BMS 9-8 Allowables
BMS 9-8 Allowables
(OP)
I have an Airbus A-320 nose landing gear door. The outer skin is cracked in the monolithic area at the upper aft end of the door, aft of the aft hinge. I am looking to substitute BMS 9-8 dry carbon fabric and EA 9396 resin for the SRM callout of G-806 fabric and Ciba Redux 501 resin. I would be willing to sell our director of quality's soul to the devil for a copy of the BMS 9-8 allowables so I can compare baseline values. We don't want to buy a roll of the G-806 to do one repair. I have the Airbus allowables. Willing to do some horse trading.





RE: BMS 9-8 Allowables
You need a more compelling offer. Hell is already overpopulated with quality people.
RE: BMS 9-8 Allowables
RE: BMS 9-8 Allowables
2) I don't know of a way to legally get a copy of the Boeing allowables for BMS 9-8/BMS 8-301.
3) There are some allowables published in Mil-Handbook-17, Volume 2, section 4.2.27 for T300/EA9396. T300 is qualified to BMS 9-8. EA9396 is qualified to BMS 8-301.
Hope this helps,
Steve
RE: BMS 9-8 Allowables