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Bill: Have you sumped your tanks for water.AV GAS sucks up water like a
sponge in humid climates it is a real concern for fast climbing aircraft
into the freezing levels.When fuel temp is Hi fuel holds water and is no
problem. When the fuel cools it cannot hold the water any longer and it
freezes. I think it is fuel line ice blockage.Just my two cents.
Tom Giddings
133TB
0290/235
I experienced an engine failure while leveling off at FL220 this
afternoon. I have almost 200 hours over 15 months on this 2007 IV-P with
the TSIO-550B engine, which has 450TT and 220 STOH. We had been tweaking
the baffles and checking the CHT probes by swapping probes 5 with 3 and
2 with 4. We had just seen a great improvement in CHTs with the
modifications. I was in the process of climbing to FL220 to get some
cruise data at 75, 65, and 55 %. Because of the typical ISA+25 Gulf
Coast afternoon temps, I had to level off at 12 and 18 for about 4-5
minutes to let the oil temp cool off. The climb temps looked good
passing 200 and 210 to continue to 220. When I reached 220 and began the
level off, immediately I noticed a very sudden rise in CHTs and EGTs
from about 400 where I had expeced them to peak in the climb. 6 + 8
elashing red temps will get your attention right away. (I have the early
warnings set at 420 and 1700). The temps came rapidly up to just
below red line in the high 430s. I have not seen this pattern before in
200 hours in this airplane and with many hot day climbs to the FL200s. I
began to slowly reduce throttle, trying to guess whether it was better to
keep cooling fuel flow and high power or throttle back to counter the
rising temps.
As I pulled the throttle back, I was able to arrrest the rise but soon
noticed the EGTs rapidly dropping. At this point there was no response to
throttle inputs. I notified center of my descent, to which he replied
that I should ask for a descent clearance first. I replied that I was
aware of that procedure, but believed I had a powerplant failure and did
not have an option. I turned toward PSX, the nearest long piece of
concrete and pulled the prop back for max glide. The engine windmills
nicely at max glide of 120KIAS( I have wondered if it might stop the
windmill at 120, best L/D and then loss of oil pressure would send the
prop back to flat pitch). I got out the engine fail/airstart checklist
and switched from the left to the right tank. I notified center of my
intention to airstart. Passing 17K, I recall telling him I had about 17
minutes and could easily make the airport at 17 miles. Shortly thereafter
at 16500 the engine responded to throttle
inputs, but initially roughly like a cold start. Slowly allowing the
engine to rewarm, I got normal power back. Satisfied with the recovery
and airstart, I turned back to homebase about 35 milees away and shot a
precautionary approach to high key at Houston Southwest.
Our best guess after review with my mechanic and a conversation with Tim
Wilson at Lancair was that the culprit was temporary fuel starvation. I
am guessing that the sudden rise in the EGTs and CHTs was the result of
an uncommanded leaning of the mixture as the fuel supply dropped. I did
not catch a good record of the fuel flow until after the successful
recovery. From then on it was normal. The tanks both had been filled
before the previous flight and only about ten gals had been used from
both tanks, so there was about 42 gal. in each. Preflights indicated no
obstruction to the wingtip vents and this was true postflight. Fuel
samples are done first flight of each day and this was the third flight
today. The low boost was on passing 10,000 in the climb in accordance
with the checklist. I did not get around to trying the high boost because
the failure appeared to clear by switching tanks. when I reached a safe
glide range, I tried switching back to the
left tank and saw no change in fuel flow. I suspect a fuel vent blockage
at the freezing level, but I had not flown through any visible moisture
this afternoon. Tops of the towering CU was about 10K widely scattered,
so they were easy to dodge and avoid moisture and ice in the climb. The
engine behaved perfectly thereafter and responded well to clearing
procedures during the precautionary approach.
1. Anybody see this pattern before?
2. Any suggestions on troubleshooting or where to look for the cause?
3. What would you check prior to continuing operations other than a
thorough engine inspection and fuel system check?
Thanks for the good information and guidance on the LML,
Bill Miller
USN Test Pilot
L-IVP, 191 hours
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