Navair F-14B, Emergency Procedure Tabs

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NAVAIR 01-F14AAP-1B
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MAXIMUM BRAKING — HARD DRY RUNWAY
WING
LE
= 20
_
AIRCRAFT CONFIGURATION:
ALL DRAG INDEXES
ALL DECELERATION DEVICES
FULL ANTISKID BRAKING
35
_
FLAPS, GEAR DOWN
ENGINES (2) F110-GE-400
IDLE POWER
DATE: JANUARY 1990
DATA BASIS: ESTIMATED BASED
ON FLIGHT TEST
DISTANCE IN FEET
RUNWAY
TEMP
F
HEADWIND
(KNOTS)
PRESSURE
ALTITUDE
(FEET)
GROSS
WEIGHT
(LBS)
TOUCH-
DOWN
SPEED
F
0 10 20 30 40
(FEET) (LBS) SPEED
(KNOTS)
20 2525 2210 1995 1740 1555
59 2730 2400 2130 1900 1710 SEA
90 2890 2555 2270 2035 1855 LEVEL
120 3050 2700 2410 2160 1955
20 2895 2560 2275 2040 1840
59 3130 2775 2480 2230 2020 4000 55,000 141
90 3315 2950 2645 2390 2165
120 3495 3120 2805 2535 2305
20 3365 2995 2690 2426 2200
59 3635 3255 2930 2650 2415
90 3850 3455 3120 2830 2585 8000
120 4055 3650 3305 3005 2745
20 2775 2445 2170 1940 1750
59 3000 2655 2370 2125 1920 SEA
90 3180 2820 2525 2270 2055 LEVEL
120 3350 2985 2675 2415 2190
20 3185 2830 2535 2280 2065
59 3445 3075 2760 2495 2265 4000 60,000 149
90 3650 3265 2940 2665 2425
120 3845 3450 3120 2830 2580
20 3700 3315 2990 2710 2470
59 4000 3600 3255 2960 2705 8000
90 4415 3985 3615 3295 3015
120 4815 4355 3960 3615 3320
LANDING DISTANCE GROUND ROLL — FLAPS DOWN
(Sheet 2)