Statements (59)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:helicopter
|
| gptkbp:avionics |
modern glass cockpit
|
| gptkbp:crew |
2
|
| gptkbp:diameter |
4.5 m
16.3 m |
| gptkbp:engine_type |
turboshaft
|
| gptkbp:features |
enhanced situational awareness
high endurance modular design advanced communication systems advanced avionics high reliability redundant systems advanced navigation systems high thrust-to-weight ratio low vibration levels advanced flight management system high visibility cockpit large cargo door high altitude performance large cabin space crashworthy seats dual hydraulic systems easy maintenance access noise reduction technology multi-role capability high payload capacity automatic flight control system ice protection system state-of-the-art safety features flexible interior configurations advanced rotor design high performance in adverse weather conditions |
| gptkbp:first_flight |
gptkb:1998
|
| gptkbp:fuel_capacity |
1,200 liters
|
| gptkbp:height |
5.34 m
|
| https://www.w3.org/2000/01/rdf-schema#label |
S-92 T
|
| gptkbp:length |
19.76 m
|
| gptkbp:manufacturer |
gptkb:Sikorsky_Aircraft_Corporation
|
| gptkbp:max_speed |
165 knots
|
| gptkbp:military_technology |
gptkb:CH-148_Cyclone
|
| gptkbp:notable_users |
gptkb:Bristow_Helicopters
gptkb:PHI_Inc. gptkb:Canadian_Forces gptkb:Sikorsky_Global_Helicopters |
| gptkbp:power_output |
2 × General Electric C T7-8 A
|
| gptkbp:range |
600 nautical miles
|
| gptkbp:role |
gptkb:mythological_figure
transport helicopter offshore oil and gas transport |
| gptkbp:safety_record |
high safety standards
|
| gptkbp:seating_capacity |
gptkb:19
2,500 kg |
| gptkbp:service_ceiling |
15,000 ft
|
| gptkbp:variant |
gptkb:S-92_A
|
| gptkbp:weight |
8,600 kg
|
| gptkbp:wingspan |
15.9 m
|
| gptkbp:bfsParent |
gptkb:S-92
|
| gptkbp:bfsLayer |
4
|