Hawker Beechcraft Hawker 800XP, Руководство по эксплуатации для пилотов, Страница: 337 / 923

Page 17-10
Section III Sub-section 17
AVIONICS
P/N 140-590032-0007
Revision A4: Sep, 2010
Pilot’s Operating Manual
RADIO SENSOR SYSTEM (RSS)
The Radio Sensor System consists of the radios and controls used for voice communication, navigation
and operation in the Air Traffic Control (ATC) environment.
AUDIO INTEGRATING SYSTEM
The audio integrating system controls the output of the communications and navigation receivers to the
flight crew and airplane speakers.
The system consists of two Audio Control Panels (ACP) which command two digital audio control
amplifiers and an audio interphone amplifier for signal processing. The ACPs also command a
passenger speaker amplifier which provides the Seat Belt and No Smoking sign chime tones and also
allows the flight crew to address the passengers. An aural warning generator is installed which provides
aural warnings to both digital audio control amplifiers.
Audio Control Panel (ACP) Figures 2 and 5
An ACP is installed on the forward area of the pilot and copilot side consoles.
An optional ACP installation is provided, reference Figure 5 on the following page.
The power supply for No. 1 ACP is provided by the PE busbar through the AUDIO 1 CTL circuit breaker.
The power supply for No. 2 ACP is provided by the PS2 busbar through the AUDIO 2 CTL circuit
breaker.
For aircraft with KIT 149-3410 installed, the power supply for No. 1 and No. 2 ACPs are provided by the
PE busbar through the AUDIO 1 CTL and AUDIO 2 CTL circuit breakers.
HF Radio Transmissions
Hawker Beechcraft Corporation considers the following indication fluctuations to be normal and
acceptable providing that the indications return to a normal reading when the HF radio transmission
ceases (the interference should be noted by the Flight Crew, but it is not considered to be detrimental
to flight safety):
• Fuel quantity indications may increase, depending on frequency set and amount of fuel
in the tanks.
• Flight deck or cabin indications/indicators (i.e. oil temperature, oil pressure, flap position,
cabin/duct temperature and OAT, etc.).
• N
1
indications.
• N
2
indications.
• ITT indications.
• Erroneous ELT annunciations, without ELT activation.
• No fluctuations are permitted in navigational indications (i.e. VOR, LOC, GPS, Glide Slope, etc.)
except as permitted in the Airplane Flight Manual Section 2 - LIMITATIONS.