TM 55-1680-358-12 & Proller assembly (13); right-hand inboard ramp rollerassembly (14); and ramp extension roller assembly (15)for cracks or breaks. No cracks or breaks are allowed.3-5. Special Tools and Equipment. No special toolsare required to maintain the Helicopter Internal CargoHandling System. All common tools required can befound in tool kits available to aircraft maintenancepersonnel.3-6. Disassembly.Disassembly of the system is notrequired, except as necessary for replacement ofspecific components (refer to para 3-7).3-7. Repair and Replacement.The components listedin Table 3-1 may be replaced as required, without thenecessity of removal of any other components. Refer toSection III for specific part numbers and locations.Table 3-1. Replaceable PartsDescriptionLocationOutboard teeter roller shaftsSee Section 3 of Chapter 3Inboard teeter roller shaftsSee Section 3 of Chapter 3Transition roller shaftsSee Section 3 of Chapter 3Inboard roller shaftsSee Section 3 of Chapter 3Ramp extension shaftsSee Section 3 of Chapter 3ShaftsSee Section 3 of Chapter 3Inboard rollersSee Section 3 of Chapter 3Outboard rollersSee Section 3 of Chapter 3Cotter pinsSee Section 3 of Chapter 3Split cotter pinsSee Section 3 of Chapter 33-8. Tolerances.There are no wear tolerances thatapply to the Helicopter Internal Cargo Handling System.Replace parts only if damaged. (Refer to paragraphs 3-7 and 3-10.)3-9. Torque Values.Table 3-2 lists torque values tobe applied to fasteners of the Helicopter Internal CargoHandling System.Table 3-2. Torque ValuesTorque inPart NumberDescriptionInch-Lbs18049 D 555Special Bolt100 to 140AN3-10AHex Head Bolt20 to 25AN3-11AHex Head Bolt20 to 25AN4-5AHex Head Bolt50 to 70AN4-11AHex Head Bolt50 to 70AN4-12AHex Head Bolt50 to 70AN6-13AHex Head Bolt160 to 190AN8-17ABolt480 to 690MS21250-05028Point Bolt100 to 140NAS517-4-11Countersunk Bolt50 to 70NAS517-4-12Countersunk Bolt50 to 70NAS6608-14Hex Head Bolt480 to 690NAS6608-15Hex Head Bolt480 to 6903-10. Assembly.Assembly of the system is notnormally required, except when necessary forreplacement of specific components. (Refer toparagraph 3-7.) Reassemble in reverse order ofdisassembly.3-11. Preservation. Refer to Section V.3-2
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