GE GEnx-1B76/P2
Exact GE GEnx-1B76/P2 turbofan certification variant listed in EASA’s current IM.E.102 Issue 12 TCDS, with 349.2 kN take-off thrust and 6,147.1 kg dry weight. Identity remains certification-level only; no family link, actor attribution, sibling variant, lineage edge, or vehicle installation is inferred.
Identity
- Aliases
- GEnx-1B76/P2GE GEnx-1B76/P2GEnx 1B76/P2
- Domains
- aviation
- Identity Level
- variant
- Kind
- turbofan
- Name
- GE GEnx-1B76/P2
- Status
- active
Details
- Air Breathing Specs
- Max Thrust Kn
- 349.2
- Description
- Exact GE GEnx-1B76/P2 turbofan certification variant listed in EASA’s current IM.E.102 Issue 12 TCDS, with 349.2 kN take-off thrust and 6,147.1 kg dry weight. Identity remains certification-level only; no family link, actor attribution, sibling variant, lineage edge, or vehicle installation is inferred.
- Developers
- Dry Mass Kg
- 6147.1
- Family
- Manufacturers
Links
- Official Url
- https://www.easa.europa.eu/en/downloads/7641/en
Assets & Meta
- Creation Time
- August 7, 2026 at 07:50:47 UTC
- Updated Time
- August 22, 2026 at 11:57:14 UTC
Other
- Sources
- Accessed Date
- 2026-08-22
- Note
- EASA’s current IM.E.102 Issue 12 TCDS explicitly lists GEnx-1B76/P2 as an exact model and specifies 349.2 kN take-off thrust plus 6,147.1 kg dry weight for the GEnx-1B/P2 models.
- Publisher
- European Union Aviation Safety Agency
- Title
- EASA IM.E.102 — GEnx Series Engines, Issue 12
- Accessed Date
- 2026-08-22
- Note
- FAA/EASA safety material preserves GEnx-1B-series and P-series model boundaries; this record retains its certification-level identity boundary.
- Publisher
- Federal Aviation Administration
- Title
- FAA GEnx engine applicability