|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
commercial aviation
|
|
gptkbp:average_temperature
|
1,500 ° F
|
|
gptkbp:combustor_type
|
annular combustor
|
|
gptkbp:compressor_type
|
gptkb:5
|
|
gptkbp:control_system
|
hydromechanical control system
|
|
gptkbp:development
|
gptkb:JT8_D-1
gptkb:JT8_D-15
gptkb:JT8_D-17
gptkb:JT8_D-7
JT8 D-219
|
|
gptkbp:diameter
|
3 ft 9 in
|
|
gptkbp:emissions_standard
|
ICAO Chapter 3
|
|
gptkbp:engine
|
gptkb:Pratt_&_Whitney_PW1000_G
gptkb:JT8_D_family
gptkb:General_Electric_CF6
gptkb:Rolls-Royce_RB211
gptkb:CFM_International_CFM56
gptkb:Pratt_&_Whitney_JT9_D
|
|
gptkbp:engine_configuration
|
twin-spool
|
|
gptkbp:fan_art
|
single-stage fan
|
|
gptkbp:first_flight
|
gptkb:1965
|
|
gptkbp:fuel_economy
|
0.8 lb/lbf/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Pratt & Whitney JT8 D
|
|
gptkbp:introduced
|
gptkb:1965
|
|
gptkbp:length
|
12 ft 4 in
|
|
gptkbp:maintenance
|
3,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:noise_level
|
Stage 3
|
|
gptkbp:notable_users
|
gptkb:Delta_Air_Lines
gptkb:United_Airlines
gptkb:Alaska_Airlines
gptkb:Eastern_Air_Lines
gptkb:Northwest_Airlines
|
|
gptkbp:number_built
|
over 14,000
|
|
gptkbp:propulsion
|
18,500 to 22,000 lbf
|
|
gptkbp:retired
|
2000s
|
|
gptkbp:successor
|
gptkb:Pratt_&_Whitney_PW4000
|
|
gptkbp:turbine_type
|
2
|
|
gptkbp:type
|
axial-flow engine
|
|
gptkbp:used_in
|
gptkb:Boeing_737-100
gptkb:Boeing_727
gptkb:Mc_Donnell_Douglas_DC-10
|
|
gptkbp:water_requirement
|
600 lb/hr
|
|
gptkbp:weight
|
3,000 lb
|
|
gptkbp:bfsParent
|
gptkb:Mc_Donnell_Douglas_DC-9-10
gptkb:Mc_Donnell_Douglas_DC-9-50
gptkb:Mc_Donnell_Douglas_MD-82
gptkb:Mc_Donnell_Douglas_MD-88
gptkb:Pratt_&_Whitney_JT3_D
gptkb:Mc_Donnell_Douglas_MD-83
gptkb:Boeing_727
gptkb:Mc_Donnell_Douglas_DC-9-30
gptkb:Mc_Donnell_Douglas_MD-80
gptkb:Pratt_&_Whitney_JT3_C
gptkb:Pratt_&_Whitney_JT9_D
|
|
gptkbp:bfsLayer
|
5
|