C208 Caravan Multiple Choice Questions

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1/151 Questions

The CSU and Brakes is actuated how?
- Pneumatically
- Hydraulically
- Cable

About This Quiz

The Cessna 208 caravan is an American single engine turboprop, fixed with tricycle landing gear and seats nine passengers with a single pilot although with the FAR part 23 waivers it can seat up to 14 passengers. Take the C208 caravan multiple-choice questions below and learn more about it.

C208 Caravan Multiple Choice Questions - Quiz

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2.

What is the primary purpose of the wing spoilers on the C208? (page 1-8 flight safety)
- Decreases speed of aircraft
- Improves lateral control of aircraft at Low airspeed
- Primarily turns the aircraft
Correct Answer

A. Improves lateral control of aircraft at Low airspeed

Explanation

Improves lateral control of aircraft at Low airspeed(Disrupting lift over specific flap), by greatly reducing lift while making little change in Drag(increase). Causing roll whilst reducing Adverse aileron Yaw.

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4
3.

14.) When will the Generator be disconnected from the Buses?
- In the vent of a high voltage situation only
- In the event of a high voltage or reverse current situation
- In the event of a reverse current situation only
Correct Answer

A. In the event of a high voltage or reverse current situation

Explanation

The generator will be disconnected from the buses in the event of a high voltage or reverse current situation. This means that if the voltage exceeds a certain threshold or if there is a flow of current in the opposite direction, the generator will be disconnected from the buses. This is done to protect the generator and the buses from any potential damage that could occur in such situations.

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3
4.

How many fuel nozzle assemblies does the C208 have?
- 14
- 7
- 2
Correct Answer

A. 14

Explanation

The C208 aircraft has 14 fuel nozzle assemblies.

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2
5.

What function does the static dischargers serve on the C208?
- To To improve radio communication through rain
- To improve radio communication through Dust
- To improve radio communication through snow
- To improve radio communication through ice crystals
- All of the above
Correct Answer

A. All of the above

Explanation

The static dischargers on the C208 serve to improve radio communication through various weather conditions, including rain, dust, snow, and ice crystals. These dischargers help to dissipate static electricity that can interfere with radio signals, ensuring clear and reliable communication in different environmental conditions.

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2
6.

Before the 1st flight of the day and after refuelling. Which points must you strain fuel?
- Fuel tank sump quick drain valves(2 valves)
- Fuel reservoir quick drain valve
- Fuel filter quick drain valves
- All of the above
Correct Answer

A. All of the above

Explanation

page 5-6

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7.

The starter-Generator is rated as how many ampere-hour?
- 28 volt, 200 Ampere-Hour
- 24 volt, 200 Amper-Hour
- 24 volt, 150 Ampere- Hour
Correct Answer

A. 28 volt, 200 Ampere-Hour

Explanation

The correct answer is 28 volt, 200 Ampere-Hour. This means that the starter-generator is rated to provide a voltage of 28 volts and a capacity of 200 ampere-hours. Ampere-hour is a unit of electrical charge, representing the amount of charge that can flow in one hour at a constant current of one ampere. Therefore, the starter-generator is capable of delivering a higher voltage and a larger capacity compared to the other options provided.

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6
8.

If the chip detector light comes on, what does it mean?
- Metal chips have been detected in either the reduction gearbox or accessory gearbox.
- Metal chips have been detected in the reduction gearbox
- Metal chips have been detected in the accessory gearbox
Correct Answer

A. Metal chips have been detected in either the reduction gearbox or accessory gearbox.

Explanation

The chip detector light coming on indicates that metal chips have been detected in either the reduction gearbox or accessory gearbox. This could potentially be a sign of wear or damage to the gears, which may require inspection and maintenance to prevent further issues or failure.

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2
9.

What can happen if the fuel can drain is not drained after Flight(6 shut downs)?
- Can will overflow its contents overboard automoatically
- Fuel can drain lines can burst by the 7th flight
- Nothing will happen
Correct Answer

A. Can will overflow its contents overboard automoatically

Explanation

If the fuel can drain is not drained after 6 shut downs, the can will overflow its contents overboard automatically. This means that the fuel can will become full and exceed its capacity, causing the excess fuel to spill out. This can lead to fuel wastage and potential safety hazards if the spilled fuel comes into contact with ignition sources. Therefore, it is important to drain the fuel can after a certain number of shut downs to prevent overflow.

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1
10.

