In the new edition of the 912 MML (Ed 4, Rev 2) I see that Rotax have introduced a new task in the 200h maintenance checklist: "Measure heat up of air intake." For the last week or so I've been trying to figure out how I would accomplish the new procedure (see 12-20-00, page 17) on my aircraft at its next 200h inspection. (fortunately not due for quite a while)
Having come up short on ideas myself, I figured that this would be a good time to ask for advice:
1. How does one extract a usable temperature measurement out of the specified Rotax P/N 222421 temperature sensor without a functional 912iS ECU? I cannot find any details on the electrical interface or calibration curve in any Rotax documentation, especially not in the manuals for a 912A.
2. I also can't find any sensor dimensions or mounting specs. Even then, I cannot see how you could perform the test using the specified sensor with my plane's airbox (see attached pictures) without making major modifications which would require an engineering order. (The aircraft is a Skyfox CA-25N. It's type certified but no longer has a type certificate holder)
Does anyone have some helpful suggestions, information or advice they could share?
(What's really annoying is that on this partictular airframe, the front of the airbox is the air filter - and it's in a ram-air inlet right on the front of the cowl. As long as carby heat is off, any warming of the air would occur in the ducts between the airbox and the carburettors — well after the temp sensor, somewhat defeating the purpose of the exercise)