Thank you Sparweb.
I know that the interface load on the unit will be 9.0 Forward, 8.6 Down, 5.4 Up, 4.0 Side (+/-), and 1.6 Aft per Boeing requirements with a fitting factor of 1.33 and a 15% growth factor.
The LRU max. weight is 3.2 lbs.
No abuse loads are required by Boeing due to the size...
I'm fairly new to IFE and I was task to performed Interface load calculation for a video monitor. Can some one help? I have company previous test plans but I do not understand how they came up with the formulas. I have looked in Static books but was unable to locate any method to calculated...