TM 55-1510-221-10
L A N D I N G D I S T A N C E W I T H O U T P R O P E L L E R R E V E R S I N G - F L A P S 0%
ASSOCIATED CONDITIONS:
EXAMPLE:
POWER RETARDED TO MAINTAIN APPROPRIATE
FLAPS - 100% LANDING
DESCENT RATE ON FINAL APPROACH. ABOVE
DISTANCE OVER
13.500 LBS USE 500 FT/MIN: AT OR BELOW
50-FT OBSTACLE.. 2510 FT
13,500 LBS USE 600 FT/MIN:
FLAPS
0%
RUNWAY PAVED, LEVEL, DRY SURFACE
APPROACH SPEED.. IAS AS TABULATED
50-FT OBSTACLE. _. 3410 FT
APPROACH SPEED 111 KTS
BRAKING
MAXIMUM
LANDING WEIGHT 10,309 LBS
FLAPS-UP LANDING
DISTANCE OVER
NOTES:
1.
LANDING WITH FLAPS FULL DOWN (100%) IS NORMAL PROCEDURE. USE THE GRAPH BELOW WHEN IT
IS NECESSARY TO LAND WITH FLAPS UP (0%).
2.
TO DETERMINE FLAPS-UP LANDING DISTANCE, READ FROM THE “NORMAL LANDING DISTANCE WITH-
OUT PROPELLER REVERSING - FLAPS 100%” GRAPH THE LANDING DISTANCE APPROPRIATE TO
FAT, ALTITUDE, WIND, AND 50-FT OBSTACLE, THEN ENTER THE GRAPH BELOW WITH DERIVED VALUE
AND READ THE FLAPS-UP LANDING DISTANCE.
Figure 7-61. Landing Distance Without Propeller Reversing - Flaps 0%
7-90
