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camber-toein-toeout
Posted: Wed Jun 11, 2003 10:37 pm
by phantomphixer
Can anyone give me any info on toein/toeout and camber settings/measurements for a "55" C170B? I've looked at the shims and realize they are tapered front to back and top to bottom. Does the Cessna 170 Service Related Articles Manual have this info? And is it worth the price?
Posted: Thu Jun 12, 2003 12:12 am
by GAHorn
The Cessna 100 Series has this info. The camber, toe-in/out should be zero degrees at 2,000 lbs. weight.
Posted: Thu Jun 12, 2003 5:32 am
by russ murri
Is that level or tail down? I did mine with the tail on the ground loaded up to full gross. Russ
Posted: Thu Jun 12, 2003 2:53 pm
by 3993v
the owners manuel for a 48 sais wheels should have zero toe in and zero camber at approximately 2000 lbs. weight in the three point taxi attitude. nick