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Aircraft N617AC Photo

N617AC, 2003 Bell 407, C/N: 53570

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Photo ID: AC141445

N617AC, 2003 Bell 407 C/N 53570, 2003 Bell 407, one Rolls-Royce (Allison) 250-C47B turboshaft with FADEC, 814 shp for takeoff, 700 shp max continuous, evolutionary development of Bell LongRanger

2003 Bell 407, one Rolls-Royce (Allison) 250-C47B turboshaft with FADEC, 814 shp for takeoff, 700 shp max continuous, evolutionary development of Bell LongRanger

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: 2007-12-09
Airport: CMA
Camarillo Airport
Upload Date: 2007-12-10
Views: 459

Photo MetaData

Device Manufacturer: Hewlett-packard
Device Model: HP PhotoSmart R607 (V01.00)
Device Type:
Shot Time: 2007:12:09 14:44:26
Original Image Size: 1792 x 1312 pixels
Exposure Time: 33/23741 sec
F Number: f/7.7
Exposure Bias: 0
ISO Speed: 3776
Focal Length: 17.39 mm
Flash: Unknown: 3664
Exposure Mode: 3904
White Balance: 3920
Scene Type: 2f8c03
Contrast: 3984
Saturation: 4000
Sharpness: 4016
Total 9 photos. View all photos
More photos of N617AC

  • N617AC @ OXR - 2003 Bell 407, one Rolls-Royce (Allison) 250-C47B Turboshaft with FADEC, 814 sHp for takeoff, 700 sHp continuous, on Aspen Helicopters, Inc. ramp - by Doug Robertson by Doug Robertson @ OXR
  • N617AC @ FTW - At Meacham Field - by Zane Adams by Zane Adams @ FTW
  • N617AC @ OXR - 2003 Bell 407, one Rolls-Royce(Allison) 250-C47B turboshaft with FADEC, 814 shp for takeoff, 700 shp max continuous, evolutionary development of Bell LongRanger, at Aspen's ramp - by Doug Robertson by Doug Robertson @ OXR
  • N617AC @ OXR - 2003 BELL 407, one Rolls-Royce (Allison) 250-C47B Turboshaft with FADEC, 814 shp for takeoff, 700 shp continuous. Evolutionary development of Bell LongRanger. On Aspen Helicopters ramp - by Doug Robertson by Doug Robertson @ OXR
  • N617AC @ CMA - 2003 Bell 407, one Rolls-Royce (Allison) 250-C47B turboshaft with FADEC, 814 shp for takeoff, 700 shp max continuous, evolutionary development of Bell LongRanger - by Doug Robertson by Doug Robertson @ CMA