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IAC 1 IAC 2
AURAL WARNING
MUTED MUTED
INHIBITS
During takeoff
and landing, the IAC fault warning computer, will process inhibit logic to minimize
spurious or distracting messages. Warnings and status messages are not inhibited except for
CABIN ALT and APU OVERTEMP (TO only).
During takeoff,
the caution and advisory messages are inhibited when:
· Weight On Wheels.
· Indicated airspeed transitions from less than 80 knots to greater than or equal to 80 knots.
The caution and advisory messages’ inhibit is removed 25 seconds after:
· Weight Off Wheels.
· Pressure Altitude is greater than or equal to takeoff
altitude +400 feet.
· Indicated airspeed is less than 50 knots.
· Takeoff
inhibit has been active for 60 consecutive seconds.
During landing, the caution and advisory messages are inhibited when:
· Landing gear down.
· Radio altitude transitions from 200 feet to less than or equal to 200 feet.
The caution and advisory messages’ inhibit is removed:
· 25 seconds after air to ground transition.
· Radio altitude greater than 200 feet.
· Indicated airspeed less than 50 knots.
AURAL AND VISUAL WARNINGS
Flight Crew Operating Manual REV 41, Jul 08, 2004
CSP 700−6
Volume 2
03−10−20
INHIBITS (CONT'D)
The following caution and advisory messages are NOT inhibited during takeoff
and/or landing.
Airplane System Caution Messages Advisory Messages
AFCS AP MISTRIM NOSE UPDN
(Ldg only)
AP MISTRIM LWDRWD
(Ldg only)
YD OFF
YD NOT CENTERED (TO only)
Air Conditioning
Pressurization
EMER DEPRESS
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
Hydraulic Power HYD 1−2−3 LO PRESS
HYD RAT PUMP FAIL (Ldg only)
Ice and Rain
Protection
ICE
Instruments ALL ADC MISCMP ADC 1−2−3 FAIL
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 2
03−10−21
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 ANTISKID
FAIL
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 FUEL FILTER
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 41, Jul 08, 2004
CSP 700−6
Volume 2
03−10−22
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.
　
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