TM 55-1680-358-12&P(5) Install three hex head bolts (30, Figure 3-2)and flat washers (31) to secure each ramp center rollermounting plate (12, Figure 3-11) to the helicopter rampfloor.(6) Attach each inboard ramp roller assembly(13 and 14, Figure 3-2) to forward and aft ramp centerroller mounting bar assemblies (16 and 17). Use twohex head bolts (36), flat washers (33) and self-lockingnuts (37). Make certain that the flat washers are usedunder the component which turns, either the nut or bolt.e. Ramp Skid Pad. Install ramp skid pad (20,Figure 3-2) as follows:(1) Refer to steps 2-9a. and 2-9a.(1) andFigure 2-13 to gain access to screw locations.(2) Install ramp skid pad (20, Figure 3-2) asshown in Figure 2-19, using previously removedhardware. Seal ramp skid pad periphery with (PR-1440-Class B) BMS-5-44 Sealant.2-10. System Installation - Ramp Extension RollerAssembly. Install ramp extension roller assemblies(15, Figure 3-2) as follows:a. Ramp Extension Roller Assemblies.Install rampextension roller assemblies (15, Figure 3-2) as follows:(1) Position a ramp extension roller assembly(15) on the left ramp extension. Make sure that sixquick-release pins (1, Figure 3-12) engage the holesdrilled in paragraph 2-7 as shown in Figure 2-20.(2) Install the remaining ramp extension rollerassembly (15, Figure 3-2) on right ramp extension asdescribed in paragraph 2-10b.(l).b. Ramp and Ramp Extension Support Assemblies.Install ramp support assembly (19, Figure 3-2) and rampextension support assembly (18) as follows:(1) Refer to Figures 2-21 and 2-22 and positionramp support assembly (19, Figure 3-2) so that indexsupport ramp support weldment (1, Figure 3-15)engages both ramp support holes in ramp skid pad (20,Figure 3-2). Adjust support assembly to the properheight.(2) Refer to Figures 2-21 and 2-22 and positiona ramp extension support assembly (18, Figure 3-2)under each ramp extension roller assembly (15) so thatramp extensions support index support (1, Figure 3-14)is engaged. Ensure that FWD/AFT marking on supportassembly is oriented parallel with aircraft centerline.2-30
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