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Santa Paula Airport (SZP), 2010-02-07 1967 Bell 47G-2, Lycoming VO-435 200 Hp 6 cylinder vertical mount |
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Santa Paula Airport (SZP), 2009-09-12 1965 Bell 47G-4A, Lycoming VO-540 305 Hp. The Bell 47 was the world's first practical mass-produced helicopter offering reliabilty in a simple airframe. Approach to SZP's helipad. |
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Santa Paula Airport (SZP), 2009-09-12 1965 Bell 47G-4A, Lycoming VO-540 305 Hp. The Bell 47 was the world's first practical mass-produced helicopter offering reliabilty in a simple airframe. Hover. |
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Santa Paula Airport (SZP), 2009-09-12 1965 Bell 47G-4A, Lycoming VO-540 305 Hp. The Bell 47 was the world's first practical mass-produced helicopter offering reliabilty in a simple airframe. Nearly landed. |
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Camarillo Airport (CMA), 2009-08-22 1975 Bell 212 TWIN TWO-TWELVE, P&W (Canada) PT6T-3 Twin-Pac coupled free-turbine turboshaft 1,800 shp, Ventura County Sheriff's Department #9 |
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Camarillo Airport (CMA), 2009-08-22 1963 Bell 47G-3B-1 TROOPER (civil version of Army OH-13S SIOUX), Lycoming TVO-435-A1A 260 Hp |
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Camarillo Airport (CMA), 2009-08-22 1963 Bell 47G-3B-1 TROOPER (civil version of Army OH-13S SIOUX), Lycoming TVO-435-A1A 260 Hp |
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Camarillo Airport (CMA), 2009-08-22 1963 Bell 47G-3B-1 TROOPER (civil version of Army OH-13S SIOUX), Lycoming TVO-435-A1A 260 Hp |
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Camarillo Airport (CMA), 2009-08-22 1963 Bell 47G-3B-1 TROOPER (civil version of Army OH-13S SIOUX), Lycoming TVO-435-A1A 260 Hp |
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Camarillo Airport (CMA), 2009-06-13 1997 Bell 407, one Rolls Royce (Allison) 250-C47 turboshaft with FADEC, 814 shp for takeoff, 700 shp continuous. Four blade main rotor composite construction, blades & hub have NO life limits. Popular siccessor to Bell JetRanger & LongRanger light singles |
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Camarillo Airport (CMA), 2009-05-13 1999 Bell 407, one Allison 250-C47 Turboshaft with FADEC, 814 shp takeoff rated, 700 shp max continuous driving four blade main rotor & two blade tail rotor, evolutionary development of the LongRanger |
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Camarillo Airport (CMA), 2009-05-13 1999 Bell 407, one Allison 250-C47 Turboshaft with FADEC, 814 shp takeoff rated, 700 shp max continuous driving four blade main rotor & two blade tail rotor, evolutionary development of the LongRanger |