Bell 430

Bell 430

Features

unparalledled speed and ride quality	advanced digital avionics
bearingless composite main rotor design	open, spacious cabin
full glass cockpit	ergonomic control systems

Performance (Projected)

max gross weight		9,300 lbs	4,218 kg
useful load		3,964 lbs	1,800 kg
Vne (never exceed speed)		150 kn	278 km/hr
engine take-off (2)		1,616 hp	1,205 kw
max range		353 nm	654 km

Mission profiles

Corporate:	hand-stitched leather seating, limousine privacy windows, infrared sound system
EMS:	large 159-cu-ft cabin, optional litter door kit for easier gurney loading, skid or wheeled landing gear
Utility:	3,975-lb useful payload, low DOC, flexible cabin space, nine-passenger capacity
Law Enforcement:	smooth hover, quiet ride, nimble handling, cutting-edge avionics and surveillance capabilities

Range

With Skid Gear	353 nm	654 km
Without Skid Gear	275 nm	510 km

Safety Features

• Composite hub & rotor system
• Rollover prevention wings
• High OEI ratings:
  • 940 SHP 30 second OEI
  • 880 SHP 2 minute OEI
  • 835 SHP 30 minute OEI
  • 808 SHP continuous OEI
• Optional external popout life raft
• Shoulder harness for all seats
• Energy attenuating seats for crew (optional passenger seats)
• Tail rotor guard
• Glass windshields with wipers standard
• Integrated Instrument Display (IIDS)
• Collective mounted throttles
• Optional particle separator
• Rollover bulkheads
• Rupture resistant fuel system with self sealing breakaway fittings
• Torque stick shaker
• Popout cabin windows
• FADEC – 30 second ratings exceedance monitoring

Bell 429

Bell 429

Features

best-in-class range	seating for up to eight	full glass cockpit
spacious flat-floor cabin	cutting-edge digital avionics	exceptional cost efficiency

Specs & Performance (Projected)

max gross weight	7,000 lbs	3,175 kg
useful load	2,700 lbs	1,225 kg
max cruise speed	142 kn	264 km/h
max range	350 nm	648 km
empty weight	4,300 lbs	1,950 kg
standard fuel capacity	215 usg	814 l
Vh (skid gear configuration)	142 kts	264 km/hr
Vh (wheel gear configuration)	147 kts	273 km/hr
HIGE (ISA)	12,000 ft	3,658 M
HOGE (ISA)	11,000 ft	2,835 M
Range (LRC)	350 nm	676 km
Endurance	2.25 hr (at Vh)

Mission Profiles

Corporate:	luxurious amenities; leather seating; smooth, quiet ride
EMS:	massive flat-floor cabin, optional rear clamshell doors, flexible configurations for two litters and medical crew
Utility:	superior load capacity, low DOC, quick to jobsite
Law Enforcement	smooth hover and ride, advanced surveillance capabilities, precise control

Safety Features

• Composite hub & rotor system
• Rollover bulkheads
• Direct engine input to transmission
• Energy attenuating seats (FAR/JAR 27)
• FADEC for responsiveness
• Engine exceedance monitoring & recording
• Energy attenuating skid landing gear
• Collective mounted throttles
• Rupture resistant fuel system
• Integrated Instrument Display System (IIDS) to reduce pilot workload

Bell 427

Bell 427

Maximum Gross Weight

Internal	6550 lb	2971 kg
External	6550 lb	2971 kg

Useful Load

Internal	2960 lb	1220 kg
Max External	3000 lb	1361 kg

Speed & Range

Max Cruise Speed	138 kn	225 km/h
Maximum Range	290 nm	537 km

Safety Features

• Composite hub & rotor system
• Rollover bulkheads
• Direct engine input to transmission
• Energy attenuating seats (FAR/JAR 27)
• FADEC for responsiveness
• Engine exceedance monitoring & recording
• Energy attenuating skid landing gear
• Collective mounted throttles
• Rupture resistant fuel system
• Integrated Instrument Display System (IIDS) to reduce pilot workload

Bell 412

Bell 412

Maximum Gross Weight

External

11900 lb

5398 kg

Useful Load

Standard VFR	5039 lb	2286 kg
Max External	4500 lb	2041 kg
Internal	5068 lb	2299 kg

Speed & Range

Max Cruise Speed	122 kn	226 km/h
Maximum Range	356 nm	659 km

Safety Features

• Tail rotor clearance 2 Meters (6.5 Feet)
• Main rotor clearance 2.6 Meters (8.6 Feet)
• Rupture resistant fuel system
• Jettisonable crew doors
• Sturdy structure and bulkheads for roll over protection
• Optional wire strike protection system
• Emergency cabin egress through 4 push-out windows
• Collective mounted engine controls
• 166,700 hours mean time between inflight shutdowns
• Dual electrical, hydraulic and fuel systems
• Dual digital automatic flight control system

Bell 407

Bell 407

Maximum Gross Weight

Internal	5000 lb	2268 kg
External	6000 lb	2722 kg

Useful Load

Internal	2347 lb	1065 kg
Max External	2646 lb	1200 kg

Speed & Range

Max Cruise Speed	133 kn	246 km/h
Maximum Range	330 nm	612 km

Safety Features

• FADEC for responsiveness
• Shoulder harness for all seats
• Pilot exceedances warnings
• Rupture resistant fuel system
• Powerful transmission ratings
• Collective mounted throttle
• Composite hub and rotor system
• Improved engine margins
• Rollover bulkheads
• Rugged energy attenuating skid landing gear

Bell 210

Bell 210

Maximum Gross Weight
Internal 10,500 lb 4763 kg
External 11,200 lb 5080 kg

Useful Load
Internal 5034 lb 2284 kg
Max External 5000 lb 2268 kg
Speed & Range (at 10,500 lbs)
Max Cruise Speed 106 kn 196 km/h
Maximum Range 225 nm 416 km

Safety Features

* Throttle on collective
* High inertia rotor for safe autorotation
* Rupture resistant fuel cells
* Rugged energy attenuating skid gear
* Sturdy cabin structure for rollover protection
* Optional wirestrike protection

Bell 206B3 Jetranger III

Bell 206B3 Jetranger III

Features

lowest operating costs in class superior autorotation characteristics
robust cabin structure collective mounted throttle
rupture resistant fuel cells shoulder harnesses

Performance

standard max gross weight 3,350 lbs 1,519kg
standard useful load 1,487lbs 674kg
Vne (never-exceed speed) 122kn 226km/h
engine take-off power 420shp 313kW
max range 374nm 694km

Mission Profiles

Corporate Plenty of room for 4 passengers and 1 pilot, powerful and dependable turbine engine, best safety record in its class

Law Enforcement Max. range of 374 nautical miles at max. cruise speed,
endurance of 4.5 hours at loiter speed, low acquisition
costs, economical operating costs and great resale value.

Utility External loads of up to 1,500 lb., Rolls-Royce 250-C20J engine,
rated at 420 SHP, power for speeds to 122 kts. margin-of-safety
features include collective-mounted twist-grip engine throttle
control and rupture-resistant fuel system.

Safety Features

* Optional wire strike protection
* High inertia rotor for safe autorotation
* Rugged energy attenuating skid gear
* Sturdy cabin structure (rollover protection)
* Throttle on collective
* Rupture resistant fuel cells