Statements (113)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:helicopter
|
| gptkbp:avionics |
modern digital systems
modern glass cockpit |
| gptkbp:capacity |
up to 8 passengers
up to 7 passengers |
| gptkbp:cargo_capacity |
1,200 lbs
|
| gptkbp:certification |
noise and emissions compliant
|
| gptkbp:climb_rate |
1,500 ft/min
|
| gptkbp:color_scheme |
various customizable options
|
| gptkbp:competitors |
Eurocopter EC135
competes with Sikorsky S-76 competes with Agusta Westland AW109 competes with Eurocopter EC135 |
| gptkbp:control_system |
fly-by-wire
fly-by-wire system |
| gptkbp:country_of_origin |
gptkb:United_States
|
| gptkbp:crew |
2
1-2 pilots |
| gptkbp:customer_support |
global support network
|
| gptkbp:design |
twin-engine
twin-engine design based on Bell 420 |
| gptkbp:design_features |
high performance
modular design advanced safety systems spacious cabin low vibration user-friendly cockpit |
| gptkbp:diameter |
gptkb:Fenestron
11.0 m two-bladed |
| gptkbp:emergency_services |
floatation gear
|
| gptkbp:engine_type |
gptkb:turbofan_engine
gptkb:Rolls-Royce_250-C20_B turboshaft |
| gptkbp:environmental_impact |
designed for reduced noise footprint
|
| gptkbp:first_flight |
gptkb:1994
|
| gptkbp:fuel_capacity |
1,200 liters
|
| gptkbp:height |
3.8 m
|
| gptkbp:historical_significance |
first helicopter with a fully integrated glass cockpit.
part of Bell's legacy in helicopter design |
| https://www.w3.org/2000/01/rdf-schema#label |
Bell 430
|
| gptkbp:interior_features |
spacious cabin
|
| gptkbp:introduced |
gptkb:1994
|
| gptkbp:landing_gear |
skid type
skid |
| gptkbp:length |
13.1 m
|
| gptkbp:maintenance |
relatively easy maintenance
|
| gptkbp:manufacturer |
gptkb:Bell_Helicopter
|
| gptkbp:market |
commercial and private use
commercial and private sectors |
| gptkbp:market_segment |
gptkb:military_aircraft
gptkb:emergency_services commercial aviation private aviation |
| gptkbp:max_speed |
140 knots
|
| gptkbp:max_takeoff_weight |
3,175 kg
4,536 kg |
| gptkbp:modifications |
various mission-specific modifications possible
|
| gptkbp:noise_level |
low noise footprint
|
| gptkbp:notable_case |
few accidents reported
|
| gptkbp:notable_features |
advanced rotor system
|
| gptkbp:notable_operators |
various air medical services
|
| gptkbp:notable_users |
gptkb:health_services
Law enforcement agencies Medical services search and rescue operations law enforcement agencies Search and rescue operations Firefighting services Corporate transport corporate transport |
| gptkbp:number_built |
approximately 200
|
| gptkbp:number_of_engines |
2
|
| gptkbp:operational_cost |
moderate
|
| gptkbp:operational_range |
300 nautical miles
effective for short to medium distances |
| gptkbp:passenger_capacity |
gptkb:7
|
| gptkbp:performance |
high performance in hot and high conditions
|
| gptkbp:power_source |
2 x Pratt & Whitney Canada PT6 T-3 B
|
| gptkbp:primary_use |
gptkb:law_enforcement
gptkb:emergency_services |
| gptkbp:production_location |
gptkb:Fort_Worth,_Texas
|
| gptkbp:production_status |
out of production
|
| gptkbp:production_years |
1994-2005
1994-2010 |
| gptkbp:propulsion |
turboshaft
|
| gptkbp:range |
400 nautical miles
|
| gptkbp:regulatory_compliance |
FAA certified
|
| gptkbp:related_aircraft |
gptkb:Bell_222
gptkb:Bell_206 gptkb:Bell_429 gptkb:Bell_412 gptkb:Bell_407 |
| gptkbp:retired |
gptkb:2010
|
| gptkbp:role |
gptkb:helicopter
|
| gptkbp:safety_features |
crashworthy design
|
| gptkbp:service_ceiling |
15,000 ft
|
| gptkbp:service_entry |
gptkb:1995
|
| gptkbp:successor |
gptkb:Bell_429
|
| gptkbp:training |
pilot training programs available
pilot training available |
| gptkbp:training_programs |
available worldwide
|
| gptkbp:type |
twin-engine helicopter
|
| gptkbp:variant |
Bell 430 EMS
Bell 430 Utility Bell 430 VIP Bell 430-1 |
| gptkbp:weight |
2,500 kg
3,175 kg |
| gptkbp:wingspan |
11.0 m
|
| gptkbp:bfsParent |
gptkb:Bell_Helicopter
|
| gptkbp:bfsLayer |
4
|