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 = 6%
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 2535 3595 5190
59 2775 3925 5690 0
90 3125 4475 6590
120 3850 5585 8460
20 2000 2885 4225
59 2210 3170 4665 20 58,000 152 142
90 2505 3640 5435
120 3100 4565 7010
20 1620 2365 3510
59 1800 2620 3900 40
90 2055 3020 4565
120 2555 3805 5910
20 3245 4630 6785
59 3555 5060 7440 0
90 4030 5820 8755
120 4990 7405 —
20 2585 3750 5575
59 2860 4130 6155 20 65,000 160 150
90 3260 4775 7280
120 4055 6105 9690
20 2115 3105 4665
59 2350 3440 5185 40
90 2695 3995 6160
120 3365 5125 8225
20 4130 5940 8836
59 4515 6500 9710 0
90 5160 7570 —
120 6475 9855 —
20 3325 4855 7325
59 3665 5350 8100 20 72,000 168 158
90 4215 6265 9800
120 5315 8200 —
20 2740 4050 6175
59 3040 4485 6870 40
90 3510 5275 8345
120 4445 6930 —
DISTANCES NOT SHOWN EXCEED 10,000 FEET
TAKEOFF SPEED AND GROUND
ROLL DISTANCE — FLAPS DOWN (Sheet 1 of 2)