What is the manuevring speed of a C208 at 5000 LBS ?
- 148 KIAS
- 143 KIAS
- 137 KIAS
- 125 KIAS
- 112 KIAS
Correct Answer

A. 112 KIAS

Explanation

The correct answer is 112 KIAS. This is the manuevring speed of a C208 at 5000 LBS. Manuevring speed is the maximum speed at which full control deflection can be applied without causing structural damage to the aircraft. It is important to maintain this speed during certain maneuvers to ensure the safety and integrity of the aircraft.

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11.

What is the maximum speed that you are allowed to fly with 30 degrees of flap?
- No limit
- 125 KIAS
- 150 KIAS
- 175 KIAS
- 200 KIAS
Correct Answer

A. 125 KIAS

Explanation

When flying with 30 degrees of flap, the maximum speed allowed is 125 KIAS. This is because flaps increase the lift and drag of the aircraft, allowing it to fly at slower speeds. However, exceeding the recommended maximum speed with flaps deployed can cause damage to the aircraft and compromise safety. Therefore, the correct answer is 125 KIAS.

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0
12.

Below +4 degrees celsius with visible moisture, should the Inertial seperator be put into the BYPASS postion? (As per POH)
- Yes
- No
Correct Answer

A. Yes

Explanation

According to the POH (Pilot's Operating Handbook), when the temperature is below +4 degrees Celsius and there is visible moisture, the Inertial Separator should be put into the BYPASS position. This is likely because in such conditions, there is a higher risk of ice formation or other moisture-related issues, and using the Inertial Separator in the BYPASS position helps prevent these issues by allowing the moisture to bypass the engine intake.

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13.

If the gound plug receptacle is plugged in(with power ON) and Battery is ON aswell, will the ground plug receptacle overpower the electrical system and cause a short?
- Yes
- No
Correct Answer

A. No

Explanation

The ground plug receptacle will not overpower the electrical system and cause a short. The ground plug receptacle is designed to provide a path for electrical currents to flow safely into the ground, preventing electrical shocks and protecting the electrical system. It does not have the capability to overpower the system or cause a short circuit.

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6
14.

If the ejector boost pump fails, will the auxiliary boost pump come on automatically, If fuel boost pump is in the "Normal" position?
- No
- Yes
Correct Answer

A. Yes

Explanation

At 4.75 PSI

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4
15.

The Vortex generators on the C208, what are their functions?
- They Provide enhanced lateral stability
- Reduce stall speed
- Increases STOL
- Re-energizes boundary layer
- All of the above
Correct Answer

A. All of the above

Explanation

The vortex generators on the C208 have multiple functions. They provide enhanced lateral stability by controlling the airflow over the wings. They also reduce stall speed by creating vortices that energize the boundary layer, allowing the aircraft to maintain lift at lower speeds. Additionally, they increase STOL (short takeoff and landing) capabilities by improving the aircraft's ability to generate lift at slower speeds. Therefore, the correct answer is "all of the above."

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16.

What is the maximum glide speed of a C208 at 6250 LBS equipped with Cargo pods?
- 104 KIAS
- 100 KIAS
- 95 KIAS
- 87 KIAS
- 79 KIAS
Correct Answer

A. 79 KIAS

Explanation

The maximum glide speed of a C208 at 6250 LBS equipped with cargo pods is 79 KIAS. This means that when the aircraft is in a glide without any engine power, it can maintain a maximum speed of 79 knots indicated airspeed. This speed is specific to the given weight and configuration of the aircraft, and it is important for pilots to be aware of this limitation to ensure safe operation.

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17.

What is Vmo(maximum operating speed on the C208)?
- 200 KIAS
- 175 KIAs
- 150 KIAS
- 125 KIAs
- 250 KIAS
Correct Answer

A. 175 KIAs

Explanation

The maximum operating speed on the C208 is 175 KIAS. This means that the aircraft should not exceed this speed during normal operations to ensure safe and efficient performance. Going beyond this speed limit may result in increased stress on the aircraft structure and systems, potentially leading to damage or failure. Therefore, it is important for pilots to adhere to this speed restriction to maintain the safety and integrity of the aircraft.

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1
18.

When using any Avgas in any way on a C208. Should the auxilliary Boost Pump be On for all flight operations?
- Yes
- No
Correct Answer

A. Yes

Explanation

The auxiliary boost pump should be turned on for all flight operations when using any Avgas in a C208. This is because the auxiliary boost pump helps maintain a consistent fuel flow and pressure to the engine, ensuring proper engine performance and preventing fuel starvation. By keeping the boost pump on, the pilot can ensure a reliable fuel supply throughout the flight, especially during critical phases such as takeoff and landing.

