The Bell OH-58D Kiowa Warrior served as the U.S. Army's primary armed reconnaissance helicopter, operating a deployment footprint of 338 active-duty and 30 National Guard airframes. Engineered with an extremely low acoustic signature and high maneuverability, the Kiowa Warrior executes concealed target acquisition, artillery spotter guidance, and direct troop support while remaining undetected behind terrain features.
The defining feature of the OH-58D is its distinctive Boeing-produced Mast-Mounted Sight (MMS) mounted directly above the main rotor hub. Procurement officers can cross-reference critical replacement hardware using our military CAGE code to support fleet availability.
Flying nap-of-the-earth (NOE) missions exposes the Kiowa Warrior airframe and mast-mounted sensor assemblies to persistent operational friction:
Rotor Mast & MMS Thermal Degradation
Positioning sensor packages directly above the rotating main rotor hub transfers continuous mechanical vibration and turbine heat to optical gimbals and boresight alignment linkages.
Quick-Change Pylon Mechanical Fatigue
Repeated firing of .50-caliber machine guns and unguided Hydra 70 rocket pods generates dynamic vibration across wing pylon attachment points and electrical wiring harnesses demanding high-tensile hardware indexed across our rotary-wing platform database.
Low-Altitude Environmental Erosion
Hovering near ground obstacles subjects Rolls-Royce Allison 250 turboshaft engines and composite rotor blades to particulate ingestion, accelerating compressor vane erosion and main gearbox seal degradation, similar to maintenance requirements found in light utility helicopters.
Defense procurement officers must verify that replacement airframe parts, transmission bearings, and avionics modules carry total trace documentation back to approved OEMs or defense supply depots. Providing fully documented parts compliant with AS9120B, ISO 9001:2015, and FAA AC 00-56B quality protocols ensures seamless insertion into military flight lines without administrative holds.
| Crew | 2 pilots |
| Height | 12 feet 10.6 inches |
| Length | 41 feet 2.4 inches |
| Rotor Diameter | 35 feet |
| Maximum Gross Weight | 4,500 pounds (unarmed); 5,500 pounds (armed) |
| Maximum Airspeed | 125 KIAS |
| Cruise Airspeed | 80 KIAS |
| Endurance | 2 hours |
| Cargo Hook Capacity | 2,000 pounds |
| Litter Capacity | 4 (externally) |
| Troop-Carrying Capacity | 6 (externally) |
| Avionics | Data transfer system ground, data transfer module, data transfer receptacle in the aircraft; video tape recorder records up to 2 hours of co-pilot's MFD; ANVIS display symbology system provides basic flight information |
| Mast-Mounted Sight | Thermal imaging sensor; television sensor; laser range finder/designator; optical boresight system |
| Weapons | .50-caliber heavy machine gun; 70-millimeter folding fin aerial rocket; air-to-air Stinger missile; Hellfire modular missile system |
| Communication Equipment | Two VHF-FM AN/ARC-186; one UHF AN/ARC-164 Have Quick; one VHF-AM AN/ARC-186; two TSEC/KY-58; HF capable; FM homing; airborne target handover system |
| Navigation Equipment | Attitude and heading reference system (Litton LR-80 Inertial); AN/ASN-137 doppler; AN-ASN-43 directional gyro |
| Aircraft Survivability Equipment | A/APX-100 IFF; AN/ALQ-144 IR jammer; AN/APR-39A radar warning receiver; AN/APR-44(V)3 radar warning receiver; AN/AVR-2 laser detecting set |
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AS9120B and ISO 9001:2015 |
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Aviation Suppliers Association Member |
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FAA AC 0056B Accredited |
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AS 6081:2012 Certification |
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ESD S20.20-2014 Certification |
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