曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
3. ICS -Check.
4. Laodinggearindicatorandtransitionlight-Check.
Check gear position indication down and transition
light off,
5. MASTER TEST switch-check.
Coordinate with RIO.
a. LTS.
ORIGINAL 7-10
NAVAIR Ol-Fl4AAD-1
(6)
(7)
(8)
FUEL QTY - 2,000 +200 Pounds (both
cockpits).
Backup oxygen pressure - 1,800 to
2,100 Psi.
L and R FUEL LOW lights - Illuminated
(both cockpits).
d. MASTER TEST switch - OFF.
6. Ejections eatS AFE/ARMED handles- ARMED.
Verify seat armed with RIO.
7. CANOPY -Clear RIO To Close.
(,,,,,,,I
Flightcrews shall ensure that hands and foreign
objects are clear of front cockpit handholds
and top of ejection seats and canopy
sills to prevent personal injury and/or structural
damage during canopy opening or closing
sequence. Only minimum clearance is
afforded when canopy is transitioning fore
and aft.
Note
If CLOSE does not close the canopy, depress
the grip latch, release and push handle outboard
and forward into BOOST. If it is necessary
to use BOOST, the handle shall be
returned to CLOSE to avoid bleed-off of
pneumatic pressure.
8. LAD/CANOPY light - OFF.
Plane captain shall stow boarding ladder and steps.
9. Inform RIO -Ready To Start.
10. Starter air -ON.
The ECS air source shall remain off during
engine start until external air is disconnected
in order to reduce the possibility of bleed air
duct contamination.
7.43 Engine Start - Pilot. Prior to engine start,
the pilot and plane captain should ascertain that the
turnup area is clear of FOD hazards, adequate tiresuppression
equipment is readily available, and engine
intakes and exhausts are clear. Although the engines
cannot be started simultaneously, either can be started
fmt. The following procedure establishes starting the
right engine first. Whenever possible the aircraft should
be positioned so as to avoid tailwinds, which can increase
the probability of hot starts.
pi&-(
Coordinate movement of any external surfaces
and equipment with the plane captain
or director.
If engine chugs and/or rpm hangup is encountered
with one engine turning during
normal ground start, monitor EGT for
possiblehot start. AIRSOURCEpuahbutton
should be set for the operating engine
until ‘pm stabilizes at idle; then set to
BOTH ENG.
To prevent possible engine overtemperature
during crossbleed start attempts, select
the operating engine for air soume and
retam to BOTH ENG after rpm stabilizes
at idle or above.
1. ENG CRANK switch - L (left engine).
2. ENG CRANK switch -OFF.
3. ENG CRANK SWITCH - R (right engine).
4. ENG CRANK SWITCH - OFF.
5. EMERG FLT HYD switch -Cycle.
a. EMERG FLT HYD switch - LOW.
Check that ON flag is displayed in EMER FLT
LOW hydraulic pressure window. Verify control
over horizontal tail and rudder control surfaces
as viewed on surface position indicator.
7-11 ORIGINAL
NAVAIR 01-Fl4AAD-1
b. EMERG FLT HYB switch-HIGH.
Check that ON flag is displayed in EMER FLT
HI hydraulic pressure window. Verify control
over empennage flight control surfaces and
higher surface deflection rate.
c. EMERG FLT HYD switch -AUTO (LOW).
Check that OFF flags are displayed in both
EMER FLT HI and LOW hydraulic pressure
windows.
Combined and brake accumulators should be
charged prior to backup module checks.
Checks should be made slowly enough to
ensure continuous ON indication in the hydraulic
pressure indicator and to prevent
damage to the pump or motor.
Note
Ensure combined and flight hydraulic pressures
are zero prior to testing emergency
flight hydraulic system to allow proper check
I of 300-psi priority valve.
6. ENG CRANK switch - R (right engine).
Place the crank switch to the R position where the
switch is solenoid held until automatically released
to the neutral (OFF) position at the starter
cutout speed of approximately 49- to 5 1 -percent
‘pm. Manual deselect of the switch to OFF will
interrupt the crank mode at any point in the start
cycle. Oil pressure and flight hydraulic pressure
rise will become evident at 20-percent rpm.
If no oil pressure or hydraulic pressure is
indicated, start shall be aborted by setting
ENG CRANK switch to OFF.
Ifthe ENG CRANK switch does not automatically
return to the OFF position by
SO-percent‘p m during start, ensure that
the ENG CRANK switch is offprior to 60-
percent ‘pm to prevent starter overspeed.
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
F-14D 飞行手册 Flight Manual 2(18)
