View Full Version : B744 Engine Fail EICAS
OneTwoTree
24th Jun 2012, 11:38
Good day everyone,
Just a quick question regarding the 744.
What parameters trigger the ENG 1,2,3,4 FAIL message to show up?
I am assuming the EEC's compare the EPR, N1, N2 and others and then determine that one engine is toast when they drop beyond a certain point.
Any idea what these figures are?
Thanks for your input!
OneTwoTree
TopSwiss 737
24th Jun 2012, 12:29
Standing by to be corrected, but this is what my FCOM 2 (General Electric CF6-80) says... Might be different for different engines.
It does not directly give the exact trigger parameters as such, but a bit of reading gives the following:
ENG 1, 2, 3, 4 FAIL
Condition: One of these occurs:
•An engine failure
•An engine flameout
The explanation of the auto-relight feature says the following:
"A flameout is detected when a rapid decrease in N2 occurs, or N2 is less
than idle RPM."
By the way, the ENG 1, 2, 3, 4 FAIL EICAS Caution and it's associated beeper are inhibited on the ground, until lift-off occurs.
For the Roller on the 744
ENG FAIL _
N3 less than 50%,
Oil Pressure less than 25 psi,
Fuel Control Switch ON.
GCB is open,
and Airplane in Air Mode.
737Jock
25th Jun 2012, 21:27
What parameters trigger the ENG 1,2,3,4 FAIL message to show up?
Volcanic ash clouds!!!;) (>4mg volcanic ash per cubic meter)
Volcanic ash and aviation safety - Wikipedia, the free encyclopedia (http://en.wikipedia.org/wiki/Volcanic_ash_and_aviation_safety)