HELICOPTERS

BELL 407



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AIRCRAFT DESCRIPTION

The Bell 407 is a four-blade, single-engine, civil utility helicopter; a derivative of the Bell 206L-4 LongRanger. The 407 uses the four-blade, soft-in-plane design rotor with composite hub developed for the United States Army's OH-58D Kiowa Warrior instead of the two-blade, semi-rigid, teetering, rotor of the 206L-4. The Bell 407 is frequently used for corporate and offshore transport, as an air ambulance, law enforcement, electronic news gathering and movie making.

The Bell 407 integrates reliability, speed, performance, and maneuverability with a cabin configurable for an array of missions and payloads. Its Rolls Royce 250-C47B turbine FADEC engine delivers exceptional hot & high performance with the ability to cruise at 140 knots (259 km/hr). The 407's spacious cabin seats up to five passengers in wide-open club-passenger seating and can be reconfigured to accommodate any number of tasks and payloads.

For added passenger comfort, the Bell 407 also provides a very quiet and smooth ride in virtually all weather conditions. In addition to offering outstanding product features, the 407 is backed by Bell's renowned in-service support, voted #1 by our customers for nineteen years running. The Bell 407 is proof that you don’t have to sacrifice comfort for performance

Power.Reliability.Maneuverability. The 407 has everything you'd expect from a Bell helicopter and more. The 407 is also exceptionally quiet. This makes the 407 not just a great way of getting to work, but also a great place to do work. It seats up to seven, comfortably. In fact, very comfortably, thanks to wide-open club seating and the smoothest ride in its class. In today's business world, it's all about performance. No wonder the 407 is so successful

  • A spacious 85 ft³ (2.4 m³) cabin that accommodates five passenger
  • Club seating with an available Quiet Cruise™ kit for decreased cabin noise
  • All composite, four-blade rotor provides superior hover performance, speed and a smooth quiet ride
  • Expanded safety and reduced operating costs from the FADEC (Full Authority Digital Engine Control) engine fuel management system of the proven Rolls Royce 250-C47B turbine engine
  • Supported by Bell Helicopter's #1 ranked Customer Support and Services


AIRCRAFT CHARACTERISTICS & SPECIFICATIONS(CJ2)


 

Engine
1 × Allison 250-C47 turboshaft
Power
700.00 Horsepower
Avionics
AP-85 Two-Axis Autopilot
Maximum Cruising Speed
244.61 km per hr 152.00 mph
Service Ceiling
5,696.71 metres 18,690.00 feets
Rate of Climb
243.84 mpm 800.00 fpm
Cabin Height

1.28 metres  4.20 feets

Cabin Width
1.37 metres  4.48 feets
Cabin Length
1.52 metres  5.00 feets
Exterior Length
12.70 metres  41.67 feets
Wingspan / Rotor Diameter

10.67 metres  35.01 feets

Baggage Volume
0.45 cubic metre   16.00 cubic feet
Max Take Off Weight
2,721.60 kgs   6,000.00 lbs
Maximum Payload
1,064.60 kgs   2,347.00 lbs
Fuel Tank Capacity
110.17 gallon   417.00 litres
Fuel Economy
1.44 km per litre   3.39 NM per gallon
Seating Chart /Seats
7
Travel Range
598.00 Km -323 Nm
Country of Manufacture
United States

 

AIRCRAFT AVERAGE PRICE USED/NEW
( Rs 15 CRORE TO 22+ CRORE)

 

 

 

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