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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.
Bell 427 cockpit. The Bell 427 is powered by two Pratt & Whitney Canada PW207D turboshaft engines with FADEC. [2] Like the Bell 407, the 427 uses a four-blade main rotor system with a rigid, composite rotor hub and a two-blade tail rotor. [2] The Bell 427's cabin is 13 in (33 cm) longer than the 407, and consists primarily of composite ...
The Bell 407-based MQ-8C has an endurance of 12 hours, a range of 150 nmi (170 mi; 280 km), and a payload capacity of about 318 kg (701 lb); [8] it has twice the endurance and three times the payload as the MQ-8B. [9] In early July 2013, Northrop Grumman delivered the first MQ-8C to the Navy.
The Bell 430 was formally launched in February 1992, with two prototypes modified from Bell 230s. The first of these flew in its new configuration on October 25, 1994, and the second prototype, featuring the full 430 avionics suite, first flew on December 19, 1994. [1] Production of the Bell 230 ended in August 1995, and 430 production began.
The Bell 412 is a utility helicopter of the Huey family manufactured by Bell Helicopter. It is a development of the Bell 212 , with the major difference being the composite four-blade main rotor. It is a twin-turbine helicopter that has been popular on the civilian and military markets, and major users include Canada, Italy, and Japan.
Data from Bell 429 brochure, Bell Helicopter 429 product specifications, Flug Revue Bell 429 page, Aviation Week General characteristics Crew: 1 pilot Capacity: 7 passengers (six in passenger compartment; one beside pilot) / 2,755 lb (1,250 kg) payload Length: 41 ft 8 in (12.70 m) Height: 13 ft 3 in (4.04 m) Cabin volume: 204 cu ft (5.78 m 3) Empty weight: 4,245 lb (1,925 kg) Max takeoff ...
1 Bell 407 ICAO designation. 2 comments. ... 2.3 Decision. 3 Photos. 1 comment. 4 Specifications. 4 comments Toggle Specifications subsection. 4.1 Performance. 5 ...
Data from MD500E Performance Specifications, The International Directory of Civil Aircraft General characteristics Crew: 2 Capacity: 3 passengers Length: 32 ft 7 in (9.93 m) Height: 8 ft 9 in (2.67 m) Empty weight: 1,591 lb (722 kg) Max takeoff weight: 3,550 lb (1,610 kg) Powerplant: 1 × Allison 250-C30 turboshaft engine, 650 shp (480 kW) Main rotor diameter: 27 ft 4 in (8.33 m) Main rotor ...