Me stoooopid.
So, it's education time, as I need to learn this. How does the fuel injection system work? I have only a basic knowledge.
What I'm especially interested in... What are the failure modes that could cause a dual engine failure on a Seneca. So far, I can think of...
1. Pilot error in its many forms (both on crossfeed, crossfeed in the wrong direction after engine failure, pulling the mixtures, incorrectly identifying and shutting down the wrong engine, etc. etc.)
2. Fuel contamination.
3. ??? (I'm not in much of a thinking mode yet today, got home at 3:30 AM)
Water in the fuel and cold weather spells for potential ice accumulation in the fuel servo, and this can effect and shut down both engines. The fuel servos put simply regulate the amount of fuel that goes to the distribution block and consequently the nozzles. Mechanical fuel injection as it is used on aircraft, is a constant flow excess volume system feeding the servo. The positive pressure in the feed system is maintained by the "pill", a restricting orifice in the fuel return port which is post fuel usage port. If you clog the pill, the pressure at the fuel usage port increases which in turn increases the pressure and flow at the nozzles which will in effect richen the mixture. The ice can further accumulate and totally block the fuel flow to the usage port. If that happenned to me, especially if I had just fuel the aircraft, I would suspect moisture in the fuel and ice blocking the pill. The reason I would suspect this, is because until PROVEN otherwise, I always suspect what will kill me. Wishfull thinking has no place in aviation.