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Ground School - C Middleton > Prefect Systems/Limitations Revision (correct V2 ANA5) > Flashcards

Prefect Systems/Limitations Revision (correct V2 ANA5) Flashcards

1
Q

What are the 4 main components of the Electrical System?

A
  • External Power Connector
  • Busbars
  • Battery
  • Starter/Generator
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2
Q

Where is the External Power Connector located; how many and what type of voltage does it accept; and how many pins does it have?

A

Just behind wing on right side

28 volt DC

3 pins

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3
Q

How many and name the busbars?

A

5 Busbars

  • Hot Battery
  • Battery
  • Main Bus
  • Avionics Bus 1
  • Avionics Bus 2
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4
Q

Where is the battery; how many volts and what is it’s capacity?

A

Right rear of engine compartment

24 volts

28 Ah

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5
Q

What is the starter/generator’s power rating and amp output?

A

6kW at 28V DC corresponding to 200A continuous load

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6
Q

The MFDs show what electrical parameters?

A

Volts of

  • Main bus
  • Battery bus

Amps of

  • Battery
  • Generator
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7
Q

The battery is always connected to what busbar?

A

Hot Batt Bus

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8
Q

Name the busbar that provides for each of the following:

  • VITAL equipment
  • ESSENTIAL equipment
  • NON-ESSENTIAL equipment
A

VITAL - Hot Batt Bus
ESSENTIAL - Batt Bus
NON-ESSENTIAL - Main Bus

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9
Q

What are the 4 CAS messages associated with the electrical system?

A

VOLT - Warning
GEN OFF - Caution
BATT OFF - Caution
BUS TIE OFF - Caution

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10
Q

When will the VOLT warning caption illuminate?

A

<23V or >29V

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11
Q

Where are the lighting controls located?

A

Under the right MFD of the left seat pilot

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12
Q

What is the maximum imbalance allowed across wing tanks?

A

45.3kg

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13
Q

What is the MAX capacity fuel figure?

A

282.7kg

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14
Q

What is the MAX useable fuel figure?

A

275.0kg

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15
Q

How long does the fuel transfer pump run and how much fuel does it transfer?

A

2 mins

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16
Q

What is the fuel pressure range?

A

12-25psi

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17
Q

When EMERGENCY transfer is selected for fuel. What tank does is begin taking fuel from?

A

Right

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18
Q

How do you initiate fuel transfer?

A

Fuel Transfer Pump to ‘TIMER’

Fuel Transfer Pump to ‘INIT’

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19
Q

Where is the collector tank located?

A

Left wing

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20
Q

What is the MAX fuel in each wing for aerobatics?

A

115.0kg

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21
Q

TRUE or FALSE. The right fuel tank has a flop tube helping to draw fuel during aeros?

A

FALSE!!!

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22
Q

How many jet pumps feed the collector tank?

A

2

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23
Q

What is the name for the fuel being used to generate low pressure allowing the jet pumps to funciton?

A

Motive Fuel

Recirculated fuel from the engine

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24
Q

How many flapper valves are on the collector tank and what is their purpose?

A

2 flappers valves

Allow gravity fed fuel into the collector tank. One-way valve

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25
Q

What is the of the collector tank?

A

16.8kg

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26
Q

What is the amount of unusable fuel in each wing?

A

Left - 6.3kg

Right - 1.4kg (10.0kg during Emergency Transfer)

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27
Q

Name the 2 Fuel related WARNING captions?

A

F PRESS

F LOW LEVEL

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28
Q

F LOW LEVEL warning caption indicates?

A

Collector tank half full

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29
Q

F PRESS warning caption indicates?

A

Low fuel pressure, <12psi

30
Q

Name the 3 CAUTION captions?

A

STBY PUMP ON
F FILTER OFF
F TRANS FAIL

31
Q

F FILTER OFF caution caption indicates?

A

Fuel filter is blocked

32
Q

F TRANS FAIL caution caption indicates?

A

Transfer pressure <2.5psi

OR

Left Wing fuel level high

33
Q

Name the advisory caption associated with the fuel system?

A

F TRANS ON

34
Q

F TRANS ON advisory caption indicates?

A

Fuel transferring from RH to LH tank

35
Q

What is the Prefect engine’s…

  • Manufacturer
  • Engine type
  • Rated HP
  • Model
A

Manufacturer - Rolls-Royce
Engine type - Turbo-Propeller
Rated HP - 450 SHP
Model - 250-B17F

36
Q

What is the Max Continuous Speed of the propeller (N2)?

37
Q

What engine parameters are shown on the engine page of the EFIS?

