Dave –
Remarkable story! Thanxomuch for sharing
your experience. It helps combat my own tendency to let schedule drive my
decisions.
I’m very very very very glad it
worked out well for you – good job flying and landing.
Joe Hull
Cozy Mk-IV #991 (preping for DAR inspection
- details, details)
Redmond (Seattle),
Washington
From: Rotary motors in aircraft
[mailto:flyrotary@lancaironline.net] On
Behalf Of David Leonard
Sent: Sunday, January 15, 2006
10:54 PM
To: Rotary
motors in aircraft
Subject: [FlyRotary] Anatomy of an
almost crash.
I had to
set my RV-6 down on highway 395 near Bishop Tuesday, and here is the story.
Mostly things I could have done better, some that I did right or otherwise got
lucky. It is an RV6 tip up with a turbocharged Mazda rotary engine.
I took
the RV up to Mammoth to ski for the weekend. When I returned to the plane
Sunday evening I discovered a small puddle of coolant under the engine. I had
some concerns about the cold as my antifreeze had been recently diluted with
water when I had to make a field repair of a coolant leak but I neglected to
replace the antifreeze (big mistake #1). I estimated 25/75 antifreeze/water and
the temperatures were supposed to be in the low 20's overnight. This I thought
would be enough but I was not sure. The puddle of coolant seemed to prove that
overnight the temp got low enough to freeze some coolant and crack something.
A quick
look under the cowl failed to reveal the souce of the leak other than it was
not coming from the previously fixed coolant line or anywhere other than the
radiator itself. I didn't have time to trouble shoot as I had to get home to be
at work the next day.
I was
able to hitch a ride home in another aircraft, then drive back up the following
evening after work. When I arrived at the airport at 10pm the temperature was 3
deg F. In order to prevent any further damage, I added some anti freeze and ran
the engine for a while to circulate it. When I left the airport at 11:30 pm the
temperature was -3 deg. This is obviously colder than I had expected and was
probably responsible for the damage. The temperature in town was 20 deg despite
the fact that town is higher in elevation. The only explanation I have for the
extreme low temp at the airport is temperature loss from sublimation of the
vast deep snow fields around the airport in the very dry air (just a guess).
I arrived
at sun-up the next morning (temp again 4 deg at airport but 19 in town) and got
to work on fixing the leak. After several engine runs I determined that the
leak was indeed coming from somewhere in the radiator. There did not seem to be
any coolant in the oil, but I identified and fixed an oil leak in the turbo oil
return line. Also, the engine breather tube (which vents down in the gear leg)
had frozen and was causing the turbo to burn oil. That issue was fixed as well.
In order
to temporize the radiator leak I decided to use a can of radiator stop-leak and
switch coolant to Evan's NPG. NPG is a pure propylene glycol coolant that has a
very high boiling temp and can therefore be run with little or no coolant
system pressure. I switched out the coolant, added the stop-leak, and changed
to a 7 psi radiator cap. The stop-leak appeared to do it's job as there was no
visible continued leak after an hour of running the engine on the ground at
fast idle with some brief runs at higher RPM.
At about
2pm I was cold (temp at the airport now in the mid 20's) and tired (had slept
in the car overnight) but decided it was safe to make the flight to Bishop - 27
miles away and 3000 feet lower. There I would remove the cowl and give
everything a good look. Since the coolant leak had only lost about a quart in 3
days, was now sealed and would be flown with low pressure I assumed the most I
could loose in the 15 min flight would be about a cup of coolant (Big mistake
#2?)
The first
8 minutes of flight all systems were green. Then over the course of a minute
the coolant temp went up to over 280, oil temp up to over 200 (the highest it
has ever been). Being about half-way I decided to continue to the lower Bishop
airport. Then the alternator quit (buss voltage dropped to 11.7 and battery
showed a discharge). Then oil pressure dropped to zero, followed shortly after
by the engine stopping to make power and a puff of smoke coming in into the
cockpit thought the heater vent (cowl air - not a heat muff).
It
appeared as though I would be able to glide to the Bishop airport. I was at
9000 feet. Bishop was 13 miles away at 4000 feet with no significant winds.
This distance is solidly within the typical glide ratio of the RV6 so I calmly
assumed there would be an easy dead-stick onto the airport.
I tried
to get the prop to stop windmilling by slowing. In my initial flight testing I
had been able to stop the prop from windmilling at about 80 kts. However, even
by slowing to 65kts IAS I was unable to stop the windmilling. It turns out that
overheating the engine had caused the loss of compression on all rotor faces
and this prevented me from stopping the windmilling. I was seeing descent rates
of 800-1000 fpm at 90 KIAS and it soon became apparent that making the airport
would be sketchy at best, so I opted for a quality highway rather than try to
overfly the town to make the airfield.
I was
able to spot a section of Hwy 395 that was 4-lane divided (no opposing traffic)
that also seemed to be free of turns, power lines and intersections. I relayed
my situation to the Bishop unicom and got a prompt response. I turned off my
fuel pump and in accordance with my training turned off the master power on
short final... Doh! I have all electric flight instruments and now had no time
to re-boot either of my 2 air speed indicators.
My plan
for traffic avoidance was to come in faster than typical traffic speed, then
bleed off that speed at 20 feet over the highway. That way any traffic has
plenty of time to see me and slow down while I am bleeding off speed. Touchdown
was uneventful and quite a relief. No injury or damage.
The
Bishop police were there within minutes, and 2 hours later the plane was tied
down at the Bishop airport. I had no time or desire to remove the cowl so the
cause is still very unclear. A loss of the accessory belt would explain both
the inability to cool and the loss of the alternator, but my bet is still on
something to do with the extreme cold and radiator leak. I have to shamefully
admit that time pressures were a contributing factor. Feeling the need to
return home, I probably rushed the testing process after making repairs. I
should have circled Mammoth airport in order to test the repairs at high power
before attempting continued flight, especially in mountainous terrain (though
there is no freeway in SoCal that would be as forgiving as that section of
395).
I plan to
rent some kind of truck next weekend and drive up, remove the wings, and bring
the plane home. It will remain in our garage for the next 8 months while I
deploy to Iraq.
(Suggestions or offers for use of an adequate truck or trailer would be much
appreciated). This will also give me a chance to paint the plane and do a lot
of the finishing touches that will be easier to do at home than at the airport.
Obviously I will need to rebuild the engine as well, but that is a relatively
minor issue.
This was quite
a learning experience I obviously hope I never have to repeat. All things
considered, I feel quite lucky that things turned out so well.
Lastly, I
want to thank the Bishop Unicom, Police Dept, Highway Patrol, Cal Trans, and
Fire Department who were all very professional and helpful. Also, thank you to
the fellow RV6 owner was passing by and took an hour and a half out of his day
to drive back up to Mammoth and get my car for me.
--
Dave Leonard
Turbo Rotary RV-6 N4VY
http://members.aol.com/_ht_a/rotaryroster/index.html
http://members.aol.com/_ht_a/vp4skydoc/index.html