Navair F-14B, Emergency Procedure Tabs

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NAVAIR 01-F14AAP-1B
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WING SWEEP
LE
= 20
_
MILITARY POWER
CG = 16.2%
AIRCRAFT CONFIGURATION:
ALL DRAG INDEXES
35
_
FLAPS
GEAR DOWN
ENGINES (2) F110-GE-400
HARD DRY RUNWAY
DATE: JANUARY 1990
DATA BASIS: ESTIMATED BASED
ON FLIGHT TEST
DISTANCE IN FEET
PRESSURE ALTITUDE
(FEET)
HEAD- GROSS TAKEOFF ROTATION
RUNWAY
TEMP
F
SEA
LEVEL
4000 8000
HEAD-
WIND
(KNOTS)
GROSS
WEIGHT
(POUNDS)
TAKEOFF
SPEED
(KNOTS)
ROTATION
SPEED
KNOTS
20 1795 2500 3535
59 1960 2730 3875 0
90 2200 3065 4390
120 2640 3745 5415
20 1370 1945 2795
59 1510 2140 3090 20 58,000 132 122
90 1710 2420 3520
120 2060 2975 4365
20 1080 1555 2270
59 1200 1730 2525 40
90 1365 1960 2890
120 1655 2420 3600
20 2340 3270 4690
59 2550 3570 5125 0
90 2860 4045 5860
120 3475 4980 7340
20 1810 2575 3755
59 1995 2835 4135 20 65,000 140 130
90 2250 3230 4760
120 2750 4005 5990
20 1450 2085 3080
59 1605 2310 3415 40
90 1820 2645 3945
120 2335 3295 4985
20 2940 4150 6015
59 3215 4540 6580 0
90 3625 5155 7585
120 4425 6425 9665
20 2300 3305 4865
59 2540 3645 5365 20 72,000 147 137
90 2885 4165 6215
120 3540 5220 7960
20 1855 2695 4020
59 2060 2995 4460 40
90 2355 3440 5195
120 2900 4325 6680
TAKEOFF SPEED AND GROUND
ROLL DISTANCE — FLAPS DOWN (Sheet 2)