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350 Limits, Opspecs, etc. DDAL > Limitations > Flashcards

Limitations Flashcards

1
Q

Maximum Ramp Weight CL300

A

39,000 lbs.

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2
Q

Maximum Takeoff Weight CL300

A

38,850 lbs.

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3
Q

Maximum Zero Fuel Weight CL300

A

27,200 lbs.

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4
Q

Maximum Landing Weight CL300

A

33,750 lbs.

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5
Q

Minimum Flight Weight CL300

A

23,100 lbs.

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6
Q

VRA-Rough Air

A

265 KIAS/0.75 M

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7
Q

VLO-Retraction

A

200 KIAS

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8
Q

VLO-Extension

A

250 KIAS

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9
Q

VLE-Extended

A

250 KIAS

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10
Q

VFE Flaps 10

A

210 KIAS

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11
Q

VFE Flaps 20

A

210 KIAS

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12
Q

VFE Flaps 30

A

175 KIAS

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13
Q

Maximum Tire Speed

A

182 kts

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14
Q

Maximum T/O and Landing Pressure Altitude

A

10,000’

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15
Q

Maximum Tailwind Component

A

10 knots

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16
Q

Maximum Runway Slopes

A

+2% to -2%

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17
Q

Maximum Pressure Altitude

A

45,000’

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18
Q

Maneuvering Load Factors Flaps Up

A

+2.6 to -1.0

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19
Q

Maneuvering Load Factors Flaps Extended

A

+2.0 to 0.0

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20
Q

RVSM Required Equipment

A

Autopilot-1
Altitude Alerting System-1
Altitude Reporting Transponder-1
Air Data Computers-2

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21
Q

Minimum Oil Temp for starting?

A

-40C

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22
Q

When side window icing is observed you may be in ______ and should?

A

SLD and turn on anti ice equipment and exit conditions.

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23
Q

Engine Anti-ice must be on when on the ground and for takeoff if?

A

OAT is below 10C and visible moisture is present.

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24
Q

Flight Icing conditions as described by Bombardier are?

A

OAT is from 10C to -40C and visible moisture is present.

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25
Q

What are two conditions that require engine anti-ice to be on?

A
  1. In icing conditions.

2. ICE DETECTED CAS

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26
Q

The wing anti-ice must be on when on the ground when?

A

The OAT is 5C or below and visible moisture or standing moisture is present.

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27
Q

The wing anti ice must be on in flight when?

A
  1. In icing conditions (10C to -40C with visible moisture).
    (and speed less than 210 KIAS)
  2. ICE DETECTED CAS displayed.
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28
Q

Maximum operating speed up to 8,000’ is?

A

300 KIAS

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29
Q

Maximum operating speed from 8,001’ to 29,475’ is?

A

320 KIAS

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30
Q

Maximum operating speed above 29,475’ is?

A

0.83 M

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31
Q

Vra is

A

265 KIAS/0.75 M

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32
Q

When on the ground do not select the AIR SOURCE to?

A

TRIM AIR ONLY

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33
Q

The pack must be operating when aircraft electrical power is on for more than _______ minutes and the OAT is?

A

more than 30 minutes and OAT is above 40C.

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34
Q

Crew and passenger oxygen masks are not APPROVED for use above?

A

40,000’ cabin altitude.

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35
Q

Prolonged operation of passenger masks above _______ is not RECOMMENDED.

A

25,000 cabin altitude.

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36
Q

The maximum cabin differential pressure on the ground must not exceed?

A

0.1 PSI

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37
Q

The maximum cabin differential during landing must not exceed?

A

1.0 PSI

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38
Q

The maximum positive differential pressure is?

A

9.4 PSI

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39
Q

The maximum negative differential pressure is?

A

-0.5 PSI

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40
Q

Autopilot operation with an ILS glidepath angle that exceeds ______ is prohibited.

A

4.49 degrees

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41
Q

Autopilot minimum use height for Climbs, Enroute, or Descents is?

A

700’ AGL

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42
Q

Autopilot minimum use height for Precision Approach is?

<3.5 >3.5

A

80’ AGL less than 3.5 glidepath/ 3.5 to 4.5 glidepath angle is 160’ AGL

43
Q

Autopilot minimum use height for Visual or Non-Precision approach is?

A

200’ AGL

44
Q

Maximum altitude with Yaw Damper off is?

45
Q

DATALINK is approved for tx/rx of messages that?

