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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
AIR CONDITIONING / PRESSURIZATION How many pressurization modes?
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.
26
AIR CONDITIONING / PRESSURIZATION TAKE OFF - Pre-pressurization logic.
(-) 300ft under takeoff field elevation to 6,000 ft or 10 minutes has elapsed after takeoff. 300-500 fpm.
27
AIR CONDITIONING / PRESSURIZATION Landing - Pre-pressurization logic.
(-) 300 below landing field elevation after landing or aborted takeoff. 500 fpm.
28
AIR CONDITIONING / PRESSURIZATION Manual Pressurization Control knob range?
Full L or R (max)- 2500 fpm 12’o’clock position - 0 fpm 1/2 of full L or Right - 1000 fpm
29
AIR CONDITIONING / PRESSURIZATION EMERGENCY DEPRESS button.
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
30
AIR CONDITIONING / PRESSURIZATION DITCHING button.
Depressurization the Cabin Shuts off the AC system Closes the Outflow Valve Inhibited >15,000ft
31
AURAL / VISUAL ALERTS CVR - How long does it record? When is it powered on?
2 hours Essential Busses are powered (Battery switch on)
32
AURAL / VISUAL ALERTS SYNOPTIC PAGES - COLOR(s). RED, AMBER, GREEN, WHITE, MAGENTA, CYAN
``` RED - Exceedance AMBER - No flow or pressure GREEN - Normal Operation WHITE - No flow and Operations normal MAGENTA - Unknown data CYAN - Advisory ```
33
AVIONICS IAPS?
Integrated Avionics Processor System?
34
AVIONICS How do you erase the CVR?
Weight-on-wheels Parking brake on Hydraulic system pressure
35
AVIONICS When is 1/2 bank mode engaged?
Selecting it on the mode control panel | Automatically - >31,600 ft
36
AVIONICS To get TO/TO on the PFD for Takeoff what must be previously selected?
Flaps >0 Speeds set (Manually or automatically) Engines Running
37
APU Primary function?
Electrical
38
APU How does the APU shutdown?
ECU sends and overspeed signal to close the fuel solenoid valve.
39
APU What happens when there’s an APU fire on the ground? Flight (all NJA planes are modded SB 350-49-001)
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
APU Why is the right BATTERY isolated from the RIGHT ESSENTIAL bus during start?
To prevent a voltage drop momentarily. The LEFT ESSENTIAL bus maintains power to both ESSENTIAL busses during the APU start.
41
APU When does the APU surge control valve commanded open?
>15,000 ft when supplying electrical loads
42
AVIONICS The EMERGENCY button on the AUDIO panels does what?
Directly connects the headphones to the onside audio panel bypassing the RIU.
43
ELECTRICAL Turning on the R BATT switch does what?
``` 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
ELECTRICAL External power. Green Indications? What is the parameters?
Correct Voltage and Polarity (Green light on the switch in the cockpit) 28 VDC - 1500 AMPS
45
ELECTRICAL With ground power ON and selected can you bring online any engine or APU generator(s)?
NO
46
ELECTRICAL When do the Cockpit floor heaters load shed?
Loss of Auxiliary busses (1 generator)
47
OXYGEN Oxygen MAX quantity read at service panel? Cockpit?
1850 psi | 5438 liters
48
OXYGEN FLOW RATE when the passenger mask are dropped automatically? Manually?
Automatically - Lower rate | Manually - High Rate
49
OXYGEN Pilots O2 mask certified height?
40,000 ft
50
OXYGEN Passenger O2 mask certified height?
No prolonged periods > 25,000 ft
51
OXYGEN What altitude does the pilots 02 mask go to 100% automatically?
> 35,000 ft
52
OXYGEN How long does the PBE last when in use?
15 minutes
53
OXYGEN How does the passenger 02 start the flow once they are deployed?
Must pull on the lanyard to start the flow of 02.
54
FIRE What is the FIREX-CU
System that controls the fire protection.
