Gnav 501-550

Given: TAS: 150 kts Actual HDG: 270° Wind: 245/12 kts What is the wind correction angle?

• 4° to the left.

• 4° to the right.

• 2° to the right.

• 2° to the left.

The equivalent of 70 m/sec is approximately:

• 136 kts

• 145 kts

• 210 kts

• 35 kts

Given: True Heading: 180° TAS: 500 kts W/V: 225°/100 kts Calculate the GS.

• 600 kts

• 450 kts

• 535 kts

• 435 kts

Your pressure altitude is FL55, the QNH is 998, and the OAT is +30°C. What is density altitude?

• 6 980 feet.

• 7 750 feet.

• 8 620 feet.

• 10 020 feet.

An aircraft is flying at FL180 and the outside air temperature is -30°C. If the CAS is 150 kts, what is the TAS?

• 195 kts

• 115 kts

• 180 kts

• 145 kts

An aircraft is following a true track of 048° at a constant TAS of 210 kts. The wind velocity is 350°/30 kts. The GS and drift angle are:

• 200 kts, 3.5° right

• 192 kts, 7° left

• 192 kts, 7° right

• 225 kts, 7° left

The distance between A and B is 90 NM. At a distance of 75 NM from A the aircraft Is 4 NM right of course. The track angle error (TKE) is:

• 3°R

• 19°R

• 6°R

• 22°R

Tags

NGSS.MS-PS2-2

An aircraft at FL140, IAS 210 kts, OAT -5°C and wind component minus 35 kts, is required to reduce speed in order to cross a reporting point 5 min later than planned. Assuming that flight conditions do not change, when 150 NM from the reporting point the IAS should be reduced by:

• 25 kts

• 20 kts

• 30 kts

• 15 kts

An aircraft is descending from FL270 to FL100 following MT 054° and maintaining CAS 250 kts. Given are variation 13°E, temperatures ISA-10°C, W/V 020/60. What is your GS?

• 277 kts

• 265 kts

• 325 kts

• 298 kts

Tags

NGSS.HS-PS2-1

You are required to descend from FL230 to FL50 over a distance of 32 NM in 7 minutes. What is the required TAS when you expect a Wind Component (WC) of -25 kts during the descent?

• 317 kts

• 329 kts

• 308 kts

• 300 kts

Tags

NGSS.HS-PS2-1