Pratt & Whitney Canada PT6 T-3 Twin-Pac
GPTKB entity
Statements (86)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:application |
helicopters
|
| gptkbp:armament |
gptkb:4
|
| gptkbp:certification |
FAA certified
|
| gptkbp:compression_ratio |
16:1
8:1 |
| gptkbp:controls |
gptkb:full_authority_digital_engine_control_(FADEC)
digital control system |
| gptkbp:cooling_system |
air-cooled
air-cooled system oil-cooled |
| gptkbp:design |
modular design
|
| gptkbp:diameter |
approximately 16 in
16 in |
| gptkbp:displacement |
1,200 in³
|
| gptkbp:drivetrain |
reduction gearbox
|
| gptkbp:emissions_standard |
ICAO Chapter 4
free turbine |
| gptkbp:engine |
gptkb:advanced_technology
commercial aviation pilot training programs active user community high reliability Brayton cycle high efficiency electric starter utility aircraft ongoing research and development global support network pylon-mounted excellent performance 5,000 hours continuous innovation twin-shaft upgrade kits available long-standing legacy turbine engine design 2,000 rpm civil and military applications P T6 family twin-turbine design 1,000 shp at takeoff P T6 T series |
| gptkbp:engine_type |
turboprop
twin-turbine engine various airframes P T6 T-6 P T6 T-3 B P T6 T-3 |
| gptkbp:first_flight |
gptkb:1964
gptkb:1969 |
| gptkbp:fuel_capacity |
54 in
24 in high efficiency 400 lb 0.5 lb/hp/hr 16 in |
| gptkbp:fuel_type |
gptkb:Jet_A-1
gptkb:Jet_A hydromechanical fuel control |
| https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney Canada PT6 T-3 Twin-Pac
|
| gptkbp:ignition_system |
dual ignition system
dual ignition |
| gptkbp:launched |
starter-generator
|
| gptkbp:length |
54 in
approximately 54 in |
| gptkbp:maintenance |
modular design
1,500 hours scheduled maintenance required |
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney_Canada
|
| gptkbp:noise_level |
low noise
|
| gptkbp:notable_users |
gptkb:Bell_Helicopter
|
| gptkbp:operational_range |
up to 30,000 ft
|
| gptkbp:power_output |
1,000 shp
|
| gptkbp:propulsion |
1,000 lb
1,000 lbf variable pitch propeller 1,000 lbf at takeoff |
| gptkbp:service_ceiling |
20,000 ft
|
| gptkbp:setting |
twin-engine
|
| gptkbp:type |
gptkb:engine
twin-turbine engine |
| gptkbp:used_in |
gptkb:Bell_212
gptkb:Bell_214 |
| gptkbp:weight |
400 lb
approximately 400 lb |