55
FIRE How many engine / APU fire bottels? # of squibs
2 ``` #1 - 2 squibs #2 - 3 squibs (1 for APU). Only bottle that can discharge into the APU ```
56
FIRE ENGINE/APU fire bottle types?
Halon 1311
57
FIRE Engine FIRE switch selected does what?
``` 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
FIRE FIRE DETECTION where?
Core Engine Area Fwd Nacelle Pylon Area Dual Detection Loops
59
FIRE Overheat Detection Area?
Main wheel well areas Single Loop Conectted to FIREX-CU
60
FIRE Smoke Detector area?
Cargo bay Light - scatter type detector
61
FLIGHT CONTROLS Aileron Bent Tab?
Keeps upfloat to a minimum at high speeds
62
FLIGHT CONTROLS Aileron Balance Tabs
Move in opposite direction of corresponding aileron movement to reduce the pilot effort against the aerodynamic force of the aileron.
63
FLIGHT CONTROLS Roll Spoilers - SECU
Spoiler Electronic Control Units (2) Panels 1,2, 7,8 SECU #2 - Outboard 1 & 8 SECU #1 - Inboard 2 & 7
64
FLIGHT CONTROLS Aileron Disconnect gives you what on each side?
Left - Roll Spoilers | Right - Ailerons
65
FLIGHT CONTROLS Aileron effectiveness?
Roll spoilers - 60% | Ailerons - 40%
66
FLIGHT CONTROLS Aileron Trim is on what side?
Left
67
FLIGHT CONTROLS Where do you see the roll spoilers moving in flight?
NOT ON MFD | (FLT) synoptic page ONLY
68
FLIGHT CONTROL When do the roll spoiler and ground spoilers deploy?
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
FLIGHT CONTROLS RUDDER PCU’s?
2 Top - Right Hydraulic Bottom - Right Hydraulic & AUX Hydraulic
70
FLIGHT CONTROLS How many YDs?
1
71
FLIGHT CONTROLS When is the YD active?
``` Selected on (button or automatically when you select Autopilot on) >60 kts and disabled when WOW is achieved on landing. ```
72
FLIGHT CONTROLS How many Elevator PCUs?
4 | 2) Left Elevator (Left and Right Hydraulic (2) Right Elevator (Left and Right Hydraulic)
73
FLIGHT CONTROL MACH TRIM?
Makes allowance for the rearward shift of the aerodynamic center-of-pressure as the mach number increases.
74
FLIGHT CONTROLS When is Mach Trim active
In flight with or without the autopilot engaged.
75
FLAPS What hydraulic system is NORMAL laps associated with?
RIGHT
76
FLAPS The AUX HYDRAULIC switch?
Uses LEFT hydraulic power.
77
FLIGHT CONTROLS Primary TRIM mode (speed)?
When going fast the trim goes slow | When going slow the trim moves fast
78
FLIGHT CONTROLS Secondary TRIM mode?
Slow speed all the time NO Autopilot No Mach Trim No Config Trim
79
FLIGHT CONTROLS SPS (Stall Protection System) Shaker sides and pusher side?
Shaker - Both yokes Pusher - Left yoke Shaker Activates so does the ignition. Can stop the pusher by selecting either yoke’s MWS button.
80
FLIGHT INSTRUMENTS Standby Instrument Batteries last how long?
3.5 hours
81
FUEL Which ejectors feed fuel to the collector tanks.
Scavenge ejectors
82
FUEL What ejectors feed fuel to the engine?
Main ejectors.
83
FUEL NACA Vents do what?
Provide static ventilation of the fuel tank
84
FUEL Dual channel fuel computer protections? Inputs from what?
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
HYDRAULICS What is fluid migration?
#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
HYDRAULIC Why do we turn on the #2 hydraulic before the PTU and AUX pump?
To prime the system before activation to prevent cavitation.
87
HYDRAULICS What is the PTU?
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
HYDRAULIC AUX HYDRAULIC PUMP
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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