According to the FAR's if fir is up to spec it can be used in any area that
spruce is used.
>Wing ribs?
>From what I remember, (if that is right) douglas fir of the same
>dimentions, is heavier, and slightly stornger than spruce.
Fir is about 25% heavier and about 21% stronger than Sitka Spruce.
>I am just wondering in which areas of construction douglas fir could be
>used, whithout violating some reasonable conventions of safety. And also
>just how much you would save in money and gain in weight, if you used as
>much douglas fir as would be resonable. Its just that spruce seems so
Cost savings varies, but if you can find a good deal on fir it can save you
up to 80%.
Gordon Nichol
Steve Eldredge
Stan Hall (Cherokee II wooden sailplane designer) had a rather nice
article on just this topic in Soaring magazine back in the 70's.
I'll see if I can find the reference, as it was very well done and
should answer just about all of your questions.
The essentials, as I recall, are that a direct substitution is quite
possible with about a 16% increase in weight, although the dimensions
can be reduced (due to greater strength) in a few select applications.
The drawbacks to fir are wilder grain, slightly less glue-ability, and
a greater propensity to split and splinter. And weight, of course.
The article was quite positive overall, however, and Stan (for whom us
oldtimers have great respect) was definitely in favor of the substitution
in most cases.
BTW, I believe this article (as part of a SHA (Sailplane Homebuilder's
Association) series of articles) was also reprinted in the EAA Wood
Aircraft Constuction Handbook, although I could be mistaken.
Craig Wall
The article describes the different attributes and contains tables
of data.
I think that would answer your questions
Regards,
Mark Morin,
Montreal, Canada