I am about to install the
pressurized door seal on my unpressurized LIV. .
For my aircraft, I wonder if the
mating silicone tape that is bonded to the door frame is truly required.
The greatest delta P I can imagine across the door is about 0.3 psi, far short
of the 5.5 psi of the pressurized aircraft. I can see that the silicone
tape may be required to hold the door seal in place against the pressurization
forces, but it seems like overkill for the unpressurized
aircraft.
Earlier discussions suggested
reducing the air pressure from 20 psi to about 11 psig (if I recall correctly)
to extend the seal lifetime. This was for pressurized
aircraft.
Questions:
1)
Can I eliminate the silicone tape on the door frame
and let the seal seat on the paint of the door frame? Eliminating the
silicon tape would save a step and provide a cleaner
installation.
2)
Can I further reduce the required pressure? I
would think I could go to a low pressure (say 5-8 psi), flight test, raise it
a bit if I get a leak, test again, etc.
Any of you non-pressurized guys
have any advice or recommendations?
Thanks,
Fred
Moreno