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CL-350 - BM > CL-350 Personal Notes > Flashcards

CL-350 Personal Notes Flashcards

1
Q

PRESSURIZATION

Max Cabin Altitude

A

7850ft at FL450

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2
Q

ELECTRICAL

Where are CB-1, CB-3, CB-5 breaker panels?

A

Left side.
CB-1 - Left Cockpit
CB-3 - Left Side Equipment Rack (Secondary Power Center)
CB-5 - Left DCPC (DC Power Center)

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3
Q

ELECTRICAL

Where are CB-2, CB-4, CB-6 breaker panels?

A

Right side.
CB-2 - Left Cockpit
CB-4 - Left Side Equipment Rack (Secondary Power Center)
CB-6 - Left DCPC (DC Power Center)

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4
Q

PRESSURIZATION

To prevent cabin bump the AC supply should be turned off?

A

Prior to closing the main cabin door.

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5
Q

GENERAL

How much runway witdth is needed to do a 360˚ turn?

A

53ft. That includes 5 feet for safety.

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6
Q

PRESSURIZATION

The plaque card above the pressurization panel 1.0 and .5 is for what mode?

A

Manual

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7
Q

DOORS

T or F? Does the Main Cabin Door and Cargo door each have a vent flap?

A

Yes

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8
Q

DOORS

What is the purpose of the Vent flaps on the main and cargo doors?

A

To relieve cabin pressure (residual) to allow the door to open.

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9
Q

DOORS

What monitored doors have an amber CAS message associated when OPEN on the ground with the LEFT engine switch OFF.

A

Emergency Exit
Aft Service Compartment Door
Battery Door

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10
Q

DOORS

What monitored doors have a white CAS message associated when OPEN on the ground with the LEFT engine switch OFF.

A

Main Cabin Door

Cargo Door

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11
Q

DOORS

What monitored doors have an AMBER CAS message associated when OPEN on the ground with the LEFT engine switch ON.

A 
Main CabinDoor
Cargo Door
Emergency Exit
Aft Service Compartment Door
Battery Door
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12
Q

DOORS

Emergency Exit Door Weight?

A

45 pds

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13
Q

DOORS

Is the Cargo door certified as an Emergency Exit?

A

NO

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14
Q

DOORS

Total number of service doors?

A

12

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15
Q

DOORS

What doors per (NJA- AOM) must remain UNLOCKED prior to flight?

A

Cargo Door
Battery Door
Outflow Valve Door
Aft Service Compartment Door

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16
Q

DOORS

Why do the Battery Door, Aft Service Compartment Door and Outflow Valve Door must remain unlocked for flight?

A

Pressure from systems can build up and pop (relief) the door open to relieve pressure without damaging the door. Designed to open up into the wind without damage.

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17
Q

PRESSURIZATION

When must you manually enter the field elevation into the pressure controller?

A

No airport data in the FMS (selected) or the FMS has failed.

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18
Q

PRESSURIZATION

When you manually select the field elevation what color was the FMS selection vs the manual selection.

A

FMS - Magenta

Manual - Cyan

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19
Q

OXYGEN

What is the minimum temp to test the pilots oxygen mask?

A

-5˚C

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20
Q

AIR CONDITIONING / PRESSURIZATION

What is the IASC? How many on the CL-350?

A

Integrated Air System Controller

2

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21
Q

AIR CONDITIONING / PRESSURIZATION

Temperature control (cockpit) range in Automatic? Manual?

A

Automatic - 15˚C - 35˚C

Manual - 3˚C to 70˚C

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22
Q

AIR CONDITIONING / PRESSURIZATION

IP air supplies air to what systems? HP

A

IP - Environmental Control System

HP - Anti-Ice

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23
Q

AIR CONDITIONING / PRESSURIZATION

RAM Air on the ground provides what?

A

A fan driven by the ACM increases airflow through the Ram Air duct to increases cooling the heat exchangers.

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24
Q

AIR CONDITIONING / PRESSURIZATION

Avionics Cooling fan speeds on Ground? Flight? Controlled by?

A

Ground - HIGH
Flight - LOW

IASC #1 controls and monsters. IASC #2 provides downgraded mode with failure of # 1.

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25
Q

AIR CONDITIONING / PRESSURIZATION

How many pressurization modes?

A

2

(2) Auto Mode - IASC’s drives outflow valve
(1) Manual Mode - Manual Control of outflow valve

**(2) Safety Valves - Independent valves for overpressure and negative pressure.

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26
Q

AIR CONDITIONING / PRESSURIZATION

TAKE OFF - Pre-pressurization logic.

A

(-) 300ft under takeoff field elevation to 6,000 ft or 10 minutes has elapsed after takeoff. 300-500 fpm.

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27
Q

AIR CONDITIONING / PRESSURIZATION

Landing - Pre-pressurization logic.

A

(-) 300 below landing field elevation after landing or aborted takeoff. 500 fpm.

