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22 I <br /> 7.3 MAXIMUM PAVEMENT LOADS: MODEL 787-8, 787-9, 787-10 I <br /> VNG = MAXIMUM VERTICAL NOSE GEAR GROUND LOAD AT MOST FORWARD CENTER I <br /> OF GRAVITY <br /> VMG = MAXIMUM VERTICAL MAIN GEAR GROUND LOAD AT MOST AFT CENTER OF <br /> GRAVITY <br /> H = MAXIMUM HORIZONTAL GROUND LOAD FROM BRAKING I <br /> NOTE: ALL LOADS CALCULATED USING AIRPLANE MAXIMUM DESIGN TAXI WEIGHT <br /> 1 <br /> A I <br /> I <br /> i..• 0 000000000 0 0000000000000000...• ^� 000000 0000 ✓ - <br /> in <br /> o O..O <br /> V NG I <br /> H I <br /> VMG <br /> I <br /> VNG VMG PER H PER STRUT <br /> STRUTMAX <br /> AIRPLANE DESIGN STATIC AT STATIC+ AT STEADY AT I <br /> MODEL UNIT TAXI BRAKING LOAD AT BRAKING INSTANTANEOUS <br /> MOST WEIGHT FWD C.G. 10 FT/SEC2 STATIC 10 FT/SEC2 BRAKING <br /> DECEL AFT C.G. DECEL (µ=0.8) ' <br /> LB 503,500 54,716 85,086 229,798 78,194 183,838 <br /> 787-8 <br /> KG 228,383 24,819 38,594 104,234 35,468 83,388 <br /> LB 561,500 47,006 76,161 259,564 87,201 207,651 I <br /> 787-9 <br /> KG 254,692 21,322 34,546 117,736 39,554 94,189 <br /> LB 561,500 42,193 68,209 261,787 87,201 209,430 <br /> 787-10 <br /> I <br /> KG 254,692 19,138 30,939 118,745 39,554 94,996 <br /> I <br /> I <br /> I <br /> I <br /> D6-58333 <br /> REV M March 2018 7-5 I <br />