Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:jet_engine
|
| gptkbp:application |
gptkb:business_jet
|
| gptkbp:cancellation_reason |
yes
|
| gptkbp:compressor_type |
axial compressor
|
| gptkbp:configuration |
twin-spool
|
| gptkbp:control_system |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:diameter |
approximately 36 in
|
| gptkbp:emissions_standard |
CAEP/6
|
| gptkbp:first_flight |
gptkb:2018
|
| gptkbp:fuel_type |
gptkb:Jet_A-1
|
| https://www.w3.org/2000/01/rdf-schema#label |
Pearl 30 engine
|
| gptkbp:length |
approximately 60 in
|
| gptkbp:maintenance |
5,000 hours
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:propulsion |
up to 30,000 lbf
|
| gptkbp:related_aircraft |
gptkb:Dassault_Falcon_10_X
gptkb:Gulfstream_G700 gptkb:Bombardier_Global_7500 |
| gptkbp:service_entry |
gptkb:2020
|
| gptkbp:turbine_type |
high bypass turbofan
|
| gptkbp:weight |
approximately 1,200 lb
|
| gptkbp:bfsParent |
gptkb:Pearl_15_engine
|
| gptkbp:bfsLayer |
7
|