Has
the fuel pump been inspected, especially the aneroid bellows? I have had
a similar issue on takeoff, high fuel flow with a very rich mixture to the
point that people on the ground radioed that I was pouring black smoke. I
reduced the throttle as I had excess power and it smoothed the very rough
running engine so I felt confident it would continue running. I was
afraid to do much more and left it alone until I got back to terra firma.
After this exercise, the ignition was completely gone through, the fuel setup
was redone and all appeared perfect on run up, including a high speed
taxi. I took off again and it occurred once more. I local mechanic
suggested the fuel pump and aneroid valve. I sent the pump in for
inspection and rebuild if necessary. The aneroid was found to be
sticking, it was rebuilt and the problem has been gone for about 100
hours. I believe this could very well be the problem, especially if the
fuel set up was off to begin with. The symptoms are exactly what I
experienced. Placing the fuel pump on would increase the problem.
The engine on each takeoff was indicating
a perfect running engine until I reached about 100 AGL. This is when the
engine is able to wind up and the fuel flow is at the maximum. It did not
do it on run up or high speed taxi. Hope this is of some help.
Pat Brunner
LVP
-----Original Message-----
From: Lancair Mailing List
[mailto:lml@lancaironline.net] On Behalf Of Rick
Argente
Sent: Tuesday, June 05, 2007 6:15
AM
To: lml@lancaironline.net
Subject: [LML] Hickman's Accident:
NTSB Probable Cause Report
The NTSB's probable cause report is now out on Dave
Hickman's accident:
http://www.ntsb.gov/ntsb/brief.asp?ev_id=20060522X00601&key=1
http://www.ntsb.gov/ntsb/GenPDF.asp?id=NYC06LA112&rpt=fi
The National Transportation Safety Board determines
the probable cause(s) of this accident as follows:
The pilot's failure to maintain
sufficient airspeed after takeoff to preclude a stall, which resulted in a loss
of control and an inadvertent stall. Factors associated with the accident are
the inadvertent stall, the loss of engine power due to the pilot's inadvertent
activation of the high pressure auxiliary fuel pump, and the pilot's failure to
abort the takeoff after receiving abnormal engine and fuel flow warnings on the
primary flight display.
IMHO, I find it difficult to believe that
accidentally activating the auxiliary fuel pump will cause the fuel flow to
increase approximately 10 gallons/hour (see detailed report) and cause the
engine to fail. I read the report a few times and cannot find any testing
of the engine fuel pump. Only the electric/auxiliary fuel pump was tested
based on the report.
Has any IV drivers here ever accidentally switched
the aux fuel pump on while in flight? What happened?
-Rick