RotorAndWing
Final Approach
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Rotor&Wing
So the APU caught fire or the engine itself? RJs have hot start prevention?
Judging by the pic, I'd say tailpipe fire vs "hot start". A number of years ago a buddy of mine had a very similar start up fireball while parked right next to me (we were starting up together).....even 100 or so feet away, with the canopy open and my arm on the rail, I could feel some pretty intense heat. It wasn't actually a "hot start" (no unusual EGT rise), just a surprising and self correcting tailpipe fire. It was a really cold day (20-ish degrees F), and he didn't crank the motor long enough to get the motor and air going through it warmed. So I guess failure to atomize the fuel or something and it all just started pooling in the tailpipe until finally it lit off, which it most certainly did. Luckily he knew to cut the throttle, keep cranking and blow it out rather than blow the fire bottles. It was quite a show for us and the plane captains/maintainers though!
Not a turbine guy. Can someone explain what happens in a hot start or tailpipe fire or whatever? Seems like fuel isn't atomized or is making its way out the back and catching fire but how does that happen?
Well this is a turbine helo explanation so don't know how accurate it is for FW. A hot start generally happens when the fuel has pooled in the combustion chamber after shutdown and wasn't purged properly with compressor (P3) air. Or, you could have a weak battery and its not spinning the NG section fast enough to sustain start. Or, you could be at high altitude and trying a dual engine start and the APU can't provide enough air to spool up the NG fast enough for start. Or, like I said above, you can get a compressor stall (loud popping) where the airflow isn't going from front to back but reverse. In that case, if you don't cut the fuel, she'll generally go right thru redline.
In the turbine helos that I've flown, generally they have what's called an ECU or electrical control unit or even a FADEC that has an ECU. Anyway, what it does is it monitors several inputs, one of which is temp (TGT, MGT, TIT) to make sure it doesn't exceed a predetermined level on start up. If it does, the ECU has authority to cut the fuel on its own. In theory that's what is suppose to happen but in practice, on rare cases I've had friends who had a hot start because the temp rose so fast the ECU couldn't cut fuel in time. The ECU also has the power to prevent the engine from over speeding but that's a whole other discussion.
Hopefully that explaination covers the FW hot start description as well.
Plane caught fire after pilot turned on its engine
Not a turbine guy. Can someone explain what happens in a hot start or tailpipe fire or whatever? Seems like fuel isn't atomized or is making its way out the back and catching fire but how does that happen?
Lol! That would get the heart rate up.
Does the Hornet have hot start prevention or do you have to cut manually? The GEs in the 60 have it. Never Had one but had plenty of compressor stalls on start up in Astan though. Hot start prevention won't work in that situation so at some point you have pull the PCL off to keep from over temping. Had a fire balls come from the APU occasionally from over priming as well.
Another cause (not that it was the case here....I know the Captain and he's pretty sharp), is initiating the start sequence without the ignition armed. Fuel is introduced and just pools in the engine. When you don't get a start you begin looking for the problem. You then notice you didn't arm the igniters! AVOID THE INTINCTIVE IMPULSE TO TURN THEM ON! Either an explosion or fire is almost guaranteed!
Proper procedure is to cut off the fuel and continue to dry motor it to blow out/dry out the pooled fuel, respecting starter time limits.
THEN arm the igniters and go through a normal start sequence.
Obviously seeing as though it's August in North America, this isn't the issue, but....Not a turbine guy. Can someone explain what happens in a hot start or tailpipe fire or whatever? Seems like fuel isn't atomized or is making its way out the back and catching fire but how does that happen?
Obviously seeing as though it's August in North America, this isn't the issue, but....
I have heard of similar occurrences in the winter. Just a few drops of dew that fall to the bottom of the inlet can freeze the fan. You can fry an engine in an instant if that happens.
Another cause (not that it was the case here....I know the Captain and he's pretty sharp), is initiating the start sequence without the ignition armed. Fuel is introduced and just pools in the engine. When you don't get a start you begin looking for the problem. You then notice you didn't arm the igniters! AVOID THE INTINCTIVE IMPULSE TO TURN THEM ON! Either an explosion or fire is almost guaranteed!
Proper procedure is to cut off the fuel and continue to dry motor it to blow out/dry out the pooled fuel, respecting starter time limits.
THEN arm the igniters and go through a normal start sequence.
Obviously seeing as though it's August in North America, this isn't the issue, but....
I have heard of similar occurrences in the winter. Just a few drops of dew that fall to the bottom of the inlet can freeze the fan. You can fry an engine in an instant if that happens.
It doesn't work that way for all airplanes. Sometimes N2 is spinning fast but no N1 yet. Can't wait too long with N2 too high to introduce fuel.Except that you do not add fuel and ignition until you have at least positive rotation of the fan. Besides, in the winter part of the pre-flight should include spinning the fan by hand to make sure it rotates.
Are you guys sure about this ignition issue? I am typed in 4 jets and flown 3 other turboprops (and nowhere current in all of them), but I am about 100% sure I never touched the ignition switches during start in any of them. The start sequence took care of it always and then turned them off. All I had to do was remember to introduce fuel at XX% RPM and wait for light off at another higher %. If light off didn't occur then you did some other things, doubtful that throwing ignitions on manually was one of them. Again this is from my fading memory has it has been many years since I flew some of the types.
Can only speak for the CRJ. You arm either ignition A or ignition B, which automatically fires when certain rotation parameters are met. You then disarm (turn off) the ignition after start. You can go through the entire start prices and introduce fuel without arming them.
Are you guys sure about this ignition issue? I am typed in 4 jets and flown 3 other turboprops (and nowhere current in all of them), but I am about 100% sure I never touched the ignition switches during start in any of them. The start sequence took care of it always and then turned them off. All I had to do was remember to introduce fuel at XX% RPM and wait for light off at another higher %. If light off didn't occur then you did some other things, doubtful that throwing ignitions on manually was one of them. Again this is from my fading memory has it has been many years since I flew some of the types.