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gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
gptkb:Flight
|
|
gptkbp:armament
|
gptkb:24
composite
|
|
gptkbp:bypass_ratio
|
5.4:1
|
|
gptkbp:compressor_type
|
axial
|
|
gptkbp:control_system
|
gptkb:FADEC
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:derived_from
|
gptkb:CF34-8_C
|
|
gptkbp:diameter
|
34 in
|
|
gptkbp:emissions_standard
|
CAEP/6
|
|
gptkbp:engine
|
gptkb:Lynn,_Massachusetts
air start
|
|
gptkbp:engine_type
|
CF34-8 C5 A1
CF34-8 C5 B1
CF34-8 C5 B1 A
CF34-8 C5 B1 B
CF34-8 C5 B1 C
CF34-8 C5 B1 D
CF34-8 C5 B1 E
CF34-8 C5 B1 F
CF34-8 C5 B1 G
CF34-8 C5 B1 H
CF34-8 C5 B1 I
CF34-8 C5 B1 J
CF34-8 C5 B1 K
CF34-8 C5 B1 L
CF34-8 C5 B1 M
CF34-8 C5 B1 N
CF34-8 C5 B1 O
CF34-8 C5 B1 P
CF34-8 C5 B1 Q
CF34-8 C5 B1 R
CF34-8 C5 B1 S
CF34-8 C5 B1 T
CF34-8 C5 B1 U
CF34-8 C5 B1 V
CF34-8 C5 B1 W
CF34-8 C5 B1 X
CF34-8 C5 B1 Y
CF34-8 C5 B1 Z
CF34-8 E5
|
|
gptkbp:first_flight
|
gptkb:1996
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
|
gptkbp:high_pressure_compressor
|
9 stages
|
|
gptkbp:high_pressure_turbine
|
1 stage
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
General Electric CF34-8 C5
|
|
gptkbp:is_tested_for
|
gptkb:Peebles,_Ohio
|
|
gptkbp:length
|
60 in
|
|
gptkbp:low_pressure_turbine
|
2 stages
|
|
gptkbp:maintenance
|
4,000 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:noise_level
|
Stage 4 compliant
|
|
gptkbp:notable_users
|
gptkb:Embraer_E-Jet_family
gptkb:Bombardier_CRJ-900
|
|
gptkbp:produces
|
over 1,000 engines
|
|
gptkbp:propulsion
|
18,500 lbf
|
|
gptkbp:service_entry
|
gptkb:1999
|
|
gptkbp:turbine_type
|
high bypass
|
|
gptkbp:weight
|
3,800 lb
|
|
gptkbp:bfsParent
|
gptkb:Bombardier_CRJ900
|
|
gptkbp:bfsLayer
|
6
|