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19.

Is the EPA CAN(fuel drain can) fireproof?
- Yes
- No
Correct Answer

A. Yes

Explanation

The EPA CAN (fuel drain can) is fireproof.

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20.

How many Nav lights does a C208 Have?
- 1
- 2
- 3
Correct Answer

A. 3

Explanation

(flight safety page3-1, POH page 7-67) 2 Nav lights on the wingtips. 1 Nav lght on the tail cone stinger

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5
21.

When is it not recommended to use the strobe light?
- On the ground
- In fog
- In haze
- In precipitation
- All of the above
Correct Answer

A. All of the above

Explanation

The strobe light is not recommended to be used in any of the given conditions: on the ground, in fog, in haze, and in precipitation. This is because these conditions can affect visibility and make it difficult for other pilots or vehicles to see the strobe light, increasing the risk of accidents or confusion. Therefore, it is best to avoid using the strobe light in these situations.

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2
22.

When the “door warning annunciator” comes on, what does that mean?
- Uppr aft passenger door is open
- Upper aft cargo door is open
- Upper aft cargo door or passenger door is open
- Lowe aft passenger door is open
- Lower aft cargo door is open
Correct Answer

A. Upper aft cargo door or passenger door is open

Explanation

The "door warning annunciator" indicates that either the upper aft cargo door or the passenger door is open.

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3
23.

During start if one of the fuel selectors L or R are off. Will an aural warning + fuel selector off anaunciator go off?
- Yes
- No
Correct Answer

A. Yes

Explanation

During start, if one of the fuel selectors L or R is off, an aural warning and fuel selector off annunciator will go off. This is because the fuel selectors need to be on in order for the engine to receive fuel and start properly. The aural warning and annunciator serve as a safety measure to alert the pilot if the fuel selectors are not in the correct position. Therefore, the correct answer is yes.

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1
24.

What can be the consequences if the power lever is retarded below IDLE into Beta during flight?
- Engine might overspeed
- Loss of airplane control
- A and B
Correct Answer

A. A and B

Explanation

Retarding the power lever below idle into Beta during flight can have two consequences. Firstly, the engine might overspeed, meaning it rotates at a higher speed than it is designed for, potentially causing damage or failure. Secondly, there can be a loss of airplane control, as the reduction in power can affect the aircraft's stability and maneuverability, making it difficult for the pilot to maintain control. Therefore, both options A and B are correct.

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1
25.

When should the avionics power switches be off?
- Prior to turning ON the battery switch
- Prior to starting the engine
- Before applying external power source
- All of the above
Correct Answer

A. All of the above

Explanation

The avionics power switches should be turned off prior to turning ON the battery switch, prior to starting the engine, and before applying an external power source. This is important to ensure the safety and proper functioning of the avionics system. By turning off the power switches before these actions, any potential electrical issues or malfunctions can be avoided.

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26.

The fuel shut off valves is AKA.....
- Fuel selectors
- Fuel manifold
- Fuel boost pump
Correct Answer

A. Fuel selectors

Explanation

The fuel shut off valves are commonly referred to as fuel selectors. These valves are responsible for controlling the flow of fuel to the engine. They allow the pilot to select which fuel source to use, such as different fuel tanks in an aircraft. By using the fuel selectors, the pilot can ensure a steady supply of fuel to the engine and manage the fuel consumption effectively.

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3
27.

The fuel tank selectors located on the overhead panel:
- Are BOTH normally on for flight
- Are BOTH Normally off during refueling
- Are turned off during ground OPS
- A and B
Correct Answer

A. A and B

Explanation

The correct answer is A and B. The fuel tank selectors located on the overhead panel are normally on for flight to allow fuel to flow from both tanks. However, during refueling, they are normally turned off to prevent any fuel flow. Additionally, during ground operations, the fuel tank selectors are also turned off as a safety measure to prevent any accidental fuel flow.

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28.

If the power lever is moved aft of the IDLE position without engine running and the props feathered. Can any damage be done?
- Yes
- No
Correct Answer

A. Yes

Explanation

the propeller reversing linkage can be damaged

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29.

