Hello,
Has anyone seen any data related to the in-service breakdown of liquid shim in aircraft? I've seen some papers on it, but no real life reports.
TIA
In looking at failure conditions, should the resulting stresses be compared against Ftu or Fty. Is the criteria different between military and commercial programs.
Thanks.
Can someone reccomend from firsthand experience, test houses that perform static and/or environmental testing at a reasonable cost. They should be able handle composite and metallic structures-parts.
I'm also looking for one that handles composite database qualification testing.
Thanks
Does anyone know if there is/was an FAA requirement for thermal, mechanical, or other anti-ice system to be incorporated in the horizontal stabilizer leading edge on commercial aircraft? I haven't been able to find any mention in 2 days of web searching.
I worked on the MD11 HS years ago in the...
