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1800 psi
1800 psi
3000 psi
1800 psi
1900 f 50 psi
800~10 psi
Figure 1-2. Characteristics and Limitations (Sheet 1 of 2) NZl97
l-3 ORIGINAL
NAVAIR 01.Fl4AAD-1
Aft-Left Tank Group Capacity 5900 - 6200 Ibs
Fwd-Right Tank Group Capacity 6300 - 6600 Ibs
Max split between cockpit totals 300 Ibs
Fuel dump rate 1500 Ibs/min
Fuel dump auto shutoff with 4000 Ibs remaining
Ground refuel rate @ 50 psi 450 gal/min
In-flight refuel rate @ 57 psi 475 gallmin
Normal Hyd. system operating press
BIDI activates when one system is
BIDI output w/3000 psi on good side
BIDI shuts off when failed system is
Emer. Fit. Hyd. on if both systems
Outb’d Spoiler Module
electrically inhibited @
Outb’d Spoiler Module
depressurized @
3000 f 100 psi
c2100 psi
2400 - 2600 psi
400 psi for
IOsec
<2100 psi
62” W/S
65” W/S
450
300
250
400
400/0.9 TMN
400
300
300/0.6 TMN
350/l .5 TMN
>0.7 TMN
>0.5 TMN
2.4 TMN
Windmill airstart airspeed required
Spooldown airstart airspeed required
Rudder authority limits inputs to <IO”
Rudder authority limits inputs to ~9.5”
Lateral stick inputs limited to l/4
Speedbrake blowback
Hook blowback in transit
Max speed w/ airsource off-o’wing fair
Max ramdoor airspeed - heat from
friction
Coordinate stick and rudder input
No cross controls above
Reduce speed light (airframe limit)
<350 Ejection Safe
350 - 450 Ejection Hazardous
>450/0.9 TMN Ejection Extremely Hazardous
650
700
650
1.75 TMN
1.52 TMN
Max below 12,000 ft
Max 12 - 25,000 ft
Max 25 - 34,000 ft
Max above 34,000 ft
Max with roll SAS off
170-200 Approach configuration
200 - 300/0.8 TMN Cruise configuration
400/0.6 TMN Max IFR probe speed
CRUISE: Pitch SAS off None
YawSASoff l.OTMN
Roll SAS off 1 .O TMN (wing
mounted AIM-54)
1.52 TMN (EX tank,
fuselage AIM-54,
A/G stores)
1.6 TMN (all other
configurations)
APPROACH: Pitch SAS off . None
Yaw SAS off None
Roll SAS off not permitted during
T/O & Land flap
transitions
1. Intentional Spins
2. During AB operations; sustained 0 to -0.5 g flight:
flight from -0.5 g to -2.4 g’s for more than
IO seconds.
3. At MIL power or less; zero or negative g flight for
more than 20 seconds.
4. AIM-9 launch with flaps/slats extended.
5. Fuel dump while in A/B or with S/Bs extended.
6. Dual eng AB takeoff, waveoffs, bolters or cal
launches
7. Single eng MAX AB takeoff, waveoff, or cat
launches
3. ACLS mode l/IA approaches
9. Rolling maneuvers with bank angle changes in
excess of 360
Sear Down Symmetric Limit
Sear Down Rolling
[coordinated turns only 225 - 280 KTS) 0 - 2.0
Flaps/Slats Down 0 - 2.0
Rolling Limit w/ maneuvering flaps/slats
sxtended (50,000 lb aircraft) 5.2
56,000 lb aircraft symmetric limit 4.6
38,000 lb aircraft symmetric limit 5.5
53,000 lb aircraft symmetric limit 6.0
50,000 lb aircraft symmetric limit 6.5
Figure 1-2. Characteristics and Limitations (Sheet 2 of 2)
ORIGINAL l-4
TACTICAL
STANDARD CENTRAL AIR DATA COMPUTER
(AIRCRAFT INCORPORATING AFC 793) ................................ CPU-175/A
CENTRAL AIR DATA COMPUTER .................................... CP-11666/A
CHAFF DISPENSING SET. ........................................... AN/ALE-39
JOINT TACTICAL INFORMATION DISTRIBUTION SYSTEM. ............... ANIARQ-107
DIGITAL DATA LINK ............................................. ANIASW-27BlC
ELECTRONIC COUNTERMEASURES SET ............................. AN/AL@165
FUSE FUNCTION CONTROL SET ..................................... ANlAWW-4
GUN CONTROL UNIT .......................................... C-11414/AYQ-15
IFF INTERROGATOR SET. .......................................... ANIAPX-76C
IFF TRANSPONDER SET ......................................... AN/APX-100(V)
lRSTS......................................................~AN/AAS-429XN- 1
MISSILE LAUNCHEWBOL CHAFF DISPENSER ......................... LAU-138AIA
INTERFERENCE BLANKER ......................................... MX-10666/A
MISSILE POWER SUPPLY ............................................ PP-8043/A
PANORAMICCAMERA ................................................. KA-99A
RADAR WARNING SET. ...........................................
SERIAL FRAME CAMERA.
ANIALR-67(V)
.............................................. KS-876
　
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