Specs Flashcards

1
Q

What are the aircraft dimensions?

A

14’ tall

47’ 3” long

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2
Q

What is Tail height?

A

14’

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3
Q

What is wing height?

A

5’ 4”

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4
Q

What is prop diameter?

A

8’ 9” diameter

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5
Q

Wingspan?

A

53’ 4”

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6
Q

Wing area

A

277.8 square feet

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7
Q

Tail dimensions

A

17’ wide x 14’ tall

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8
Q

Wingtip radius for turning?

A

35’ 7”

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9
Q

Emergency exit overwing

A

1 piece 26” high x 18” wide
No pilot warning if removed
May be opened inside or outside

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10
Q

Dv window

A

Closed - normal operations

Located on captains side
Ventilation on ground - help smoke evacuations

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11
Q

Passenger door

A
Air stair type door
24" wide x 53" 
Secured by 6 locking pins
2 micro switches
Approved emergency exit
6 indicator lights
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12
Q

Cargo door

A
52" H x 53" wide
Secured by 2 shoot bolts
3 hook latches
2 micro switches 
Gas cylinder assist
Electric or manual closing
Not approved emergency exit
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13
Q

Cargo area

A

400 lbs Max

Light automatically goes off after 5 minutes

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14
Q

MAU

A

Computer controls everything

  • box full of modules
  • integrated avionics system
  • Divided into 2 channels for Redundancy
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15
Q

Cockpit display

A

Consists of 4 units
DU 1-4

Captain
Copilot
Systems
MFD

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16
Q

iNav MFD

A

Map on the bottom
- can toggle between systems and charts
Make sure to switch to top center display per Planesense!

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17
Q

Monitoring Warning system

A

Tells when something is wrong

  • CAS
  • FAS
  • Aural Warning
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18
Q

Cas

A

Crew alerting system

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19
Q

Fas

A

Aircraft flight alert

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20
Q

Aural warning

A

Voice call outs and chimes

Red - bad on top

Amber

Cyan

White - state the system is in

21
Q

What engine is installed?

A

PT6A-67P

  • 1200 Shaft HP
  • free turbine design
  • reverse flow
22
Q

Np

A

Speed of prop

23
Q

Ng

A

Compressor speed

24
Q

Engine is canted…. and why?

A

Canted 2 degrees down and 2 degrees right

For torque

25
Q

True or False

Majority of the air compressed is not for combustion?

A

True
25% for combustion
65% cool combustion
10% for secondary air systems

26
Q

Describe back of engine

A

4 stage axial compressor

Bands of air moved opposite directions

27
Q

Describe center of engine

A

Centrifugal compressor

Pushes air into combustion chamber

28
Q

Compressor

A

Draws air into engine before delivery into combustion chamber

Air not used creates a cushion of air

29
Q

What is the compressor turbine speed?

A

39000 max RPM @ 104% Ng

30
Q

What is RGB?

A

Reduction Gear Box

Reduces turbine speed low/high planetary gear

steps down

   - 30,000 RPM  -> 1700 RPM
31
Q

Explain Exhaust system

A

Direct exhaust gases with minimal flow restrictions

32
Q

Accessory Gearbox

A

Mounted to rear of engine

Low/high press fuel pump
FCU fuel control
Fuel/Air heat exchanger
Oil pumps
Generator
Starter
33
Q

Oil Tank

A

Pumps oil

34
Q

Bleed Air Valve

A

Prevents compressor stall

Prevents Reverse flow @ low power

35
Q

Where does the secondary air come from?

A

Air within compressor section

36
Q

Igniters

A

Provides spark to igniters
4-9 o’ clock position

Comes on automatically ITT less than < 500C
Ng > 10%

37
Q

True or false

Ignitors
Should be turned on for Heavy Precipitation and strong turbulence

A

True

38
Q

Where is ITT probe located?

A

Between Power Turbine and compression Turbine

39
Q

Describe oil system

A

Pressure oil system

Oil drawn from tank

                            - to filter
                                        - pressure regulating valve

Delivered through core passages
Lubricates all major bearings, accessories, RGB

Scavage oil system

40
Q

What oil is used?

A

BP 2380 Turbo

41
Q

Oil / Fuel heater

A

Warm oil passes through exchanger to heat up fuel

amount of oil depends on temp of fuel passing

42
Q

Describe chip detector

A

Detector attracts ferrous material with magnets

2 detectors

   - reduction gear box
   - accessory gear box
43
Q

Torque system

A

Works off of oil pressure which is equivalent to Ng

44
Q

Torque limiter

A

Spring thing that vibrates around and measures oil pressure

Limits engine torque below 44.3 psi

Bleeds off Py air to reduce fuel flow from FCU

45
Q

Fire detection system

A

Stainless steel tube with Helium
Internal core with Hydrogen

Tube heats up
Pressure increases
Actuated pressure switch

46
Q

True

ACS must be shutoff when fire is detected

A

True

Airflow to cabin - stops toxin gases from entering cowling

47
Q

PCL

A

Power Control Lever

Controls Ng compressor power speed

Both forward and reverse

48
Q

MOR lever

A

Manual Override Lever
Emergency system

Used for uncommanded “NG rollback or engines”