Revisions to above pages posted on the mothership site dealing with sealing the rear window. The issue with the landing gear/channel has not been finally cleared but is that a skin doubler I see on page 25-06??
There was already a hint given to the doubler in the landing gear analysis pdf. My RV-12 is ready for paint but I wait now until the doublers and the final fix for the gear is available.
Revisions to above pages posted on the mothership site dealing with sealing the rear window. The issue with the landing gear/channel has not been finally cleared but is that a skin doubler I see on page 25-06??
No I don't know, but a huge amount of the engineering departments resources have been working on this since SB 12-09-2 was issued, so it hopefully wont be too much longer.
This is probably a silly question, but can you confirm that the instruction in the October 12 engineering update to drill out 60-70 rivets applies to BOTH sides of the fuselage? (In other words, is there a doubler on each side?)
This is probably a silly question, but can you confirm that the instruction in the October 12 engineering update to drill out 60-70 rivets applies to BOTH sides of the fuselage? (In other words, is there a doubler on each side?)
Yes, it applies to both sides.
Personally, my suggestion would be to wait until the fully developed service bulletin comes out before you remove rivets. The primary reason being that it will include info for removing blind rivets without damaging the existing holes.