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OEI landing DA42

So the question is: When does an over-temp event on a Thielert and/or Austro require an engine tear down or replacement ?

Last Edited by Michael at 08 Jun 17:25
FAA A&P/IA
LFPN

When the computer says so. :)

An aside, I’ve operated TIO540s in very hot climates and there are times that the oil goes ‘off’ rather rapidly at about the 25-30hr point resulting in low oil pressure and high temps (both still in the yellow but going the wrong way). A precautionary shutdown is company SOP under such circumstances.

Fly safely
Various UK. Operate throughout Europe and Middle East, United Kingdom

If you ejected the coolant you will be lucky (and quick off the mark with a shut down) not to over temp and require a tear down or replacement but the diagnostics report I understand will be the determining factor. I hope you are lucky.

Hi Emir, which engines do you currently have?

Thielert 2.0

LDZA LDVA, Croatia

Update:
- root cause – broken clamp – by its condition it can be concluded that it was partially broken when installed (different colors along the crack – the beginning is corroded while the rest is new) – probably a mistake of guy who changed the hose
- consequence – coolant started to leak when hose slipped which caused insufficient quantity of coolant in the system which caused rise of temperature
- result – water pump was damaged with too hot coolant which caused additional leakage of coolant through broken pump
- diagnosis – everything is ok with engine, timely shutdown prevented any damage
- fix – changed pump and clamp, tested on ground and in flight – everything is OK

LDZA LDVA, Croatia

Great news, Emir. A perfect example of twin redundancy over water.

A perfect example of twin redundancy over water.

Actually it was water then mountains and night.

Last Edited by Emir at 11 Jun 04:06
LDZA LDVA, Croatia

Emir, congrats on the good outcome!
In a SEP this would have turned into a Mayday very quickly, especially at night and over water/terrain.

You won’t notice stuff like a partially broken clamp during preflight checks.
The Thielert 2.0 is a reliable engine but it needs to be maintained properly. Switching to the 2.0S will give you more HP, and a known maintenance history. But since the 2.0S is just a modified 2.0 engine, it won’t have a better safety record.

Emir wrote:

root cause – broken clamp – by its condition it can be concluded that it was partially broken when installed (different colors along the crack – the beginning is corroded while the rest is new) – probably a mistake of guy who changed the hose

What’s the liability situation in a case like this?

ESKC (Uppsala/Sundbro), Sweden
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