Self Notes Flashcards
(70 cards)
If the door is armed and opened from the outside, will the slides deploy?
No, the lever moves to the disarmed position
How many doors are on the aircraft?
10
If trying to open the doors and the mechanism does not budge, what is the next step?
Look at the outflow valves and see if its closed
Where is P1, P2, P3, P5
P1 - Captain
P2 - Centre console
P3 - Co-pilot
P5 - Overhead
What are the 3 modes of HLCS
P - Primary
S - Secondary
A - Alternate
What are PFCS?
N - Normal
S - Secondary
D - Direct
What panel is used to switch between the 3 MFDs?
P55 - Display select panel - Glareshield
How many DUs in total?
x6
What are the 3 positions of the Standby Power Switch?
OFF
BATT ON
AUTO
What switches are to be checked before removing aircraft power?
Emergency power switch - OFF
ADIRU switch - OFF
Batt switch - OFF
What must be checked before starting APU?
- Ensure correct oil level
- BATT switch - ON
- Bus - BATT BUS section 2
- Check brake accumulator gauge for power
- At least 433kg in LEFT TANK
What are the Primary and Auxilliary jack points?
Primary - ABC
Aux - D E F G
Which jack points use Intergral jacks compared to jack pads?
Integral - A B
Jack Pads - D, G, H
What must be ensured before jacking up aircraft?
- Do not lift nose more than 6”
- Do deactivation procedure
Where is the Ground Crew Call System panels?
Located on the:
- SERVICE & APU SHUTDOWN panel (P40)
- Flight call light - AUDIO CONTROL - P8
Where is the service interphone switch? What is it powered by?
P5
- powered by captains flight instrument bus
Where is AIMS?
x2 in MEC
What is a caution regarding Cursor Control Device on the Primary Display System?
- Don’t put too much pressure on cursor.
When landing gear flaps are down, when will the message dissapear?
10s
Where is the brake accumulator and pressure indicating light shown?
On P1 - Captain
What does the EICAS status page show?
- Hydraulic system info
- APU
- Crew Oxygen
- Status messages / clock
Where is the MAT located?
Central Maintenance Computing System (CMCS)
What are the two conditions that the AVAIL light comes on in the secondary external power switch.
- Primary receptacle has power
- Battery switch in ON
What can be switched on the BATT switch if the plane has power with no person on board?
- BATT switch can be switched to OFF. Prevents auto operation of STBY POWER if Gound power is lost.