airplane construction
wrote:
Robert M. Gary wrote:
Mike wrote:
Robert M. Gary wrote:
The 172 has a 7/16" bolt on the front spar attach, and a 3/8" at
the rear, IIRC without going downstairs and looking it up. Both are in
double shear. The bolt is stronger than the aluminum fittings, and the
fittings are much stronger than they look or need to be. The airplane
is rated for 3.8g positive, with 150% design limits beyond that, and I
can't remember the last time I heard of a 172 shedding a wing unless
the pilot tried to fly through a thunderstorm, in which case he'd have
died anyway. The stabilizer is weaker than the wing in many light
aircraft.
Agreed. I understand 172's are not falling from the sky, just an
emotional reaction to seeing what is actually holding the wings on. I
wonder what holds the wings on the C-177 if the struts old the wings on
the c-172.
The Mooney's one-piece wing spar is made of many smaller
pieces, all held together with tiny rivets. No stronger than the 172, I
bet. The Mooney's POH should give a g rating for the airframe.
The 3.8g limit you mention for the c-172 is just a function of the
certification category. Since the Mooney and the 172 share the same
category they are both 3.8g's with 150% minimum overdesign by
definition. Note sure what the actual structural limits are though. The
manufactors don't tell us the actual limits, just the certification
limits.
The Mooney is known for being amazingly strong though. Rememeber the
picture of the 201 coming off the line with several dozen people
standing on the wing? They flew that plane afterwards w/o problem. I
have a friend who survived a nasty accident in his 201 and credits the
steel tube cabin for saving his life.
Which reminds me: a friend recently told me of an accident in
the Southeastern US where a new Commercial pilot flew a Monney into a
thunderboomer at night. They found the wreckage scattered far and wide,
and the Mooney engineers that examined the bits and pieces estimated
that the aircraft experienced an upward acceleration of between 20 and
23 Gs. The passenger, complete with seat, went through the bottom of
the airplane and was found some distance behind the rest of the mess.
Even if the airplane had held together the occupants would have been
incapacitated or killed by the damage wrought by the acceleration.
Do you have a reference for this? A possible date range, the state if
happened in or something I can search on? I'd like to pull up the NTSB
on it.
-Robert
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