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Figure 3-2. Aircraft Servicing Data (Sheet 2 of 2)
3-3 ORIGINAL
NAVAIR O1-FlUAD-1
Ensure that both the fueling unit and the aircrafi
are properly grounded, bonding cable is
connected between aircraft and refueling
source, and that fue extinguishing equipment
is readily available.
During ground refueling operations, the
direct-reading vent pressure indicator shall
be observed and refueling stopped ifpressure
indication is in the red band (above 4 psi).
Note
l If the aircraft is being regularly serviced
with JP-4 type fuel, the main fuel-control,
fuel-grade (specific gravity adjustment)
selector on each engine should be reset to
the IP-4 position, If the aircraft is being
regularly serviced with JP-8 or JP-5 fuel,
the fuel-control, fuel-grade (speciticgravity
adjustment) selector on each engine
should be reset to the JP-8 or JP-5 position.
Satisfactory engine performance depends
upon trimming of the engine fuel
controls to ensure rated thrust, to prevent
exceeding engine temperature limits, and
to ensure airflow compatibility with the
air inlet duct opening.
l Removal of JP-8 type fuel from the aircraft
is not required before refueling with
JP-5. If removal of JP-8 from the aircraft
aboard ship is necessary, it shall not be
defueled into the storage tanks containing
JP-5.
3.1.2 Engine Oil. Engine oil level is proper when
overflow oil starts to exit the discharge port during servicing.
For normal servicing, the sight gauge on the oil
storage tank is the primary indicator determining when
servicing is required. During servicing, overflow oil exits
the overflow dischargep ort when the tank is properly
serviced (Figure 3-3, sheet 2). Servicing is accomplished
using PON-6 servicing cart. Normal oil consumption
is 0.03 gallon per hour with the maximum
being 0.1 gallon per hour. For oil servicing procedures,
refer to NAVAIR Ol-F14AAD-2-1. The protrusion of a
bypass indicator underneath the oil scavenge pump indicates
a clogged filter element and requires replacement.
l Lubricating oil (MIL-L-23699) is toxic
and flammable. Protection includes
chemical splashproof goggles, gloves,
and good ventilation; keep sparks, flames,
and heat away. Keep lubricating oil off
skin, eyes, and clothes; do not breathe
vapors. Wash hands thoroughly after
handling.
l Do not overservice oil storage tank.
Overservicing can cause scavenge pump
failure and subsequenet ngine failure.
Note
Engine oil level should be checked within 30
minutes of engine shutdown, otherwise run
engine at 80 percent or greater for 10 minutes
to ensure proper servicing.
3.1.3 Integrated Drive Generator Oil. The IDG
has a filter bypass indicator at the bottom of the
filter bowl (Figure 3-3, sheet 2). Extension of the
indicator indicates contamination of the filter and the
need for filter element replacement. Refer to NAVAIR
Ol-F14AAD-2-1 for IDG oil filter replacement and
servicing.
IDG oil level is checked at the IDG mounted on the
forward right side of the forward accessory gearbox of
each engine. It is serviced at the pressure till port on the
right side.
3.1.4 Hydraulic Systems. The main hydraulic
systems are serviced at the flight and combined hydraulic
system ground servicing panels. A hydraulic pressure
filling cart is required to service the systems with fluid,
and an air-nitrogen cart is required to preload the reservoirs.
The outboard spoiler backup module is serviced
at the servicing panel on the outboard nacelle of the port
engine. Additional hydraulic servicing is required at the
main landing gear shock strut (Figure 3-3, sheet 2), the
nosewheel shock strut (Figure 3-3, sheet 2), and the
arresting hook dashpot (Figure 3-3, sheet 1).
The flight reservoir fill and ground hydraulic power
accessp anel and the flight system filter module (Figure
3-3, sheet 1) are on the starboard side. The combined
hydraulic system reservoir till and filter module (Figure
3-3, sheet 3)areontheportsideoftheaircratLIndication
of hydraulicsystem thtidcontaminationcanbedetected
by the position of the buttons on the Delta-P type filter
units.
ORIGINAL 3-4
NAVAIR 01.Fl4AAD-1
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Figure 3-3. Aircraft Servicing (Sheet 2 of 3)
ORIGINAL 3-6
NAVAIR 0%Fi4AAD1
Figure 3-3. Aircraft Servicing (Sheet 3 of 3)
3-7 ORIGINAL
NAVAIR 01-Fl4AAD-1
Temperature recording gauges at the filter modules
indicate the maximum temperature attained by the hydraulic
fluid during the last tumup or flight. After a
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