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Aircraft N618AC Photo

N618AC, 1997 Bell 407, C/N: 53153

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Photo ID: AC282644

N618AC, 1997 Bell 407 C/N 53153, 1997 Bell 407, one Rolls Royce (Allison) 250-C47 turboshaft with FADEC, 814 shp for takeoff, 700 shp continuous. Up to seven place, 407 utility helicopter is huge sales success. At SUN AIR JETS ramp on dolly.

1997 Bell 407, one Rolls Royce (Allison) 250-C47 turboshaft with FADEC, 814 shp for takeoff, 700 shp continuous. Up to seven place, 407 utility helicopter is huge sales success. At SUN AIR JETS ramp on dolly.

Folder: Doug Robertson's photo gallery > Rotary Wing Prod. Acft.-Std. Restr. class > Bell/Bell Textron

Photo Info

Photographer: Doug Robertson
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Please do NOT ask photographer about aircraft data, instead use forum for these questions
Shot Date: 2009-01-31
Airport: CMA
Camarillo Airport
Upload Date: 2009-02-10
Views: 647

Photo MetaData

Device Manufacturer: Canon
Device Model: Canon PowerShot A720 IS
Device Type: Digital Still Camera
Shot Time: 2009:01:31 13:32:23
Original Image Size: 1600 x 1200 pixels
Exposure Time: 1/800 sec
F Number: f/4.8
Exposure Bias: 0
ISO Speed: 80
Focal Length: 34.8 mm
Flash: No Flash
Exposure Mode: 0
White Balance: 0
Scene Type:
Contrast:
Saturation:
Sharpness:
Total 8 photos. View all photos
More photos of N618AC

  • N618AC @ CMA - 1997 Bell 407, one Rolls Royce (Allison) 250-C47 Turboshaft with FADEC, 814 shp for takeoff, 700 shp continuous. Max hook capacity 2,645 lbs. Max takeoff with internal load 5,000 lbs. Max takeoff with sling load 5,500 lbs. At SUN AIR JETS ramp on dolly - by Doug Robertson by Doug Robertson @ CMA
  • N618AC @ KCMA - Camarillo Airshow 2008 - by Todd Royer by Todd Royer @ KCMA
  • N618AC @ CMA - 1997 Bell 407, one Rolls Royce (Allison) 250-C47 turboshaft with FADEC, 814 shp for takeoff, 700 shp continuous - by Doug Robertson by Doug Robertson @ CMA
  • N618AC @ CMA - Parked on it's dolly facing the airstrip - by Helicopterfriend by Helicopterfriend @ CMA
  • N618AC @ CMA - 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 - by Doug Robertson by Doug Robertson @ CMA