Tesis

Páginas: 3 (507 palabras) Publicado: 6 de febrero de 2013
3.0 KNOWLEDGE OF GENERIC AIRCRAFT SYSTEM & JET ENGINES.

3.1 Pitot-Static System instruments

1. Witch pressure is defined as station pressure?

Actual pressure at field elevation

2. What iscorrect altitude (Approximate true altitude)?

Indicated altitude corrected for temperature variation from standard

3. When setting the altimeter, pilots should disregard

Effects ofnonstandard atmospheric temperatures and pressures

4. If the ambient temperature is colder than standard at FL310, what is the relationship between true altitude and pressure altitude?

True altitude islower than 31.000 feet

5. If the ambient temperature is warmer than standard at FL350, what is density altitude compared to pressure altitude?

Higher than pressure altitude

6. En route atFL270, the altimeter is set correctly. On descent, a pilot fails to see the local altimeter setting of 30.57. If the field elevation is 650 feet, and the altimeter is functioning properly, what willindicate upon landing?

Sea level

7. During an en route descent in a fixed-thrust and fixed-pitch attitude configuration, both the ram air input and drain hole of the pitot system become completelyblocked by ice. What airspeed indication can be expected?

Decrease in indicated airspeed

8. What can a pilot expect if the pilot system ram air input and drain hole are blocked by ice?

Theairspeed indicator may act as an altimeter

9. If both the ram air input and drain hole of the pitot system are blocked by ice, what airspeed indication can be expected?

No variation of indicatedairspeed in level flight if large power changes are made

10. How will the airspeed indicator react if the ram air input to the pilot head is blocked by ice, both the drain hole and static port arenot?

Indication will drop to zero

TAKEOFF SPEEDS.

Witch is a defined of V2 speed?

Takeoff safety speed

What is the correct symbol for minimum unstick speed?

Vmu

The maximum speed...
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