Pratt & Whitney PW6122A
Pratt & Whitney PW6122A turbofan variant in the PW6000 series. EASA TCDS IM.E.020 identifies the axial-flow dual-spool design and rates PW6122A at 9,830 daN (98.30 kN) five-minute takeoff thrust; certification is distinct from lifecycle, which remains unknown here.
Identity
- Aliases
- PW6122APratt & Whitney PW6122APW6000 PW6122A
- Domains
- aviation
- Identity Level
- variant
- Kind
- turbofan
- Name
- Pratt & Whitney PW6122A
- Status
- unknown
Details
- Air Breathing Specs
- Max Thrust Kn
- 98.3
- Spool Count
- 2
- Description
- Pratt & Whitney PW6122A turbofan variant in the PW6000 series. EASA TCDS IM.E.020 identifies the axial-flow dual-spool design and rates PW6122A at 9,830 daN (98.30 kN) five-minute takeoff thrust; certification is distinct from lifecycle, which remains unknown here.
- Developers
- Family
- Manufacturers
Links
Assets & Meta
- Creation Time
- August 7, 2026 at 23:35:21 UTC
- Updated Time
- August 15, 2026 at 23:38:14 UTC
Other
- Sources
- Accessed Date
- 2026-08-07
- Note
- The type-certificate sheet explicitly lists PW6122A and PW6124A as distinct PW6000 variants.
- Publisher
- European Union Aviation Safety Agency
- Title
- TCDS IM.E.020 — PW6000 series engines
- Accessed Date
- 2026-08-07
- Note
- Manufacturer collateral establishes the PW6000 commercial turbofan family; this packet preserves the exact PW6122A suffix and does not infer an installation.
- Publisher
- Pratt & Whitney
- Title
- PW6000 Engine