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Air Conditioning
Pressurization
EMER DEPRESS
L−R PACK FAIL
Aural and Visual
Warnings
CHECK DU 1−2−3−4−5−6
SG 1−2−3 FAIL
Electrical Power BATT MASTER OFF BATT EMER PWR ON
RAT GEN ON (Ldg only)
Doors and Exits CARGO DOOR
LARGE SERV DOORS
L−R EMER EXIT
PASSENGER DOOR
SMALL SERV DOORS
Flight Controls ELEVATOR SPLIT
FLT SPLR DEPLOYED
FLT SPOILERS FAIL
GND LIFT DUMP
ROLL SELECT
ROLL SPOILERS FAIL
RUD AUTHORITY LOW
SLAT−FLAP FAIL
STAB TRIM
STALL PROTECT FAIL
FLT SPOILERS FAULT
GND LIFT DUMP
NO TAKEOFF (TO only)
SHAKER 1−2 FAIL
SLAT−FLAP HALFSPD
STALL WRN ADVANCE
RUD AUTHORITY SAFE
SLAT−FLAP BIT
Hydraulic Power HYD 1−2−3 LO PRESS
HYD RAT PUMP FAIL (Ldg only)
Ice and Rain
Protection
ICE
Instruments ADC 1−2−3 MISCMP ADC 1−2−3 FAIL
AURAL AND VISUAL WARNINGS
Rev 2A, Apr 11, 2005 Flight Crew Operating Manual
CSP 700−5000−6
Volume 2
03−10−19
INHIBITS (CONT'D)
The following caution and advisory messages are NOT inhibited during takeoff
and/or landing.
Airplane System Caution Messages Advisory Messages
Landing Gear BRAKE 50% DEGRADED
CPLT BRAKE FAULT
GEAR DISAGREE
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
BRAKE TEMP (TO only)
GEAR SYS FAULT
NO TAKEOFF (TO only)
Lighting EMER LIGHTS OFF
Navigation ALL IRS MISCMP
Power Plant A/T NOT IN HOLD (TO only)
L−R FADEC N1 CTL
L−R REV LOCK FAIL
L−R REVERSER FAIL (Ldg only)
L−R FUEL FILTER
A/T 1−2 FAIL
AURAL AND VISUAL WARNINGS
Flight Crew Operating Manual Rev 2A, Apr 11, 2005
CSP 700−5000−6
Volume 2
03−10−20
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
harddisk
contains approximately 8MB of operational software files and 25MB of loadable diagnostic
files. A CDROM
is installed in the PMAT CDROM
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)
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
RETURN
MAIN
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DETAIL
GF0310_021
· DATA UPLOAD/DOWNLOAD switch and PRINT MAINT REPORT switch (located on bulkhead
behind pilot).
AURAL AND VISUAL WARNINGS
Rev 2A, Apr 11, 2005 Flight Crew Operating Manual
CSP 700−5000−6
Volume 2
03−10−21
CENTRAL AIRCRAFT INFORMATION AND MAINTENANCE SYSTEM (CAIMS) (CONT'D)
FGF0310_006
CAIMS PRINT MAINT REPORT SWITCH
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).
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