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Hawker 800

executive aircraft model by BAE Systems

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General referenceInterpretive dossier study · Crown Archives visual atlas
Record originEnglish Wikipedia
Text licenseCC BY-SA 4.0
Source revisionSep 21, 2026
Entity authorityQ485226
Source-derived summary

The Hawker 800 is a mid-size twinjet corporate aircraft. It is a development of the British Aerospace 125, and was assembled by Hawker Beechcraft.

Development

In April 1981, the British Aerospace (BAe) board sanctioned the programme to improve the British Aerospace 125-700 series. By May 1983, the new aircraft was ready for its first test flight.

The BAe 125-800 series has a number of modifications and changes over the 700, the most noticeable being the redesigned cockpit windscreen. Accompanying this are a modified rear fuselage fairing, as well as a glass cockpit and uprated (from 3,700 to 4,300 lb thrust) Garrett TFE731-5R-1H engines. British Aerospace incorporated wingtip devices to reduce drag and improve aerodynamic efficiency.

From the first BAe 125 flight in August 1962, it took nineteen years until the 500th airframe was sold. In about five years, British Aerospace was registering the 200th sale of the 800 series.

In 1994, Raytheon (which bought Beech Aircraft Corporation in 1980) acquired BAe Corporate Jets.

Editorial summary

“Hawker 800” enters the record as executive aircraft model by BAE Systems. Crown Archives preserves that source wording while asking what Hawker, executive and aircraft can confirm, complicate or overturn.

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—1981, 1983, 1962, 1994—that can be checked directly. The selected authority fields contribute no independent date. Its strongest next move is a source search built around Hawker, executive and aircraft.
Editorial analysis

Why this record matters

“Hawker 800” is worth following because a concise public description often conceals a longer documentary argument. Here, Hawker, executive and aircraft provides the most credible route into that argument.

Evidence profile

Vocabulary and entity names are the principal evidence signals here, because they determine the precision of every later search. The source revision retrieved here is dated Sep 21, 2026. The linked authority identifier is Q485226. None of the 0 selected statements returned an explicit reference. The first chronological checks are 1981, 1983, 1962 and 1994.

Critical limits

The absence of detail may reflect summary conventions rather than a lack of surviving documentation. The source lead contains qualifying language; that uncertainty should survive quotation, summary and reuse. Authority statements aid reconciliation but still require their own references, qualifiers and ranks to be checked.

How to read it

Use the entry as an orientation point, then follow its citations and revision history. Names, dates and institutional relationships should be checked against the original record.

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  • Search vocabulary
  • Locating named sources
Verify next

The closest primary source, responsible institution and strongest cited specialist reference.

Three-step research path

  1. Establish the record: confirm the title “Hawker 800”, its source revision and the description used here.
  2. Expand the search: follow Hawker 800 primary sources, Hawker 800 archive and Hawker 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.

Questions for further research

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  2. What terminology or title could unlock a more precise catalogue search?
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Source & attribution

This entry incorporates text from Hawker 800” 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.