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Contractor:
Sikorsky Aircraft, Division of United Technologies
Type:
- General purpose, single rotary wing, twin turbine powered helicopter with emergency amphibious capabilities
- Available in Anti-Submarine Warfare (SH-3H/D) and Utility (UH-3H/SH-3G) configurations
Power Plant:
- SH-3H/UH-3H: Two General Electric T-58-GE-402 turboshaft engines. Each engine can produce approximately 1,500 shaft horsepower. Standard since 1991.
- SH-3D: Two General Electric T58-GE-10 turboshaft engines. Each engine can produce approximately 1,400 shaft horsepower.
- SH-3G: Two General Electric T58-GE-8F turboshaft engines. Each engine can produce approximately 1,250 shaft horsepower.
Accommodations:
- SH-3H/D: Crew of four (two pilots, two sensor operators) and up to three passengers
- UH-3H/SH-3G: Can be configured for up to 15 passengers in addition to the aircrew
Performance: Return to Top
- SH-3D/H helicopters are capable of airspeeds up to 120 KIAS.
- Endurance varies between 3.5 and 5.5 hours depending on the mission.
- Maximum allowable weight (SH-3H/UH-3H): 21,000 pounds
- Maximum allowable weight (SH-3D): 20,500 pounds
- Maximum allowable weight (SH-3G): 19,100 pounds
- Provisions for carrying up to 6,000 pounds of external loads can be added.
Countermeasures:
Not applicable
Armament:
- Two MK-46/44 anti-submarine torpedoes
- Various sonobouys and pyrotechnic devices
Mission and Capabilities: Return to Top
- Class IB aircraft designed for both shore- and ship-based operations
- U.S. Navy missions have included anti-submarine warfare, search and rescue, and miscellaneous utility roles, including limited external cargo capability.
- In the ASW role, major sensors include: AQS-13 and AQS-18 dipping sonar systems, various sonobuoys, and the ASQ-81 Magnetic Anomaly Detector. In addition, airborne search and weather radar have been mounted on the radar.
- Fully configured instruments for all weather operations
- Capable of automatic approach to a stabilized sustained hover
- The Teledyne AQS-123 TACNAV, a Doppler-based tactical navigation system, is installed in the SH-3H and UH-3H.
- Provisions for installation of a Global Position System (GPS) are being added to some models.
Program Summary: Return to Top
- The SH-3H completed its last active duty deployment in 1995 and has been replaced in the USN carrier force by the SH-60.
- Eighty SH-3H helicopters will be converted to the UH-3H model, which are expected to remain in service with the U.S. Navy in a utility role through 2010.
- The U.S. Naval Reserves use six SH-3H helicopters in the ASW mission.
- The SH-3H and UH-3H have undergone a Service Life Extension Program (SLEP), which included improvements to the airframe, electrical wiring, main transmission, and main rotor systems.
- SH-3D/G models and a few out-of-service SH-3H aircraft have not received the SLEP improvements.
- Significant aircrew safety enhancements have been affected by the addition of the Helicopter Emergency Egress Lighting System (HEELS) and Crash-Resistant Crew Seats.
- Installation of the Inflight Blade Integrity System (IBIS) for the in-service aircraft is planned during CY1996-97.
- Standard Depot Level Maintenance (SDLM) capability was transitioned in 1995 from organic to civilian contract depot support at PEMCO World Air Services, Dothan, AL.
- The H-3 is currently operated by numerous foreign governments, including: Spain, Egypt, Brazil, and Malaysia. These countries have active Security Assistance cases with the U.S. Navy for maintenance, logistics, and engineering support.
External Dimensions
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| Main rotor diameter |
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| Main rotor blade chord |
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| Tail rotor diameter |
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| Tail rotor blade chord |
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| Distance between rotor centers |
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| Wing span |
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| Wing aspect ratio |
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| Length: overall, rotors turning |
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| fuselage |
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| Width overall |
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| Height: to top of rotor head |
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| Overall Height |
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| Ground clearance, main rotor, turning |
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| Elevator span |
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| Width over skids |
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| Main rotor blades (each) |
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| Tail rotor blades (each) |
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| Main rotor disc |
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| Tail rotor disc |
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| Vertical fin |
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| Horizontal tail surfaces |
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Weights and Loadings
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| Weight empty |
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| Mission fuel load (usable) |
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| Maximum useful load (fuel and disposable ordinance) |
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| Maximum Take off and landing weight |
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| Maximum disc loading |
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| Maximum power loading |
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| Never -exceed speed (Vne) |
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| Maximum level speed at S/L |
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| Rate of climb at S/L, OEI |
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| Service ceiling |
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| Service ceiling, OEI |
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| Hovering ceiling |
- IGE
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- OGE
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| Range at S/L with standard fuel, no reserves |
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