BAND GND TX feature prohibited?

A
  1. During deice operations
  2. 100 feet or less from a building higher than the aircraft
97
Q

Fuel quantity required for parking aircraft in inclement weather?

A

6500-8500#

CL-650S (6 decks)

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