Advanced Aero Safety, Inc.
                                         
"LTDS"   "Low Thrust Detector Systems"
                                
                               

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Fuel Pump Failure

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Survived  -  In-Flight Breakup

CHOMERICS

 Advanced Aero Safety, Inc.

  Dear Mr. Hall,

 I operate out of a 1,700’ grass runway, which inclines slightly to the north. It has a 400’ very soft overrun which is part of a runway extension that is under construction. The overrun terminates in a 15' deep gully. Immediately beyond the gully there are trees 35 to 40 feet above the mean height over the runway.

 My aircraft is a Seneca II and has a Robertson Conversion with full span fowler flaps and spoilers for roll control.

 Two weeks ago I lost an engine just after takeoff. The plane had 60 gallons of fuel and three heavy guys in it. We took off to the north because winds of 3 to 5 mph favored that direction. The standard STOL departure is 30 degrees of flaps with rotation at 60 knots. The aircraft broke ground at about 750', at which time the flaps were reduced to 20 degrees. I was waiting to get out of ground effect before retracting the gear when the plane yawed sharply to the right about 20 feet above the ground. Immediately thereafter your zero thrust indicator on the right engine was activated. (It was interesting to learn that the noise and the light, both of which I thought were inadequate in practice, seemed very bright and loud at that moment.) I continued the takeoff by feathering the right engine and retracting the gear. A ground observer said the gear was in the wells by the 1,7001 mark. The engine was completely feathered just as I cleared the trees, which I missed by about ten feet. My airspeed at that moment was 61-62 knots. Flaps were reduced to 10 degrees. The trees in my line of flight were rising and I was able to climb above them. I was able to break left and swap altitude for airspeed by descending over the hillside which fell away to the west, during which time flaps were fully retracted. I landed uneventfully at a nearby airport.

 The Seneca, with full take-off power in the left engine, was able to climb at approximately 100’ per minute at 89 knots (VYSE).

 The diaphragm in the fuel pump had ruptured, a failure, which simply could not have been predicted. The plane is very well maintained, the Robertson Conversion works perfectly and I have had good training, but I must say that the immediate confirmation of right engine failure by your zero thrust indicator probably saved my ass.