How many igniters does a PT6A engine have?
- 1
- 2
- 3
- 4
- 5
Correct Answer

A. 2

Explanation

A PT6A engine has two igniters. Igniters are used to ignite the fuel-air mixture in the combustion chamber of the engine. Having two igniters provides redundancy and ensures that the engine can still operate even if one igniter fails.

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30.

Can the fuel selector warning horns go off simultaneously?
- No
- Yes
Correct Answer

A. Yes

Explanation

The fuel selector warning horns can go off simultaneously because they are designed to alert the pilot if both fuel tanks are not selected properly. This ensures that the pilot is aware of any potential issues with the fuel selection and can take appropriate action to prevent fuel starvation during the flight.

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31.

When the lef/right fuel low annunciator comes on. How much fuel is left in the Rh/LH tank?
- 20 Gallons
- 25 Gallons
- 30 Gallons
- 35 Gallons
- Half full or less
Correct Answer

A. 25 Gallons

Explanation

The correct answer is 25 gallons. When the left/right fuel low annunciator comes on, it indicates that there is only 25 gallons of fuel left in the respective tank.

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1
32.

Where is the ejector pump + electrical auxillary boost pump situated?
- Just before the fuel manifold
- Just before the firewall shut off valve
- Inside the fuel reservoir tank
Correct Answer

A. Inside the fuel reservoir tank

Explanation

The correct answer is inside the fuel reservoir tank. The ejector pump and electrical auxiliary boost pump are located within the fuel reservoir tank. This placement allows for efficient fuel transfer and ensures that the pumps are submerged in fuel at all times, preventing cavitation and maintaining proper fuel flow.

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2
33.

When is the stall warning activated?
- At the stall
- 2kts before the stall
- 5-10 kts before the stall
- 4-8 kts before the stall
Correct Answer

A. 5-10 kts before the stall

Explanation

The stall warning is activated 5-10 knots before the stall. This is because the stall warning system is designed to provide pilots with an early indication that the aircraft is approaching the critical angle of attack, which could result in a stall. By activating the warning 5-10 knots before the stall, pilots have enough time to take corrective action and prevent the stall from occurring.

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34.

Ng is a % of how many RPM?
- 32500 RPM
- 35000 RPM
- 37500 RPM
- 40000 RPM
- 42500 RPM
Correct Answer

A. 37500 RPM

Explanation

Ng is a percentage of the maximum RPM. In this case, the correct answer is 37500 RPM, which means that Ng is 37.5% of the maximum RPM.

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35.

On the newer models of C208. To unlock the Rudder gust lock if you forgot to unlock it during the preflight(rear of the aircrft near to the Rudder). You will....
- Press yoke forward
- Pull back on yoke to the fully aft position
Correct Answer

A. Pull back on yoke to the fully aft position

Explanation

Refer to supplements 2 C

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36.

Is it recommended to charge The Battery with external power(By switiching on the Battery switch and switching the external power switch to “BUS”)?
- Yes
- No
Correct Answer

A. No

Explanation

It is not recommended to charge the battery with external power by switching on the battery switch and switching the external power switch to "BUS". This is because it can lead to overcharging and damage the battery. It is advisable to use the appropriate charging method recommended by the manufacturer to ensure the battery's longevity and safety.

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3
37.

What is the oil capacity for a C208?
- 9.5 Qts
- 10.5 QTS
- 12 Qts
- 14 Qts
- 16 Qss
Correct Answer

A. 14 Qts

Explanation

The correct answer is 14 Qts. This refers to the oil capacity for a C208 aircraft. The oil capacity is the maximum amount of oil that the aircraft's engine can hold. In this case, it is 14 Qts, which stands for quarts. This information is important for maintenance and ensuring that the engine has the appropriate amount of oil for optimal performance and lubrication.

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38.

The ITT sensing system is situated where?
- Just before the Turbine section
- Just before the Compressor section
- Behind the Turbine section
- Near the exhaust
- Between the Power turbine and Compressor turbine
Correct Answer

A. Between the Power turbine and Compressor turbine

Explanation

The correct answer is "Between the Power turbine and Compressor turbine". This is because the ITT (Interstage Turbine Temperature) sensing system is typically located in the section between the power turbine and compressor turbine in a gas turbine engine. This allows it to measure the temperature of the gases exiting the power turbine and entering the compressor turbine, which is important for monitoring and controlling the engine's performance and efficiency.

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39.

