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Adapter plate failed !!!

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  • #16
    Re: Adapter plate failed !!!

    Originally posted by ERicter View Post
    It's a McCauley 7142 put on when I bought the plane in August of 14. It is broken all the way around, at high rpm no vibration because it was pulling forward and locking in.

    Gary brought up a good point about the ring gear. If that has anything to do with it. I'm happy to be in one piece and have the craft also.

    Haven't talked to Fred yet Gary.
    7142?

    What model? 1A90? 1B90?

    7142 is too short according to TCDS.

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    • #17
      Re: Adapter plate failed !!!

      It's Eddie's choice of course, but involving the FSDO comes with a degree of risk. I'd not do it if it were me without first consulting my with maintenance folks and agreeing on a plan of action.

      Bringing in inspectors who may have no idea what the part is can create confusion, strife, and a great paper inquisition. Was a MDR filed; were there preceding activities that may have led to the failure of the part; and how's everybody's logs and documentation BTW? I needn't go on.

      I went through this with my former PA-11 and their unrequested presence due to major issues from a lack of prior maintenance. While eventually ending well due to plenty of $ and a conformity inspection it made the well qualified mechanic's job more stressful than it needed to be.

      It also assumes they're capable of diagnosing the source(s) of the problem, and unless they are, then what will they bring to the party?

      Gary
      N36007 1941 BF12-65 STC'd as BC12D-4-85

      Comment


      • #18
        Re: Adapter plate failed !!!

        All good points Gary but I would not want to have someone hurt or killed due not having this looked into.

        It is a very odd failure.

        Dave

        Comment


        • #19
          Re: Adapter plate failed !!!

          Yes I agree it needs to be examined, and the how of best to do that is out of my frame of reference and training. I suggested to Eddie he have the prop looked at for conformity (maybe as you noted via TCDS compliance plus balance and pitch). The other components...hub assembly, starter gear, and crank runout would be good to look at.

          Having it done with his mechanic's agreement is important.

          I guess a question needs to be asked: Where would someone find similar reports of failure? I looked on the FAA's "broken or defective stuff reports" but couldn't bring up anything regarding the failed A-3745 part.

          And yes going forward safety is #1 even if it takes some form of suggested or mandatory inspection procedure or interval. If it doesn't depart the plane a broken part and excessive vibration can create a hazard in flight and a distraction to the plane's occupants. Think "auto rough" over bad terrain or water.

          EDIT: I believe Eddie has a McCauley 1A90 round tip @ 71/42. It's Item 7 in TCDS A-696 I think so's that ok for a C-85 with tapered crank?

          Gary
          Last edited by PA1195; 04-26-2016, 18:31.
          N36007 1941 BF12-65 STC'd as BC12D-4-85

          Comment


          • #20
            Re: Adapter plate failed !!!

            I see another AD in the works......
            N29787
            '41 BC12-65

            Comment


            • #21
              Re: Adapter plate failed !!!

              Originally posted by PA1195 View Post
              Yes I agree it needs to be examined, and the how of best to do that is out of my frame of reference and training. I suggested to Eddie he have the prop looked at for conformity (maybe as you noted via TCDS compliance plus balance and pitch). The other components...hub assembly, starter gear, and crank runout would be good to look at.

              Having it done with his mechanic's agreement is important.

              I guess a question needs to be asked: Where would someone find similar reports of failure? I looked on the FAA's "broken or defective stuff reports" but couldn't bring up anything regarding the failed A-3745 part.

              And yes going forward safety is #1 even if it takes some form of suggested or mandatory inspection procedure or interval. If it doesn't depart the plane a broken part and excessive vibration can create a hazard in flight and a distraction to the plane's occupants. Think "auto rough" over bad terrain or water.

              EDIT: I believe Eddie has a McCauley 1A90 round tip @ 71/42. It's Item 7 in TCDS A-696 I think so's that ok for a C-85 with tapered crank?

              Gary

              I assumed it was an A65, was that a bad assumption?

              Comment


              • #22
                Re: Adapter plate failed !!!

                This plane with the C-85 upgrade: http://gallery.taylorcraft.org/main....3332&g2_page=1

                Gary
                Last edited by PA1195; 04-26-2016, 19:33.
                N36007 1941 BF12-65 STC'd as BC12D-4-85

                Comment


                • #23
                  Re: Adapter plate failed !!!

                  yeah, that's not normal failure for those. You either had a bolt torque related failure or at some point in its life that hub had been in an accident.

                  Comment


                  • #24
                    Re: Adapter plate failed !!!

                    Bolt torque? For discussion and not being an A&P I looked up what I could in the most recent C-85 Overhaul Manual I have, and both Sensenich and McCauley's data on prop torque for the SAE 0 tapered crankshaft that I could find.

