Statements (51)
Predicate | Object |
---|---|
gptkbp:instanceOf |
gptkb:helicopter
|
gptkbp:armament |
various weapons systems
|
gptkbp:crew |
2
|
gptkbp:design |
fuel efficiency
modular design advanced avionics high reliability low noise levels easy maintenance high visibility cockpit wide cabin dual hydraulic systems retractable landing gear multi-role capability high payload capacity versatile configuration turbine helicopter |
gptkbp:engine |
2 × Pratt & Whitney Canada PT6T-3B
|
gptkbp:firstFlight |
1968
|
gptkbp:height |
4.5 m
|
https://www.w3.org/2000/01/rdf-schema#label |
Bell 212
|
gptkbp:length |
15.5 m
|
gptkbp:manufacturer |
gptkb:Bell_Helicopter
|
gptkbp:maxSpeed |
130 knots
|
gptkbp:maxTakeoffWeight |
4,500 kg
|
gptkbp:notableUsers |
gptkb:Philippine_Air_Force
gptkb:Colombian_Air_Force gptkb:Mexico gptkb:Royal_Australian_Air_Force gptkb:United_Nations gptkb:United_States_Army gptkb:Canadian_Forces |
gptkbp:passengerCapacity |
15
|
gptkbp:primaryFunction |
law enforcement
transport search and rescue offshore transport firefighting aerial survey VIP transport medevac utility missions |
gptkbp:productionCompany |
present
|
gptkbp:productionStartYear |
1968
|
gptkbp:range |
400 nautical miles
|
gptkbp:role |
utility helicopter
|
gptkbp:services |
15,000 ft
|
gptkbp:setting |
twin-engine
|
gptkbp:usedBy |
military
|
gptkbp:variant |
gptkb:Bell_412
|
gptkbp:weight |
2,800 kg
|