|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:aircraft_operated
|
gptkb:Cessna_Citation_Longitude
gptkb:Bombardier_Challenger_300
gptkb:Dassault_Falcon_7_X
gptkb:Mitsubishi_Space_Jet
gptkb:Embraer_Legacy_600
gptkb:Gulfstream_G650
gptkb:Bombardier_Global_Express
|
|
gptkbp:application
|
commercial aviation
|
|
gptkbp:certification
|
FAA certified
|
|
gptkbp:combustor_type
|
annular
|
|
gptkbp:compressor_type
|
axial
|
|
gptkbp:control_system
|
gptkb:FADEC
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:diameter
|
68 in
36 in
|
|
gptkbp:emissions_standard
|
CAEP/6
|
|
gptkbp:engine
|
bleed air start
|
|
gptkbp:engine_configuration
|
wing-mounted
|
|
gptkbp:engine_type
|
PW817 D
PW817 C
PW817 E
PW817 F
PW817 G
PW817 H
PW817 I
PW817 J
PW817 K
PW817 L
PW817 M
PW817 N
PW817 O
PW817 P
PW817 Q
PW817 R
PW817 S
PW817 T
PW817 U
PW817 V
PW817 W
PW817 X
PW817 Y
PW817 Z
|
|
gptkbp:fuel_economy
|
0.5 lb/lbf/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
PW817
|
|
gptkbp:is_tested_for
|
Pratt & Whitney test facility
|
|
gptkbp:length
|
60 in
|
|
gptkbp:maintenance
|
on-wing maintenance
4,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:noise_level
|
Stage 4 compliant
|
|
gptkbp:number_of_engines
|
2
|
|
gptkbp:number_of_stages
|
gptkb:10
|
|
gptkbp:operational_range
|
30,000 to 40,000 ft
|
|
gptkbp:original_run
|
gptkb:1997
|
|
gptkbp:propulsion
|
no
17,000 lbf
|
|
gptkbp:service_entry
|
gptkb:1998
|
|
gptkbp:successor
|
PW812
|
|
gptkbp:turbine_type
|
high-pressure turbine
|
|
gptkbp:type
|
gptkb:turbofan_engine
|
|
gptkbp:weight
|
1,200 lb
|
|
gptkbp:bfsParent
|
gptkb:PW800
|
|
gptkbp:bfsLayer
|
8
|