Statements (30)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:alsoKnownAs |
gptkb:Honeywell_T55
|
| gptkbp:application |
helicopters
fixed-wing aircraft |
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:developedBy |
Lycoming LTC4B-2
|
| gptkbp:diameter |
22.5 in
|
| gptkbp:firstFlight |
1955
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| https://www.w3.org/2000/01/rdf-schema#label |
Lycoming T55
|
| gptkbp:length |
75.6 in
|
| gptkbp:manufacturer |
gptkb:Lycoming_Engines
|
| gptkbp:notableVariant |
gptkb:T55-L-714
T55-L-11 T55-L-7 T55-L-712 |
| gptkbp:powerOutput |
up to 4,800 shp
|
| gptkbp:status |
in production
|
| gptkbp:successor |
gptkb:Honeywell_T55-GA-714A
|
| gptkbp:type |
turboprop
turboshaft |
| gptkbp:usedBy |
gptkb:United_States_Army
civilian operators |
| gptkbp:usedIn |
gptkb:Boeing_Vertol_CH-47_Chinook
gptkb:Boeing_CH-47_Chinook gptkb:Bell_214ST gptkb:Boeing_Vertol_107 |
| gptkbp:weight |
1,200 lb
|
| gptkbp:bfsParent |
gptkb:Anselm_Franz
|
| gptkbp:bfsLayer |
6
|