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CL-350S Study Cards > AIRPLANE GENERAL/MANUALS > Flashcards

AIRPLANE GENERAL/MANUALS Flashcards

1
Q

WHAT EMERGENCY EQUIPMENT IS LOCATED IN THE LAVATORY?

A
  1. ACCESS TO OXYGEN BOTTLES
  2. FIRE EXTINGUISHER
  3. PBE
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2
Q

HOW IS THE MAIN CABIN DOOR CLOSED NORMALLY?

A

ELECTRICALLY

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3
Q

IS IT POSSIBLE TO OPEN THE MAIN CABIN DOOR FROM THE INSIDE IF SOME CABIN PRESSURE REMAINS?

A

NO.

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4
Q

WHY IS IT NOT POSSIBLE TO OPEN THE MAIN CABIN DOOR FROM THE INSIDE IF SOME CABIN PRESSURE REMAINS?

A

CABIN PRESSURE ENGAGES A PRESSURE LOCK LEVER CONNECTED TO THE VENT FLAP, AND PREVENTS MOVEMENT OF THE INNER DOOR HANDLE. AFTER CABIN PRESSURE IS RELEASED, SPRINGS ALLOW THE VENT FLAP TO OPEN, THE PRESSURE LOCK DISENGAGES AND THE DOOR HANDLES CAN OPERATE.

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5
Q

Under what conditions will you get a white (status) PASSENGER DOOR and or CARGO DOOR message?

A

The aircraft is on the ground, the passenger door and or cargo door(s) is open, and the LEFT engine run switch is in the OFF position.

** All other monitored doors will always be displayed as an AMBER CAS Caution message.

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6
Q

Under what conditions will you expect to see an amber caution PASSENGER DOOR CAS message?

A
  1. Aircraft is on the ground, the door is open and the LEFT engine RUN switch is in the RUN position.
  2. In flight, the passenger door rollers are not fully engaged into the fitting guides.
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7
Q

Under what conditions will you expect to see an amber CARGO DOOR caution CAS message?

A

Aircraft is on the ground, cargo door is open, and the LEFT engine RUN switch is in RUN.

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8
Q

ENGINES INSTALLED

A

2, Honeywell HTF7350

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9
Q

Which 5 doors are monitored by the door warning system?

A
  1. PASSENGER DOOR
  2. EMERGENCY EXIT HATCH
  3. AFT EQUIPMENT BAY
  4. CARGO BAY
  5. BATTERY BAY
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10
Q

Assume the left engine run switch is OFF. If all 5 monitored doors are open, what indications would you see on CAS?

A 
PASSENGER DOOR (WHITE STATUS)
CARGO DOOR (WHITE STATUS)
EMERGENCY EXIT (AMBER CAUTION)
BATTERY BAY DOOR (AMBER CAUTION)
AFT EQPT BAY DOOR (AMBER CAUTION)
**Only the passenger door and cargo doors will be either white or amber depending on LEFT engine RUN  switch position.
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11
Q

With the nose gear torque link connected, what is the towing angle limit left or right of center?

A

120°

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12
Q

How will we know that the nose wheel has been rotated beyond 120 degrees?

A

Amber NWS LIMIT EXCEEDED caution CAS message.

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13
Q

What happens when the nose-wheel is rotated to 123 degrees left or right of center?

A

Indicator pins will shear and indicate the need to inspect the nose-wheel for possible damage.

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14
Q

What is the minimum pavement width required for a 180 degree turn with a 5 foot margin.

A

58 feet.

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15
Q

How long does the CVR tape for?

A

2 hours.

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16
Q

How long does the FDR record for?

A

25 hrs.

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17
Q

How much nose-wheel steering authority do you have with the tiller?

A

65 degrees left and right of center.

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18
Q

How much nose-wheel steering authority do you have with the rudder pedals?

A

7 degrees left or right of center.

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19
Q

What is the APU danger area?

A

19 feet (500 F)

20
Q

What are the engines’ danger areas? Exhaust and Inlet

A
  1. Exhaust: 200 feet
  2. Inlet: 15 feet
21
Q

What is the radar danger area?

A

5 feet

22
Q

WINGSPAN

A

69 feet

23
Q

Why must the battery bay, aft equipment bay, and outflow valve doors be unlocked prior to aircraft movement?

