Aircraft Performance Part II

(Refer to Figure 38.) Determine the total distance required to land over a 50-foot obstacle. Pressure altitude 7,500 ft Headwind 8 kts Temperature 32°F Runway Hard surface

1,004 feet.

(Refer to Figure 40.) Determine the approximate ground roll distance required for takeoff. OAT 100°F Pressure altitude 2,000 ft Takeoff weight 2,750 lb Headwind component Calm

1,150 feet.

(Refer to Figure 37.) Determine the total distance required to land. OAT 32°F Pressure altitude 8,000 ft Weight 2,600 lb Headwind component 20 kts Obstacle 50 ft

1,400 feet.

(Refer to Figure 40.) Determine the total distance required for takeoff to clear a 50-foot obstacle. OAT Std Pressure altitude Sea level Takeoff weight 2,700 lb Headwind component Calm

1,400 feet.

(Refer to Figure 37.) Determine the total distance required to land. OAT 90°F Pressure altitude 3,000 ft Weight 2,900 lb Headwind component 10 kts Obstacle 50 ft

1,725 feet.

(Refer to Figure 40.) 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 feet.

(Refer to Figure 37.) Determine the approximate total distance required to land over a 50-foot obstacle. OAT 90°F Pressure altitude 4,000 ft Weight 2,800 lb Headwind component 10 kts

1,775 feet.

(Refer to Figure 37.) Determine the total distance required to land. OAT Std Pressure altitude 10,000 ft Weight 2,400 lb Wind component Calm Obstacle 50 ft

1,925 feet.

(Refer to Figure 35.) 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.

(Refer to Figure 35.) Approximately what true airspeed should a pilot expect with full throttle at 10,500 feet with a temperature of 36 degrees F above standard?

165 knots.

(Refer to Figure 36.) What is the crosswind component for a landing on Runway 18 if the tower reports the wind as 220° at 30 knots?

19 knots.

(Refer to Figure 35.) Determine the approximate manifold pressure setting with 2,450 RPM to achieve 65 percent maximum continuous power at 6,500 feet with a temperature of 36°F higher than standard.

21.0" Hg.

(Refer to Figure 36.) What is the headwind component for a landing on Runway 18 if the tower reports the wind as 220° at 30 knots?

23 knots.

(Refer to Figure 36.) What is the maximum wind velocity for a 30° crosswind if the maximum crosswind component for the airplane is 12 knots?

24 knots.

(Refer to Figure 36.) Determine the maximum wind velocity for a 45° crosswind if the maximum crosswind component for the airplane is 25 knots.

35 knots.

(Refer to Figure 35.) What is the expected fuel consumption for a 500-nautical mile flight under the following conditions? Pressure altitude 4,000 ft Temperature + 29°C Manifold pressure 21.3" Hg Wind Calm

36.1 gallons.

(Refer to Figure 38.) Determine the approximate landing ground roll distance. Pressure altitude 1,250 ft Headwind 8 kts Temperature Std

366 feet.

(Refer to Figure 38.) Determine the approximate landing ground roll distance. Pressure altitude Sea level Headwind 4 kts Temperature Std

401 feet.

(Refer to Figure 38.) Determine the approximate landing ground roll distance. Pressure altitude 5,000 ft Headwind Calm Temperature 101°F

545 feet.

(Refer to Figure 40.) Determine the approximate ground roll distance required for takeoff. OAT 95°F Pressure altitude 2,000 ft Takeoff weight 2,500 lb Headwind component 20 kts

650 feet.

(Refer to Figure 35.) What is the expected fuel consumption for a 1,000-nautical mile flight under the following conditions? Pressure altitude 8,000 ft Temperature 22°C Manifold pressure 20.8" Hg Wind Calm

70.1 gallons.

(Refer to Figure 38.) Determine the total distance required to land over a 50-foot obstacle. Pressure altitude 3,750 ft Headwind 12 kts Temperature Std

816 feet.

(Refer to Figure 38.) Determine the total distance required to land over a 50-foot obstacle. Pressure altitude 5,000 ft Headwind 8 kts Temperature 41°F Runway Hard surface

956 feet.

(Refer to Figures 32 and 33.) With the airplane loaded as follows, what action can be taken to balance the airplane? Front seat occupants 411 lb Rear seat occupants 100 lb Main wing tanks 44 gal

Add a 100-pound weight to the baggage compartment.

(Refer to Figures 32 and 33.) Which action can adjust the airplane's weight to maximum gross weight and the CG within limits for takeoff? Front seat occupants 425 lb Rear seat occupants 300 lb Fuel, main tanks 44 gal

Drain 9 gallons of fuel.

(Refer to Figure 67.) What effect does a 30-gallon fuel burn have on the weight and balance if the airplane weighed 2,784 pounds and the MOM/100 was 2,222 at takeoff?

Moment will decrease to 2,087 lbs-in.

(Refer to Figure 36.) With a reported wind of south at 20 knots, which runway (10, 14, or 24) is appropriate for an airplane with a 13-knot maximum crosswind component?

Runway 14.

(Refer to Figure 36.) With a reported wind of 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 32.

(Refer to Figures 32 and 33.) Upon landing, the front passenger (180 pounds) departs the airplane. A rear passenger (204 pounds) moves to the front passenger position. What effect does this have on the CG if the airplane weighed 2,690 pounds and the MOM/100 was 2,260 just prior to the passenger transfer?

The CG moves forward approximately 3 inches.

(Refer to Figures 32 and 33.) What effect does a 35-gallon fuel burn (main tanks) have on the weight and balance if the airplane weighed 2,890 pounds and the MOM/100 was 2,452 at takeoff?

Weight is reduced by 210 pounds and the CG is aft of limits.