Downloaded from https://www.everyspec.com MIL-STD-810C 4 Wo -------------- Ji4 H? pz. , G , \o/ b%/ I ~,cn / I .04 - I I I t f 1 I I I I I I 1 I I t I I I I I 1 L 1 15 VAR 300 1000 2000 FREQUENCY (Iiz) RANDOM VIBRATION ENVELOPE o -2 - . -4 - -6 - ., I I ! I 1 80 100 120’ 140 160 EQUIPMENT WEIGHT-LBS REDUCTION FACTOR FOR MASS LOADING Figure 514.2-2A. Random Vibration Test Curve and l.lassLoading Reduction Factor for Jet Aircraft Equipment. METHOD 514.2 514.2-24