TM 55-1510-215-10
Section XVII. LANDING
7-60. Description.
7-62. Conditions.
The Landing Chart (fig. 7-73), shows the total
a. Power - As required (on final approach).
ground roll distance required for varying air
temperatures, altitudes, weights and flap positions.
b. Flaps - As selected.
NOTE
c. Landing Gear - DN.
Landing data is provided up to
d. Technique - Establish 800 FT/MIN descent on
weights of 9650 pounds in the event
final approach at the appropriate airspeed from the
emergency
landing
is
required
Approach Speed Chart (fig. 7-72). When landing is
immediately after takeoff. Any time
assured, reduce power and speed.
the maximum landing weight of 9168
pounds is exceeded, an appropriate
e. Runway - Runway conditions for this chart are
entry shall be made on DA Form
based on a dry, level, hard-surface. Conditions other
2408-13.
than these may vary aircraft landing distance. Distance
decreases approximately 4% per 1% uphill gradient.
7-61. Use of Chart.
Distance increases approximately 4% per 1% downhill
gradient.
Performance is based on the approach speed
obtained from the Approach Speed Chart (fig. 7-72).
f. Wind - All data presented are based on calm
wind conditions. Distance decreases approximately 1%
per knot headwind. Distance increases approximately
4% per knot tailwind.
7-120
