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(b)   Trailing Arm Assembly.
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TM-1-1520-238-T-4 Army Model AH-64 Helicopter (NSN 1520-01-106-9519) (EIC: RHA) Manual
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(d)   Wheel and Tire Assembly

TM 1-1520-238-T-4 3–16 3–7. SYSTEM DESCRIPTION (cont) 3–7 (e)   Normal/High–Impact Landing. During normal operation, the fuse collar holds the lower piston in an extended position. The lower cylinder is filled with hydraulic fluid which provides a solid column of fluid against the lower piston chamber. In the event of a high impact landing, the force shears the retaining flanges on the piston and rupture a burst–disc. The lower piston then moves into the cylinder and hydraulic fluid flows into the upper piston chamber at a restricted rate through an orifice. This action aids the upper piston in absorbing excessive shock loads by providing a controlled rate of collapse. (f)   Wheel and Tire Assembly. The wheel and tire assembly rotates on the trailing arm axle bearings. The wheel and tire assembly provides the helicopter with ground movement capability for taxiing, run–on landings, towing, aids in cushioning landing shocks, and provides parking support. M58-094A TRAILING  ARM ASSEMBLY PIVOT  CONNECTION STRUT  ARM VENT  PORT  (2) PIVOT  MOUNT HELICOPTER  FRAME UPPER  PISTON NITROGEN  FILL  PORT (LOWER  CYLINDER  CHAMBER) KNEELING  COUPLING  PORT CHAMBER) HYDRAULIC  FILL  PORT (UPPER  CYLINDER SHEAR  COLLAR CYLINDER (NORMAL  POSITION) LOWER  PISTON FAIRING SHOCK   STRUT   ASSEMBLY MLG  WHEEL AND  TIRE ASSEMBLY CROSS  TUBE ASSEMBLY HYDRAULIC BLEED  PORT RETAINING  PIN  (3) FUSE  COLLAR SQUAT SWITCH TARGET Figure   3–13. MLG Assembly

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