Vortex Generators on top of the Horizontal stabilizer serves what purpose?
- The vortex generators enhance the nose down elevator trim authority.
- Increases effectiveness of controls.
- Increases STOL/MTOW
- Provide enhaced lateral stability
- All of the above
Correct Answer

A. All of the above

Explanation

The vortex generators on top of the horizontal stabilizer serve multiple purposes. Firstly, they enhance the nose down elevator trim authority, allowing for better control of the aircraft's pitch. Secondly, they increase the effectiveness of controls, improving maneuverability. Additionally, they contribute to Short Takeoff and Landing (STOL) capabilities and Maximum Takeoff Weight (MTOW) by increasing lift and reducing stall speed. Lastly, they provide enhanced lateral stability, ensuring a more stable flight. Therefore, the correct answer is "All of the above."

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13
40.

The GCU controls the starter-Generator and serves what functions?
- Overspeed protection
- Speed sensor
- Starter cut out
- Voltage regulation and protection from high voltage + reverse current
- All of the above
Correct Answer

A. All of the above

Explanation

The GCU (Generator Control Unit) controls the starter-generator and serves multiple functions. It provides overspeed protection to prevent the generator from operating at excessive speeds. It also functions as a speed sensor to monitor the rotational speed of the generator. Additionally, the GCU includes a starter cut out feature, which disables the starter once the generator is running. Lastly, it is responsible for voltage regulation and protection, ensuring that the generator operates within safe voltage limits and is protected from high voltage and reverse current. Therefore, the correct answer is "all of the above."

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4
41.

When the “fuel Press low” light goes on. What pressure is available in the fuel manifold?
- 4.75 PSI
- 4.25 PSI
- 2.75 PSI
- 5 PSI
Correct Answer

A. 4.75 PSI

Explanation

The correct answer is 4.75 PSI. When the "fuel Press low" light goes on, it indicates that the pressure in the fuel manifold has dropped below a certain threshold. In this case, the available pressure in the fuel manifold is 4.75 PSI.

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2
42.

When the battery Voltage is below 20 volts (Before start). Will the Battery contactor be connected to the distribution bus, internal start contactor, Generator contactor?
- Yes
- No
Correct Answer

A. No

Explanation

In most aircraft electrical systems, the battery contactor is designed to prevent the connection of a low-voltage battery to the electrical bus. This is to protect the battery from excessive discharge and potential damage. When the battery voltage is below a certain threshold (typically around 20 volts), the battery contactor will remain open, preventing the battery from connecting to the distribution bus, internal start contactor, or generator contactor.

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6
43.

What is the purpose of the Ground power monitor? Page 2-6 Flight safety
- Senses the voltage level applied to the external power receptacle
- Senses the airplane bus voltage and illuminates the “voltage low” annunciator (below 24.5 volts system voltage)
- A and B
Correct Answer

A. A and B

Explanation

The purpose of the Ground power monitor is to sense the voltage level applied to the external power receptacle and also to sense the airplane bus voltage and illuminate the "voltage low" annunciator if the system voltage is below 24.5 volts.

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1
44.

With the Starter switch in the “motor” / “start” position during flight/start sequence. Will the Generator come online?
- Yes
- No
Correct Answer

A. No

Explanation

Caused a accident in the USA...Read up

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3
45.

How do you check the standby electrical system?(As per the POH)
- “Trip” the generator
- Selector knob “ALT” observe a 1 volt drop between “GEN” and “ALT”
- A and B
Correct Answer

A. A and B

Explanation

To check the standby electrical system as per the POH, you need to perform two steps. First, you need to "trip" the generator. Second, you need to select the knob to "ALT" and observe a 1 volt drop between "GEN" and "ALT". Both steps A and B are necessary to properly check the standby electrical system.

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1
46.

What advantages does a Nicad Battery have over a Lead Acid Battery?
- Good starting capability
- Cheaper
- Higher service life
- Short recharge time
- All of the above
Correct Answer

A. All of the above

Explanation

A Nicad Battery has several advantages over a Lead Acid Battery. Firstly, it has good starting capability, meaning it can provide a strong initial burst of power. Secondly, it is cheaper than a Lead Acid Battery, making it more cost-effective. Thirdly, it has a higher service life, meaning it lasts longer before needing to be replaced. Lastly, it has a short recharge time, allowing it to be quickly replenished. Therefore, all of the above advantages make the Nicad Battery a preferable choice over the Lead Acid Battery.

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2
47.

