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"RIGHT REVERSER UNLOCKED" aural
"NORMAL BRAKE FAIL" aural
FIRE TEST OFF
Single Chime (any caution)
STALL TEST OFF AURAL WARNING TEST 1 OFF
"GEAR" aural
AURAL WARNING TEST 2 TEST
Single Cavalry Charge tone
LAMP TEST 1 OFF
(autopilot disengage)
LAMP TEST 2 OFF
"AUTOTHROTTLE" aural
After 60 seconds
TEST CONTROL 1/1
FIRE TEST OFF
STALL TEST OFF
AURAL WARNING TEST 1 OFF
LAMP TEST 2 AURAL WARNING TEST 2 LAMP TEST 1 OFF OFF OFF
"ALTITUDE" aural (altitude alert departure)
C.chord tone (altitude alert capture)
Double C.chord tone
(vertical track alert)
Single Chime
Trim clacker (trim in motion)
"MINIMUMS, MINIMUMS" aural
(DH and MDA).
GF0720_121
Rev 3, Apr 25, 2005 Flight Crew Operating Manual Volume 2
ELECTRICAL
EMS CIRCUIT PROTECTION
TEST KEY (CONT'D)
LAMP TEST
LAMP TEST:
After 20 seconds (duration approximately 20 seconds for
each test)
Press the LAMP TEST 1 (2) activation
button and note the following:
All overhead pushbutton annunciators illuminate.
Glareshield panel lights illuminate.
Pedestal panel lights illuminate.
After 20 seconds
RAT TEST
At the completion of the test, confirm that a RAT GEN FAIL caution message is not displayed on EICAS.
GF0720_122a
Volume 2 Flight Crew Operating Manual Rev 3, Apr 25, 2005
ELECTRICAL
EMS CIRCUIT PROTECTION
TEST KEY (CONT'D)
RAT TEST
RAT TEST (on ground only):
(duration approximately 5 seconds)
Press the RAT TEST activation button and note the following:
.
RAT ICON displayed on AC and HYDRAULIC synoptic pages.
.
ESS TRU 2 is momentarily lost and DCPC reconfigures accordingly.
.
AC ESS BUS is momentarily lost.
After 5 seconds
Rev 3, Apr 25, 2005 Flight Crew Operating Manual Volume 2
ELECTRICAL
EMS CIRCUIT PROTECTION
EMER CONT
EMER CONT Key used to display bus isolation status. To isolate a primary bus, (during an emergency), select associated activation key. When selected, associated bus is isolated from the electrical system (no alternate power transfer to bus).
Volume 2 Flight Crew Operating Manual Rev 3, Apr 25, 2005
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