A

will not create an unsafe condition if the message is improperly received.

46
Q

FMS V-speed data is prohibited for temperatures?

A

Above ISA + 33C

47
Q

To be used for navigation the FMS must be receiving suitable nav data from? (CL300 only)

A
  1. One VOR/DME or
  2. Two DMEs or
  3. GPS
48
Q

Maximum continuous amps with 2-3 generators operating?

49
Q

Maximum continuous amps with one generator operating on the ground?

50
Q

Maximum continuous amps with one generator operating in flight?

51
Q

Transient amp limit?

52
Q

Do not takeoff if battery temperatures are below?

53
Q

Do not extend flaps above?

54
Q

Flight spoilers must not be extended in flight at airspeeds?

A

below approach speed plus 8 KIAS

55
Q

Flight spoilers must not be extended in flight below _____’ AGL

56
Q

Do not extend landing gear above?

57
Q

Maximum usable fuel with a pressure refuel?

A

14,150 lbs. total/7,075 lbs per side

58
Q

Maximum usable fuel with a gravity refuel?

A

13,000 lbs. total/6,500 lbs per side

59
Q

Minimum fuel for go-around?

A

500 lbs. per side

60
Q

Idle N2 minimum?

A

46.0%

45% for PMA to power FADEC

61
Q

Idle oil pressure minimum?

62
Q

Maximum Continuous Climb oil temp?

63
Q

Normal Takeoff oil temperature range?

A

27C minimum to 138C maximum

64
Q

APU Max Altitude Operation

65
Q

APU Max Altitude for use as generator?

66
Q

APU max altitude for bleed air for engine start?

67
Q

The APU may be started up to an altitude of?

ground/flight

A

30,000’ in flight and 14,000’ on the ground

68
Q

Hydraulic Fluid type?

69
Q

Approve Fuels?

A

Jet A, Jet A-1, Jet B, JP-4, JP-5, JP-8

70
Q

What type of engines?

71
Q

Takeoff Power time limit?

72
Q

Time limit on APR power?

A

10 minutes if automatically selected, 5 minutes for manually selected

73
Q

Max reverse thrust is automatically reduced at what speed?

74
Q

What is the minimum oil temperature required to operate engines above ground idle?

(minimum oil temperature to advance the TLs at all after starting)

75
Q

With oil temperatures between 5C and 14C engines may be?

A

operated from idle up to but NOT including climb power.

76
Q

How many consecutive engine start cycles may be conducted?

A

3, followed by a cooling period of 15 minutes.

77
Q

After an aborted start the engine…?

A

must be motored for 30 seconds.

78
Q

APU type?

A

Honeywell 36-150BD

79
Q

Do not use the APU to start the left engine above?

80
Q

APU starting limitations?

A

1-60 seconds
2-60 seconds
3-20 minutes

81
Q

Max APU RPM?

82
Q

Max APU EGT for start?

83
Q

Max APU ITT for normal operations?

84
Q

Reverse thrust above idle reverse is prohibited below _____ KIAS.

85
Q

Thrust reversers on touch and go landings are_______.

A

prohibited.

86
Q

When deicing the aircraft with fluid operation of the APU is ______.

A

prohibited.

87
Q

Wingspan CL300 CL350

A

63’10” / 69’00”

88
Q

Length CL 300/350

A

68’08”

89
Q

Height. CL300/350

A

20’00”

90
Q

Minimum Pavement for a 180

CL300 and CL350

A

58’00”

91
Q

Wingtip Clearance for 180 turn CL300 CL350?

A

95’5” / 101’00”

92
Q

Do not hold in icing conditions with flaps _________?

93
Q

CL350 Max Ramp Wt?

94
Q

CL350 Max T/O Weight?

95
Q

CL350 Max Zero Fuel Wt?

96
Q

CL350 Max Landing Weight?

97
Q

CL350 Min Flight Weight?

98
Q

Max demo x-wind takeoff?

99
Q

Max demo x-wind landing?

100
Q

CL350 FMS as a navigation source must be receiving?

A

2 GNSS or
1 VOR/DME or
2 DMEs or
1 IRS

101
Q

If a life raft is required, the maximum PASSENGERS on board is?

102
Q

Maximum lap children?

A

2

*more are possible with mgmt approval considering oxygen and life rafts.

103
Q

Minimum bleed air for normal start?

350 Limits, Opspecs, etc. DDAL (2 decks)

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