Spin Training

That was due to the worn plastic collar around the control yoke tube shifting sideways when it was pulled full aft. When you pushed it forward, it locked in place.
.....and when the NTSB scrapes your bone fragments out of the control linkage and says "gee, look at that", the details don't really much matter to the pilot.
 
If you get time though, I'd like to read your more extended thoughts on the cause of the AD.

I think the original AD is stupid because in the two crashes cited the investigators found that the aircraft did not have correctly installed rudder horns/stops. There was no evidence of problems with the original design.

Tom Carr of CPA, an experienced A&P mechanic with decades of experience concerning Cessna aircraft maintenance, commented that since the two aircraft involved in fatal spin-related accidents cited in the proposed AD issued in 2007 were not in compliance with the aircraft’s type design the issues surrounding the proposed AD were better served by the issuance of a Special Airworthiness Inspection Bulletin, rather than an AD.

NTSB from Crash 1:
Examination of the wreckage revealed that the rudder was jammed approximately 35°, which is beyond its left travel limit. Further examination revealed that the two rudder bumpers had been installed inverted and that the right rudder bumper had traveled beyond the rudder stop and had locked behind it

Crash 2:
Examination of the wreckage revealed that the rudder was jammed beyond its left travel limit. Further examination revealed that the two rudder bumpers had been installed inverted

If they really needed to issue an advisory on this it should've simply been a mandatory inspection to ensure the rudder horns/stops were installed according to original type specs.

The 150 has a very solid spin safety record, there was no need for this AD, it was a shotgun reaction that I can only imagine had some other political motivation behind it.

If 150's are going to jam rudders during full deflection, why is it that during ground steering, where full deflection is used all the time for tight turns, we dont see rudders jamming up all the time? They made a non-issue into a problem, they should retract the whole thing.
 
.....and when the NTSB scrapes your bone fragments out of the control linkage and says "gee, look at that", the details don't really much matter to the pilot.


Been there on both ends. I made it out through a combination of good training and luck. Had a few friends that weren't so lucky. I just happened to have time & altitude on my side, they didn't. All were a result of control malfunctions/failures (This was during during aerobatic flight NOT spin training. None were in a flight school plane). Mine was the only one that could not have been discovered through regular preflight/MX, the wing had to be torn apart. The causes were found and corrections or operating practices were changed as a result, preventing the problems in the future. I'd say there's a purpose. It's just extremely unfortunate how certain problems only seem to get noticed after a fatality. And that just stresses how important a thorough preflight and proper MX really is on airplanes that will be operated as spin trainers. You need mechanics looking for things that wouldn't normally be a problem. Parts should be replaced as they wear NOT when they break....

As pilots we try the best we can to mitigate risk. But there comes a point were you have to accept no matter how hard you try, you just can't plan for the unknown. If you think your 100% in control of the outcome of every flight, you're just fooling yourself. Better off staying on the ground if that bothers you. The pilots in the Tomahawk did the best they could with a really bad situation. If I remember right, after the spin stopped they kicked the yoke to break it lose. Ill have to look it up...

Training for control failures often get overlooked and there nothing for it in the PTS. Honestly, if I had to choose, I'd rather have an engine failure. At least you can still fly the airplane.
 
If 150's are going to jam rudders during full deflection, why is it that during ground steering, where full deflection is used all the time for tight turns, we dont see rudders jamming up all the time? They made a non-issue into a problem, they should retract the whole thing.

During a spin the empennage tends to flex a bit. For a 150, I really don't know how much. I've never seen a video of the tail section during a spin. This would be though to duplicate on the ground. I believe that was the reasoning behind giving the new stops so much more surface area.
 
That's like saying "I'm not going to fly aerobatics because the prop governor might fail, or the spar or rib might be cracked or a control surface might jam, or my 'chute might not open, or.... or...." Lots of things can happen and that's what a good preflight and MX is for.

Right, but why would a flight school want to risk that for some random guy? I think that is what he was getting at. Lots of risk with little reward for your normal, generic flight school.
 
Right, but why would a flight school want to risk that for some random guy? I think that is what he was getting at. Lots of risk with little reward for your normal, generic flight school.

MX wise, if your fleet of 172s (or any approved trainer) is maintained properly there's very little risk compared to normal flight training. They probably don't want to spin their IFR trainer or have a syllabus addressing spin training. If its not something you're used to doing on a regular basis you really need to take a step back and make sure all your ducks are in a row. I think the schools are doing good by directing him elsewhere. He will no doubt get a better & more thorough experience.
 
NTSB from Crash 1:
Examination of the wreckage revealed that the rudder was jammed approximately 35°, which is beyond its left travel limit. Further examination revealed that the two rudder bumpers had been installed inverted and that the right rudder bumper had traveled beyond the rudder stop and had locked behind it

Crash 2:
Examination of the wreckage revealed that the rudder was jammed beyond its left travel limit. Further examination revealed that the two rudder bumpers had been installed inverted

Man... that had to be a hell of a way to go. Terrifying.
 
Hi,

I'm having a real difficult time finding someone to give me spin training in the North NJ/NYC area. I call flight schools and they give me the "You are better off contacting someone with a decathlon or other aerobatic plane." Which is fine if these people would actually call me back, but they don't. Is the aviation teaching industry in such good shape that they don't need new clients?

Anyway, can anyone suggest an instructor or flight school that can give me the training in the Northern NJ or NYC/Long Island Area.

Thanks
Felix

Ocean Aire in Toms River, NJ has CFI's that offer spin training in their 152.
 
To OP...have you looked at the IAC website? They have a list of aerobatic flight schools.
What he said. Find an aerobatic school that will actually teach you about spins, have YOU teach spins (read the FAA requirement), and uses parachutes.
 
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