BigHitDH
7th Dec 2003, 19:38
Hi all.
I have a question about the A318 thru A321 ENG Master switches, although I suppose this applies to Boeing aircraft as well.
The way I understand it, switching the engine master switch to "on" during an auto engine start opens the HP fuel valve, provided the ENG MODE selector is in the IGN/START, and starts the engine with bleed air from the APU or ground air unit.
Selecting "off" closes the HP and LP fuel valves, and resets bith channels of the FADEC. This will effectivly shut the engine down I presume?
Are these switches protected in any way? Do they have a "gate" to stop accidental activation, or is there some other method of failsafe in place?
Looking at the position of these switches (between the flap/spoiler selector handles, and immediately aft of the the throttles) this seem like the kind of position where one could easily get caught by a shirt cuff or accidentally knocked with a hand, shutting down the engine. (I'm presuming here that that's what it does).
If this is the case, it seems to me like this could only happen during takeoff (flaps up) a manual descent at TOD (thottles to flight idle) or when activating the spoilers in flight for a speed bleed.
I've seen on Boeing aircraft, the switches are "guarded" bu loops either side. Why doesn't Airbus do this?
Thanks in advance!
Edited to correct my poor typing...
I have a question about the A318 thru A321 ENG Master switches, although I suppose this applies to Boeing aircraft as well.
The way I understand it, switching the engine master switch to "on" during an auto engine start opens the HP fuel valve, provided the ENG MODE selector is in the IGN/START, and starts the engine with bleed air from the APU or ground air unit.
Selecting "off" closes the HP and LP fuel valves, and resets bith channels of the FADEC. This will effectivly shut the engine down I presume?
Are these switches protected in any way? Do they have a "gate" to stop accidental activation, or is there some other method of failsafe in place?
Looking at the position of these switches (between the flap/spoiler selector handles, and immediately aft of the the throttles) this seem like the kind of position where one could easily get caught by a shirt cuff or accidentally knocked with a hand, shutting down the engine. (I'm presuming here that that's what it does).
If this is the case, it seems to me like this could only happen during takeoff (flaps up) a manual descent at TOD (thottles to flight idle) or when activating the spoilers in flight for a speed bleed.
I've seen on Boeing aircraft, the switches are "guarded" bu loops either side. Why doesn't Airbus do this?
Thanks in advance!
Edited to correct my poor typing...