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ATP > Sample Oral Questions > Flashcards

Sample Oral Questions Flashcards

1
Q
  1. Recite the v-speeds
A

…

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2
Q
  1. What is the maximum demonstrated crosswind component?
A

17 knots

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3
Q
  1. Describe the PA-28-181 engine.
    A. How many cylinders?
    B. Who is the manufacturer?
    C. What is the horsepower rating?
    D. Does it have fuel injectors or a carburetor?
    E. Is the engine turbo-charged or normally aspirated?
    F. How are the cylinders arranged?
    G. How is ignition provided?
    H. What are the minimum and maximum oil capacities?
A 
A. 4 cylinders
B. Lycoming
C. 180 horsepower @ 2,700 rpm (red line)
D. Carbureted
E. Normally Aspirated
F. Horizontally Opposed
G. 2 engine driven magnetos independent of electrical system and each other
H. min 6, max 8 quarts
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4
Q
  1. Describe the propeller system.
    A. Who makes the propellers?
    B. How is propeller RPM adjusted?
    C. Define fixed pitch.
A

A. Sensenich (two-bladed, fixed pitch, metal propeller - 76 in diameter)
B. Change the power setting
C. The angle of attack of a fixed pitch propeller is set at installation and cannot be changed during aircraft operation. The blade angle is a compromise between the optimum pitch for takeoff, climb and cruise.

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5
Q
  1. Describe the electrical system.
A
  • 28 VDC electrical system and a 24 VDC lead acid batt
  • Elect pwr supplied by a 70-amp, eng driven alternator
  • Voltage regulator maintains 28-volt output
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6
Q
  1. What are the indications of a failed alternator?
A

An annunciator light “ALTERNATOR INOPERATIVE” and a zero indication on the ammeter

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7
Q
  1. Will the engine continue to run with the alternator and battery master switches turned off?
A

Yes, the magnetos are engine driven and not part of the electrical system and are independent of each other

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8
Q
  1. Describe the stall warning system.
A

An electric stall detector located on the leading edge of the left wing. The stall warning horn emits a continuous sound and is activated between 5 and 10 knots above stall speed.

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9
Q
  1. Describe the fuel system.
A
  • Uses 100 (LL) low lead avgas (blue)
  • (2) 25 gal fuel tanks. 1 gal is unusable in each tank
  • 1 engine-driven and 1 electrically-driven fuel pump
  • Electric engine priming system - to facilitate starting
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10
Q
  1. Explain how to change fuel tanks in cruise flight.
A
  1. Electric fuel pump on
  2. Fuel selector from “L” to “R” or from “R” to “L”
  3. Check fuel pressure
  4. Electric fuel pump off
  5. Check fuel pressure
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11
Q
  1. Describe the landing gear system.
    A. How is steering accomplished on the ground?
    B. What is the range of travel on the nose wheel?
A
  • Fixed, tricycle type gear, w/ oleo (air/oil) struts provide shock absorption for all three wheels
  • Nose wheel contains a shimmy dampener (damps nose wheel vibrations during grnd ops and centers the nose wheel in the air)
  • The nose wheel is linked to the rudder pedals by a steering mechanism which turns the nose wheel up to 20° each side of center
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12
Q
  1. What type of braking system is used by the Archer? Where is the brake fluid reservoir?
A
  • Hydraulically actuated disc brakes on the MLG wheels
  • Brake fluid reservoir on top left front face of the firewall - Toe/parking brake have separate brake cylinders, but share the hydraulic reservoir
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13
Q
  1. What type of flaps does the Archer have?

