Yes it does.
If I soak the turbo in diesel, do you think that there is a chance of getting
it unstuck ?-Jeff Wilder CISSP,CCE,C/EH -BEGIN GEEK CODE BLOCK-
Version: 3.1 GIT/CM/CS/O d- s:+ a C+++ UH++ P L++ E- w-- N+++ o-- K- w O- M--
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An 8" inboard move on a 11.5' (= 23/2) wing would mean approximately a 6%
inboard move of the WAF point. Which would mean an increase to (1.06)^2 times
the shear load at the old WAF point and an increase to (1.06)^3 times the
bending moment at the old WAF point.
Hope that helps.
Ameet Savant
O
Jeff, the RayJay turbo runs in a shell bearing much like that in which a
camshaft runs, which uses oil to both lubricate and support the shaft.
If the engine has not run for as long as you say then it is possible the
bearing has seized. The other thing to note with regard to the RayJay
units i
Netters;
This is a little off the KR subject, but I think I will interject it
anyway. I've spent the last 2 summers flying out of Talkeetna, Alaska...which
was Don Sheldon's base of operations. You might find it interesting to know
that he is credited with crashing 32 airplanes. He is m
All,
For those who are interested, I have 2 engines for the taking.
1 Subaru E81b
1 Corvair ( I cannot find the serial #'s )
I am North of Denver. If I cant find a good home for them, I am going to send
them off to the junkyard/dump
-Jeff
All,
I have a Revmaster 2180 turbo which has not run in some time... I am trying to
figure out should I keep it.. or just source an O200 for it.
My question is this, the turbo impellers currently do not rotate. I've spent
some time and disassembled the intake out and output housing to remove
Hi Allen I down loaded this early today
Here's the one from http://www.ae.uiuc.edu/m-selig/ads/coord_database.html#A
.01454 .02625
.00721 .01805
.00240 .01003
.00014 .00239
.00041 -.00424
.00441 -.00990
.01248 -.01556
.02377 -.02150
Data just got corrupted along the line. .01454 .02625 0
.00721
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