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  1. USACompositeGuy

    JT8D - Pratt and Whitney Service Bulletin Supplemental Document No 5411

    I'm working on an old JT8D and have a copy of SB 5411, however there is a Supplemental Document referenced "Supplemental Document No 5411." Which I'm having a hard time finding. Does anyone have a copy?
  2. USACompositeGuy

    Service Bulletin 727-55-0092

    This is an old aircraft that I'm working on, does anyone have a copy of Boeing Service Bulletin 727-55-0092? Thanks
  3. USACompositeGuy

    Freeze Plugs in 6AL-4V Titanium

    Does anyone have any references for installing freeze plugs in Titanium? The SRMs cover installation of freeze plugs and bushings in aluminum however I can’t find anything that provides this same level of guidance in titanium. I have reviewed this thread...
  4. USACompositeGuy

    A356 Casting Conductivity

    I am trying to find a source for the %ICAS value for the conductivity of A356 Cast Al. I am doing an on-wing inspection to check if an overheat condition changed the temper of a casting. It is A356-T6, but I can't find this value in any of the traditional documents. I can find hardness from...
  5. USACompositeGuy

    Rockwell Hardness B Values for A356-T6 Casting

    I have an A356-T6 casting that was repair welded and stress relived per AMS 2771. The AMS spec sends you to the material spec which provides Brinell values for process verification coupons. I only have access to a Rockwell B hardness machine and can’t find a conversion factor from Brinell to...
  6. USACompositeGuy

    Effects of UV on epoxy composite laminates

    I would like to know if anyone has any recommended literature for the short term effects of UV exposure on a carbon/epoxy laminate. By short term I mean a few days and exposure would be to the sun on an unpainted laminate.
  7. USACompositeGuy

    How to analyze the stress caused by a Freeze plug

    I have a fitting that has oversized fastener holes. The upper and lower portions of the fitting (flanges) are approx. .180 thick and have ample edge margin to support a freeze plug from a standard tear out strength vs fastener shear (Each flange can support higher load than the fastener shear...
  8. USACompositeGuy

    Post Weld Heat Treat/Stress Relief Requirements

    Does anyone have any recommendations for books on the topic of post weld heat treatment/stress relief? I am having a hard time finding some general guidelines as to when PWHT is required and what the effects of not doing it actually are. I am analyzing weld repairs on aircraft engines...
  9. USACompositeGuy

    Post Weld Stress Relief For CRES

    I am currently working a repair of an elongated fastener hole on the flange of a Duct assembly. The duct material is 0.063" thick 321 Annealed CRES per MIL-S-6721, Comp T1. The repair is to fusion weld the surfaces using AMS 5689 filler. I am unsure if it is possible to not perform a post...
  10. USACompositeGuy

    TR Sleeves -RB211-535E4-Rohr Drawings.

    I am working on a composite repair for the TR sleeve on an RB211-535E4 engine. The actual TR sleeves are made by Rohr. I am in need of a DWG for the TR sleeve. The damaged area is located on the outer skin in the lower corner of the part at the slider fitting. The area has a graphite doubler...
  11. USACompositeGuy

    British Aerospace BAER 3068

    I also posted this in the Composite section, but I think it is as or more relevant here. Does anyone know a good source to find the BAER specs? I am specifically in current need of BAER 3068. I know this is a 350 degree Prepreg Carbon, 5-H Satin Fabric, But I need to know the specifics. In...
  12. USACompositeGuy

    BAER (British Aerospace) Specs

    Does anyone know a good source to find the BAER specs? I am specifically in current need of BAER 3068. I know this is a 350 degree Prepreg Carbon, 5-H Satin Fabric, But I need to know the specifics. In addition I would like to have a QPL (Qualified Purchase List) or a cross-reference for...
  13. USACompositeGuy

    Bombardier Learjet Data

    I am currently working on a repair for a Bombardier Learjet. We do not usually work on these aircraft and therefor do not have any technical information on them. I was wondering if anyone has any information on these planes, specs, allowables, SRMs, etc.... Any help you could provide would be...
  14. USACompositeGuy

    Starting a new consultant business, need advise!

    A co-worker and I are considering starting a consultant business on the side. We have already accomplished several jobs and feel that to truly reap the benefits we must become a real business. We work in the commercial airline industry and the majority of our work is for the military. It is...
  15. USACompositeGuy

    Airbus Composite Design Allowables

    Does anyone know what airbus uses for composite design allowables? Do they have a spec like Boeing, MD, etc…, or do they use vendor test data? Can anyone provide any information on this?

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