Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
turbofan engine
|
| gptkbp:application |
gptkb:Boeing_767
|
| gptkbp:certifications |
gptkb:FAA
|
| gptkbp:controls |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:diameter |
3.0 ft
2.5 ft |
| gptkbp:engineConfiguration |
twin-spool
|
| gptkbp:engineType |
2
6 |
| gptkbp:firstFlight |
1972
|
| gptkbp:fuelType |
gptkb:Jet_A-1
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce RB.211-22B
|
| gptkbp:introduced |
1972
|
| gptkbp:length |
11.5 ft
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce_Holdings
|
| gptkbp:notable_feature |
three-shaft design
|
| gptkbp:operational_status |
commercial aviation
|
| gptkbp:propulsion |
22,000 lbf
|
| gptkbp:related_engine |
gptkb:Rolls-Royce_RB.211-524
|
| gptkbp:successor |
Rolls-Royce Trent 800
|
| gptkbp:type |
high-bypass turbofan
|
| gptkbp:weight |
3,800 lb
|