Cruisemaster accident at Falcon Field

leadsledfan

New member
A red and white master had the gear collapse on landing today at Falcon field. I think it might be the master with the extended range wing tanks that was for sale.
Everyone was ok, and the damage didn't look too bad.
 
My sister was flying out of falcon field and sent me a (grainy) photo. The door was open, plane was on its belly, definitely a cruisemaster. White on the top half, red on the bottom half. Only red and white cruisemaster I know of in phoenix is the one that was for sale (listed in our fly market).
The story I was given was that everyone walked away unharmed, and the pilot was quoted as saying the "gear collapsed" on landing.

Luckily, if it is the master for sale in our fly market, the engine was fairly high time anyways, so a decent time for a rebuild!
 
Looks like it was in fact the master in our fly market that had the gear collapse.

http://www.kathrynsreport.com/2017/02/bellanca-14-19-2-cruisair-senior-n9842b.html?m=1
 
Very sad, but at least no injuries. Better than the people that crashed in Riverside. Feb 27 was a bad day.
 
I have written to Ron, the owner of record, to learn more information and offer some help. He is a member of the forum as well and a very nice guy. I will post whatever I find out.
 
As an aside,
Given the landing gear design on our birds, the only way I can imagine it "Collapsing" would be if it was only part way down? Or am I wrong?
Perhaps it was a hydraulic issue?
 
Adam, there are several possible failure modes that will result in a collapse. Certainly a problem in the hydraulic circuit can be one such cause, often by the inadvertent retraction of the gear when the pilot meant to reach for the flap lever. The design intent of the gear is that drag strut should be adjusted to go "over center" upon gear extension. In addition to the static force of the hydraulic cylinder there is a spring designed to hold the strut in this position. Because there should be virtually no "retraction" force acting on the drag strut at this point, even the relatively small spring should keep the gear extended. Remember the hydraulic power pack does not maintain pressure on the actuating cylinder after the level pops back to the neutral position. If there is a leak anywhere in the system the hydraulic cylinders are not actively holding the gear down with any force - only force is coming from the spring.

Now, looking beyond the hydraulic system a frequent cause of gear collapse is the bracket that attaches the drag strut to the rear spar. This, of course, was the subject of a recent thread which we all participated in. Another failure can occur if the scissor mechanism fails, usually due to a problem with one of the bolts.

I did have an email exchange with the owner of the plane in the Falcon Field accident. The gear collapsed after a normal landing. Sadly this was a demonstration flight with a prospective buyer of the plane. He did indicate there was minimal damage to the airframe, but an engine and prop teardown will be necessary. The owner does not yet know where the failure was and given his obvious grief over the situation I did not press him for more information. As time goes by we will learn more.
 
Well as sad as it is, I'm glad the previous owner was at the controls, seeing as it is most likely insured.
Hopefully there will be a newly repaired cruisemaster with a 0 time engine and prop on the market soon!
 
As an aside, given these modes of failure, is there a way to know that a failure has occurred before landing?

Would the wing indicators still be all the way up?

Would the gear indicator lights be green or unlit?
 
Adam, in reality there are some failure modes that cannot be detected from the cockpit. Of course the pop-up visual indicators and the green "gear down" indicators are the first level of confirmation - if you don't have these indicators looking as they should you probably have a problem. However there are other scenarios where everything looks good on final, but only after the gear touches the runway or you apply the brakes, thus placing a load on the various components, does the actual failure occur. Prevention by good maintenance is by far the best medicine here.
 
Rob,
Thanks!
I think that my gear is going to come off at some point soonish to replace the springs in the gear, so I will look into the mentioned parts.
 
Adam, I have parted out a lot of Cruisairs, and the rear spar bracket for the gear has been cracked on many of them. There is a SB or AD (I cant remember which) to remove paint and check for cracks. In actually removing the brackets, I have found several that had cracks on the inside that were not visible with the bracket still on the spar. The Cruismaster rear spar bracket is a better design, but if you are going to be working on your gear, it might be worth a couple of extra hours to pull the rear brackets for inspection. This might be overkill, but maybe worth the trouble. The other thread about the cylinder attach bracket is one to pay close attention to. Just my 2 cents worth. ____Grant.
 
Grant,
I remember checking my crusair spar bracket at the last annual, I'll do the same for this one.
Has anyone compiled a list of the parts needed for a gear refreash? Seals and such?
I know the springs are occasionally produced but that should be fairly straightforward
 
Adam, I went looking thru my note book and found the numbers for the seals for the retract cylinders. AN 6227B-19 (3 each), AN6227B-7 (1 each) AN 6227B-10 (1 each). That is the number per cylinder. I think I got the numbers from Dan, but I am not sure. They worked fine for rebuilding mine. I bought them from Aircraft Spruce. I hope it helps. _____Grant.
 
Thanks Grant!
I am more worried about the packings and what not inside the gear legs themselves, which seem to be a problem on the crusairs.
Hopefully they aren't elk hide on the master?
 
As a side note, where would I go about finding the drawings for the gear leg taxi springs?
Is there a diagram that shows assembly / disassembly of the gear legs?
 
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