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600 fpm. Emergency jettison of stores may
be required to establish adequate rate of
climb.
3. Wing-sweep angle greater than 35” - Not
permitted.
4.10 CENTER OF GRAVITY POSITION LIMITS
Unless otherwise stated, the following cg limits
1. Field takeoff and emergency landing (minimum
rate of descent only) - 72,000 pounds.
apply:
2. Field landings - 60,000 pounds,
Maximum Maximum
store Configurations Forward Aft
3. Field carrier landing practice or carrier landings
- 54,000 pounds.
a. Landing approachest o touchdown should not
exceed 17 units AOA to avoid nozzle/ventral
tin damage.
1 ;;i;2c, 2c,-4 r3% MAC j 18.5% MAC
IBl, 182, lC, TARPS, 6.3% MAC 17.5% MAC
All other
configurations
6.3% MAC 17.0% MAC
b. Only minimum descent rate landings are permittedwhilecarrying
AIM-7E/F and/orAIM-9
on the multipurpose pylon, or AIM-7E/F mis-
4-17 ORIGINAL
NAVAIR Ol-F14AAD.1
Throughout these flight operating limits, all cg positions
are quoted at the following reference conditions:
1. Zero fuel gross weight (includes weight of stores
carried on flight).
2. Wing-sweep angle = 20”.
3. Landing gear and flaps extended.
1 WARNING 1
The aft cg limit will be exceeded if all stations
are configured for AIM-54 missiles or
Mk 83/84 bombs and only stations 4 and 5
are loaded or remain as a result of tiring,
dropping, or jettison of stations 1, 3, 6, and
8. If the aft cg limit is exceeded, airspeed/
AOA control may be difftcult. Fuel states of
5,000 to 6,000 pounds result in the most favorable
cg position. Slightly aft wing- sweep
positions of 25” to 30° will move the neutral
point aft and should restore normal longitudinal
stability.
4.11 EXTERNAL STORES AND GUN LIMITS
4.11.1 280-Gallon External Fuel Tank Limits
1. Catapult launch with a partially tilled external
tank is not authorized because of surge load
considerations.
2. Carriage of external tanks not incorporating AYC
598 is limited to 300 KCAS/0.72 TMN.
1 WARNING 1
CV arrestment, CV touch and go, or normal
field landings with full or partial fuel in the
external tanks is not authorized because of
overload of the nacelle backup structure.
Only minimum descent rate landings are
authorized.
Dive angles in excess of 10“ nose down with
900 pounds or more fuel in an external tank
will result in fuel venting (dumping).
4.11.2 External Baggage Container (CNU-
188/A). The external baggage container (blivet) may
be carried on station 4 or 5 with all loadings authorized
fortheTARPSpod(Figure4-11). Simultaneouscarriage
of a blivet and a TARPS pod or hvo blivets is not authorized.
The blivet must be configured with a long tail cone
and no fins.
1. Maximum airspeed - 520 KCASI0.90 TMN.
2. Acceleration limit - LBA.
3. AOA limit - Figure 4-7.
4. Jettison - Not authorized.
5. Carrier operations - Authorized.
6. Maximum load:
200 pounds maximum - forward shelf
150 pounds maximum - aft shelf
350 pounds total.
4.11.3 Gun Burst Limits
1. Burst limit - 200 rounds.
If two consecutive 200-round bursts are tired, a 30-
second cooldown period is required.
4.11.4 Launch Limits. Maximum flight conditions
for launch of external stores are listed in the following
paragraphs.
4.11.4.1 AIM-7FIM
Note
Missiles with K-9 autopilot are identified by
a segmented black line under the missile serial
number or letters “POP” after the serial
number.
1. Stations 1B and 8B - Vmin to 1.3 Th4N, all
altitudes, +lg to limits of basic aircratt for nonzero
bank angles and limits of basic aircraft for
zero bank angle.
2. Stations 3 and 6 - Vmin to Vmax for Og to +2g,
Vmin to 1.4 TMN for +2g to +4g, and Vmia to 1.2
TMN greater than +4g, all altitudes, +lg to limits
of basic aircraft for non-zero bank angles and Og
to limits ofbasic aircraft for zero bank angle.
ORIGINAL 4-18
3. Station 4 - Vmin to 0.9 TMN for less than
15,000 feet MSL for Og to +Ig, Vmin to Vm,
greater than 15,000 feet MSL for Og to +lg, and
Vmin to vma~ greater than +lg, all altitudes, +lg
to limits of basic aircraft for non-zero bank angles,
and Og to limits of basic aircraft for zero bank
angle.
4. Station 5 - Vmin to 650 KCAS less than 30,000
feet MSL for Og to +l g, Vmia to Vm, greater than
30,000 feet MSL for Og to +lg, and Vmin to Vma
greaterthan+Ig,allaltitudes,+lgtolimitsofbasic
for non-zero bank angles, and Og to limits of basic
aircraft for zero bank angle.
　
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