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Flight Controls ELEVATOR SPLIT FLT SPOILERS FAULT
FLT SPLR DEPLOYED GND LIFT DUMP
FLT SPOILERS FAIL NO TAKEOFF (TO only)
GND LIFT DUMP SHAKER 1.2 FAIL
ROLL SELECT SLAT.FLAP HALFSPD
ROLL SPOILERS FAIL STALL WRN ADVANCE
RUD AUTHORITY LOW RUD AUTHORITY SAFE
SLAT.FLAP FAIL SLAT.FLAP BIT
STAB TRIM
STALL PROTECT FAIL
Hydraulic Power HYD 1.2.3 LO PRESS
HYD RAT PUMP FAIL (Ldg only)
Ice and Rain ICE
Protection
Instruments
ADC 1.2.3 MISCMP ADC 1.2.3 FAIL
Rev 2A, Apr 11, 2005 Flight Crew Operating Manual Volume 2
INHIBITS (CONT'D)
The following caution and advisory messages are NOT inhibited during take-off and/or landing.
Airplane System
Caution Messages Advisory Messages
Landing Gear BRAKE 50% DEGRADED BRAKE TEMP (TO only)
CPLT BRAKE FAULT GEAR SYS FAULT
GEAR DISAGREE NO TAKEOFF (TO only)
INBD BRAKE LO PRESS
L.R INBD BRAKE FAIL
L.R OUTBD BRAKE FAIL
NOSE STEER FAIL
OUTBD BRAKE LO PRESS
PARK/EMER BRAKE ON (Ldg only)
PLT BRAKE FAULT
UNCOMMANDED BRAKE
Lighting EMER LIGHTS OFF
Navigation ALL IRS MISCMP
Power Plant
A/T NOT IN HOLD (TO only) A/T 1.2 FAIL
L.R FADEC N1 CTL L.R REV LOCK FAIL L.R REVERSER FAIL (Ldg only) L.R FUEL FILTER
Volume 2 Flight Crew Operating Manual Rev 2A, Apr 11, 2005
CENTRAL AIRCRAFT INFORMATION AND MAINTENANCE SYSTEM (CAIMS)
The CAIMS collects diagnostic and fault data from other airplane systems. From this data, the CAIMS assembles a fault record that can be used to monitor system performance during the flight. The maintenance personnel uses CAIMS to accomplish system tests and to isolate defective components.
The CAIMS supplies fault data during all phases of airplane operation through the Portable Maintenance Access Terminal (PMAT), touch screen, located in the passenger cabin . The PMAT hard-disk contains approximately 8MB of operational software files and 25MB of loadable diagnostic files. A CD-ROM is installed in the PMAT CD-ROM drive and contains an electronic copy of the Aircraft Maintenance Manual (AMM).
The crew has the option of monitoring the PMAT display for active faults and/or may print the report on the cockpit printer. For more information on the printer, refer to chapter 6 COMMUNICATIONS.
The CAIMS is comprised of the following components:
.
PMAT (located in the cabin)
.
DATA UPLOAD/DOWNLOAD switch and PRINT MAINT REPORT switch (located on bulkhead behind pilot).
Rev 2A, Apr 11, 2005 Flight Crew Operating Manual Volume 2 CSP 700.5000.6 03.10.21
CENTRAL AIRCRAFT INFORMATION AND MAINTENANCE SYSTEM (CAIMS) (CONT'D)
CAIMS PRINT MAINT REPORT SWITCH
Used to get a report of active faults from the cockpit printer.
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