l oil lo press 
Left engine has low oil pressure while the engine is running.
l reverser unlkd
Left thrust reverser not stowed with thrust lever in forward thrust range.
r oil lo press
Right engine has low oil pressure while the engine is running.
r reverser unlkd
Right thrust reverser not stowed with thrust lever in forward thrust range.
l eng flameout
Left engine has experienced a flame-out and stopped without manual selection or shut-down signals from the FADEC.
l eng fuel lo temp
Left engine inlet fuel temperature is below 5 degrees C with engine running.
l eng overspeed
Left engine shutdown caused by Independent Overspeed Protection.
l fadec fail
Left FADEC failure in both lanes. Engine operation may be affected.
l fadec n1 ctl
Left engine is in N1 control; left FADEC has detected a fault and reverted to N1 control.
l rev lock fail
Left thrust reverser locks (2 of 3) not locked with thrust lever in forward thrust range. Thrust reverser will not deploy.
l reverser fail
Left thrust reverser has failed and doors will stay in current position.
l throttle fail
Left throttle has failed. Engine operation will be affected as a function of aircraft configuration.
r eng flameout
Right engine has experienced a flame-out and stopped without manual selection or shut-down signals from the FADEC.
r eng fuel lo temp
Right engine inlet fuel temperature is below 5 degrees C with engine running.
r eng overspeed
Right engine shutdown caused by Independent Overspeed Protection.
r fadec fail
Right FADEC failure in both lanes. Engine operation may be affected.
r fadec n1 ctl
Right engine is in N1 control; right FADEC has detected a fault and reverted to N1 control.
r fadec ovht
Right internal EEC temperature monitor tripped.
r rev lock fail
Right thrust reverser locks (2 of 3) not locked with thrust lever in forward thrust range. Thrust reverser will not deploy.
r reverser fail
Right thrust reverser has failed and doors will stay in current position.
r throttle fail
Right throttle has failed. Engine operation will be affected as a function of aircraft configuration.
ats envelope
FADEC has determined that the aircraft is within the starter assisted envelope.
l fadec fault
Minor left FADEC fault. Engine operation should not be affected.
l rev lock fault
One of two primary stow switches on left thrust reverser indicating unstowed with thrust lever in forward thrust range.
l reverser fault
Minor fault in the left thrust reverser system. Thrust reverser operation should be normal.
r fadec fault
Minor right FADEC fault. Engine operation should not be affected.
r rev lock fault
One of two primary stow switches on right thrust reverser indicating unstowed with thrust lever in forward thrust range.
r reverser fault
Minor fault in the right thrust reverser system. Thrust reverser operation should be normal.
windmill envelope
FADEC has determined that the aircraft is within the windmill start envelope.
