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OPERATING MANUAL
PRODUCTION AIRCRAFT SYSTEMS 2A-26-00
Page 1
January 31/02
Revision 6
(a) SPZ-8000 equipped aircraft:
• Red SMOKE DETECT warning message on CAS
• Red SMOKE DETECT warning message on Standby
Warning Lights Panel (SWLP)
• Red BAG COMPT SMOKE annunciator illuminating
above copilot’s NAV display (Figure 1)
(b) SPZ-8400 equipped aircraft:
• Red AFT BAG SMOKE warning message on CAS
• Red SMOKE DETECT warning message on SWLP (if
installed)
(2) Other Smoke Detector Annunciations:
(a) On SPZ-8400 equipped aircraft, a red FWD LAV SMOKE
DETECT warning message is displayed on CAS if the
forward smoke detector detects smoke in the forward
lavatory / radio rack area.
(b) On SPZ-8000 and SPZ-8400 equipped aircraft with ASC 415
incorporated, and airplanes SN 1390 and subsequent, a red
RADIO RACK SMOKE warning message is displayed on
CAS if the forward smoke detector detects smoke in the radio
rack area. This CAS message is accompanied by a red
SMOKE DETECT warning message on the SWLP (if
installed).
(3) Smoke Detector Test Switch:
A test switch, labeled SMOKE DET TEST and shown in Figure 2, is
provided to test the smoke detection system. The location and type
of switch (pushbutton on center pedestal or toggle switch on
copilot’s console) depends on production serial number of the
aircraft and operator preference during outfitting. Provided Essential
DC bus power is available, selection of the TEST function results in
the annunciations listed in (1).
B. Smoke Evacuation System:
Aircraft having ASC 18 (CAA Aircraft); SN 1000 through 1155
(excluding SN 1034) having ASC 157; SN 1034; SN 1156 and
subsequent: Rotation of the emergency smoke evacuation valve handle
(Figure 3) to the EVAC SMOKE position allows deflation of the baggage
compartment door seal. With the door seal deflated, pressurized cabin air
escapes around the door frame, drawing with it any smoke. Cabin altitude
will climb accordingly. When smoke ceases, rotation of the valve handle to
NORMAL OPS allows the door seal to reinflate.
Aircraft not having ASC 18; SN 1000 through 1155 (excluding SN
1034) not having ASC 157: Rotation of the baggage compartment door
handle 45°, without opening the door, depressurizes the baggage
compartment door seal.
OPERATING MANUAL
2A-26-00 PRODUCTION AIRCRAFT SYSTEMS
Page 2
January 31/02
Revision 6
3. Controls and Indications:
A. Circuit Breakers (CBs):
Circuit Breaker Name: CB Panel: Location: Power Source:
SMOKE DET CP E-14 ESS DC Bus
B. Messages and Annunciations:
CAS Message: SWLP Indication Cause or Meaning:
AFT BAG SMOKE (1) SMOKE DETECT Smoke detected in aft baggage
compartment.
FWD LAV SMOKE
DETECT (1)
None Smoke detected in forward
lavatory area or radio rack area.
RADIO RACK SMOKE
(2)
SMOKE DETECT Smoke detected in radio rack
area.
SMOKE DETECT SMOKE DETECT Smoke detected in area
illuminated by annunciation.
NOTE(S):
(1) For SPZ-8400 equipped airplanes.
(2) For SPZ-8000 and SPZ-8400 equipped airplanes with ASC 415, and
airplanes SN 1390 and subsequent.
Annunciation: Cause or Meaning:
Red BAG COMPT SMOKE light above
copilot’s NAV display. (1)
Smoke detected in aft baggage
compartment.
NOTE(S):
(1) For SPZ-8000 equipped aircraft.
4. Limitations:
There are no limitations established for this system as of this revision.
OPERATING MANUAL
PRODUCTION AIRCRAFT SYSTEMS 2A-26-00
Page 3
January 31/02
Revision 6
Baggage Compartment Smoke Annunciator
Figure 1
OPERATING MANUAL
2A-26-00 PRODUCTION AIRCRAFT SYSTEMS
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January 31/02
Revision 6
Smoke Detector System TEST Switch
Figure 2
OPERATING MANUAL
PRODUCTION AIRCRAFT SYSTEMS 2A-26-00
Page 5
January 31/02
Revision 6
Emergency Smoke Evacuation Valve
Figure 3
OPERATING MANUAL
2A-26-00 PRODUCTION AIRCRAFT SYSTEMS
Page 6
January 31/02
Revision 6

　
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