A. What are the flap settings on the Archer?

A
  • Manual flap system

- Flap settings are 0°, 10°, 25°, and 40°, and are spring-loaded to return to the 0 ° position

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14
Q
  1. What are the maximum taxi, takeoff, and landing weights?
A

Max taxi = 2558lbs

Max TO/L = 2550lbs

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15
Q
  1. What is the maximum baggage capacity?
A

200lbs

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16
Q
  1. Define Vx and Vy.
A

Vx is the best angle of climb (64 KIAS)

Vy is the best rate of climb (76 KIAS)

17
Q
  1. What aircraft equipment checks are required under FAR Part 91?
A
  • VOR every 30 days
  • Transponders every 24 calendar months
  • Pitot Static every 24 calendar months
  • ELT every 12 months or after half of the battery life or after 1 cumulative use
  • Current 100hr and annual insp
18
Q
  1. What documents are required to be on the aircraft?
A

A. Airworthiness Certificate
R. Registration Certificate
O. Operating Limitations (POH), placards, markings, etc.
W. Weight & Balance

19
Q
  1. Explain lost communications procedures.
A

VFR - squawk 7600, remain VFR and land as soon as practicable.

IFR - squawk 7600 and fly:
- Route (First that applies), Assigned, Vectored, Expected, Filed…
- Altitude (Whichever is highest until descent is required for landing), Minimum IFR Altitude, Expected,
Assigned

20
Q
  1. Explain the pitot-static system.
    A. Does the PA-28 have an alternate static source? If so, how is it activated and what actions are necessary to acquire the most accurate reading?
    B. What instruments are pitot-static?
    C. Where is the pitot-static port located?
A

A. Yes, Alternate source located inside cabin under left side of the instrument panel
- Activated in static port blockage
- Storm window and cabin vents closed with cabin heater and defroster on for most accurate reading (reduces the pressure differential between the cockpit and atmosphere, reducing pitot-static error)
B. Pitot-static instruments: airspeed indicator, altimeter, and vertical speed indicator.
C. Primary pitot/static press port from the pitot head (bottom/left wing)

21
Q
  1. What is the fuel capacity? How many gallons are unusable?
A
  • 50 gallons (25 per tank)

- 2 gallons unusable (1 gallon per tank)

22
Q
  1. What grade fuel is to be used in the PA-28?
A

100 LL (low lead) avgas (blue)

23
Q
  1. How many fuel pumps are on the aircraft?
A

2: 1 engine driven and 1 electrically driven

24
Q
  1. When is the electric fuel pump to be used?
A

All takeoffs, landings and when switching fuel tanks

25
Q
  1. What are the various positions on the fuel selector control?
A

“L”, “R”, and “OFF”

26
Q
  1. In the event of an electrical failure, what pilot actions are necessary to ensure continued operation of the standby attitude indicator?
A

Within 60 seconds while an amber blinking LED prompts you…press the “STBY PWR” button

27
Q
  1. If the standby power button on the attitude indicator is not pressed within one minute of electrical failure, what will happen?
A

If the pilot fails to activate the standby battery within 60 seconds, the STBY PWR button can still be pressed to activate the standby battery; however, the gyro may not be oriented to the airplane depending on the time elapsed prior to pressing the STBY PWR button.

28
Q
  1. How do you determine a standard rate turn on an aircraft with a G500 system?
A

Use the reference lines and the magenta line that appears above the heading indicator to identify a standard rate or half-standard rate turn.

29
Q
  1. In the event of an AHRS failure, which indications will no longer be displayed on the PFD? Which indications will still be visible on the PFD?
A 
No longer visible: 
- Heading indicator (compass rose and ground track still available supplied by GPS) 
- Turn Coordinator
- Attitude Direction Indicator 
Visible:
- Airspeed
- Altitude 
- Vertical Speed
30
Q
  1. Which approaches can be accomplished with an AHRS failure?
A

Any precision (ILS) or non-precision (GPS) approach is available using the HSI on the PFD.

31
Q
  1. What instrument approaches are available with the PFD inoperative? With the MFD inoperative? With a total PFD/MFD failure?
A

PFD inop: Only non-precision (GPS) approaches can be accomplished.
MFD inop: all approaches are available for use.
Both inop: Only GPS approach

32
Q
  1. How long does the internal battery last when providing power to the standby attitude indicator? With the loss of the ADC, which lost instrument does not have a backup? What should you do to compensate for the lack of information?
A
  • 1 hour
  • There is no backup for the VSI
  • Use stby instr’s, known pitch attitudes using the attitude indicator, power settings, and airspeeds produce consistent rates for VSI

ATP (4 decks)

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