In aviation maintenance, "level" is flat. 

When you weigh an aircraft to determine empty CG, for instance, it is
placed on jacks and leveled--both along the X-axis and along the Y-axis
as well. However when an aircraft such as the 172 is sitting (empty) on
a ramp, the "pitch attitude" is determined in large part by the
inflation of the oleo nose strut. With the proper oil quantity and
nitrogen gas inflation, the strut will be extended by some distance. As
the main gear legs are relatively rigid, it is therefore the nose strut
that will determine the angle in question. In Aviation Maintenance
school, we were taught that the proper distance is "about a pack of
cigarettes," which is about 3 inches give or take, and allows for a
compromise of view over the nose during ground operations, and the
avoidance of bottoming of the strut upon landing. However to some
degree, there is a range of acceptable values--and one person's "pack of
cigarettes" is another's cigar, I suppose. Never having been a smoker I
simply measured it at about three inches, and this is the value I always
tried to achieve. But I stress that this is only a guideline, as it is
rare to achieve an *exact* degree of extension; simply due to the nature
of the process. And as soon as the pilot/copilot/passengers get into the
aircraft, this amount changes of course.

That being said, I believe that I do have access to service manuals for
the 172-series of aircraft. Although I don't work in the industry any
longer, several friends do--and I could likely get the proper dimensions
from one of them without any difficulty. I will make a couple phone
calls and report back in a day or so. Given the limitations of setting
the exact oleo strut inflation, I would simply recommend that the nose
angle be computed and set based upon the dimensions given in the Cessna
drawings, which *should* be available in the service manual.

TB


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