week three worksheet

When flying at 300 kts CAS at a pressure altitude of 31000 feet with an Indicated outside Air Temperature (IAOT) of -35°C the TAS will be

A pilot is flying on a heading of 358°C. Variation is +2° and deviation is 4°W. If drift is 3°P the aircraft track is

From the following find drift, track and groundspeed. Heading 355°, TAS 400 kts, W/V 210/60

From the following find drift, track and groundspeed. Heading 170°, TAS 200 kts, W/V 090/50:

The angle between the HDG and the Tk is called

An aircraft is flying at FL390, temperature ISA + 7, at Mach 0.85. The TAS is

An aircraft is cruising at 38,000 ft, temperature is ISA -4, and CAS is 330 kts. The TAS will be

True Heading 340

True Airspeed 250Kts

Wind Velocity 080/70

What is the Drift, True Track, and Groundspeed?

True Heading 270

True Airspeed 350Kts

Drift 10R

Groundspeed 400Kts

What is the Wind Velocity

True Track 090

True Airspeed 300Kts

Wind Velocity 350/60

What is the Heading and Groundspeed

Runway 34

Wind Velocity 270/40

What are the Headwind and Crosswind Components.

Refer to the figure below. True Heading, Airspeed, and wind velocity are as shown. What is the drift and true track.

Runway 18 is in use, wind direction is 215, minimum headwind is 15Kts, maximum crosswind is 20Kts. What is the minimum and maximum wind speed?

Convert 6 feet to both meters and yards.

Using a specific gravity of .75 convert 600 Imperial Gallons to both Pounds and Kilograms.

10 degrees Centigrade is equal to ____________ degrees Fahrenheit.

An aircraft burns 200 pound of fuel in 20 minutes, what is it's fuel flow per hour?

How many minutes will it take an aircraft flying at a groundspeed of 480Kts to fly 160 nm?

Pressure Altitude is 35, 000 feet, COAT is - 60 degrees, CAS is 150, what is the TAS?

Given the above conditions what is the Mach Number?

What must be taken into account when calculating True Airspeeds above 300Kts that need not be taken into account when finding True Airspeeds below 300Kts?

Pressure Altitude is 35, 000 feet, COAT is - 60 degrees, CAS is 250Kts, what is the TAS?

COAT is - 55C, Mach Number is .85, what is the TAS?

TAS is 440Kts, OAT is -25C, what is the COAT?

COAT is 130C, Pressure Altitude is 30,000 feet, What is the True Altitude?

An Airfield is 5000' amsl and the temperature is 10 degrees, what is the Density Altitude?

For a RAS of 280 For a TAS of 300