General Electric T64-GE-416A
General Electric T64-GE-416A is a historical T64 turboshaft variant identified by official Marine Corps aircraft data as the three-engine CH-53E powerplant at 4,380 shaft horsepower per engine. NAVAIR describes the later T64-GE-419 improvement path; this exact variant remains distinct from the current -419 installation and the T64 family.
Identity
- Aliases
- T64-GE-416AGE T64-GE-416AT64-416A
- Domains
- aviation
- Identity Level
- variant
- Kind
- turboshaft
- Name
- General Electric T64-GE-416A
- Status
- unknown
Details
- Air Breathing Specs
- Shaft Power Kw
- 3,266
- Description
- General Electric T64-GE-416A is a historical T64 turboshaft variant identified by official Marine Corps aircraft data as the three-engine CH-53E powerplant at 4,380 shaft horsepower per engine. NAVAIR describes the later T64-GE-419 improvement path; this exact variant remains distinct from the current -419 installation and the T64 family.
- Developers
- Family
- Manufacturers
Links
Assets & Meta
- Creation Time
- September 8, 2026 at 08:53:16 UTC
- Updated Time
- September 8, 2026 at 08:53:16 UTC
Other
- Search Name
- General Electric T64-GE-416A T64-GE-416A GE T64-GE-416A T64-416A
- Sources
- Accessed Date
- 2026-09-08
- Note
- The Marine Corps aircraft reference identifies CH-53E with three General Electric T64-GE-416A engines at 4,380 shaft horsepower each; the normalized value is 3,266 kW per engine.
- Publisher
- U.S. Marine Corps
- Title
- Marine Corps Aircraft 1913-2000
- Accessed Date
- 2026-09-08
- Note
- GE's T64 data sheet separately lists the T64-416A turboshaft configuration and distinguishes it from T64-419 and other T64 configurations.
- Publisher
- GE Aerospace
- Title
- T64 turboshaft/turboprop engines datasheet
- Accessed Date
- 2026-09-08
- Note
- NAVAIR describes the upgrade path from T64-GE-416 toward the more powerful T64-GE-419, supporting separate historical and current installation records.
- Publisher
- Naval Air Systems Command
- Title
- H-53 engine improvement article