AVP 142 Takeoff Distance
(3707) (Refer to Figure 40.) Determine the approximate ground roll distance required for takeoff. OAT..............................................Std Pressure altitude...................2,000 ft Takeoff weight.......................2,750 lb Headwind component......Calm A- 1,150 ft B- 1,300 ft C- 1,800 ft
A- 1,150 ft (See pg. 8-31 in PPTP)
(3708) (Refer to Figure 40.) Determine the approximate ground roll distance required for takeoff. OAT............................................95F Pressure altitude..................2,000ft Takeoff weight......................2,500 lb Headwind component.....20 kts A- 650 ft B- 850 ft C- 1,000 ft
A- 650 ft (See pg. 8-32 in PPTP)
(2283) The most critical conditions of takeoff performance are the result of some combination of high gross weight, altitude, temperature, and A- unfavorable wind. B- obstacles surrounding the runway. C- powerplant systems.
A- unfavorable wind The most critical conditions of takeoff performance are the result of some combination of high gross weight, altitude, temperature, and unfavorable wind. In all cases, the pilot must make an accurate prediction of takeoff distance from the performance data of the AFM/POH, regardless of the runway available, and strive for a polished, professional takeoff procedure.
(2234) The most critical conditions of takeoff performance are the result of some combination of high gross weight, altitude, temperature, and A- unfavorable wind. B- obstacles surrounding the runway. C- powerplant systems.
A- unfavorable wind. The most critical conditions of takeoff performance are the result of some combination of high gross weight, altitude, temperature, and unfavorable wind. In all cases, the pilot must make an accurate prediction of takeoff distance from the performance data of the AFM/POH, regardless of the runway available, and strive for a polished, professional takeoff procedure.
(3706) (Refer to Figure 40.) Determine the total distance required for takeoff to clear a 50-ft obstacle. OAT.............................................Std Pressure Altitude..................Sea Level Takeoff Weight......................2,700 lb Headwind component......Calm A- 1,000 ft. B- 1,400 ft. C- 1,700 ft.
B- 1,400 ft (See pg. 8-31 in PPTP)
(3705) (Refer to Figure 40.) Determine the total distance required for takeoff to clear a 50-ft obstacle. OAT..............................................Std Pressure altitude...................4,000 ft Takeoff weight.......................2,800 lb Headwind component......Calm A- 1,500 ft. B- 1,750 ft. C- 2,000 ft.
B- 1,750 ft (See pg. 8-31 in PPTP)
(2199) What effect does an uphill runway slope have on takeoff performance? A- Increases takeoff speed. B- Increases takeoff distance. C- Decreases takeoff distance.
B- Increases takeoff distance The effect of runway slope on takeoff distance is due to the component of weight along the inclined path of the aircraft. An upslope would contribute a retarding force component, while a downslope would contribute an accelerating force component. In the case of an upslope, the retarding force component adds to drag and rolling friction to reduce the net accelerating force.
