Quote:
Originally Posted by rjbob
What make & model jet was it?
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The problem is not the make or model, it was the compressor wash that was done without flying and drying the engines , before it was put away.
It was quite a sequence of events in hindsight.
The morning of the dual oil pressure loss it was pulled out of a warm hangar into -26 deg C , then quickly filled with -26 deg C fuel before cranking up and doing a rolling checklist to avoid ice buildup before take off.
On take off we went through 3000 feet of light mixed icing in seconds.
13 minutes into the flight and passing 32500 for 38K planned, the master warning lit up. The RH oil pressure dropped to 2 psi from normal in less than 3 seconds. Right side was shut down as the pressure hit zero. While calling ATC for the turn around, the left side did the same as the right. I heard something that sounded like "Cheese is nice" from the other seat, then he looked at me and said we won't be shutting this one down.
The AMO was the same company that looked after the provincial air ambulance fleet at that time.
If you ask me, the heat from the oil in the PW615's was not sufficient to overcome the volume of cold in the -26 Deg fuel and the oil got too viscous in the filter elements (right after the heat exchangers) Or it was ice crystals from water in the oil system from the compressor wash.
The pressure in the LH engine recovered slightly before landing, but that was from the bypass valve unseating. Evidently the damage to the bearings was done while there was no pressure for a few moments (or minutes) before the bypass unseated.
To answer your question it was a Mustang 1 / C510.
The AMO, the owner and the PIC were all happy to believe the G1000 had a tiny brain fart. The truth hit home when the left side seized a few days later.
I am reminded the Robinson R44 helicopters have a lower engine failure rate per 100K hours with IO 540's than Bell 206's do with allison turbines.