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Anti-Skid Test
The TEST button on the LDG GEAR control panel initiates a built-in test of the ASCU and associated components, during which time the A/SKID IN TEST advisory EICAS message will be displayed. The test can only be performed with the parking brake off.
LANDING GEAR/BRAKES Description Vol. 2 15.10.17
Oct 05/06
The landing gear system provides control of the landing gear, brakes, anti-skid, and the overheat warning system. Flight deck controls activate normal gear extension and retraction, emergency gear extension, nosewheel steering, warning horn mute, anti-skid operations, and anti-skid test functions.
The EICAS page presents indications of landing gear position.
Landing Gear Panel
Figure 15.10.11
Landing Gear Manual Release
Figure 15.10.12
LANDING GEAR/BRAKES Description Vol. 2 15.10.18
Oct 05/06
Landing Gear EICAS Page
Figure 15.10.13
LANDING GEAR/BRAKES Description Vol. 2 15.10.19
Oct 05/06
MESSAGE MEANING
Landing gear position does not match the gear lever position.
High temperature detected in the main landing gear wheel bins.
Nose doors are open for 10 seconds after the landing gear is locked in position, or when airspeed is >250 KIAS.
The parking brake is set with the aircraft in the takeoff mode, with N1 greater than 70% rpm.
The respective anti-skid channel has failed or is not armed.
The respective brake system pressure is below 1,015 psi.
The overheat detection loop in the gear bay is shorted out.
The parking brake shutoff valve does not match the commanded position.
Indicates a failure in the PSEU output circuitry (may be accompanied by GND
SPLRS caution message).
Nosewheel steering has failed.
The PSEU is unable to determine if the aircraft is airborne or on the ground
(WOW CH 1 & CH 2 disagree).
One or more critical drivers are not in expected state (see following table).
Anti-skid system is in self-test.
The parking brake is activated, aircraft not in takeoff mode (WOW and N1 less
than 70% rpm).
Indicates a failure in the proximity sensor electronics unit.
Indicates a weight-on-wheels output fault in a non-critical system (see following
table).
AURAL WARNING (IF ANY)
“GEAR DISAGREE” “GEAR BAY OVERHEAT” “NOSE DOOR”
”CONFIG BRAKES”
CL.605 Flight Crew Operating Manual
PSP 605.6
LANDING GEAR/BRAKES Description Vol. 2 15.10.20
Oct 05/06
PSEU Critical & Non-Critical Drivers
CL.605 Flight Crew Operating Manual
PSP 605.6
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