Hmm...177? 210? I know our mechs use the one on 172 all the time. I trust their judgment that it won't break anything.
There was a service bulletin on one model calling for inspections I believe. I have heard it in more than one place. I used to be a mech, and build planes in a former life, but that was about 20 years ago. I still though am not totally ignorant on the subject. It is a poor practice. Either heed it or not...
Did a quick search and got this off AOPA site on doing preflights.
http://flighttraining.aopa.org/ft_magazine/fullstory.cfm?id=518&issue_title=July+1994
TAIL ASSEMBLY - 3
Make sure any exterior gust locks are removed from the tail and check the control cables and connectors to ensure everything is secure and not worn or frayed. Check the elevator and horizontal stabilizer/stabilator surfaces for damage. Dented or bowed surfaces are often not just skin deep; they may be an indication of structural problems.
Tail sections on Cessnas are particularly susceptible to structural damage caused by those who push down on them to raise the nose while repositioning the aircraft.
Don't forget to check the bottom of the horizontal surfaces; serious damage may be more likely to occur there. This area is prone to damage from rocks kicked up by the tires or from a tail strike during a botched landing. Also inspect the outer edges of the elevator or stabilator, and the tail tiedown, as they can also be damaged from a tail-low landing.
When inspecting a Cessna 152 damaged in a tail-low crosswind landing, the only evidence of damage on the top of the horizontal stabilizer was a slight inward bowing of the skin - a condition that perhaps a dozen pilots attributed to mere cosmetic damage. The aircraft flew for three weeks in this condition and nobody suspected a problem. Then a particularly observant student questioned the indentation and checked underneath the stabilizer, where he found major scrape marks on the bottom of the stabilizer tip. The bowing of the skin was due to a bent spar. The aircraft was unairworthy and the stabilizer had to be replaced.
On aircraft equipped with stabilators rather than horizontal stabilizers and elevators, grasp the stabilator on the outboard edge and check for any play in the hinge assembly. Excess play can lead to flutter and subsequent catastrophic failure of the control surface. Don't forget the trim tab. In one case, a cracked trim tab on a Cherokee required full nose down trim to keep the aircraft in level flight. Make sure it is securely attached and free of any cracks.
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then there is from apparently very experienced mechanic.
http://www.littleflyers.com/Questions/cessna/172issues.htm
Problems and issues with a high time Cessna 172
Sent: Sunday, February 15, 2004 12:28 PM
Subject: High Time Cessna 172
Roger,
What are the issues in buying a high time 1973 Cessna 172; total hours 9100?
Thanks,
P.A.
<HR>
Roger's reply,
The Cessna 172 is a good aircraft. However, high time aircraft tend to have issues. For the year you specify gear leg fatigue can occur, and the fatigue will cause the tires to wear very prematurely. The main gear support structure can crack or buckle. There is a high probability of firewall damage at the nose gear strut attach. Fuel tanks can be fatigued from the expansion and contraction of the fuel tank. Flap tracks can be excessively worn from very repetitive usage. The flap arms may be worn if the improved wear washers were not installed. Fatigue and cracking of flap skins may occur from the number of powered stalls performed. The horizontal stabilizer may be damaged from ground handling from pushing down on the tail. Finally, expect issues with baffles, exhaust, and the propeller. Roger