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28
Q

AIR CONDITIONING / PRESSURIZATION

Manual Pressurization Control knob range?

A

Full L or R (max)- 2500 fpm
12’o’clock position - 0 fpm
1/2 of full L or Right - 1000 fpm

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29
Q

AIR CONDITIONING / PRESSURIZATION

EMERGENCY DEPRESS button.

A

Functions in both Automatic and Manual Modes

Auto Mode - 2500 up to 14, 000 +/- 100 ft
Manual Mode - 3000 up to 14,500 +/- 500 ft

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30
Q

AIR CONDITIONING / PRESSURIZATION

DITCHING button.

A

Depressurization the Cabin
Shuts off the AC system
Closes the Outflow Valve

Inhibited >15,000ft

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31
Q

AURAL / VISUAL ALERTS

CVR - How long does it record? When is it powered on?

A

2 hours

Essential Busses are powered (Battery switch on)

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32
Q

AURAL / VISUAL ALERTS

SYNOPTIC PAGES - COLOR(s).

RED, AMBER, GREEN, WHITE, MAGENTA, CYAN

A 
RED - Exceedance
AMBER - No flow or pressure
GREEN - Normal Operation
WHITE - No flow and Operations normal
MAGENTA - Unknown data
CYAN - Advisory
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33
Q

AVIONICS

IAPS?

A

Integrated Avionics Processor System?

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34
Q

AVIONICS

How do you erase the CVR?

A

Weight-on-wheels
Parking brake on
Hydraulic system pressure

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35
Q

AVIONICS

When is 1/2 bank mode engaged?

A

Selecting it on the mode control panel

Automatically - >31,600 ft

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36
Q

AVIONICS

To get TO/TO on the PFD for Takeoff what must be previously selected?

A

Flaps >0
Speeds set (Manually or automatically)
Engines Running

37
Q

APU

Primary function?

A

Electrical

38
Q

APU

How does the APU shutdown?

A

ECU sends and overspeed signal to close the fuel solenoid valve.

39
Q

APU

What happens when there’s an APU fire on the ground? Flight (all NJA planes are modded SB 350-49-001)

A

The APU automatically shuts down and 6 seconds later discharges the #2 fire bottle into the APU compartment. Flight and on the Ground with the mod.

40
Q

APU

Why is the right BATTERY isolated from the RIGHT ESSENTIAL bus during start?

A

To prevent a voltage drop momentarily. The LEFT ESSENTIAL bus maintains power to both ESSENTIAL busses during the APU start.

41
Q

APU

When does the APU surge control valve commanded open?

A

> 15,000 ft when supplying electrical loads

42
Q

AVIONICS

The EMERGENCY button on the AUDIO panels does what?

A

Directly connects the headphones to the onside audio panel bypassing the RIU.

43
Q

ELECTRICAL

Turning on the R BATT switch does what?

A 
Prevents automatic start of the APU
Starts the Stabalizer Trim Test
Closes the battery contractor
Powers ALL busses (on the ground)
Starts the IRS Alignment process
CVR starts
System Self Test
BRAKE Test (Assuming the hydraulic system is NOT in the YELLOW range)
44
Q

ELECTRICAL

External power. Green Indications? What is the parameters?

A

Correct Voltage and Polarity (Green light on the switch in the cockpit)
28 VDC - 1500 AMPS

45
Q

ELECTRICAL

With ground power ON and selected can you bring online any engine or APU generator(s)?

A

NO

46
Q

ELECTRICAL

When do the Cockpit floor heaters load shed?

A

Loss of Auxiliary busses (1 generator)

47
Q

OXYGEN

Oxygen MAX quantity read at service panel? Cockpit?

A

1850 psi

5438 liters

48
Q

OXYGEN

FLOW RATE when the passenger mask are dropped automatically? Manually?

A

Automatically - Lower rate

Manually - High Rate

49
Q

OXYGEN

Pilots O2 mask certified height?

A

40,000 ft

50
Q

OXYGEN

Passenger O2 mask certified height?

A

No prolonged periods > 25,000 ft

51
Q

OXYGEN

What altitude does the pilots 02 mask go to 100% automatically?

A

> 35,000 ft

52
Q

OXYGEN

How long does the PBE last when in use?

A

15 minutes

53
Q

OXYGEN

How does the passenger 02 start the flow once they are deployed?

A

Must pull on the lanyard to start the flow of 02.

54
Q

FIRE

What is the FIREX-CU

A

System that controls the fire protection.

55
Q

FIRE

How many engine / APU fire bottels? # of squibs

A

2

#1 - 2 squibs
#2 - 3 squibs (1 for APU). Only bottle that can discharge into the APU
56
Q

FIRE

ENGINE/APU fire bottle types?

A

Halon 1311

57
Q

FIRE

Engine FIRE switch selected does what?

A 
Arms both fire bottles arm and switch lights illuminate
Fuel Shutoff valve closses
Hydraulic Shutoff valve closes
Bleed-Air shutoff valves close
Generator is selected offline
FADEC commands Engine Shutdown
58
Q

FIRE

FIRE DETECTION where?

