TM 1-1510-223-10
LANDING DISTANCE - ONE ENGINE INOPERATIVE
FLAPS DOWN
APPROACH SPEED: 111 KNOTS (ALL WEIGHTS)
ASSOCIATED CONDITIONS-
POWER......................................................RETARDED TO MAINTAIN 500
FT/MIN ON FINAL APPROACH
PROPELLER CONTROL'
INOPERATIVE ENGINE................FEATHERED
RUNWAY...................................................PAVED. DRY SURFACE
POWER LEVERS-
OPERATIVE ENGINE......................GROUND FINE AT TOUCHDOWN
BRAKING...................................................MAXIMUM WITHOUT SLIDING TIRES
OBSTACLE HEIGHT........................50 FT
EXAMPLE:
FLAPS-DOWN NORMAL LANDING DISTANCE............................3437 FT
ONE-ENGINE-INOPERATIVE LANDING DISTANCE.................4152 FT
NOTE. TO
DETERMINE
THE
ONE-ENGINE-INOPERATIVE
LANDING DISTANCE, READ FROM THE "NORMAL
LANDING DISTANCE FLAPS DOWN" GRAPH THE
LANDING
DISTANCE
APPROPRIATE
TO
TEMPERATURE, ALTITUDE, RUNWAY GRADIENT, AND
WIND. THEN ENTER THE GRAPH BELOW WITH THE
DERIVED VALUE, AND READ THE ONE-ENGINE-
INOPERATIVE LANDING DISTANCE.
Figure 7-146. Landing Distance - One Engine Inoperative - Flaps Down
Change 2 7-237/(7-238 blank)
