Statements (64)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:application |
general aviation aircraft
|
| gptkbp:compression_ratio |
8.5:1
|
| gptkbp:controls |
mechanical control
manual throttle |
| gptkbp:cooling_system |
air-cooled
finned cylinders |
| gptkbp:displacement |
540 cubic inches
|
| gptkbp:emissions_standard |
dual exhaust
|
| gptkbp:engine |
gptkb:Lycoming_IO-540
gptkb:TIO_series gptkb:6 gptkb:battle electric starter inline engine horizontally opposed TIO-540-U2 A TIO-540-U2 B TIO-540-U2 C TIO-540-U2 D TIO-540-U2 E TIO-540-U2 F TIO-540-U2 G TIO-540-U2 H TIO-540-U2 I TIO-540-U2 J TIO-540-U2 K TIO-540-U2 L TIO-540-U2 M TIO-540-U2 N TIO-540-U2 O TIO-540-U2 P TIO-540-U2 Q TIO-540-U2 R TIO-540-U2 S TIO-540-U2 T TIO-540-U2 U TIO-540-U2 V TIO-540-U2 W TIO-540-U2 X TIO-540-U2 Y TIO-540-U2 Z |
| gptkbp:engine_type |
four-stroke engine
|
| gptkbp:first_introduced |
1960s
|
| gptkbp:fuel_capacity |
8 quarts
|
| gptkbp:fuel_type |
aviation gasoline
carbureted |
| https://www.w3.org/2000/01/rdf-schema#label |
TIO-540 engine
|
| gptkbp:ignition_system |
removable
dual ignition |
| gptkbp:maintenance |
100 hours
|
| gptkbp:manufacturer |
gptkb:Textron_Aviation
|
| gptkbp:power_output |
300 horsepower
|
| gptkbp:propulsion |
constant speed propeller
|
| gptkbp:rating |
TBO 1,500 hours
|
| gptkbp:setting |
V-type
|
| gptkbp:type |
reciprocating engine
|
| gptkbp:used_in |
gptkb:aircraft
gptkb:Piper_Navajo |
| gptkbp:valve_configuration |
overhead valve
|
| gptkbp:water_source |
15-20 gallons per hour
|
| gptkbp:weight |
approximately 300 pounds
|
| gptkbp:bfsParent |
gptkb:Lycoming_Engines
|
| gptkbp:bfsLayer |
4
|