JT8 D-7 B

GPTKB entity

Statements (47)
Predicate Object
gptkbp:instance_of gptkb:turbofan_engine
gptkbp:application commercial aviation
gptkbp:certification FAA certified
gptkbp:combustor_type annular
gptkbp:compressor_type axial
gptkbp:control_system hydromechanical
gptkbp:cooling_system air-cooled
gptkbp:diameter 0.94 m
3 ft 1 in
gptkbp:engine high bypass ratio
air start
widely used in the 1970s and 1980s
gptkbp:engine_configuration modular design
pylon-mounted
gptkbp:engine_power high reliability
gptkbp:engine_replacement replaced by newer engines in the 1990s.
gptkbp:engine_type gptkb:turbofan_engine
compatible with various aircraft types
JT8 D-1, JT8 D-9, JT8 D-15
gptkbp:fan_art single-stage fan
gptkbp:first_flight gptkb:1965
gptkbp:fuel_economy 0.6 lb/lbf/hr
gptkbp:fuel_type gptkb:Jet_A
https://www.w3.org/2000/01/rdf-schema#label JT8 D-7 B
gptkbp:impact significant impact on commercial aviation
gptkbp:length 10 ft 6 in
gptkbp:maintenance 4,000 hours
scheduled maintenance required
gptkbp:manufacturer gptkb:Pratt_&_Whitney
gptkbp:noise_level Stage 3 compliant
acoustic liners
gptkbp:number_of_stages gptkb:5
gptkbp:operational_range 30,000 to 40,000 ft
gptkbp:propulsion 14,000 lbf
gptkbp:service 20,000 hours
gptkbp:successor gptkb:JT8_D-200
gptkbp:thrust_reverser cascade type
gptkbp:total_length 3.2 m
gptkbp:uses gptkb:Lockheed_L-1011_Tri_Star
gptkb:Boeing_737-100
gptkb:Boeing_727
gptkb:Boeing_737-200
gptkb:Mc_Donnell_Douglas_DC-10
gptkbp:weight 2,500 lb
1,134 kg
gptkbp:bfsParent gptkb:Boeing_737-100
gptkbp:bfsLayer 6