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庞巴迪环球5000公务机机组操作手册 Bombardier_Global-电源(24)

时间:2011-11-08 15:49来源:蓝天飞行翻译 作者:公务机
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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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