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The main landinggearoverheatdetection system maybe tested,from thelandinggear controlpanel, by simulating an overheat condition orasystemfault condition. The EICAS willdisplaythe applicable warning orcaution messageduringthetest.
Flight Crew Operating Manual MASTER
CSP A-
013
FIRE PROTECTION Main Landing Gear Overheat Detection Vol. 1 10-
40-
2
REV 56, Jan 31/03
anoverheat condition exists in both of the mainlandinggear bays.
<0039> GEARBAYOVERHEAT
MLG OVHT FAIL Caution (amber)
afault exists in the mainlanding gearbayoverheat detection system.
Main Landing Gear Overheat ---EICAS Indications <MST>
Figure 10---40---1
Flight Crew Operating Manual MASTER
CSP A-
013
FIRE PROTECTION Vol. 1 10-
40-
3
Main Landing Gear Overheat Detection REV 56, Jan 31/03
28VDC BATTERYBUS MLG BAYOVHT
MAIN LANDING GEAR BAY OVERHEAT WARNING FAIL TEST Switch (Spring-
loaded to normal position)
WARN FAIL-
Simulates afailure in the mainlandinggear bay overheat detection system. Messageis annunciated on EICAS.
GEARBAYOVERHEAT
DCU’S
OVHT
WARN FAIL
MLG BAY OVHTTEST PANEL
Main Landing Gear Overheat ---System Test Figure 10---40---2
Flight Crew Operating Manual MASTER
CSP A-
013
FIRE PROTECTION Main Landing Gear Overheat Detection Vol. 1 10-
40-
4
REV 56, Jan 31/03
A. System Circuit Breakers
SYSTEM SUB-
SYSTEM CB NAME BUS BAR CB PANEL CB LOCATION NOTES
Main Landing Gear Overheat Detection MLG BAY OVHT DET DC BATT 2 N9
Flight Crew Operating Manual MASTER
CSP A-
013
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