Landing Distance From 50 Feet Above Ground Level - THRUSH S2R-H80 Flight Manual

Single & dual cockpit
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4.7.
LANDING DISTANCE FROM 50 FEET ABOVE GROUND
LEVEL
The Landing Distance from 50 feet above ground level in no wind conditions is provided
in the following two charts. The first chart provides the landing distance from 50 feet above
ground level at the maximum landing weight of 7600 lbs. The second chart allows
correcting that distance for some aircraft weight less than 7600 lbs.
The Approach Airspeed to achieve these Landing Distances is 114 MCAS at the 50 feet
above ground level. This airspeed is for a landing gross weight of 7600 lbs. (For other
weights, refer to Table 4-1 below.)As weight is reduced, this airspeed should be reduced.
In conditions of a headwind, the landing distance will be less than that shown. Downwind
landings will increase the distances provided and should be avoided.
AIRCRAFT WEIGHT – LBS.
EXAMPLE:
Assuming a 25ᵒC ambient temperature and an airport elevation of 3000 ft. Pressure
Altitude with an aircraft landing weight of 6800 lbs. To determine the Landing Distance
from 50 feet above ground level, enter the first chart at the 25ᵒC ambient temperature and
proceed vertically until reaching a pressure altitude of 3000 ft. Then proceed horizontally
to the right to read a landing distance at a 7600 lb. gross weight of 2200 ft. Enter the
second chart at that distance (2200 ft.) and from the right vertical reference, follow the
guidelines down to the point where a line drawn vertically from 6800 lbs. intersects it. Then
proceed horizontally to the right to read a Landing Distance at 6800 lbs. of 1900 ft.
AFM H8001 SINGLE & DUAL COCKPIT, Revision A
FAA APPROVAL DATE: 08/05/2014
7600
7000
6500
6000
5500
Table 4-1: Landing Distance Airspeeds
S2R-H80 Single & Dual Cockpit
AIRPLANE FLIGHT MANUAL
APPROACH AIRSPEED - MCAS
114
109
105
101
97
Page | 63

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