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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...- thomasng
- Post #3
- Forum: Aircraft engineering
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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!- thomasng
- Thread
- Replies: 2
- Forum: Aircraft engineering
