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The CAIMS is comprised of the following components:
· PMAT (located in the cabin)
POWER HARD
DRIVE
FAULT OVER
TEMP
Power Switch Mode /Fault
Annunciation
CD ROM Drive
Access Port
3.5" Disk Drive
Access Port
Active Faults page 1 / 3
Current Leg # Date ACSN Time
1 30 Jul 97 278 1530
49 − 61 Controller (FADEC)
Internal Fault
73 − 00 Engine Fuel and Control
77 − 00 Engine Indicating
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GF0310_021
· DATA UPLOAD/DOWNLOAD switch and PRINT MAINT REPORT switch (on airplanes with
SB 70045001
incorporated) (located on bulkhead behind pilot).
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 2
03−10−23
CENTRAL AIRCRAFT INFORMATION AND MAINTENANCE SYSTEM (CAIMS) (CONT'D)
GF0310_022
CAIMS PRINT MAINT REPORT SWITCH
(On airplanes with SB 700−45−001 incorporated)
Used to get a report of active faults from the cockpit printer.
Data Selector Switch
Used to select system to
upload/download a copy
of nonvolatile
data on to
a 3.5 inch disk.
PRINT MAINT
REPORT
DATA
UPLOAD/DOWNLOAD
DAU 1A
DAU 1B
DAU 2A
DAU 2B
DAU 3A
DAU 3B
DAU 4A
DAU 4B
IRS 1
IRS 2
IRS 3
WX
SPARE
IAC 1
IAC 2
IAC 3
GPWS
SATCOM SDU
CABIN COMM
GPS 1
GPS 2
ADC 1
ADC 2
ADC 3
· Pilot Event Marker (located on the landing gear control panel).
GF0310_023
FDR/CAIMS Event Button
Used to store information in
Line Replaceable Units
(LRUs), which report to CAIMS.
Landing Gear Control Panel
NOSE STEER LDG GEAR
HORN PILOT
EVENT
MUTED
AURAL AND VISUAL WARNINGS
Flight Crew Operating Manual REV 41, Jul 08, 2004
CSP 700−6
Volume 2
03−10−24
FLIGHT DATA RECORDER
EICAS channels aircraft systems data (including altitude, airspeed, heading, acceleration and radio
communications events) to the Flight Data Recorder (FDR). DAU 4B gathers sensor data for
transmission to the FDR.
DAU 4 is fully selfmonitoring
and provides CAS messages in the event of a failure. If DAU 4B
channel fails, FDR information is not available.
To record an additional event, in the FDR push the PILOT EVENT button on landing gear control
panel, located on the pedestal. Pushing the PILOT EVENT will also encode the Central Aircraft
Information Maintenance System (CAIMS).
GF0310_024
Landing Gear Control Panel
FDR/CAIMS
Event Button
NOSE STEER LDG GEAR
HORN PILOT
EVENT
MUTED
STALL WARNING
Warning of an impending stall is provided by independent stall protection systems. Both systems are
energized in flight and deactivated on the ground through air/ground logic. The flight displays indicate
airplane approach to stall speed by low speed cues (red band) and a TBD VS indicator on the
primary flight displays (PFDs) airspeed tape.
Stall warnings are provided by an aural “STALL”, a STALL icon appears on the PFD and vibration of
both control columns. If the airplane angleofattack
continues to increase, a stick pusher then
pushes the control column forward to prevent further development of a stall. For more information
refer to Chapter 10, FLIGHT CONTROLS.
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 2
03−10−25
TAKE-OFF CONFIGURATION WARNINGS
Takeoff
configuration warnings are armed when the airplane is on the ground and both engines are
accelerated towards takeoff
thrust (throttle position ³ 30°). A voice warning, EICAS warning
message, and both MASTER WARNING lights come on for any of the following:
Condition Voice Message EICAS Message
Aileron trim outside of takeoff
range
“NO TAKEOFF” CONFIG AIL TRIM
Parking brake on during takeoff
“NO TAKEOFF” PARK BRAKE ON
Rudder trim outside of takeoff
range
“NO TAKEOFF” CONFIG RUD TRIM
Flaps not in takeoff
position “NO TAKEOFF” SLATS/FLAPSLERS
Spoilers not in takeoff
position “NO TAKEOFF” CONFIG SPOICONFIG
Horizontal stabilizer outside of
takeoff
range (“green band”)
“NO TAKEOFF” CONFIG STAB TRIM
All configuration warning indications are cancelled when the configuration error is corrected, or the
　
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