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PROX SYS Indicates a failure in the PSEU output circuitry (may be accompanied by GND
SPLRS caution message).
STEERING INOP Nosewheel steering has failed.
WOW INPUT The PSEU is unable to determine if the aircraft is airborne or on the ground
(WOW CH 1 & CH 2 disagree).
WOW OUTPUT One or more critical drivers are not in expected state (see following table).
A/SKID IN TEST Anti-skid system is in self-test.
PARKING BRAKE ON The parking brake is activated, aircraft not in takeoff mode (WOW and N1 less
than 70% rpm).
PROX SYS FAULT Indicates a failure in the proximity sensor electronics unit.
WOW OUTPUT FAIL Indicates a weight-on-wheels output fault in a non-critical system (see following
table).
LANDING GEAR/BRAKES
Description
Vol. 2 15−10−19
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
EICAS MESSAGES (CONT'D)
PSEU Critical & Non-Critical Drivers
CRITICAL DRIVERS NON-CRITICAL DRIVERS
SUBSYSTEM SUBSYSTEM
ANTI-SKID INBOARD ADG LOGIC #1
STALL WARN SYS #1 HSTCU
WOW RLY #1 FSCU
CVR ATC #1
THRUST REV DPLY #1 NG WOW #1 (SBW)
CABIN PRESS CTL ADG LOGIC #2
ANTI-SKID OUTBOARD HSTCU #2
STALL WARN SYS #2 ATC #2
TCAS NG WOW #2 (SBW)
WOW RLY #2 GCU OVERVOLTAGE TEST
INTERCOM
THRUST REV DPLY #2
DC ESS TIE
SATCOM/WATER PURGE/AVIONICS MASTER
HYDRAULIC PUMP #1
THRUST REV WOW #1
HYDRAULIC PUMP #2
THRUST REV WOW #2
LANDING GEAR/BRAKES
Description
Vol. 2 15−10−20
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
POWER SUPPLY AND CIRCUIT BREAKER SUMMARY
SYSTEM SUB-SYSTEM CB NAME BUS BAR
CB
PANEL
CB
LOCATION
NOTES
Landing Gear Proximity Sensing WOW/GEAR/
SPLR 1
DC BUS 1 1 F2
WOW/GEAR/
SPLR 1
DC BATT 1 N2
WOW/GEAR/
SPLR 2
DC BUS 2 2 F2
WOW/GEAR/
SPLR 2
DC BATT 2 N2
Nosewheel Steering NOSE STEER DC BUS 1 1 F6
NOSE STEER DC BUS 2 2 F6
Anti-Skid ANTI SKID DC BUS 1 1 F7
ANTI SKID DC BUS 2 2 F7
Brakes BRAKE PRESS
IND
DC BUS 2 2 G12
LANDING GEAR/BRAKES
Summary
Vol. 2 15−20−1
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
LANDING GEAR/BRAKES
Summary
Vol. 2 15−20−2
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
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