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Rolls-Royce AE 2100

turboprop aircraft engine family

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General referenceInterpretive dossier study · Crown Archives visual atlas
Record originEnglish Wikipedia
Text licenseCC BY-SA 4.0
Source revisionAug 4, 2026
Entity authorityQ826898
Source-derived summary

The Rolls-Royce AE 2100 is a turboprop developed by Allison Engine Company, now part of Rolls-Royce North America. The engine was originally known as the GMA 2100, when Allison was a division of former corporate parent General Motors.

Development

On 11 July 1989, Saab-Scania A.B. selected the GMA 2100 to power its new Saab 2000, a 50-seat stretch of the Saab 340 turboprop, in a US$500 million deal. In July 1990, Industri Pesawat Terbang Nusantara (IPTN) of Indonesia picked the GMA 2100 as the engine for the twin-engine N-250 regional airliner. Flight testing with a 13 ft 6 in diameter (4.11 m) Dowty R373 propeller on a Lockheed P-3 Orion testbed aircraft began on 23 August 1990, and finished after over 50 hours of flight and ground testing.

The GMA 2100D3 became the powerplant for the Lockheed Martin C-130J Super Hercules. It made its first test flight on 19 March 1994, which was conducted by Marshall Aerospace on a Lockheed C-130K Hercules testbed leased from the Royal Air Force. Testing ended in June 1994 after 47 flight hours. The engine powered the initial flight of the C-130J aircraft on 5 April 1996. By April 1997, the D3 variant had received Federal Aviation Administration (FAA) type certification.

Editorial summary

Begin with the source’s own compact description: “Rolls-Royce AE 2100” is turboprop aircraft engine family. The dossier treats that line as a proposition to test through Rolls-Royce, turboprop and aircraft, not as a finished interpretation.

Editorial reviewA practical starting point whose main value is the path it opens into stronger specialist and primary sources. The current lead gives the account dated anchors—1989, 2000, 1990, 1994—that can be checked directly. The selected authority fields contribute no independent date. For this dossier, Rolls-Royce, turboprop and aircraft is the immediate research focus.
Editorial analysis

Why this record matters

The phrase “turboprop aircraft engine family” supplies a clear boundary for inquiry. It also exposes the unanswered questions: who defined that boundary, when it became stable and which sources sit outside it.

Evidence profile

Named sources, stable identifiers and responsible institutions provide the strongest route from overview to verifiable evidence. The source revision retrieved here is dated Aug 4, 2026. The linked authority identifier is Q826898. None of the 0 selected statements returned an explicit reference. The first chronological checks are 1989, 2000, 1990 and 1994.

Critical limits

A concise general-reference account can conceal disagreements about scope, terminology or the weight assigned to individual sources. The lead is largely declarative, so disagreement and counter-evidence require a deliberate search beyond the opening account. Authority statements aid reconciliation but still require their own references, qualifiers and ranks to be checked.

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  2. Expand the search: follow Rolls-Royce AE 2100 primary sources, Rolls-Royce AE 2100 archive and Rolls-Royce research across catalogues and specialist indexes.
  3. Test the account: compare the strongest cited source with the responsible institution’s current record and note any disagreement.

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Source & attribution

This entry incorporates text from Rolls-Royce AE 2100” on English Wikipedia. Contributors are listed in the page history. Text is available under the Creative Commons Attribution-ShareAlike 4.0 License. Selected authority identifiers and statements are retrieved from Wikidata under CC0; their references and qualifiers remain part of the verification path.