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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
What is the of the collector tank?
16.8kg
26
What is the amount of unusable fuel in each wing?
Left - 6.3kg | Right - 1.4kg (10.0kg during Emergency Transfer)
27
Name the 2 Fuel related WARNING captions?
F PRESS | F LOW LEVEL
28
F LOW LEVEL warning caption indicates?
Collector tank half full
29
F PRESS warning caption indicates?
Low fuel pressure, <12psi
30
Name the 3 CAUTION captions?
STBY PUMP ON F FILTER OFF F TRANS FAIL
31
F FILTER OFF caution caption indicates?
Fuel filter is blocked
32
F TRANS FAIL caution caption indicates?
Transfer pressure <2.5psi OR Left Wing fuel level high
33
Name the advisory caption associated with the fuel system?
F TRANS ON
34
F TRANS ON advisory caption indicates?
Fuel transferring from RH to LH tank
35
What is the Prefect engine's... - Manufacturer - Engine type - Rated HP - Model
Manufacturer - Rolls-Royce Engine type - Turbo-Propeller Rated HP - 450 SHP Model - 250-B17F
36
What is the Max Continuous Speed of the propeller (N2)?
2132 rpm
37
What engine parameters are shown on the engine page of the EFIS?
``` 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
What are the N1 limitations? Max continuous Max transient
Max continuous - 105% N1 | Max transient - 106% N1
39
What are the N2 limitations? Max continuous Max transient Max static ground ops with >10kts xwind comp
Max continuous - 2132 N2 Max transient - 2233 N2 (max 15 sec >2132 N2) Max static ground ops with >10kts xwind comp - 1850 N2
40
What are the TRQ limitations? Max transient Max T/O power Max continuous
Max transient (10 sec)- 115% Max T/O power (5 min at T/O, cumulative per sortie) - 111% Max continuous - 92%
41
What are the TOT limitations? Max engine start Max transient Max T/O power Max continuous
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
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% ```
``` 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
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 ```
``` 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
What is the Max, Min and recommended oil capacity?
Max - 11 L Min - 5 L Recommended - 7-9 L
45
Hot air to the cockpit is controlled with?
BLEED air
46
What are the 3 powerplant WARNING captions?
OIL LO PRESS INTAKE HEAT BLEED TEMP
47
What does OIL LO PRESS warning caption indicate?
Oil pressure <35psi
48
What does INTAKE HEAT warning caption indicate?
Intake heat malfunction
49
What does BLEED TEMP warning caption indicate?
Airflow from ECS is too hot
50
What are the 2 powerplant CAUTION captions?
OIL CHIP | BETA
51
What does OIL CHIP caution caption indicate?
Metal particle detected in oil
52
What does BETA caution caption indicate?
Propeller system in Beta range
53
Where is the HYD pack located?
Behind baggage compartment bulkhead on LHS
54
What type of motor drives the HYD pump?
Electric
55
The HYD pump relief valve operates at what maximum pressure of the pump?
2000+50 psi
56
Describe the electric parameters of the HYD motor that drives the pump and the pressure the pump supplies the system?
800W 24V DC 2000psi operating pressure
57
What is the purpose of the HYD manifold?
Regulate flow to the components of the HYD system.
58
The HYD pack operates what system?
Landing gear
59
What is the total deflection of the nose gear when using the pedals?
+/- 5 deg
60
When using the inner brake for turning the nose gear can deflect up to?
+/- 52 deg
61
When the landing gear is retracted, the rudder pedals are ________ __________ from the nose wheel.
MECHANICALLY DISCONNECTED
62
List the 4 main components of the brake system
- Fluid reservoir - Master Cylinders - Brake callipers - Discs
63
The landing gear selector is powered by what bus?
Battery bus
64
Landing gear locked down will show what?
3 GREENS
65
Landing gear locked up will show what?
No lights
66
Landing gear NOT locked or in transit will show?
Red lights
67
Where is the 'press-to-transmit' located?
Back side of the control stick
68
How many and where are the location(s) of the VHF antenna/antennae?
2 antennae VHF COM 1 - under fuselage (obtuse V shape) VHF COM 2 - tail fin
69
Where are the VOR aerials?
Either side/perpendicular to the tail fin.
70
How many and where are the location(s) of the UHF antenna/antennae?
1 antenna UHF COM 3 - Under fuselage (forward of the obtuse V VHF antenna)

Ground School - C Middleton (12 decks)

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