Technical interview Flashcards

(18 cards)

1
Q

Which engines does Ryanair fly?

A

26 airbus A320 (lauda)
411 B737 NG
206 B737 MAX gamechanger
300 B737 max10 (order)

total over 600 boeing 737 aircraft

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2
Q

Difference Boeing 737-800 and B737 max 8 gamechanger

A
  • 4% more guests (197 passengers instead of 189)
  • 16% less fuel
  • 40% less noise emissions
  • bigger screens in cockpit
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3
Q

Engines B737-800 and B737 Max 8

A

737-800: CFM56-7B
737-8 MAX: CFM LEAP-1B - LEAP = leading Edge Aviation Propulsion
CFM = joint venture GE aerospace and Safran Aircraft Engines. Both around 27k pounds of thrust

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4
Q

Bypass ratio B737-800 and 737-Max8

A

5,5 : 1 and 9 : 1

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5
Q

Why the winglets on the engine CFM-LEAP 1 B

A

to reduce drag, improve airflow, increase lift. The engines are also placed higher and further forward

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6
Q

Tell me about the B737 Max 10

A

150 orders, 150 options, delivery is delayed, 228 seats. same engines as B737 max 8 (CFM-LEAP-1B)

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7
Q

Tell me about the electrical system of the B737

A

4 sources:
- 2x engine generators
- 1x APU generator
- ground power
- 2x Battery (for emergencies)

Generators provide 3 phase, 400 hertz and 115 volts of AC power.

No AC parallel sourcing

2x AC transfer busses, which can be supplied by engine generator or APU generator

IDG = intergrated Drive Generator = inside each engine and provides power

the bigger systems run on AC power, while some smaller system work on DC power.

from AC to DC = Transformer Rectifier Unit
DC to AC = invertor

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7
Q

What is CFIT?

A

Controlled Flight Into Terrain -> means that the aircraft is working perfectly, but due to not having good situational awareness, pilots fly the aircraft into an obstacle, terrain, sea etc.

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8
Q

Explain RVR

A

Runway Visual Range –> is the visibility in meters on the runway, is mentioned in the metar if the visibility drops below 1,600 meter or when the RVR is 1,800 meter or less

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9
Q

Where does CAVOK stand for

A

Ceiling And Visibility OK

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10
Q

Which items on hydraulic A en B

A

A: - landing gear
- primary flight controls (rudder, ailerons, elevator)
- nose wheel steering
- thrust reversers A
- some of the spoilers
- left reverser

B:
- flaps and slats
- primary flight controls (rudder, ailerons and elevator)
- normal brakes
- right reverser

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11
Q

Explain LGTU

A

Landing Gear Transfer Unit = when hydraulic system A fails, and you want to raise (not lower) the landing gear, LGTU takes hydraulic power from system B to raise the gear. It only works when A fails

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12
Q

What is a CSD

A

Constant Speed Drive -> there to transform the power generated by the engines (IDG), to a stable AC current. (115 volt, 3 phase and 400 hertz)

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13
Q

What is MCAS? What does it do?

A

Maneuvering Characteristics Augmentation System –> is bases on the angle of attack and is designed to pitch down if there is a stall incoming. After 2 crashes (lion air and ethiopian airlines), the system needed changes

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14
Q

Explain coriolis effect

A

on the northern hemisphere, the earth rotate to the left. the rotation is faster at the equator. therefore, the curveture of clouds etc is to the right.

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15
Q

DALR and SALR

A

dry adiabatic lapse rate: 3 degrees per 1,000 ft
saturated (wet) adiabatic lapse rate: 2 degrees per 1,000 ft

16
Q

Cold and warm fronts

A

Cold front: pushes like a bulldozer from below the warm and moist air up. this causes the warm air to rise an being unstable with cumulus clouds, rain showers etc.
warm front: moves gradually over a cold front, which makes the air stable. drizzle can occur.

17
Q

ECU and FADEC?

A

engine control unit, which manages the Full authority Digital engine system. which manages the fuel flow, propeller pitch etc