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NAVAIR Ol-Fl4AAD-1
Individual flight briefings will include all applicable
items outlined above, with particular emphasis on
weather and bingo fuel.
8.7.2 Preflight. In addition to normal cockpit preflight,
ensure that external light switches are properly
positioned for poststart light check. Install night filters
on applicable cockpit displays.
8.7.3 Postetart. Adjust cockpit light to desired
brightness. When ready for taxi, indicate with appropriate
signal.
8.7.4 Taxi. Night deck-handling operations are ofnecessity
slower than those used during the day. When a
doubt arises as to the meaning of a signal from a taxi
director, stop.
8.7.5 Catapult Hookup (Night). Procedures for aircraA
catapult hookup at night are identical to those used
during day operations. However, it is difftcult to determine
your speed or degree of motion over the deck. The
pilot must rely upon, and follow closely, the plane director
signals.
8.7.6 Catapult Launch. On turnup signal from the
catapult officer, ensure throttles in MIL and check all
instruments. When ready for launch, place external light
master switch ON (bright and steady). After launch,
establisha n 8” to 10” pitch attitude, cross-checkingin -
struments to ensure a positive rate of climb. Retract the
landing gear. An altitude of 500 feet is considered to be
minimum altitude for retraction of flaps. When well
established in a climb, switch lights to flashing or as
applicable for an instrument climbout. The standby
indicator should be used in the event of a primary
display(s) malfunction.
If wings sweep back inadvertently, close attention
should be paid to maintaining positive
rates of climb. The loss of lift incurred
by premature wing sweep aft can result in
significantly decreasedr ates of climb, with
very little change in pitch attitude and trim
requirements.
8.7.7 Catapult Abort Procedures (Night). The pilot
no-go signal for night launches will be to not turn on
the exterior lights, and to transmit on land or launch his
aircraft side number, the catapult the aircraft is on, and
the words “Suspend, Suspend.” After the catapult is
untensioned,t he catapult offtcer will signal to raise the
a-11 ORIGINAL
NAVAIR Ol-F14AAD-1
launch bar. The pilot shall ensure that the throttles are
seated in the catapult detent or throttle friction is full
forwardbefore raisingthe launch bar with the LAUNCH
BAR ABORT switch. When the launch bar is clear of
the shuttle, the catapult officer will move the shuttle
forward of the aircraft launch bar. At this point the aircraft
is no longer in danger ofbeing launched. The catapult
offricer will signal the pilot to lower the launch bar
and then step in front of the aircraft and signal the pilot
to throttle back.
If the aircraft is down aRer the go signal is
given, transmit the words “Suspend, Suspend”;
however, the flightcrew should be
prepared for the catapult stroke and to perform
emergency procedures if required.
l If the aircraft is down prior to it being
pushed or pulled back for release from the
holdback fitting and when directed by the
catapult launching officer, the launch bar
shall be raised by the LAUNCH BAR
ABORT switch.
l Unkneelingt he nosegeawr hile the launch
bar is in the catapult track or shuttle will
damagethelaunchbarlinkageandbtmgees.
The pilot should unkneel the aircraft only
when sure that the launch bar is free to rise
and upon signal from the catapult officer
or taxi director.
8.7.8 Arrested Landing and Exit From Landing
Area (Night). During approach, all lights shall be on
bright and steady. At the end of arrestment rollout, turn
off external lights and follow the director’s signals while
effecting the normal aircraft cleanup procedures.
ORIGINAL 8-12
NAVAIR 01-Fl4AAD-1
CHAPTER 9
Special Procedures
9.1 IN-FLIGHT REFUELING PROCEDURES
Note
Before commencing in-flight refueling operations,
each flight crewmember shall become
familiar with the NATOPS Air
Refueling Manual, NAVAIR OO-80T-110,
and in-flight refueling system description.
9.1.1 In-Flight Refueling Controls. Regardless
of fuelmanagementpanesl witchpositioning, at low fuel
states the initial resupply of fuel is discharged into the
left- and right-wing box tanks. Thereafter, distribution
of the fuel to the forward, aft, wing, and external tanks
is controlled by the WfNG/EXT TRANS switch position.
The split refueling system to the left and right
engine feed group provides for a relatively balanced
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F-14D 飞行手册 Flight Manual 2(42)
