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Oil Pressure
1. Throttle (affected engine) - IDLE.
If oil pressure is below 15 psi, above 65 psi, or engine
vibration:
If shutdown is feasible:
2. Throttle (affected engine) - OFF.
3. Refer to Single-Engine Cruise Operations, paragraph
14.5.3.2.
If shutdown is not feasible:
2. Rpm - Set Miimum Rpm.
3. Avoid high-g or large throttle movements.
4. Land as soon as practicable.
14.5.13.2 L or R OIL HOT Light
Illumination of an OIL HOT caution light
may be an indication of above normal gearbox
scavenge oil temperature or high supply
temperature. Continuous engine operation
will result in reduced gearbox life and lubrication
degradation.
Note
On deck OIL HOT light may be caused by
underservicing or by excessive temperature
on deck In the event of OIL HOT light on
deck position throttles to OFF.
1. Oil pressure - Check
2. Throttle (affected engine) - 85-Percent Rpm.
3. If after 1 minute light is still illuminated, throttle
- OFF.
4. Land as soon as practicable.
5. Refer to Single-Engine Cruise Operations, paragraph
14.5.3.2.
6. Relight engine for landing, if necessary.
14.5.14 RATS Operation In Flight
1. Tailhook- DOWN.
If conditions permit:
2. ANTI ICE CONTR HOOK CONTiWSHLD/AIR
cb -Pull (8C2).
. Pulling the ANTI ICE CONTR HOOK
CONT/WSHLD/AIR cb (8C2) disables
RATS. Inform CV of increased windover-
deck requirements and gross weight
settings for a non-RATS arrestment.
. With the circuit breaker in and RATS operating,
there is reduced thrust available
for approach and use of afterburner may
be required to arrest sink rate.
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ANTI ICE CONTR HOOK CONT/
WSHLD/AIR circuit breaker (8C2) must be
in prior to hook transition. Avoid icing conditions
and rain with circuit breaker pulled.
Note
IfRATS securesw hen the hook is raisedwith
no other weight-on-wheels indication, failure
is internal to the RATS circuitty.
14.6 FUEL SYSTEM MALFUNCTIONS
14.6.1 Fuel Pressure Caution Lights. Afterburner
operations place an extreme demand on the engine the1
feed system. Aircraft maneuvers in the zero to negative
0.5g flight regime aggravate the effect and may generate
a situation where afterburnerb lowout and enginef lameout
occur. The first indication of this condition may be
a fuel pressure light.
14.6.1.1 L and/or R FUEL PRESS Light(s) On
1. Both throttles - MIL Power or Less.
2. Restore aircraft to l.Og flight.
If both lights remain on:
3. Increase positive g’s to greater than l.Og.
4. Descend below 25,000 feet.
5. Maintain cruise power settings or less.
6. Land as soon as possible.
ORIGINAL 14-18
Illumination of both lights may be indicative
of a total motive-flow failure. Zeroor
negative-g flight should be avoided.
Complete loss of motive flow will result
in the sump tank interconnect and the engine
feedcrossfeedvalveremaining in the
closed position, isolating the forward and
aft systems. Consequently, single-engine
operation will cause fuel on the opposite
side to be unavailable.
If one light remains on:
3. No afterburner above 15,000 feet.
4. Fuel distribution - Monitor (balance if required).
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If the sump tank interconnect valve has
failed, selecting AFT or FWD on the fuel
feed switch could result in fuel migration to
the inoperative side. If fuel migration occurs
after selecting AFT or FWD on the feed
switch (as indicated by a lOO- to 300-pound
per minute increase on the inoperative side),
immediately return the feed switch to
NORM.
5. Land as soon as practicable.
14.6.2 L or R FUEL LOW Light
1. DUMP switch - OFF.
2. Fuel distribution - Check (balance if required).
If wing and/or external fuel remaining:
3. WMG/EXT TRANS switch - ORIDE.
4. Land as soon as practicable.
14.6.3 Fuel Transfer Failures
14.6.3.1 Wing Fuel Does Not Transfer
1. WMG/EXT TRANS switch - ORIDE.
One wing still does not transfer:
2. FEED switch - Select High Fuselage Tape Side.
If wing fuel does not decrease after 2 minutes or wing
fuel transfer complete:
3. FEED switch -NORM.
14.6.3.2 External Tanks Fail To Transfer or
Transfer Slowly
1. WING/EXT TRANS switch - ORIDE.
If fuel continues to transfer improperly or does not
transfer:
2. REFUEL PROBE switch - All Extend, Then
Retract.
3. Apply cyclic positive or negative g’s.
4. AIR SOURCE pushbutton-OFF Then ON (below
35,000 feet, less than 300 knots).
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CV arrestment, CV touch and go, or normal
　
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