03 Jul 2025, 11:12 [ UTC - 5; DST ]
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Post subject: Re: Navajo asymmetric flap deployment - transmission failure Posted: 26 Oct 2017, 08:36 |
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Joined: 02/27/15 Posts: 119 Post Likes: +35 Location: Chicago, IL
Aircraft: Navajo
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Yeah Chris, You are right that SB 739 addresses the flexible shafts. BTW, you can download 739 on the piper website. http://www.piper.com/technical-publications-documents/Link to the actual document if it works... https://s3.amazonaws.com/pipercrm/Solut ... %20739.pdfI was just saying that regardless of the failure mode, the loss of control and corresponding use of 25 degree maximum flaps, along with all POH and performance changes (none in all but the pressurized models) are addressed there. In flying, it is nice to be able to say, "if this breaks, I won't die if I take actions a, b, c..." It just seems to me that once you put in 40 degrees of flaps (especially on a airplane with a system that you can't retract them once split) you can't say that anymore if anything fails that allows one flap to retract. Certain failure modes are common enough to warrant an AD, others are just bad luck. I realize that there are things on airplanes that if they break you are dead. But I would argue this doesn't need to be one of them. "Flaps at 25 to stay alive" 
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Post subject: Re: Navajo asymmetric flap deployment - transmission failure Posted: 26 Oct 2017, 10:15 |
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Joined: 08/15/11 Posts: 2579 Post Likes: +1182 Location: Mandan, ND
Aircraft: V35
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Username Protected wrote: It has to do with the size and position of the flap compared to the size and position of the aileron.
Put the flaps to 40 degrees and put the aileron all the way up and then go stand behind the wing of a navajo and you'll understand why that's not going to work out. Ailerons are neutral, but you get the idea... Attachment: 2017-10-26 06.22.43.jpg Attachment: 2017-10-26 06.21.42.jpg
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Post subject: Re: Navajo asymmetric flap deployment - transmission failure Posted: 26 Oct 2017, 16:04 |
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Joined: 02/27/15 Posts: 119 Post Likes: +35 Location: Chicago, IL
Aircraft: Navajo
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Username Protected wrote: Good info but this is old news and applies to many larger twins. This is the reason for keeping your hand on the flap lever in transit. If anything goes weird, immediately retract.
I do agree with not needing full flaps on final. The Navajo lands slow and short as it is. I was aware that split flap could occur in transition, that part is old news. I did not expect catastrophic type sudden retraction, that was news to me. Also, It is pretty clear to me that the part that failed is simply worn out to the point that the ball bearings were able to come loose. No signs of any other damage. Nowhere in the AD or even in the service manual does it say to inspect that part of the transmission. I think that is newsworthy. Hell, shops might rebuild the gear part of the transmission and call it "overhauled" for all I know. This part of the transmission may be as old as the airplane. It's concerning enough to me that I have an "overhauled" transmission with 50 hours on it on my other wing that I am now going to remove and inspect for this same condition.
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Post subject: Re: Navajo asymmetric flap deployment - transmission failure Posted: 31 Mar 2018, 08:24 |
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Joined: 03/30/18 Posts: 26 Post Likes: +6
Aircraft: Pa-31p
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Good job on the recovery but seems like a failure in the inspection. If the transmission failed at the jack screw then clearly the threads must have been completely worn. Should have been picked up during an annual inspection I also have the 40 to 1 flap transmission which allows 40 degree flap deployment and I make sure it is fully inspected at annual. One other thing I find unusual is using full flaps before turning towards the final approach fix. I never deploy full flaps until I'm assured of landing in case of a go around
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Post subject: Re: Navajo asymmetric flap deployment - transmission failure Posted: 03 Apr 2018, 11:15 |
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Joined: 06/17/14 Posts: 5925 Post Likes: +2669 Location: KJYO
Aircraft: C-182, GA-7
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Username Protected wrote: The pilot that was flying for me full time, up until a few months ago, had a full asymmetrical flap condition on a Cessna 310. This was about 3 weeks ago. It is a Robertson STOL equipped T310R. It wasn't a plane we were involved with, and I don't know the failure mode. Right flaps fully down, left all up. Said it took full power opposite engine, full aileron, rudder. But he managed it to the runway, no damage except the interior.  Pretty sure I would need new seat covers, too! Glad that everyone is still here to post today!
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Post subject: Re: Navajo asymmetric flap deployment - transmission failure Posted: 04 Apr 2018, 03:27 |
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Joined: 08/28/13 Posts: 339 Post Likes: +116 Location: KSEE
Aircraft: DGA-15P, C140A
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FYI, the mechanical term for that ball bearing screw is a "ball screw."
Much more reliable than a jackscrew/nut arrangement, especially when properly serviced.
E
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