                    Continental's O/H Manual calls for 200-220 in/# or 16.7-18.3 ft/# for the SAE 0 tapered crank.
                    McCauley lists 25-30 ft/# but that may be for a SAE 1 flanged crank as I couldn't find a specific listing for the SAE 0.
                    Sensenich lists 23-23 ft/# for their SAE 0 tapered crank installation.
                    Taylorcraft lists 65-75in/# but I assume it's for a wooden prop in their Service Manual subject to crushing.

                    Once the hub is mounted to the prop I can't see where the differences these torque values are that critical for metal props...it's a bolt torque that sets a pre-tension stress value on the bolt and nut fasteners and a compression value for the mated components. However if initially under tightened or if a loose condition develops through wear between adjacent components, then unwanted movement may occur and stresses develop.

                    It may be wrong so please correct as required.

                    Gary
                    N36007 1941 BF12-65 STC'd as BC12D-4-85

                    Comment


                    • #25
                      Re: Adapter plate failed !!!

                      What if the previous prop was not certified for this craft??

                      Throw another twist to the tale. Thanks for all.
                      FYI. Another adapter has been found in anchorage by my mech. Am going to check prop out.

                      To most of these questions I do not know the answers, Gary knows more than I do. He is correct on prop. I leave it up to mech. But I am learning for sure. I can not help but think that my preflight was not good enuf!!! Will be putting more torque on prop, will find out how much is acceptable, I always pushed and pulled, like one old pilot said as we were gathered around the Craft, "Congratulations, this will make you a better pilot". I will tighten up the prefilight, I take responsibility for this one, I believe it was there before takeoff and didn't find it.

                      Comment


                      • #26
                        Re: Adapter plate failed !!!

                        What if the previous prop was not certified for this craft??

                        Throw another twist to the tale. Thanks for all.
                        FYI. Another adapter has been found in anchorage by my mech. Am going to check prop out.

                        To most of these questions I do not know the answers, Gary knows more than I do. He is correct on prop. I leave it up to mech. But I am learning for sure. I can not help but think that my preflight was not good enuf!!! Will be putting more torque on prop, will find out how much is acceptable, I always pushed and pulled, like one old pilot said as we were gathered around the Craft, "Congratulations, this will make you a better pilot". I will tighten up the prefilight, I take responsibility for this one, I believe it was there before takeoff and didn't find it.

                        Comment


                        • #27
                          Re: Adapter plate failed !!!

                          The previous prop may have been longer than recommended Eddie but who knows why and what happened, just like all this thread. Don't beat yourself up...continued airworthiness is a shared and often foggy experience. Your alive and aware..."pay attention" a 26,000 hr pilot said when asked by me how he'd survived. The rest is FAR's and locating and hiring the best you can for maintenance.

                          The issue is what the owner has as responsibilities versus the maintenance person. Choose wisely is simple to say but that takes more than most owner/operator/pilots know. We're all still learning.

                          Gary
                          Last edited by PA1195; 04-27-2016, 08:40.
                          N36007 1941 BF12-65 STC'd as BC12D-4-85

                          Comment


                          • #28
                            Re: Adapter plate failed !!!

                            Awhile back i had a taper crank overhauled and the man at the shop asked if i already had my prop which i did not and his advise for the taper shaft engines was to use a wood prop only his theory was the weight of the metal prop and the power pulses are what caused the cracking in the shafts on these engines at the keyway area. Not this particlier problem but one to throw out.

                            Comment


                            • #29
                              Re: Adapter plate failed !!!

                              I flew my BC12D Wednesday and had read this thread before that so I looked for ways to check the back of the hub during pre-flight inspection.

                              Turns out to be quite easy.

                              You can see the back of the prop hub by opening and lifting the top cowl on either side and looking forward thru the hole in the nose bowl.

                              Very easy, might need so cleaning tools like cloth, tooth brush, butter spreader to scrape with...

                              Dave

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                              • #30
                                Re: Adapter plate failed !!!

                                If you look at Eddie's pic above pay particular attention to the separation pattern and exposed cracks. Each hole has a pointed separation; the exposed cracks I saw on the actual unit were oxidized, not shiny, and displayed a layer of brown (corrosion?). There was surface fretting on the adapter>starter gear interface (haven't seen the gear itself yet) and ring marks on the bolts (possibly from twisting from removal of the prop). I assume the prop had the rear internal spacer bushings but didn't see if it did.

                                I'd guess the cracks had some time to corrode as they developed; whatever time it takes to do that. I'd also guess the assembly may have lost fastener torque over some unknown period that allowed things to eventually go bad.

                                Gary
                                N36007 1941 BF12-65 STC'd as BC12D-4-85

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