With Regard to the external power switch. When the “Bus” side is selected External power is applied to the……..? Page 2-15 Flight safety
- Starter motor only
- Main bus only
- Starter and main bus
- Starter, main bus and Battery
Correct Answer

A. Main bus only

Explanation

When the "Bus" side is selected, external power is applied only to the main bus. This means that the external power is not connected to the starter motor or the battery.

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2
48.

The cabin lights are controlled by which switches?
- “Cabin” toggle switch on the lighting control panel
- Rocker switch just forward of the air stair door
- All of the above
Correct Answer

A. All of the above

Explanation

Note: the cabin lighting sytem incorporates a solid-state timer which allows courtesy lights to remain illuminated for a period of 30 minutes).

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2
49.

How many fuel selector warning horns does the Caravan have?
- 1
- 2
- 3
- 4
- 5
Correct Answer

A. 2

Explanation

The Caravan has two fuel selector warning horns.

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1

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Jan 15, 2025

Quiz Edited by
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Nov 30, 2009

Quiz Created by
Leon43

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C208 Caravan Multiple Choice Questions

The CSU and Brakes is actuated how?

Quiz Preview

What is the primary purpose of the wing spoilers on the C208? (page 1-8 flight safety)

14.) When will the Generator be disconnected from the Buses?

How many fuel nozzle assemblies does the C208 have?

What function does the static dischargers serve on the C208?

Before the 1st flight of the day and after refuelling. Which points must you strain fuel?

The starter-Generator is rated as how many ampere-hour?

If the chip detector light comes on, what does it mean?

What can happen if the fuel can drain is not drained after Flight(6 shut downs)?

What is the manuevring speed of a C208 at 5000 LBS ?

What is the maximum speed that you are allowed to fly with 30 degrees of flap?

Below +4 degrees celsius with visible moisture, should the Inertial seperator be put into the BYPASS postion? (As per POH)

If the gound plug receptacle is plugged in(with power ON) and Battery is ON aswell, will the ground plug receptacle overpower the electrical system and cause a short?

If the ejector boost pump fails, will the auxiliary boost pump come on automatically, If fuel boost pump is in the "Normal" position?

The Vortex generators on the C208, what are their functions?

What is the maximum glide speed of a C208 at 6250 LBS equipped with Cargo pods?

What is Vmo(maximum operating speed on the C208)?

When using any Avgas in any way on a C208. Should the auxilliary Boost Pump be On for all flight operations?

Is the EPA CAN(fuel drain can) fireproof?

How many Nav lights does a C208 Have?

When is it not recommended to use the strobe light?

When the “door warning annunciator” comes on, what does that mean?

During start if one of the fuel selectors L or R are off. Will an aural warning + fuel selector off anaunciator go off?

What can be the consequences if the power lever is retarded below IDLE into Beta during flight?

When should the avionics power switches be off?

The fuel shut off valves is AKA.....

The fuel tank selectors located on the overhead panel:

If the power lever is moved aft of the IDLE position without engine running and the props feathered. Can any damage be done?

How many igniters does a PT6A engine have?

Can the fuel selector warning horns go off simultaneously?

When the lef/right fuel low annunciator comes on. How much fuel is left in the Rh/LH tank?

Where is the ejector pump + electrical auxillary boost pump situated?

When is the stall warning activated?

Ng is a % of how many RPM?

On the newer models of C208. To unlock the Rudder gust lock if you forgot to unlock it during the preflight(rear of the aircrft near to the Rudder). You will....

Is it recommended to charge The Battery with external power(By switiching on the Battery switch and switching the external power switch to “BUS”)?

What is the oil capacity for a C208?

The ITT sensing system is situated where?

Vortex Generators on top of the Horizontal stabilizer serves what purpose?

The GCU controls the starter-Generator and serves what functions?

When the “fuel Press low” light goes on. What pressure is available in the fuel manifold?

When the battery Voltage is below 20 volts (Before start). Will the Battery contactor be connected to the distribution bus, internal start contactor, Generator contactor?

What is the purpose of the Ground power monitor? Page 2-6 Flight safety

With the Starter switch in the “motor” / “start” position during flight/start sequence. Will the Generator come online?

How do you check the standby electrical system?(As per the POH)

What advantages does a Nicad Battery have over a Lead Acid Battery?

With Regard to the external power switch. When the “Bus” side is selected External power is applied to the……..? Page 2-15 Flight safety

The cabin lights are controlled by which switches?

How many fuel selector warning horns does the Caravan have?