TM 55-2200-001-12Sec. 6-Fig. 39AIRCRAFT WINGS AND AFT SECTION MOUNTED ON WOOD FRAME, UNBOXED ON SKID BASE-FLAT CARSItem No. of Pcs.DescriptionABrake wheel clearance. See Fig. 2.B6 per wing, 4 ea.Anti-Skid Plates, pattern 63. Locate between skids of units and floor, as shown. Load must beper AFT Section.stenciled on both sides in one Inch letters to read, "Anti-Skid Plates".C 1 ea. end of load.Each to consist of two pieces 2 in. x 4 in. length equal to width of load. Secure lower piece tofloor with six 30-D nails and top piece to one below in like manner.D3 ea. Item "C".Each to consist of two pieces 2 in. x 4 in. x 24 in. Locate suitably spaced, as shown, against Item"C". Secure lower piece to floor with six 30-D nails and top piece to one below in like manner.E6 ea. per wingEach to consist of two pieces, 2 in. x 4 in. x 24 in. Locate at each side of load as shown. Secureunit; 4 ea. perlower piece to floor with four 30-D nails and top piece to one below in like manner.AFT Section.F2 per wing sec-2 in. x .050 in. high tension bands. Locate as shown, attaching to opposite stake pockets of car.tion. 1 per AFTSubstitute, if desired, steel cable 3/8 in. x 6 x 7.Section.G2 per wing sec-2 in. x .050 in. high tension bands. Locate as shown, attaching to opposite stake pockets of car.tion. 1 per AFTSection.See General Rules 4, 5, 7, 9, 10, 11, 14 and 15 for further details.E-49
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