The pilot side door is now installed along with the door handle and strike plate. The directions were lacking, and a backing plate needed to be made for the provided handle. I unscrewed the inside latch and measured the distance between the screw posts and the center piece.
After making the backing plates the handle was positioned using the backing plate and internal handle to determine where the strike plate needed to be.
The backing plate was then used as a template to drill into the fiberglass door and the handle as screwed together.
On the passenger side the door was thicker than the pilot side. This caused the screws not to reach through and thread into the door handle.
PROGRESS:
Controls ~2h ( 2h )
Fuselage ~251h ( 3h, 3h, 2h, 3h, 7h, 2h, 5h, 2h, 3h, 2h, 2h, 3h, 6h, 2h, 2h, 1.5h, 2.5h, 1h, 2h, 3h, 2h, 3h, 4h, 1h, 2h, 1h, 3h, 4h, 3h, 3h, 4h, 3h, 4h, 4h, 6h, 3h, 3h, 4h, 2h, 2h, 2h, 4h, 2h, 2h, 10h, 4h, 4h, 6h, 3h, 4h , 6h, 3h, 2h, 2h, 5h, 2h, 3h, 3h, 2h , 2h, 3h, 4h, 1h, 1h, 1h, 1h, 3h, 1h, 2h, 2h, 5h, 6h, 3h, 5h )
Wings: ~157.5h ( 1h, 1h, 0.5h, 2.5h, 4h, 1h, 1.5h, 1h, 1.5, 4.5, 1h, 1h, 2h, 4h, 1h, 3h, 1h, 2h, .5h, 1.5h, 2h, 2h, 2h, .5h, 1h, .5h, .5h, 2h,3h, 1h, 3h, 3h, 4h, 2h, 3h, 7h, 3h, 1h, 4h, 1h, 1h, 1h, 4h, 2h, 2h, 2h, 2h, 1h, 2h, 3h, 2h, 1h, 3h, 2h, 2h, 1h, 2h, 3h, 2h, 1h, 1h, 1.5, 2h, 2h, 3h, 2h, 1h, 3h, 2h, 1h, 2h, 1h, 5h, 2h, 1h, 2h, 4h, 2h, 3h, 3h, 3h, 2h, 3h, 2h, 3h, 6h, 3h )
Flaperons: ( DONE! ) 23.5 hours spent ( 3h, 1h, 1h, 1h, 1.5h, 3h, 6h, 3h, 4h, 1h )
Paint Design: 2 hours spent ( 1h, 1h )
Elevator DONE!: ~31.5 hours spent ( 3h, 1.5h, 3h, .5h, 3.5h, 2h, 4h, 1.5h, 2h, 4.5h, 1h, 6h )
Horizontal Stabilizer DONE!: ~28 hours spent, 3 pieces replaced ( 3h, 2h, 2h, 2h, .5h, 1.5h, 3.5h, 1.5h, 5, 4.5, 2h, .5h )
Rudder DONE!, minus horn : ~16 hours spent, ( ~8h, ~8h )
-----------------------
Total Done: ~510h
Showing posts with label problem. Show all posts
Showing posts with label problem. Show all posts
Sunday, October 05, 2008
Monday, December 31, 2007
It funny, there is no mention of drilling one of the seat back channels into place with the seat back. And when I say no mention... nothing the manual, nothing in the HBH videos, nothing in the Matronics archives. Here is a method for drilling 7F6-5 into place that I used:First, finding the notes in the plans was hard, so it is A4, pitch 40.
Don't worry about drilling it into the extrusion gusset yet. Draw your centerline on the flange that meets the seat back and push into place. I had one hole on the side extrusion that I had to match, but you are lucky you can just drill the flange into the uprights. Once the back support is positioned, extend the center line onto the uprights.
Cleco the seat back into place over 7F6-5. Now extend the centerline from the uprights onto the seat back. Now space your rivets making sure to take into account where the vertical ("L") will go in the seat back.
I drilled four test holes to make sure I had extended the line properly, which I had. The remaining holes were then drilled.
I also had to trim the bottom tabs of the engine mount for a good fit. Sadly the radius bend in the lower mount is causing fit issues. the solution may be shims, grinding away part of the frame rails, or both.
Here are some pictures detailing the issue.
PROGRESS:
Fuselage ~148h ( 3h, 3h, 2h, 3h, 7h, 2h, 5h, 2h, 3h, 2h, 2h, 3h, 6h, 2h, 2h, 1.5h, 2.5h, 1h, 2h, 3h, 2h, 3h, 4h, 1h, 2h, 1h, 3h, 4h, 3h, 3h, 4h, 3h, 4h, 4h, 6h, 3h, 3h, 4h, 2h, 2h, 2h, 4h, 2h, 2h, 10h, 4h, 4h, 6h)
Wings: ~157.5h ( 1h, 1h, 0.5h, 2.5h, 4h, 1h, 1.5h, 1h, 1.5, 4.5, 1h, 1h, 2h, 4h, 1h, 3h, 1h, 2h, .5h, 1.5h, 2h, 2h, 2h, .5h, 1h, .5h, .5h, 2h,3h, 1h, 3h, 3h, 4h, 2h, 3h, 7h, 3h, 1h, 4h, 1h, 1h, 1h, 4h, 2h, 2h, 2h, 2h, 1h, 2h, 3h, 2h, 1h, 3h, 2h, 2h, 1h, 2h, 3h, 2h, 1h, 1h, 1.5, 2h, 2h, 3h, 2h, 1h, 3h, 2h, 1h, 2h, 1h, 5h, 2h, 1h, 2h, 4h, 2h )
Flaperons: ( DONE! ) 23.5 hours spent ( 3h, 1h, 1h, 1h, 1.5h, 3h, 6h, 3h, 4h, 1h )
Paint Design: 2 hours spent ( 1h, 1h )
Elevator DONE!: ~31.5 hours spent ( 3h, 1.5h, 3h, .5h, 3.5h, 2h, 4h, 1.5h, 2h, 4.5h, 1h, 6h )
Horizontal Stabilizer DONE!: ~28 hours spent, 3 pieces replaced ( 3h, 2h, 2h, 2h, .5h, 1.5h, 3.5h, 1.5h, 5, 4.5, 2h, .5h )
Rudder DONE!, minus horn : ~16 hours spent, ( ~8h, ~8h )
-----------------------
Total Done: ~410h
Sunday, September 23, 2007
Recap of the question posed to the Matronic's Zenith list:
Photos of the gap problem with the ("L") angle that attaches from the top skin to the baggage back.


I'm having a bit of a problem. The ("L") angle that attaches to the top of the baggage back is off by exactly 10mm. This seems strange since every other junction is dead on, and the longeron splices are exactly even between the sides and the top. The flanges for the bulkheads were dead on.
So this leads me to believe it is a CNC error, but it's a little hard to get up there to measure and prove it.
Anyway, this has produced a gap too big to shim and I'm not sure what to do about it. One thought I had was to move the angle forward, but then the existing holes would be directly over the baggage back and the vertical ("L") angles.
My other idea was to ignore the gap basically since when I test fit the baggage back only the area near the gap didn't site flush. So I would add some extra rivets towards the inside of the panel to make up for it, and maybe add two gussets. My guess is that two rivets on each side would have to be skipped.
Photos of the gap problem with the ("L") angle that attaches from the top skin to the baggage back.


Subscribe to:
Posts (Atom)