A

Core Engine Area
Fwd Nacelle
Pylon Area

Dual Detection Loops

59
Q

FIRE

Overheat Detection Area?

A

Main wheel well areas

Single Loop

Conectted to FIREX-CU

60
Q

FIRE

Smoke Detector area?

A

Cargo bay

Light - scatter type detector

61
Q

FLIGHT CONTROLS

Aileron Bent Tab?

A

Keeps upfloat to a minimum at high speeds

62
Q

FLIGHT CONTROLS

Aileron Balance Tabs

A

Move in opposite direction of corresponding aileron movement to reduce the pilot effort against the aerodynamic force of the aileron.

63
Q

FLIGHT CONTROLS

Roll Spoilers - SECU

A

Spoiler Electronic Control Units (2)

Panels 1,2, 7,8
SECU #2 - Outboard 1 & 8
SECU #1 - Inboard 2 & 7

64
Q

FLIGHT CONTROLS

Aileron Disconnect gives you what on each side?

A

Left - Roll Spoilers

Right - Ailerons

65
Q

FLIGHT CONTROLS

Aileron effectiveness?

A

Roll spoilers - 60%

Ailerons - 40%

66
Q

FLIGHT CONTROLS

Aileron Trim is on what side?

A

Left

67
Q

FLIGHT CONTROLS

Where do you see the roll spoilers moving in flight?

A

NOT ON MFD

(FLT) synoptic page ONLY

68
Q

FLIGHT CONTROL

When do the roll spoiler and ground spoilers deploy?

A

1 & 8 - Spoilers selected
1, 2, 7, 8 - Emergency Spoilers selected / Ailerons Selected
1, 2, 3, 4, 5, 6, 7, 8 - Automatically or manually on the ground

69
Q

FLIGHT CONTROLS

RUDDER PCU’s?

A

2

Top - Right Hydraulic
Bottom - Right Hydraulic & AUX Hydraulic

70
Q

FLIGHT CONTROLS

How many YDs?

A

1

71
Q

FLIGHT CONTROLS

When is the YD active?

A 
Selected on (button or automatically when you select Autopilot on)
>60 kts and disabled when WOW is achieved on landing.
72
Q

FLIGHT CONTROLS

How many Elevator PCUs?

A

4

2) Left Elevator (Left and Right Hydraulic
(2) Right Elevator (Left and Right Hydraulic)

73
Q

FLIGHT CONTROL

MACH TRIM?

A

Makes allowance for the rearward shift of the aerodynamic center-of-pressure as the mach number increases.

74
Q

FLIGHT CONTROLS

When is Mach Trim active

A

In flight with or without the autopilot engaged.

75
Q

FLAPS

What hydraulic system is NORMAL laps associated with?

A

RIGHT

76
Q

FLAPS

The AUX HYDRAULIC switch?

A

Uses LEFT hydraulic power.

77
Q

FLIGHT CONTROLS

Primary TRIM mode (speed)?

A

When going fast the trim goes slow

When going slow the trim moves fast

78
Q

FLIGHT CONTROLS

Secondary TRIM mode?

A

Slow speed all the time
NO Autopilot
No Mach Trim
No Config Trim

79
Q

FLIGHT CONTROLS

SPS (Stall Protection System) Shaker sides and pusher side?

A

Shaker - Both yokes
Pusher - Left yoke

Shaker Activates so does the ignition.
Can stop the pusher by selecting either yoke’s MWS button.

80
Q

FLIGHT INSTRUMENTS

Standby Instrument Batteries last how long?

A

3.5 hours

81
Q

FUEL

Which ejectors feed fuel to the collector tanks.

A

Scavenge ejectors

82
Q

FUEL

What ejectors feed fuel to the engine?

A

Main ejectors.

83
Q

FUEL

NACA Vents do what?

A

Provide static ventilation of the fuel tank

84
Q

FUEL

Dual channel fuel computer protections? Inputs from what?

A

One channel calculates the fuel and if the onside channel fails the other channel automatically assumes control.

Fuel computer gets inputs from the fuel probes, and IRS.

85
Q

HYDRAULICS

What is fluid migration?

A

2 system powers the lower rudder PCU. When powering the AUX hydraulic pump some of the fluid moves into the intensifier thus causing fluid migration.

86
Q

HYDRAULIC

Why do we turn on the #2 hydraulic before the PTU and AUX pump?

A

To prime the system before activation to prevent cavitation.

87
Q

HYDRAULICS

What is the PTU?

A

Powered by the RIGHT hydraulic system but contained in the LEFT hydraulic system for gear retraction and retraction when you loose the Engine Driven Pump.

88
Q

HYDRAULIC

AUX HYDRAULIC PUMP

A

Powers the LOWER Rudder PCU and maintains the AUX accumulator (GEAR) pressure between 2500-3350 psi.

CL-350 - BM (6 decks)

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