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CL3500 > Memory items > Flashcards

Memory items Flashcards

1
Q

Max Ramp Weight

A

40,750 lbs

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2
Q

Max T/O Weight

A

40,600 lbs

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3
Q

Max Landing Weight

A

34,150 lbs

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4
Q

Max Zero Fuel Weight

A

28,200 lbs

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5
Q

Minimum Flight Weight

A

24,800 lbs

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6
Q

Total Fuel

A

14,150 lbs

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7
Q

Total Fuel (gravity)

A

13,000 lbs

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8
Q

Honeywell HTF7350 (AS907-2-1A) takeoff thrust to ISA +15 C

A

7,323

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9
Q

Total fuel per side

A

7,075 lbs

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10
Q

Gravity fuel per side

A

6,500 lbs

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11
Q

Max baggage compartment

A

750 lbs

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12
Q

Minimum fuel for a go-around (per side)
Minimum altitude for spoilers

A

500

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13
Q

Emergency exit door weight

A

45 lbs

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14
Q

Minimum altitude for precision approach < 3.5*

A

80’

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15
Q

Minimum altitude precision approach 3.5 to 4.5*

A

160’

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16
Q

Minimum altitude visual, non-precision, AT off if Flaps <30* RA invalid

A

200’

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17
Q

Minimum height for autopilot engagement

A

700’

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18
Q

CABIN ALTITUDE - caution

A

8,500’

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19
Q

CABIN ALTITUDE - warning
(altitude)

A

9,400’

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20
Q

Max pressure altitude for takeoff and landing

A

10,000’

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21
Q

APU Max alt (ground), Emer depress altitude (auto mode)

A

14,000’

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22
Q

Cabin Altitude masks deploy

A

14,500’

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23
Q

Ditching switch only (below)

A

15,000’

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24
Q

Max Alt for flaps and gear

A

18,000’

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25
Q

APU Bleed Air for Engine start & ECS

A

20,000’

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26
Q

Max Alt for APU START (flight) & APU Gen

A

30,000’

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27
Q

Max Alt with YD inoperative

A

31,000’

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28
Q

APU max altitude

A

37,000’

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29
Q

Max Pressure Altitude

A

45,000’

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30
Q

Minimum speed for spoiler extension Vref +

A

8 KIAS

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31
Q

Max tailwind component

A

10 kts

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32
Q

Max crosswind TO

A

28 kts

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33
Q

Max crosswind Landing

A

24 kts

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34
Q

NWS Inop or one AHRS channel inop

A

15 kts

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35
Q

Max reverse available to

A

40 KIAS

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36
Q

Autothrottle engaged and thrust verified prior to

A

80 KIAS

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37
Q

Vmca flaps 10

A

110 KIAS

38
Q

Vmcg flaps 20

A

114 KIAS

39
Q

Vmcg, Vmcl flaps 10

A

115 KIAS

40
Q

Vfe Flaps 30

A

175 KIAS

41
Q

Tire limit speed

A

182 KIAS

42
Q

Min airspeed for Dual engine flameout

A

185 KIAS

43
Q

Vlo retract

A

200 KIAS

44
Q

Vfe Flaps 10 and Flaps 20

A

210 KIAS

45
Q

Vle, Vlo extension

A

250 KIAS

46
Q

Turbulence

A

265 KIAS or M.75

47
Q

Max airspeed for Apu start

A

285 KIAS

48
Q

Vmo <8,000

A

300 KIAS

49
Q

Vmo 8,000’ - 29,475’

A

320 KIAS

50
Q

Mmo above 29,475’

A

M .83

51
Q

Minimum temp for engine & apu start

A

-40 C

52
Q

Minimum battery temperature for TO

A

-20 C

53
Q

Max bulk fuel temp for TO, engine start

A

50 C

54
Q

What is the automatic landing altitude return-to-base criteria (pressurization)?

A

6000’ or 10 minutes

55
Q

How many feet are added to cabin altitude to readjust for a HAA caution light?

A

650’

56
Q

How many feet are added to cabin altitude to readjust for a HAA warning light?

A

1550’

57
Q

When must the PACK be operating on the ground?

A

When the aircraft electrical power is ON (Batt or external power) for more than 30 minutes w/ OAT >40 C

58
Q

Where is Delta P displayed?

A

EICAS, Summary page, ECS synoptic

59
Q

Half bank mode ON at altitude?

A

31,600

60
Q

Can the pilot override the YD?

A

NO

61
Q

What is required to erase the CVR?

A

Parking brake set and hydraulic system powered.

62
Q

Audio control panel EMER/NORM switched to EMER position

A

Audio is routed directly to headphones, bypassing the radio

63
Q

L (R) BATT OVERHEAT temp

A

70*C

64
Q

IP & HP Bleed valves are closed when

A

Switch(s) is OFF
Fail closed
Fire push selected

65
Q

Standby Instrument powered by

A

R ESS Bus

66
Q

Standby Instrument receives info from

A

Nav 1

67
Q

IP Air pressure regulated to

A

50 psi

68
Q

HP Air regulated to

A

36 psi

69
Q

How do you know an External Air Cart is connected?

A

psi displayed in the manifold on the ECS page

70
Q

When will GRND spoilers Auto deploy?

A

WOW, RA > 7’, wheel speed > 16kts

71
Q

Multi-function-spoilers

A

45, Ground 60

72
Q

PSEU

A

Proximity Sensing Electric unit - WOW, TR pos, fuel door

73
Q

BCU

A

Brake Control Unit

74
Q

EPAV

A

Electrical Pneumatic Actuating Valve (brains for O2, compensator, etc.)

75
Q

O2 min - max

A

700 liters (Oxy qty low CAS) - 5458 liters

76
Q

Types of operation

A

Day, Night, VMC, IMC, Icing, Ditching

77
Q

What is the purpose of the scavenge ejectors?

A

Transfer fuel from lowest inboard section of wing to the collector tank.

78
Q

After crossing the holding fix in the FMS, what is displayed next to 6L

A

Exit Hold

79
Q

What is the minimum width for an 180 degree turn with a 5’ safety margin?

A

58’

80
Q

Load Factors
Flaps Up
Flaps Extended

A

Flaps Up +2.6 to -1.0 G
Flaps Extended + 2.0 to 0.0 G

81
Q

Generator amp limits
Normal
Single gen flight
Transient

A

Normal 400a
Single gen flight 500a
Transient (5min) 600a

82
Q

Pavement for 180* turn

A

58’

83
Q

Aircraft dimensions

A

68’8” L x 69’ W x 20’ H

84
Q

Nose wheel steering
Tiller
Pedals

A

Tiller 65*
Pedals 7*

85
Q

What is the danger area distance for the Challenger 350 weather radar?

A

5 ft

86
Q

What is the danger area distance for the Challenger 350 intake?

A

15 ft (4.5 m)

87
Q

What is the danger area distance for the APU exhaust on the Challenger 350?

A

19 ft (5.8 m)

88
Q

What is the danger area distance for the tailpipe of the Challenger 350?

A

200 ft (60.9 m)

89
Q

Minimum fuel load for takeoff

A

2,800 lbs.

90
Q

Minimum oil temp for takeoff?

A

+27C

CL3500 (3 decks)

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