Airbus A310-200 Standard-Range Widebody Airliner Variant
The Airbus A310-200 is the standard-range, shorter-fuselage twin-engine widebody airliner variant, certified across 310-203, 310-203C, 310-204, and 310-222 models and available with GE CF6-80 and Pratt & Whitney JT9D engine families. Airbus lists 144,000 kg MTOW for the A310-200 WV011 weight variant, compared with 132,000 kg for WV000 basic. Its standard single-class planning layout has 237 seats. These values describe the named weight and cabin configurations, rather than every A310-200 or a freighter conversion.
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Identity
- Aliases
- A310-200A310-203A310-203CA310-204A310-222Airbus A310-200
- Family Name
- Airbus A310-200
- Full Name
- Airbus A310-200 Standard-Range Widebody Airliner Variant
- Roles
- airlinercargo
- Status
- active
- Type
- aircraft
- Variant Name
- A310-200
Details
- Aircraft Specs
- Configuration
- fixed_wing
- Max Takeoff Mass
- …
- Operating Modes
- land
- Passenger Capacity
- 237
- Takeoff Landing Capabilities
- conventional
- Description
- The Airbus A310-200 is the standard-range, shorter-fuselage twin-engine widebody airliner variant, certified across 310-203, 310-203C, 310-204, and 310-222 models and available with GE CF6-80 and Pratt & Whitney JT9D engine families. Airbus lists 144,000 kg MTOW for the A310-200 WV011 weight variant, compared with 132,000 kg for WV000 basic. Its standard single-class planning layout has 237 seats. These values describe the named weight and cabin configurations, rather than every A310-200 or a freighter conversion.
- Dimensions
- Length
- …
- Wingspan
- …
- First Flight Year
- 1,982
- Manufacturer
- Parent Vehicle Family
- Propulsion Configurations
- Entries
- Count
- 2
- Placement
- nacelle
- Propulsion System
- Role
- main
- Stage
- airframe
- Variant Notes
- Two GE CF6-family turbofans; exact A310-200 suffix is not inferred.
- Name
- A310-200 GE CF6-80 family option
- Notes
- Airbus A310-200 planning data identifies GE CF6-80 engines; the canonical production relationship remains the existing CF6 family because no separate CF6-80A3 or CF6-80C2 variant node is present.
- Entries
- Count
- 2
- Placement
- nacelle
- Propulsion System
- Role
- main
- Stage
- airframe
- Variant Notes
- Two Pratt & Whitney JT9D-family turbofans; exact A310-200 suffix is not inferred.
- Name
- A310-200 Pratt & Whitney JT9D family option
- Notes
- Airbus planning and certification material identify Pratt & Whitney JT9D engines for A310-200, including the original JT9D-7R4D1 installation; the canonical production relationship remains family-level.
Links
Assets & Meta
- Creation Time
- August 12, 2026 at 21:44:43 UTC
- Updated Time
- October 17, 2026 at 11:57:08 UTC