Maximum payload and terrain mobility package validated through Government testing on mission profile, at gross vehicle weight rating.
Roll-Over Protective Structure (ROPS) engineered using finite element analysis (FEA) to exceed FMVSS 216 load standards. Fully TIG welded chromoly tubing anchored through multiple points to vehicle frame rails and completely non-removable.
Multi-point latch-style safety harnesses installed at each seat position.
Compression-ignition diesel/JP-8 engine avoids dangers associated with spark-ignited systems and gasoline engines.
Safety and situational awareness are enhanced through occupant comfort systems. These include a removable cabin enclosure, doors with operable windows, windshield with wipers and washers, heating/air conditioning climate control, sliding and reclining seats, rear view mirrors, and turn signals.
Hendrick Commando includes a mechanical emergency brake system that is independent of the regular hydraulic brakes.
Centrally located transmission shift lever and emergency brake lever allow occupants other than driver to stop vehicle if necessary.
Patented MIL-STD-209K certified system for CH-47 helicopter internal air transport (HIAT) available.
On Board Diagnostics (OBD) system enhances safety through fault code reporting and factory prepared troubleshooting procedure.
Hendrick Commando completed Army ATEC safety evaluation prior to OCONUS deployment.
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