Credit
Sardaka · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
Bell 412EP · including rotors
Single source56 ft 1 in (17.09 m) including rotors[source]
HH-60G · Length
Configuration
| Specification | Bell 412 | Sikorsky HH-60 Pave Hawk |
|---|---|---|
| Crew | one-two pilots[source] | four (two pilots, and two special mission aviators/aerial gunners)[source] |
| Type | Multipurpose utility helicopter[source] | Combat search and rescue helicopter[source] |
| National origin | United States / Canada[source] | — |
| Manufacturer | Bell Helicopter[source] | Sikorsky Aircraft[source] |
64 ft 10 in (19.76 m)[source]
Bell 412EP · 1 × Pratt & Whitney Canada PT6T-3D Twin-Pac or PT6T-3DF Twin-Pac coupled turboshaft engine - each, 1,250 shp (
Single source1 × Pratt & Whitney Canada PT6T-3D Twin-Pac or PT6T-3DF Twin-Pac coupled turboshaft engine - each, 1,250 shp (930 kW)[source]
HH-60G · 2 × General Electric T700-GE-700 / -701C turboshaft engines, 1,940 shp ( ) each
Single source2 × General Electric T700-GE-700 / -701C turboshaft engines, 1,940 shp (1,450 kW) each[source]
Bell 412EP · 1,350 ft/min (
Single source1,350 ft/min (6.9 m/s)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Primary users | Japan Ground Self Defence Force See Operators for others[source] | United States Air Force Republic of Korea Air Force[source] |
|---|
| Number built | 1,300+[source] | 112 (HH-60G Pave Hawk)[source] |
|---|
| Manufactured | 1979–present[source] | — |
|---|
| Introduction date | 1981 ( 1981 )[source] | 1982[source] |
|---|
| First flight | August 1979 ( 1979-08 )[source] | — |
|---|
| Developed from | Bell 212[source] | Sikorsky UH-60 Black Hawk[source] |
|---|
| Variant | Bell CH-146 Griffon[source] | — |
|---|
| Capacity | up to 13 passengers, maximum external load of almost 6,614 lb (3,000 kg)[source] | maximum crew 6 / 8 to 12 troops / litters or other cargo[source] |
|---|
| Fuselage length | 43 ft (13 m)[source] | — |
|---|
| Blade sections | root: Boeing VR-7; tip: Wortmann FX 71-H-080[source] | — |
|---|
| Main rotor area | 1,662 sq ft (154.4 m 2 )[source] | — |
|---|
| Power/mass | 0.2663 hp/lb (0.4378 kW/kg)[source] | — |
|---|
| Status | — | In service[source] |
|---|
| Country of origin | — | United States[source] |
|---|