Navair F-14B, Emergency Procedure Tabs

Page: 289 / 355

NAVAIR 01-F14AAP-1B
249
ÇÇÇÇÇÇ
ÇÇÇÇÇÇ
ÇÇÇÇÇÇ
ÇÇÇÇÇÇ
ÇÇÇÇÇÇ
ÇÇÇÇÇÇ
265
WING
LE
= 20
_
MILITARY POWER
AIRCRAFT CONFIGURATION:
ALL DRAG INDEXES
0
_
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 2070 2810 3875
59 2255 3060 4225 0
90 2510 3440 4770
120 2990 4105 5720
20 1630 2245 3140
59 1790 2465 3455 20 58,000 150 140
90 2000 2305 3285
120 2400 2780 3970
20 1315 1835 2605
59 1455 2030 2880 40
90 1635 2305 3285
120 1970 2780 3970
20 2650 3615 4995
59 2900 3940 5450 0
90 3225 4430 6170
120 3845 5325 7460
20 2110 2925 4095
59 2325 3210 4505 20 65,000 159 149
90 2605 3630 5130
120 3125 4385 6230
20 1725 2420 3425
59 1915 2670 3790 40
90 2155 3035 4335
120 2590 3680 5285
20 3330 4560 6300
59 3635 4960 6875 0
90 4065 5600 7830
120 4865 6780 9545
20 2665 3725 5225
59 2950 4085 5740 20 72,000 168 158
90 3320 4635 6570
120 3995 5640 8040
20 2190 3110 4405
50 2450 3425 4870 40
90 2765 3905 5595
120 3340 4770 6875
TAKEOFF SPEED AND GROUND
ROLL DISTANCE — FLAPS UP