A 
N1 - gas generator in % RPM
N2 - power turbine in RPM
Turbine Outlet Temp (TOT) in C
Torque (TRQ) in %
Oil press in psi
Oil press in C
38
Q

What are the N1 limitations?

Max continuous
Max transient

A

Max continuous - 105% N1

Max transient - 106% N1

39
Q

What are the N2 limitations?

Max continuous
Max transient
Max static ground ops with >10kts xwind comp

A

Max continuous - 2132 N2
Max transient - 2233 N2 (max 15 sec >2132 N2)
Max static ground ops with >10kts xwind comp - 1850 N2

40
Q

What are the TRQ limitations?

Max transient
Max T/O power
Max continuous

A

Max transient (10 sec)- 115%
Max T/O power (5 min at T/O, cumulative per sortie) - 111%
Max continuous - 92%

41
Q

What are the TOT limitations?

Max engine start
Max transient
Max T/O power
Max continuous

A

Max engine start (10 sec over 810C) - 927C
Max transient (6 sec over 810C) - 899C
Max T/O power (5 min at T/O, cumulative per sortie) - 810C
Max continuous - 752C

42
Q

What are the oil pressure limitations?

Max transient (cold weather/ engine start, Beta range)
Max (Beta range)
Min at N1 >= 94%
Min at N1 85-94%
Min at N1 <85%
A 
Max transient (cold weather/ engine start, Beta range) - 150 psi
Max (Beta range) - 130 psi
Min at N1 >= 94% - 120-105 psi
Min at N1 85-94% - 90-75 psi
Min at N1 <85% - 50-35 psi
43
Q

What are the oil temperature limitations?

Max limit at TRQ <40%
Max transient at TRG >=40%
Max continuous at TRQ >= 40%
Min temp
Min before starting
A 
Max limit at TRQ <40% - 107C
Max transient at TRG >=40% - 107C
Max continuous at TRQ >= 40% - 82C
Min temp - (0C)
Min before starting - (-40C)
44
Q

What is the Max, Min and recommended oil capacity?

A

Max - 11 L
Min - 5 L
Recommended - 7-9 L

45
Q

Hot air to the cockpit is controlled with?

46
Q

What are the 3 powerplant WARNING captions?

A

OIL LO PRESS
INTAKE HEAT
BLEED TEMP

47
Q

What does OIL LO PRESS warning caption indicate?

A

Oil pressure <35psi

48
Q

What does INTAKE HEAT warning caption indicate?

A

Intake heat malfunction

49
Q

What does BLEED TEMP warning caption indicate?

A

Airflow from ECS is too hot

50
Q

What are the 2 powerplant CAUTION captions?

A

OIL CHIP

BETA

51
Q

What does OIL CHIP caution caption indicate?

A

Metal particle detected in oil

52
Q

What does BETA caution caption indicate?

A

Propeller system in Beta range

53
Q

Where is the HYD pack located?

A

Behind baggage compartment bulkhead on LHS

54
Q

What type of motor drives the HYD pump?

55
Q

The HYD pump relief valve operates at what maximum pressure of the pump?

A

2000+50 psi

56
Q

Describe the electric parameters of the HYD motor that drives the pump and the pressure the pump supplies the system?

A

800W 24V DC

2000psi operating pressure

57
Q

What is the purpose of the HYD manifold?

A

Regulate flow to the components of the HYD system.

58
Q

The HYD pack operates what system?

A

Landing gear

59
Q

What is the total deflection of the nose gear when using the pedals?

60
Q

When using the inner brake for turning the nose gear can deflect up to?

A

+/- 52 deg

61
Q

When the landing gear is retracted, the rudder pedals are ________ __________ from the nose wheel.

A

MECHANICALLY DISCONNECTED

62
Q

List the 4 main components of the brake system

A
  • Fluid reservoir
  • Master Cylinders
  • Brake callipers
  • Discs
63
Q

The landing gear selector is powered by what bus?

A

Battery bus

64
Q

Landing gear locked down will show what?

65
Q

Landing gear locked up will show what?

66
Q

Landing gear NOT locked or in transit will show?

A

Red lights

67
Q

Where is the ‘press-to-transmit’ located?

A

Back side of the control stick

68
Q

How many and where are the location(s) of the VHF antenna/antennae?

A

2 antennae

VHF COM 1 - under fuselage (obtuse V shape)
VHF COM 2 - tail fin

69
Q

Where are the VOR aerials?

A

Either side/perpendicular to the tail fin.

70
Q

How many and where are the location(s) of the UHF antenna/antennae?

A

1 antenna

UHF COM 3 - Under fuselage (forward of the obtuse V VHF antenna)

Ground School - C Middleton (12 decks)

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