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· OFF Closes
the HP and LP fuel valves. Resets both channels of the FADEC.
ENG Mode Selector
· NORM Continuous
ignition A + B is selected when the engine is running and one of the
following is met:
· FLEX or TO/GA thrust is selected on the ground
· TO/GA thrust is selected in flight
· ENG ANTI ICE switch is ON
· Engine surge or stall occurs in flight
· FLAPS lever position is other then "0" in flight
· CRANK The
start valve opens provided the ENG MAN START switch is ON and N2 is less
than 10%. Ignition is not supplied.
· IGN / START Provides
continuous ignition if the ENG MASTER switch is ON and N2 is at idle
or greater.
During and automatic start, on airplanes placarded :EXTENDED DRY CRANK", expect
ignition and fuel flow 50 seconds after ENG MASTER switch is selected ON.
On airplanes without the placard, expect ignition and fuel flow between approximately 15%
and 20% N2.
During a manual start the HP fuel valve is open and ignition is selected when the ENG
MASTER switch is selected ON.
FIRE Light
Illuminates when the respective fire warning is activated and during engine fire test.
FAULT Light
Illuminates amber in the event of an automatic start abort, or a disagreement between the HP fuel
valve position of FADEC channel A and B.
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Flight Deck Documentation AIRBUS A320
12.11.06 Ralf Anderseck Seite 695.5.
Speed Brake, Trim and Flap Lever Panels( A320 )
Speed Brake
Speed Brake Lever
Lever provides the following speed brake and
ground spoiler functions:
· Manually pushing lever down and aft
inflight, selects surface position of
Speed Brakes. A "hard point: is
provided at the 1/2 position.
· Speed Brake deflection is limited to
approximately 1/2 with an autopilot
engaged, regardless of lever position.
· Pulling the lever up to the RET position
arms the ground spoilers to
automatically extend for landing or
when executing a rejected takeoff.
·
Trim
RUD Trim Selector
Controls the Rudder Trim actuator which
moves the neutral point of the articial feel at a
rate of 1 degree per second of rudder travel.
Selector is deactivated with A/P engaged.
RUD Trim Position Indicator
Displays Rudder Trim direction (L or R) and
value (0° to 20°).
RUD Trim RESET Switch
When pushed, the FAC commands the Rudder
Trim actuator to the zero trim position.
Flaps
Flap Lever
Commands flaps and slats for simultaneous
operation to selected position. Lever must be
pulled out of detent prior to positioning.
Detents are provided at positions 1 and 3 to
avoid excessive flap/slat travel by a single
action.
When the flap lever is in any position other
then "0" in flight, idle RPM is increased
(approach idle) and continuous ignition is
activated.
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Flight Deck Documentation AIRBUS A320
12.11.06 Ralf Anderseck Seite 705.6.
A320 Parking Brake & Landing Gears Gravity Extension
Parking Brake System
Parking Brake Handle
Sets the Parking Brake by pulling the handle
and then turning it clockwise. Activation of the
Parking Brake deactivates all other braking
modes. "PARK BRK" is displayed on the
ECAM memo page.
Landing Gear Gravity Extension System
Gravity Gear EXTN Handle
Provides Landing Gear extension in the event
of electrical, hydraulic or mechanical failure.
The handle must be extended and then rotated
clockwise three turns to shut off hydraulic
pressure, open the doors and unlock the gear.
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Flight Deck Documentation AIRBUS A320
12.11.06 Ralf Anderseck Seite 715.7.
Multifunction
Control Display Unit (MCDU) ( A320 )
To me, the MCDU, Mulifunction Control Display Unit is the heart of the A320/319. Everything
that the airbus can do, can be controled from this unit. The few pages above, that I have manage
to highlight are just a small sample of the many pages that you can access from the MCDU.
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