findings - Pappas Waiex B Forced Landing
Posted: Thu Dec 16, 2021 9:29 pm
Well, the secret is out! I spent half of the day today with the NTSB rep that is handling the engine failure and off-field forced desert landing of my nice Red Aerovee Turbo Waiex B. We met at Air Salvage in Phoenix. After a summary external inspection, we removed the cowl. There was lots of oil in the lower cowl which gave me a start. We could not find any holes in the cases. I remembered that the aircraft was upside down and we determined that it had simply been leaking while inverted.
We knew from the Dynon Black Box data dump that the # 4 cylinder immediately went cold at the moment the engine started to run rough at 2500 AGL. I checked the timing adjustment cap and it was tight and as It was supposed to be. Next, we pulled and checked the plugs, borescoped the new heads and valves, (only 20 hours on the new EMPI's), checked compression, (the engine rotated normally), and all looked as it should. Next, we pulled the #3-4 Valve cover. After about a minute of looking, we noticed that the swivel pad on the #4 exhaust valve adjuster was missing! The NTSB rep found it in some oil in the valve cover we had placed on the table.
There are two swivel pad types on the valve adjusters available for the Aerovee according to the build manual. The swivel pad that came in my engine kit is the pad with a swivel ball with a flat spot, not the large one-piece swiveling pad. There are no apparent side loads or bending moments applied to this component. They only move up and down in a linear manner between the top of the valve stem and the rocker arm end. This one failed and separated from the threaded adjuster stud.
The result was that the #4 exhaust valve was held closed by the valve spring. It could not open to let the exhaust gasses out. We viewed the assembly manual and verified that the alignment of the remaining swivel pads seemed correct according to the images and description in the build manual. He took many pictures and sent me the two that I am uploading.
I believe that with the #4 exhaust valve unable to open, the fuel and air mixture backed up into the #3-#4 intake manifold then into cylinder #3 and caused backpressure into the upstream intake manifold. The resultant loss of power from #3 and #4 was exacerbated with the reduction of exhaust gasses available to drive the turbo. Essentially, I was running on 2 cylinders, next to no turbo, and the situation was deteriorating rapidly. The engine would have failed to run completely in a short period of time.
What is likely a $6.00 part, brought down my lovely bird. The good news is that last week I purchased a partially finished Vans RV7-A kit in California, loaded it in a 26 ft Penske box truck rental, and drove it to my hangar in Phoenix. More good news is that I bought back the salvaged Waiex from my insurance company. I will take the complete Dynon HDX avionics suite including, A/P, Coms, transponder, ADSB, Intercom, knob panels, LED Nav and Pos lighting, LED landing lights, VPX Sport, Tosten stick grips, Ray Allen trim motors, and position sensors.....and stick them all in the new RV7 over the coming year.
It appears I will have quite a few remaining parts, which, somehow, are all in excellent shape, from my Waiex to sell on barnstormers to help offset the cost of the new IO-360 and C/S prop I will need to buy.
All in all, this could have been much worse. The NTSB rep was extremely professional and helpful. He was appreciative that I agreed to come down and go through the engine with him and I was glad he asked. He said the input of the pilot and builder is very helpful to have. I am surprised at how seriously they are taking this incident. No deaths, no damage to people or property on the ground, experimental aircraft, and, compared to most GA events, a relatively low-dollar aircraft. I will update as more info becomes available. Fly safe guys.
We knew from the Dynon Black Box data dump that the # 4 cylinder immediately went cold at the moment the engine started to run rough at 2500 AGL. I checked the timing adjustment cap and it was tight and as It was supposed to be. Next, we pulled and checked the plugs, borescoped the new heads and valves, (only 20 hours on the new EMPI's), checked compression, (the engine rotated normally), and all looked as it should. Next, we pulled the #3-4 Valve cover. After about a minute of looking, we noticed that the swivel pad on the #4 exhaust valve adjuster was missing! The NTSB rep found it in some oil in the valve cover we had placed on the table.
There are two swivel pad types on the valve adjusters available for the Aerovee according to the build manual. The swivel pad that came in my engine kit is the pad with a swivel ball with a flat spot, not the large one-piece swiveling pad. There are no apparent side loads or bending moments applied to this component. They only move up and down in a linear manner between the top of the valve stem and the rocker arm end. This one failed and separated from the threaded adjuster stud.
The result was that the #4 exhaust valve was held closed by the valve spring. It could not open to let the exhaust gasses out. We viewed the assembly manual and verified that the alignment of the remaining swivel pads seemed correct according to the images and description in the build manual. He took many pictures and sent me the two that I am uploading.
I believe that with the #4 exhaust valve unable to open, the fuel and air mixture backed up into the #3-#4 intake manifold then into cylinder #3 and caused backpressure into the upstream intake manifold. The resultant loss of power from #3 and #4 was exacerbated with the reduction of exhaust gasses available to drive the turbo. Essentially, I was running on 2 cylinders, next to no turbo, and the situation was deteriorating rapidly. The engine would have failed to run completely in a short period of time.
What is likely a $6.00 part, brought down my lovely bird. The good news is that last week I purchased a partially finished Vans RV7-A kit in California, loaded it in a 26 ft Penske box truck rental, and drove it to my hangar in Phoenix. More good news is that I bought back the salvaged Waiex from my insurance company. I will take the complete Dynon HDX avionics suite including, A/P, Coms, transponder, ADSB, Intercom, knob panels, LED Nav and Pos lighting, LED landing lights, VPX Sport, Tosten stick grips, Ray Allen trim motors, and position sensors.....and stick them all in the new RV7 over the coming year.
It appears I will have quite a few remaining parts, which, somehow, are all in excellent shape, from my Waiex to sell on barnstormers to help offset the cost of the new IO-360 and C/S prop I will need to buy.
All in all, this could have been much worse. The NTSB rep was extremely professional and helpful. He was appreciative that I agreed to come down and go through the engine with him and I was glad he asked. He said the input of the pilot and builder is very helpful to have. I am surprised at how seriously they are taking this incident. No deaths, no damage to people or property on the ground, experimental aircraft, and, compared to most GA events, a relatively low-dollar aircraft. I will update as more info becomes available. Fly safe guys.