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Mesa Airlines Training > Kevin's Test Questions > Flashcards

Kevin's Test Questions Flashcards

1
Q

How much thrust is produced with APR?

A

14,750 lbs

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2
Q

How much engine thrust is produced with full thrust?

A

13,560 lbs

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3
Q

When an engine fails how much mismatch thrust will be needed for FADEC to automatically increase thrust to the operating engine?

A

N1 mismatch of 15%

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4
Q

When will APR automatically arm?

A

N1 RPM of both engines within 8% of takeoff power

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5
Q

What is on the Accessory Gearbox?

A

“FISHOIL +”

Fuel Pump

Integrated Drive Generator

Starter (Air Turbine)

Hydraulic Pump

Oil Pump

FADEC Alternator (+)

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6
Q

When must continuous ignition be used?

A

Takeoffs and landings on contaminated runways

Flight through moderate or heavy rain

Flight through moderate or greater turbulence

Flight in vicinity of thunderstorms

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7
Q

What type of thrust is automatically calculated by FADEC?

A

Normal Takeoff Thrust

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8
Q

Where is the oil replenishment tank located?

A

AFT equipment bay

Reference Slide #73 - Powerplant

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9
Q

Where are the thrust lever Detents located?

A

Climb

TOGA

Max Power

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10
Q

Define a Cold Soaked Airplane…

A

First Flight of the day

Aircraft is left out for more than 8 hours with temperatures of -30 degrees C or below, things must be done:

  • Engines must be motored for 60 seconds and fan rotation verified before engine start is initiated
  • Thrust Reversers must be actuated until the deploy and stow cycles are less than 2 seconds
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11
Q

What is the Max N2 split at idle?

A

2%

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12
Q

What is the N2 limitation regarding accelerating above idle?

A

N2 is 57% or less with OAT of -20 degrees C or less

DO NOT accelerate above idle

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13
Q

Max operating altitude for APU:

A

41,000 ft

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14
Q

Max APU start altitude:

A

37,000 feet

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15
Q

Max Bleed Air Altitude using APU

A

25,000 feet

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16
Q

If APU door position is open or unknown, what is the restricted airspeed?

A

220 Knots or less

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17
Q

AVAIL Switchlight illuminates when?

A

99% plus 2 seconds

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18
Q

What’s the limitation with APU start attempt limitations?

A

No more than 3 start attempts in 1 hour

  • 2 minute delay between start attempts
19
Q

When does the APU automatically shut down?

A

On the ground after 5 seconds

20
Q

Why is gravity pressure refueling less than pressure refueling?
(this question was asked by Kevin in class)

A

Because of the dihedral of the wing

21
Q

Why is the NACA scoop designed in that shape? (This question was asked by Kevin in class)

A

To prevent ice buildup

22
Q

What conditions will cause a takeoff configuration warning? (Kevin told us to know these)

A

“PASSFAR”

Parking Brake

Autopilot

Spoilers

Stab Trim

Flaps

Aileron Trim

Rudder Trim

23
Q

When does the Flight Data Recorder start to record?

A

When BEACON or STROBE light switch is selected on

24
Q

When does the Integrated Drive Generator (IDG) automatically disconnect?

A

“HOTLOP”

High Oil Temperature, Low Oil Pressure

25
Q

How would you know if the Integrated Drive Generator (IDG) is disconnected?

A

DISC Switchlight is illuminated

26
Q

When does the AUTO XFER Switchlight illuminate?

A

When a bus fault or generator overcurrent is detected by the Generator Control Unit (GCU)

27
Q

What happens when the AUTO XFER FAIL illuminates?

A

Affected generator is taken offline, due to a possible bus fault or generator over current

28
Q

AC AVAIL Switchlight indicates what when its illuminated?

A

Proper PHASE, VOLTAGE, FREQUENCY is established

29
Q

What does the Air Driven Generator (ADG) power?

A
  • ESS BUS
  • HYD pump 3B
  • Slats/Flaps
  • Stab Trim CH2
30
Q

How is Hydraulic System 3 cooled?

A

Relies on natural convection and radiation to dissipate heat, Components are not in close proximity to any appreciable heat sources (engines)

31
Q

What does the rudder travel limiter (RTL) do?

A

Rudder travel is limited IN FLIGHT ONLY, prevents overstressing the vertical stabilizer

32
Q

What are the limitations of the Multifunction Spoilers (MFS’s)?

A
  • Must not be extended in flight below 300 feet AGL

- Must not be extended in flight at airspeed below recommended approach speed plus 10 knots

33
Q

Max altitude for slats/flaps usage?

A

15,000 feet

34
Q

What’s the limitation with regarding usage of slats/flaps enroute?

A

Prohibited

35
Q

What’s the limitation with the use of slats/flaps while holding?

A

In-flight holding with slats/flaps is PROHIBITED during icing conditions

36
Q

How are you going to change bleed air source on your panel?

A

Start from right, changing bleed source, ISOL open, then bleed valves

37
Q

How many outflow valves do we have?

A

Only 1

38
Q

What does the ice detectors vibrate at? (Kevin told us this in class, someone was asked on an oral)…

A

20,000-30,000 MHz

39
Q

Know Cowl Anti-Ice (Kevin told us this will be on test)

A
  • Double Walled A/I duct
  • Independent pressure transducer
  • L/R COWL A/I Caution message
40
Q

What is heated on the ground with AC power/probe heat on?

A

TAT and Pitot bases - OFF

Static and AOA - ON

Pitot Heats - Half Heat

41
Q

What probes are heated in flight with any switch position? (Kevin told us to know this for test)

A

All probes heated with at least one generator on-line

42
Q

When do you turn the wings and cowls anti-ice on in flight? (Kevin said to be familiar with this)

A

Below 230 knots in icing conditions

43
Q

What does the detection test (DET TEST) Switchlight test? (Kevin says to know this for test)

A

Tests both ICE detection and Air Data Sensor Heat Controller (ADHSC) Systems

  • Advisory message “ADS HEAT TEST OK”

Mesa Airlines Training (26 decks)

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