by david.2.wilcox » Thu Sep 01, 2016 2:56 pm
Hi Ed,
I have converted a tailwheel Sonex to a nose wheel, N607LT. My main reason for doing so was for ground/taxi visibility. Tailwheel takeoffs and landings were no problem.
The 50 labor hour estimate was a good one. The advice to wait for an existing nose wheel plane to come onto the market was also good.
But if you go ahead with your plan... You can shorten the standard gear struts for the tri-gear mounts. The axles are the same. I am not familiar with Sonex standard mechanical brakes. This would be a good time to get rid of them. You'll need to obtain the main gear spar mount trusses, an engine mount, the nose wheel parts and a tail skid.
The firewall penetration for the nose wheel steering arm (per Sonex plans) would never pass AC20-135 fire proof requirements. I mention that because I know of one person that decided not to build because of that. It doesn't worry me too much, as long as it will stop smoke.
I found that drilling the main strut holes on the bench is much easier than on the aircraft.* There are a group of holes for flat head screws that hold the spar gear trusses to the main spar. These screws need to be flush on the inside of the spar box. Normally the holes are prepared by dimpling, which will not be possible with the spar already completed. You will have to countersink the inner spar skin and cap using a right angle drill while reaching inside the box.
This would be a major modification, so depending on the vintage of the airworthiness operating limitations, this would put you back into phase one restricted flight. For that you need to contact the local FSDO to agree on a new restricted flight area unless you are in the same location as the original builder. When I contacted FSDO, I proposed 10 takeoffs and landings as being more appropriate for the landing gear change than the standard 5 hours flight time. The FSDO inspector agreed.
*I have built a Sonerai, but not a Sonex. I resurrected my Sonex from a wind damage incident. It was flipped upside down in a microburst at TUS. I replaced everything north of the center longeron and a repaired a lot more.
I have photos of the bench drilling setup of the gear holes. Below are the airframe logbook entires that I made for the tricycle gear modification:
2013-07-20 TSN 351.6
Converted to tricycle landing gear. Tricycle gear components from N997KK except as noted. Drilled legs on bench setup for .7 degrees toe-in per axle. Added bolt bushings at all eight locations. Mounted gear trusses to aircraft using alignment tool from Sonex plans. Installed main gear trusses onto spar box using AN509-12 flat head screws. Holes countersunk on the inside of the box. Two screw stems ground for roll control stop clearance. Roll control stops shortened 1/8 inch for screw clearance. Dynon ADAHAR relocated to cross beam on second bay behind seat. Dynon OAT sensor moved to turtle deck behind radio antenna. Dynon roll servo remounted to clear left gear truss. Parking brake valve installed on master cylinder. Brake lines rerouted and bled. Removed Arduino trim control box. Installed RAC T2-10A elevator servo. Fabricated and installed Sonex tail skid L03-07 per plans. Installed engine mount Sonex part number P12 from N414SX, zero time. Removed carburetor heat box. Replaced oil separator with Sonex part. Weight and balance data: Left 253, Right 252, Nose 131, Total 636 empty. Nose arm -28.4, Spinner arm -52.4, Main arm 24.7. Calculated empty weight center of gravity 13.8 aft of leading edge. Flight restrictions per Scottsdale FSDO, Copeland: "The Phase I restrictions for your aircraft are acceptable. Aircraft movement is limited to KPAN and KFFZ. Instead of 5 hours, you must make 10 takeoffs and full stop landings to complete the Phase I requirements." Aircraft is under phase one flight restrictions.
2013-07-21 TSN 353.9
I certify that this aircraft has completed ten landings as prescribed above and shows no detrimental characteristics, is controllable throughout the flight envelope, and is safe for operation.
David Wilcox
A&P xxxxxxx