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  1. thomasng

    Torque loading of panel

    Hi.. thanks for the prompt reply.. On some aircraft panel, we're using ziploc fastener (hexagonal stud and square receptacle) and cam-loc fastener (same type of square receptacle but torque bit stud).. And all these fasteners requires a torque loading of 30-35 inch pound. My question is, why...
  2. thomasng

    Torque loading of panel

    Hi all Can i know why aircraft panel on aircraft using Ziploc and camloc fastener need to be torque laded? How abt those panel using screws (e.g. NAS 1153) especially dorsal panel? Thanks in advance! Cheers!

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