Cockpit - Preparation - Electrical Flashcards
BUS TIE switch position
- APU GEN ON or EXT PWR ON - CLOSED
- APU GEN ON and EXT PWR ON - OPEN
- Battery power only - OPEN
EICAS message
PRIMARY STAB TRIM FAIL (-5.1 - 2)
System Test - Auto Test
Auto Test is completed automatically upon system power-up
STATUS - Verify PASS
System Test - Stall Warn
Amber X on both AoA windows
Stick shakers activate and stop, in the following order:
- Left
- Right
- Both
Master Caution
- Windshear fail and AoA Probe Fail L-R ECAIS messages are displayed
- All indications return to normal; cyan Done is displayed when completed
System - Engine Fire
Both Master Warning flash
Both Master Caution are illuminated steady
ENG FIRE light are illuminated steady
Red ENG FIRE L-R and amber FIRE DECTECT FAIL L-R EICAS message is displayed.
Cyan done is displayed when completed
System - Smoked detected
Both Master Warning flash
Both Master Caution are illuminated steady
Red BAGGAGE FIRE and white SEC BAG Bottle buttons are illuminated
Red BAGGAGE FIRE and amber SEC BAG BOTTLE EICAS messages are displayed
Cyan Done is displayed when completed
System - Annunciator - Press
All overhead Light buttons are illuminated ON
Both Master Warning flash
Both Master Cautions are illuminated steady
Both Bottle Armed buttons are illuminated steady
Halos around the Engine RUN/STOP button is illuminated steady
T/R EMER STOW buttons flash
ENG Starter and Engine Starter DISENG buttons are illuminated
FADEC RESET and FLAP RESET buttons are illuminated steady
Cyan Done is displayed when completed
System - Annunciator - Traffic
TCAS TEST EICAS message is displayed
Fly the pitch cue is displayed on ADI approx. 5 above the current attitude
Red no-fly bands are displayed on ADU above the green fly-to-pitch cue
Green VSI 0 - 2000ft, Red band are displayed outside this range
Red Traffic message is displayed on the PFD
TEST MODE traffic map is displayed on both PFD with RED, AMBER, and white symbols
Cyan Done is completed
System - Overspeed - Press
Cyan Done is displayed when completed
System - HF1 - HF 2 - Press
Green Pass is displayed
Engine anti-ice test
Thrust - Request LP et 70 - 75 % N2
ANTI-ICE ON
- L&R Engine/Stab - ON
- L&R Wing - ON
- Verify ITT increase
Following White EICAS message warning.
All EICAS messages expect ANTI-ICE ON ALL - Extinguish
- 81% N2 maximum and monitoring
Thrust Levers - Request LP to IDLE
WING XFLOW - XFLOW
WING XFLOW - OFF
Anti ice - as required