CL350 Initial Training Systems Test Flashcards Preview

Challenger 350 Flashcards rev0419 > CL350 Initial Training Systems Test > Flashcards

Flashcards in CL350 Initial Training Systems Test Deck (106)
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31

How long do the Aft Equipment bay light stay on?

20 Minutes

After 15 Minutes the lights will flash for 10 seconds and then turn off

32

IP air is used for what systems?

What is the max PSI?

Engine Starting

Environmental Control System

Pressurization

 

Max PSI = 50

33

Which pneumatic system uses HP air?

 

Day 4

Wing and engine Anti-Ice

34

Configuration Warning

Parking Brake

Disconnects (2)

Flaps

Autopilot

Spoilers

Trims (3)

 

Memory Aid: PDFAST

35

Which spoilers act as multifunction spoilers?

 

Day 2

1,2 and 7,8 (Outboard)

36

What is ROLS?

Remote Oil Level Sensor

37

When will the FDR begin recording?

 

Day 2

Beacon ON, or

WOW (weight OFF wheels)

38

What is the normal takeoff thrust for the HTF7350 engine?

 

Day 1

7,372 lbs Flat rated at ISA+15c at sea level APR

Increases power to +20c

39

Bleed air switches are normally positioned:

All on, or all off

40

What does IASC stand for?

Integrated Air System Controller

ECS and Pressurization Control

41

When are select EICAS messages inhibited for takeoff and landing?

 

Day 2

Takeoff - Airspeed above 80 kts until above 400 feet

Landing - Below 400 feet until less than 40 kts.

42

When does the CVR start recording and how long does it last?

Starts recording when Battery power is applied and records for 2 hrs

43

Max Generator Loads with 2 Generators on the ground

400 amps

44

HP air provides air for which system and at what PSI?

Anti-Ice @ 36 psi

45

Max Generator Load (Transient)

600 amps for 5 minutes

46

 At and below what temperature and with snow, ice, standing water or slush present must the engine anti-ice system be on?

Day 4

10°C OAT

47

Wing anti-ice fails in what position?

 

Day 4

Fails (spring loaded) to the CLOSED position

48

Following an aborted start, how long must the engine be dry motored before an additional start may be attempted?

 

Day 4

30 seconds

49

What is the power source for the Left DCMP?

What is the power source for the Right DCMP?

 

Day 5

Left DCMP - Right Main Bus

Right DCMP - Left Essential Bus

50

How many Air Data Computers are in the CL350?

 

Day 6

2

51

What EICAS Message will be displayed with Anti-Ice systems off and ICE DETECTED?

Anti-Ice System on?

 

 

Day 4

Anti-Ice Off - ICE DETECTED in Amber.

Anti-Ice On - ICE DETECTED in Cyan

52

Where is the fuel/hydraulic heat exchanger located?

 

 

Day 5

Wing fuel tank

53

APU Planned Fuel Burn

150 pph

54

What does the Ditching switch do?

 

Day 5

1. Depressurizes the cabin

2. Disables the ECS (Flow Control Valves)

3. Closes the outflow valve

55

With less than 1,000 lbs of fuel per side, limit flight to less than?

30 Minutes

56

When will the Auxiliary buses load shed?

 

Day 3

Single generator operation in flight.

57

After shutdown, what is the time range to check the oil?

5 to 30 minutes after shut-down

58

Total Circuit Breaker panels

7 total CB panels

 

2 in cockpit (Cockpit prep check)

2 in galley (Cockpit prep check)

1 additional in galley storage

2 in aft equipment bay

59

Dual fire detection loops in the engine and APU fire provide information to what component?

 

Day 3

FIREX-CU

Fire Detection and Extinguishing Control Unit.

60

When will the Bus Tie open?

 

Day 3

2 or more generators online.