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
INBD SPOILERS, SPEED BRAKES
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 3480 3100 2780 2510 2275
59 3760 3360 3030 2740 2495 SEA
90 3980 3570 3225 2930 2670 LEVEL
120 4295 3865 5500 3180 2910
20 3990 3585 3235 2940 2680
59 4475 4035 3655 3330 3050 4000 55,000 164
90 4985 4510 4095 3740 3430
120 5485 4975 4530 4145 3810
20 5105 4620 4205 3840 3525
59 5860 5320 4855 4450 4100 8000
90 6480 5900 5400 4960 4570
120 7085 6470 5930 5460 5040
20 3770 3375 3040 2755 2510
59 4360 3920 3540 3220 2940 SEA
90 4850 4375 3965 3615 3305 LEVEL
120 5335 4825 4385 4005 3670
20 4840 4365 3960 3610 3305
59 5570 5045 4590 4200 3855 4000 60,000 171
90 6150 5585 5045 4670 4295
120 6720 6120 5595 5155 4735
20 6290 5715 5220 4785 4405
59 7180 6545 5995 5515 5090 8000
90 7905 7230 6635 6115 5655
120 8600 7885 7250 6695 6205
LANDING DISTANCE GROUND ROLL — FLAPS UP
(Sheet 2)