Aircraft Performance. Flight Performance Charts.

Determine the total distance required for takeoff to clear a 50-foot obstacle OAT std pressure altitude 4,000 ft takeoff weight 2,800 lb headwind component calm

1,750 ft. See picture for explanation. Pretty much just starting on the chart on the left and moving over to the chart on the right with the ruler. When you get to the weight go to the line that is at 2,800. When you get to the obstacle then go up 50 because of the obstacle. Use performance (takeoff) chart.

Determine the approximate total distance required to land over a 50-foot obstacle. OAT 90°F Pressure Altitude 4,000 ft Weight 2,800 lbs Headwind component 10 kts

1,775 ft. -F is below C on the chart -Use the major lines as references as you keep moving over to the right -See picture for details -Use Airplane Landing Distance Graph -Headwind so you go down if it was a tailwind then you would go up

Determine the total distance required to land. OAT std Pressure Altitude 10,000 ft Weight 2,400 lbs Wind component Calm Obstacle 50 ft

1,925 feet. -When no temp is given use the ISA line -See picture for details

What fuel flow should a pilot expect at 11,000 feet on a standard day with 65 percent maximum continuous power?

11.2 gallons per hour. Note: Look all the way to the left at "Press ALT." and the feet is listed there. 11.5 + 10.9=22.4 22.4/2=11.2

Approximately what true airspeed should a pilot expect with full throttle at 10,500 feet with a temperature of 36°F above standard?

165 KTS.

What is the crosswind component for a landing on Runway 18 if the tower reports the wind as 220° at 30 knots?

19 knots -When the wind is coming from the South you subtract 180° when given the wind

Determine the approximate manifold pressure setting with 2,450 RPM to acheive 65% maximum continuous power @ 6,500 with a temperature of 36°F higher than standard

21.0''Hg literally do not have to do anything besides look at the chart. look at the pressure altitude feet then go over and look at the chart all the way to the right because it is 36°F. look under MAN press or manifold pressure. Note: Entire chart is for 2,450 RPM and 65% power.

Determine the approximate landing ground roll distance. Pressure Altitude- Sea Level Headwind- 4 kts Temperature- Std (standard)

401 feet. -When it says @ sea level look at the first column where it says sea level and follow that ground roll

Determine the approximate ground roll distance required for takeoff. OAT 32°F Pressure Altitude 2,000 ft Takeoff Weight 2,500 lb Headwind component 20 kts

650 feet. See picture for further explanation.

Determine the total distance required to land over a 50-foot obstacle. Pressure Altitude 3,750 ft Headwind 12 kts Temperature Std

816 feet. See picture attached.

With a reported wind or north at 20 knots, which runway (6, 29, or 32) is acceptable for use for an airplane with a 13-knot maximum crosswind component?

Runway 31 Because the wind is coming from the north you use 360 then add a 0 to the runways to see which one is the closest.

A pilot with 2 passengers landed on a 2,100 foot east-west gravel strip with an elevation of 1,800 feet. The temperature is warmer than expected and after computing the density altitude it is determined the takeoff distance over a 50 foot obstacle is 1,980 ft. The airplane is 75 pounds under gross weight. What would be the best choice?

Wait until the temperature decreases, and recalculate the takeoff performance. -Take off distance less than 6% -If it cools off a little than the performance of the aircraft will improve