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system fluid in the system return line,
and essential dc No. 2 electrical power. Extension
of the in-flight refueling probe requires
approximately 25 cycles of the pump
handle.
14.11.2 Flight Pressure Approximately 2,400
to 2,600 Psi
1 WARNING 1
If hammering (cavitation) is experienced in
the hydraulic system, component rupture is
imminent. Turn the hydraulic pump switch
(BIDI) OFF.
1. Wing sweep - Set at 20”,
2. R INLET RAMPS switch - STOW (less than 1.2
Mach).
3. Right AICS cb - Pull (LGI).
NAVAIR Ol-Fl4AAD-1
4. R INLET RAMPS switch-AUTO.
5. EMERG FLT HYD switch - HIGH (on final,
committed to landing).
Monitor remaining hydraulic system pressure
since the MASTER CAUTION and
HYD PRESS lights will not illuminate if the
remaining systems fail.
The following important equipment is inoperative:
a. NORMAL HOOK - Restored by weight on
wheels. Hook handle restowed.
Note
Arrested landing will require emergency
hook extension.
6. Land as soon as possible.
14.11.3 Combined Pressure Zero
1. HYD ISOL switch - FLT.
2. HYD TRANSFER PUMP switch - SHUTOFF.
3. REFUEL PROBE - EXTD (in CV environment).
4. Wing sweep - Set at 20”.
5. EMERG FLT HYD switch-LOW.
piil
Ifthe INLET RAMPS switch is not placed
in STOW prior to the pressure reaching
zero, do not place it in STOW after complete
loss of pressure. Trapped fluid may
be the only thing holding the affected
ramp in position.
l An outboard spoiler module failure with
flaps extended,b elow 180k nots, and with
a combined hydraulic failure rendering
the inboard spoilers inoperative, can result
in asymmetric spoiler float such that the
aircraft may not be flyable at normal approach
airspeeds. A small amount of
spoiler float can significantly increase appreach
speeds.
l Do not return to AUTO (LOW) mode
once module is selected on (HIGH or
LOW) with operating flight hydraulic system.
When operated in conjunction with
zero combined pressure, some backup
module fluid will be expelled by thermal
expansion. The module will remain fully
serviced and operate normally as long as
elevated temperatures are maintained.
Once operating, the module should not be
tmned off in flight without combined system
pressure available to reservice it. Doing
so would result in fluid contraction
and an underservicedc ondition that could
prevent subsequenpt ump operation.
l Loss of combined pressure with landing
flaps down may allow the auxiliary flaps to
cycle,c ausingm oderatep itch oscillations.
l Monitorremaininghydraulicsystempressure
since the MASTER CAUTION and
HYD PRESS lights will not illuminate if
the remaining systems fail.
The following important equipment is inoperative:
a. LAICS
b. Nosewheel steering
c. Gun drive
d. Inboard spoilers
e. Hook extend( emergencya ctuationa vailable)
f. Flaps and slats( emergencya ctuationa vailable)
g. Landing gear (emergency actuation available)
h. Wheelbrakcs (emergency actuation available)
i. Refueling probe (emergency actuation available
if fluid remains in return line)
j. Emergency generator
k. Auxiliary flaps
I. DLC
ORIGINAL 14-32
m. Speedbrakes
n. Normal hook.
6. Hook - EMERG DN.
7. EMERG FLT HYD switch - HIGH (on final
committed to landing).
8. LDG GEAR handle - EMERG DN.
9. AUX FLAP/FLAP CONTR cb - Pull (8G3).
10. Flaps (no awiliq flaps) - DN.
11. Brake accumulator (handpump) - Check.
12. ANTI SKID SPOILER BK switch -SPOILER
BK (OFF for CV).
13. Make arrested landing as soon as possible.
After landing:
14. Do not taxi out of arresting gear.
15. Engines - OFF.
14.11.4 Flight Pressure Zero
1. HYD TRANSFER PUMP switch - SHUTOFF.
2. Wing sweep - Set at 20’.
3. EMERG FLT HYD switch-LOW.
pik-)
If the INLET RAMPS switch was not placed
in STOW prior to pressure reaching zero, do
not place it in stow after complete loss of
pressure.T rappedf luid may bet he only thing
holding the affected ramp in position.
H
Monitor remaining hydraulic system pressure
since the MASTER CAUTION and
HYD PRESS lights will not illuminate ifthe
remaining systems fail.
The following important equipment is inoperative:
a. ACLS
NAVAIR Ol-F14AAD.1
b. RAICS
c. Normal hook-Restored by weight on wheels.
Hook handle restowed.
4. EMERG FLT HYD switch - HIGH (on final,
committed to landing).
5. Land as soon as possible.
　
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本文鏈接地址：F-14D 飛行手冊 Flight Manual 2(116)