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  1. alexeu

    MIL-A-008865 vs MIL-A-8865B

    Does anyone knows if MIL-A-8865B is the superseding document for MIL-A-008865? There are no history for MIL-A-008865 except that it is cancelled with no replacement. Anyone out there have a copy of MIL-A-008865? Thank you Regards aeu
  2. alexeu

    Crash Loads For Military Aircraft

    To all who have analysed or certified antenna installations in the Radome area, what are the typical crash load factors that were used? Is there also any references that defines those crash load factors? Regards AEU
  3. alexeu

    Knockdown Factor For Cold Worked Material

    Consider this, a skin panel is sitting around waiting to be loaded on the assembly jig. However, it is found that approximately 1" x 5" of the edge has wrinkled due to mishandling of the skin panel. After cold working, and the wrinkling has been straighten, a conductivity test on the damaged...
  4. alexeu

    Freeze Plug Concentricity

    For all liaison stress engineers and DERs out there, here is a detail which I never got any answer to, 1) Does a freeze plug install in a parent material has to be concentric to the blueprint rivet hole (i.e. equal wall thickness on all sides), if not, then is there a reference that tells or...
  5. alexeu

    Shaving of Rivet Heads For Countersink Fasteners

    Recently, I have been asked of the maximum allowable of material to be removed from a fastener head for a countersink rivet to be considered structural. As an example, A NAS1097AD7 rivet in a 0.040 inch thick 2024-T3 materia, the maximum depth of countersink using Boeing guideline is 66% of...
  6. alexeu

    Fastener Allowable

    Can anyone out there help me with the following fastener allowables (i.e shear strength, tensile strength) a) NAS 623 b) NAS 603 c) MS 35206 d) NAS 514 e) NAS 602 f) NASM 27039 If at all possible, does anyone know where I can download the spec sheet. Thanks in advance

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