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ADC 1, 2, 3 MISCMP ADC 1, 2 or 3 has miscompared with the other two ADCs 16
AFCS ENGAGE INVAL FWC detects invalid engagement of AP 2
AFT XFER FAIL AFT tank fuel transfer failure (Not applicable G-5000) 6
AFT XFER OFF SCHED AFT tank fuel transfer off schedule (Not applicable G-5000) 6
ALL ADC MISCMP All valid ADCs have miscompared 16
ALL IRS MISCMP All valid IRSs have miscompared 16
AOA HEAT FAIL L (R) Left and/or right AOA heater has failed when it should be ON 3
AP PITCH TRIM FAIL AP pitch trim inoperative monitor detects invalid trim (only when down to one
AP) 2
AP TRIM IS LWD Roll mistrim monitor detects excessive forces. For LWD, if AP disconnects,
A/C will roll RWD 2
AP TRIM IS ND Pitch mistrim monitor detects excessive forces. If AP disconnects, A/C will pitch
nose down 2
AP TRIM IS NU Pitch mistrim monitor detects excessive forces. If AP disconnects, then A/C will
pitch nose up 2
AP TRIM IS RWD Roll mistrim monitor detects excessive forces. For RWD, if AP disconnects,
A/C will roll LWD
APU BATT FAIL APU battery has failed 6
APU BLEED SYS FAIL Annunciated when the APU LCV position does not match command, or Bleed
leak detection has been lost and APU bleed is not to be used 4
APU DOOR FAIL Annunciated when the APU door position does not match command 4
APU EGT SENSORS Annunciated when WOW is not true and both EGT thermocouple rakes have
failed 4
APU FIRE FAIL APU detection element system dual loop failure (Complete loss or fire detection
capability in APU) 4
APU FUEL SOV APU fuel shutoff valve failure 4
APU GEN OVERHEAT APU generator is overheating (to excessive temperatures). Message generated
in-air only since the APU will not automatically shut down in flight 4
APU GEN OVLD There is an overload on APU generator 4
For Training Purposes Only
Sept 04
7-47
P I LOT T R A I N I N G GU I D E
ELECTRONIC DISPLAY SYSTEM
APU OIL HI TEMP Annunciated when WOW is not true and a high oil temperature condition exists 4
APU OIL LO PRESS Annunciated when WOW is not true and a low oil pressure condition exists 4
APU REVERSE FLOW Annunciated when WOW is not true and a reverse flow condition exists 4
ASCB FAIL Loss of communication with all three bus controllers. Loss of cockpit
instruments. All AFCS functions not operational 7
A/T NOT IN HOLD A/T not in T/O Hold Mode following the transition above 60 knots during T/O roll
and until the aircraft transitions 400 ft. AGL
AUTO PRESS FAIL Automatic pressurization control is inoperative 13
AUTOBRAKE FAIL Autobrake not available 14
AV BATT FAIL Avionics battery has failed 6
AV FANS FAIL Both fans failed on ground (Global 5000 only) 13
BATT BUS FAIL Battery bus is not powered or has a fault 6
BATT MASTER OFF Battery master switch is off 6
BLEED LEAK L (R) Bleed leak detected on left or right bleed duct 13
BLEED SYS FAIL L (R) Bleed system failure 13
BRAKE 50% DGRAD Loss of two brakes (or more brakes if indication comes from discretes in BCU) 14
CABIN ALT Cabin altitude exceedance. Note: Caution level is normally set at 8200 ft. except
when a/c takes off or lands at high altitude 13
CARGO DOOR Cargo bay door not closed 1
CAT 2 INVALID CAT 2 was active, but all conditions no longer valid 16
CB TRIP AC FEEDER A circuit breaker for an AC feeder/AC cabin feeder has tripped 6
CB TRIP DC FEEDER A circuit breaker for a DC feeder/DC cabin feeder has tripped 6
CHECK DU 1 (2) (3) (4) (5)
(6) Data wrapped around from DUs does not match data from sensor 6
COWL A/ICE FAIL L (R) Left/right CAIV closed (valve switch or low pressure) but commanded open 3
CPLT BRAKE FAULT One or both copilot brake pedals not available 14
CTR FUEL XFER FAIL Center tank fuel transfer failure 11
CTR TANK FULL Center tank high level shutoff greater than 1000 gallons (Global 5000 only) Appx
1
DC BUS 1 FAIL DC bus 1 is inop 6
DC BUS 2 FAIL DC bus 2 is inop
DC EMER BUS FAIL DC emergency bus has failed 6
DC ESS BUS FAIL DC essential bus is not powered or has a fault 6
DISP CTLS FAIL Total loss of display control 7
CAUTION MESSAGES (AMBER)
CAS MESSAGE DESCRIPTION CH.
7-48 For Training Purposes Only
Sept 04
P I LOT T R A I N I N G GU I D E
ELECTRONIC DISPLAY SYSTEM
DOOR SYS FAIL Loss of fuselage & gear door indication 1
ELEC SYS FAIL A major fault detected in the electrical system ground only 6
ELEVATOR SPLIT Asymmetric elevator operation 10
ELT TRANSMITTING ELT is transmitting 8
EMER DEPRESS Emergency depressurization (dump) has been selected 13
EMER EXIT L (R) Left or right emergency exit door not closed and locked 8
EMER LIGHTS OFF Emergency lighting selected off 8
ENG FIRE FAIL L (R) Left or right engine detection element system dual loop failure. (Complete loss of
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