Navair F-14B, Emergency Procedure Tabs

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NAVAIR 01-F14AAP-1B
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306
Do not overservice oil storage tank. Overserv-
icing can cause scavenge pump failure and
subsequent engine failure.
Note
Engine oil quantity must be checked within 30
minutes after engine shutdown, otherwise, run
engine at 80 percent rpm or greater for 10 min-
utes to ensure proper servicing.
INTEGRATED DRIVE GENERATOR
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 fill port on the right side. To obtain a
valid fluid level check, the sight gauge must be checked no
sooner than 5 minutes and no later than 60 minutes after
shutdown.
HYDRAULIC SYSTEMS
Hydraulic servicing is required on the flight and combined sys-
tems, outboard spoiler backup module, main landing gear,
nosewheel shock struts, and arresting hook dashpot. A hydrau-
lic pressure filling cart is required to service the systems with
fluid and an air-nitrogen cart to preload the reservoirs. The tem-
perature recording gauge in the flight and combined systems
indicates the maximum temperature attained by the hydraulic
fluid.
PNEUMATIC SYSTEMS
Pneumatic servicing is required for normal operations of the
canopy, emergency landing gear extension, auxiliary canopy
opening, both hydraulic systems, servicing panels, brake sys-
tems, and arresting hook.
290 Change 2