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时间:2010-04-25 14:37来源:蓝天飞行翻译 作者:admin
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Entry Switch Panel Forward LH Cabinet
PAX CTRLS (Copilot's CB
Panel) CABIN (Pilot's CB
Panel)
Lighting Control Units (LCU) LH Side Ledge
PAX CTRLS (Copilot's CB
Panel)
L SPOT (Pilot's CB Panel)
Lighting Control Units (LCU) RH Side Ledge
PAX CTRLS (Copilot's CB
Panel)
R SPOT (Copilot's CB Panel)
Speaker (Mid-range/tweeter) Convenience Panels N/A
Speaker (Subwoofer) Cabin Floor N/A
Pilot’s Manual
7-30 PM-132A
FLIGHT PHONE
Digital Airborne Telephone (Optional)
The optional Magnastar C2000 is a two voice/data system that has
direct dialing, multiple calls, fax/data modem, uplink calls, interfone,
speed dialing and call charging features. Handsets are installed in both
the cockpit and the passenger compartment.
The passenger compartment handset can be located in any of the cabin
armrest storage boxes. The handset in the cockpit is located on the aft
end of the center pedestal.
Power for the flight phone is 28-vdc through the 10-amp FLT PHONE
circuit breaker on the pilot’s circuit breaker panel.
AC ELECTRICAL OUTLETS (Optional)
Four optional 110-vac/60-Hz electrical outlets may be installed in the
cabin. One of the outlets is located in the galley cabinet. Two of the
outlets are located in the passenger compartment lower sidewall (one
on the right side and one on the left side) between the facing passenger
seats. The 110-vac outlets have a 1200-va capacity. The fourth outlet is
equipped with a Ground Fault Interrupt (GFI) circuit which, if tripped,
may be reset. This outlet is installed across from the lavatory in the cabin
stowage area at the floor. The GFI outlet can be reset by depressing
the TEST/RESET button. The inverters powering these outlets will automatically
shut down if the cabin altitude goes above 9500 feet. Power
will be restored when the cabin altitude descends below 8300 feet.
A 230-vac/50-Hz circuit is available, as an option, for aircraft which
will be used primarily overseas.
WINDOW SHADES
Each cabin window is equipped with a window shade. The shades are
adjustable and can be raised and lowered to any desired level. The
shades are made of pleated translucent material and may allow some
light in.
GASPER OUTLETS
Individual gasper outlets (air outlets) are located in the cabin overhead
convenience panels. The outlets are adjacent to the lights and can be
turned to approximately 40° around its center to direct airflow as
desired. Rotate the conical port counterclockwise to open the outlet and
clockwise to close.
Pilot’s Manual
PM-132A 7-31
AFT CABIN STOWAGE COMPARTMENT
The aft cabin stowage compartment is located on the left side of the
aircraft immediately aft of the passenger compartment. The stowage
compartment is equipped with a coat rod for hanging garments and a
restraining web. Some interiors are equipped with a fire extinguisher
which is mounted to the left partition.
LAVATORY/VANITY
The standard lavatory/vanity (Figure 7-11) is equipped with a toilet, a
vanity counter, a toilet tissue drawer and a trash/storage drawer.
Optional equipment for the standard vanity includes a belted toilet
with a life vest, a lighted vanity mirror and a wash basin with warm
running water plumbed to an overboard heated drain.
The lavatory is separated from the passenger cabin by sliding doors
which stow inside the left and right sides of the partition. The doors do
not lock and are equipped with a magnetic strip which holds them
together while closed. The toilet is located on the right side of the
lavatory compartment. The toilet is flushed by depressing the toilet
FLUSH switch, located in the lavatory switch panel on the forward side
of the toilet. The sink is located at the aft end of the lavatory. The water
faucet is operated by depressing the PUMP switch located on the lavatory
switch panel adjacent to the basin to dispense running water. Water
in the basin is drained by depressing the DRAIN button which is
also on the lavatory switch panel.
If equipped with the optional sink, the lavatory/vanity will have a
potable water tank and pump located under the vanity counter. The
potable water tank (with an internal heater) holds approximately
1.5 gallons of 100° F heated water. The pump and tank (with heater)
draw electrical power from the 15-amp LAV SINK circuit breaker located
on the pilot’s circuit breaker panel. The lavatory sink is drained
through a heated drain mast on the bottom of the aircraft. The heater
prevents ice from forming in the drain mast.
Pilot’s Manual
7-32 PM-132A
LAVATORY/VANITY (TYPICAL)
 
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