A

To provide blow-out protection because bleed air ducting runs through these areas.

24
Q

TAIL HEIGHT

A

20 FEET

24
Q

What doors must remain unlocked for flight? (BOMBARDIER)

A
  1. Outflow valve door
  2. Battery Bay Door
  3. Aft Equipment Bay Door
25
Q

In addition to the Outflow valve door, Battery Bay Door, and Aft Equipment Bay Door, why does Netjets require the Cargo door to be unlocked?

A

**Netjets requires you to have the Cargo door unlocked during flight and or aircraft movement. This allows for an additional egress door. This door should be used as a last resort as there is no way of assessing the outside conditions prior to opening.

26
Q

Do the gear pins have to be installed for towing?

A

YES.

27
Q

Where are the gear pins stored?

A

Cockpit Step Box, in blue pouch.

29
Q

Why do we not start the hydraulic pumps while the aircraft is being towed?

A

The brakes go through a test cycle and are applied.

**additionally, do not tow the aircraft while IRS’s are alligning or within 3 minutes of selecting batteries or stanby instrument to ON.

30
Q

What does the red MSW button on both yokes disconnect?

A

Autopilot
All trims including Mach Trim
deactivates stick pusher

31
Q

In what manual can you find systems information?

A

FCOM 2 (Aircraft Shipset/Manuals & Bulletins/OEM Manuals-CL350)

32
Q

In what manual can you find performance information?

A

QRH 1 (Aircraft Shipset/Manuals & Bulletins/OEM Manuals-CL350)

33
Q

In What manual can you find the failures, warning, caution, status, advisory message checklists and information?

A

QRH 2 (Aircraft Shipset/Manuals & Bulletins/OEM Manuals-CL350)

34
Q

In what manual can you find the simplified flight planning chart? (FUEL REQUIRED and FLIGHT TIME)

A

Challenger 350 CIFP supplement (Aircraft Shipset/Manuals and Bulletins/OEM Manuals-CL350)

35
Q

In what manual can you find the envelope chart?

A

Bombardier- Weight and Balance Manual- CL350 (Aircraft Shipset/Manuals and Bulletins/OEM Manuals-CL350)

36
Q

In what manual can you find the Bombardier GO NO GO guide?

A

QRH Vol. 2 (Aircraft Shipset/Manuals and Bulletins/OEM Manuals-CL350)

37
Q

Where can you find the NETJETS GO NO GO guide?

A

NJA - Discrepancy Programs - CL-350 (MEL/NEF/CDL/REFURB,CFI), CAS MESSAGE LIST (1.3)

38
Q

Other than the Engines, what other components on the aircraft are Honeywell?

A

APU

TAWS system

39
Q

The door may be electrically closed ____ consecutive times in _____ minutes, and then it must rest for _____ minutes for cooling.

A

3 times

3 minutes

5 Minutes

40
Q

During a Single engine go around, what is the FRA?

A

Emergency Safe Altitude (ESA)

41
Q

When does the FDR start recording?

A

STROBE/BEACON switch is in the BEACON or STROBE position.

Weight Off Wheels.

42
Q

When needed, how do you select TEMP COMP and where can you look up this procedure?

A

IDX>NEXT to display INDEX page 2/2.

Select TEMP COMP.

(AOM 6.3.13 Temperature Compensation)

43
Q

In what manual can you find the Maximum Altitude (FL) Capability based on weight and temp? i.e. “Execjet 762 can you accept FL450?”

A

AOM Chapter 9 (9.3.1 Climb Cruise Data)

44
Q

With the nose gear torque link connected, what happens if the nosewheel is rotated to 123 degrees left or right of center?

A

Sheers the limit pin.

45
Q

How many hand held Fire extinguishers are onboard the aircraft?

A

3

(AOM Chapter 11, 11.2.2)

46
Q

How many Rafts aboard?

A

3

(AOM 11.2.2)

47
Q

What information can you find in these Manuals:

QRH 1:
QRH 2:
FCOM 1:
FCOM 2:

A

QRH 1: Performance info
QRH 2: Abnormals
FCOM 1: Expanded POH
FCOM 2: Systems

CL-350S Study Cards (14 decks)

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