GE T700-GE-701D
Exact GE T700-GE-701D turboshaft variant. GE's datasheet documents its UH-60M/AH-64 applications and 2,000 shaft-horsepower contingency rating. This packet creates the propulsion identity only; it asserts no T700 family link, actor attribution, vehicle installation, or lineage edge.
Identity
- Aliases
- T700-701DT701DGE T700-GE-701D
- Domains
- aviation
- Identity Level
- variant
- Kind
- turboshaft
- Name
- GE T700-GE-701D
- Status
- active
Details
- Air Breathing Specs
- Shaft Power Kw
- 1,491
- Description
- Exact GE T700-GE-701D turboshaft variant. GE's datasheet documents its UH-60M/AH-64 applications and 2,000 shaft-horsepower contingency rating. This packet creates the propulsion identity only; it asserts no T700 family link, actor attribution, vehicle installation, or lineage edge.
- Dry Mass Kg
- 207
- Length M
- 1.1684
Links
Assets & Meta
- Creation Time
- August 6, 2026 at 17:28:44 UTC
- Updated Time
- August 6, 2026 at 17:28:44 UTC
Other
- Diameter M
- 0.39624
- Sources
- Note
- Official datasheet identifies the exact T700-701D model, UH-60M/AH-64 applications, 2,000 shp contingency rating (1,491 kW), dimensions, and 207 kg dry weight.
- Publisher
- GE Aerospace
- Title
- T700-701D turboshaft engine datasheet
- Note
- Official qualification announcement confirms the exact -701D variant, production status, and 2,000 shaft-horsepower rating.
- Publisher
- GE Aerospace
- Title
- T700-GE-701D Engine Awarded U.S. Army Qualification
- Note
- Official Army report independently identifies a T700-GE-701D in the UH-60M fit-check context; used as exact variant evidence only, not as a vehicle relationship write.
- Publisher
- U.S. Army
- Title
- Improved Turbine Engine Fits the Army's Most Versatile Platform
- Note
- Current official sustainment announcement supports the active lifecycle disposition of T700-GE-701D.
- Publisher
- GE Aerospace
- Title
- GE Aerospace signs contract for T700-GE-701D sustainment