Test 1 Questions Flashcards

1
Q

The G1000 Piper Seminole’s battery is ___ volts and ___ amps

A

24 Volts

13.6 Amps

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2
Q

If one, two of all three landing gear lights do not illuminate after you have selected gear down there are 3 conditions that can exist. What are they?

A
  1. Indicator bulb is burned out/PFD malfunction
  2. Failure in retraction/extension system
  3. Problem with switch system (wire corroded, not aligned, etc)
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3
Q

A ____ uses exhaust gases to compress induction air and boost engine power output at higher altitudes

A

Turbocharger

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4
Q

The overvoltage relay in the G1000 Seminole will take the alternator offline if the alternator exceeds ___ volts

A

32 Volts

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5
Q

The 4 flap positions in the Piper Seminole are __, __, __ and __ degrees

A

0
10
25
40

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6
Q

Which Bus in continuously powered on the Seminole regardless of battery master switch position?

A

Battery Bus

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7
Q

What is a sign of a tail plane stall caused by ice accumulation?

A

Severe pitch down after flap extension

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8
Q

Under what condition will the gear warning horn “mute” switch work after the horn is activated?

A

If the throttles are reduced to 14”

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9
Q

What force is the PRIMARY force that moves the propeller to the LOW pitch angle?

A

Oil pressure

- Aerodynamic Twisting assists

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10
Q

What force is the PRIMARY force that moves the propeller to the HIGH pitch angle?

A

Nitrogen charge

- Counterweights and Spring Force assist

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11
Q

Which force assists the propeller towards a LOWER pitch angle?

A

Aerodynamic Twisting

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12
Q

What type of Aileron’s is the Piper Seminole equipped with?

A

Differential Frise

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13
Q

What is the purpose of the unfeathering accumulator on the Piper Seminole?

A

Stores oil under pressure to unfeather prop in flight

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14
Q

What is TRUE about the Seminole’s heater?

A

On the ground the fan should be operated for 15 seconds with the air intake lever open to cool the heater!

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15
Q

In the Piper Seminole’s gear system, what shuts the pump OFF during gear retraction?

A

The Pressure Switch reaching about 1800 psi

on = aprox. 1500 psi

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16
Q

A squat switch in the stall warning system does not allow the unit to be activated on the ground, which landing gear is the squat switch located on?

A

Right main!

17
Q

The squat switch on the Seminole’s LEFT main gear:

A
Left = Disables landing gear pump to prevent gear retraction on the ground!
Right = Activates Mx. Hobbs and Stall Warning Horn
18
Q

When using pneumatic boots to remove ice accumulation on an a/c’s wings:

A

Use the method described by the a/c’s applicable operating manual!

19
Q

The storm window in the Seminole should not be opened above what speed?

A

129

20
Q

If 1 alternator has failed and the other alternator is drawing over 80 amps how can you quickly reduce the airplane’s total electrical load w/o significant impact to the flight?

A

Pull the non-essential bus circuit breaker

21
Q

In the Seminole’s gear system, what shuts the pump OFF during gear extension?

A

All 3 down limit switches closing

22
Q

With the LEFT fuel selector on X-Feed and the RIGHT fuel selector ON, how is fuel flowing from the tanks to the engines?

A
  • LEFT engine is getting fuel from the RIGHT tank

- RIGHT engine is getting fuel from the RIGHT tank

23
Q

During engine shutdown the Seminole’s propeller is prevented from going in the feather position by:

A

Anti-feathering pins which lock in place below 950 rpm

24
Q

How many minutes will the Emergency Battery in the G1000 Seminole provide power to the standby instruments and PFD to run the attitude indicator?

A

30 mins

25
Q

What is the purpose of the Thermal Relief Valve on the Seminole’s hydraulic gear system?

A

Provides pressure relief in the event heat expands the hydraulic fluid

26
Q

If the CHT’s get too high what should you do?

A

Open the Cowl Flaps!

27
Q

Sluggish propeller control and propeller overspeed with poor RPM recovery after rapid throttle application are indicates that:

A

The nitrogen charge is low!

28
Q

The POH recommends that prolonged slip-skids which result in an excess of ____ ft of altitude should be avoided because fuel flow could be interrupted

A

2000’

29
Q

If both ALTR FAIL warning annunciators illuminate during flight in a G1000 Seminole it is an indication that ___ alternator(s) have failed

A

Both

30
Q

The luggage compartment on the Seminole has a max weight capacity of ____

A

200

31
Q

The Seminole has an emergency window exit located on the ___ of the a/c

A

Left side!

32
Q

What is TRUE about the carburetor heat on the Seminole?

A

…all of the above?

33
Q

A T-Tail a/c like the Seminole requires ___ movements at ___ speeds

A

Larger movements / Slower speeds

34
Q

In the events that alternate static is required what configuration should be used?

A

Storm window CLOSED
Cabin vents CLOSED
HT and Defrosters ON

35
Q

The purpose of the impulse coupling with the magneto is to ____

A

Provide rotation for late and hot spark!

36
Q

What are the functions of the Alternator Control Units in the Seminole electrical system?

A
  1. Voltage regulation
  2. Load sharing
  3. Over voltage protection
    (all of the above)
37
Q

Under what conditions will the gear warning horn activate?

A
  1. Squat switch closed (in flight)
  2. Down and lock switches open (gear up)
  3. Throttle below 14”
    (All of the above)