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'ตารางท 5 - 6 Helicopter and Refueling Vehicle Characteristics.
Helicopter Overrall Dimensions,(m) Weight, (tons) Design Contact area Contact Takeoff (hard surface)
designation maximum Gera load Pressure. Sea level. O wind.ft
Design lenght width height Rasic takeoff Gear type (kgs.) (sq.cm.) PSI Ground run clear 15 m.

OH-6A a 9.2 8.0 2.5 0.58 1.2 Skid 1,161 14 0 0
OH-13H 12.6 10.7 2.9 0.98 1.38 Skid 625 0 103
OH-13S 13.2 11.3 2.8 0.96 1.43 Skid 0
OH-23G 12.4 10.5 3.1 0.87 1.4 Skid 568 0 65

UH-1B 16.1 13.4 3.9 2.27 4.25 Skid 1,955 0 0
UH-1D a 17.4 14.6 4.0 2.46 4.75 Skid 1,932 1,910 18 0 0 ข-5
UH-19 19.0 16.2 4.6 2.87 3.95 Single-quad 497 57 57 0
CH-21C 26.3 13.4 4.8 4.45 7.10 Single-tricyle 2,976 342 115 0 0

CH-34 20.1 17.1 4.8 4.0 6.80 Single-conventional 0 0
CH-37B 26.8 22.0 6.7 10.75 15.50 Twin-conventional 6,364 50 170
CH-47A a 29.9 18.0 5.6 9.02 16.50 Twin-quad 5,557 Main 291 Main 138 Main 0 0
CH-54A a 27.0 22.0 7.7 10.4 21.00 Single-tricycle 7,727 Main 607 Main 181 Main 0 0
AH-1G 16.1 13.4 3.5 2.78 4.75 Skid 0 0

Vehicle Gross Weigth Weel confiuration Tire Pressure Tire contact area Tread

Truck, 2 1/2 ton 6x6 kg. psi sq.cm. cm.
1,200 gallon 10,048 Tandem axle,dual wheel 45 246 176,Front
186,Rear