Short Scion

Twin engine short haul aircraft


title: "Short Scion" type: doc version: 1 created: 2026-02-28 author: "Wikipedia contributors" status: active scope: public tags: ["1930s-british-airliners", "short-brothers-aircraft", "high-wing-aircraft", "aircraft-first-flown-in-1933", "twin-piston-engined-tractor-aircraft"] description: "Twin engine short haul aircraft" topic_path: "geography/united-kingdom" source: "https://en.wikipedia.org/wiki/Short_Scion" license: "CC BY-SA 4.0" wikipedia_page_id: 0 wikipedia_revision_id: 0

::summary Twin engine short haul aircraft ::

::data[format=table title="Infobox aircraft"]

FieldValue
nameS.16 Scion/Scion II
imagePOBJOY SHORT "SCION" 5 SEATER LANDPLANE OF THE PALESTINE AIRWAYS COMPANY, FOUNDED BY PINHAS RUTHENBERG IN 1934. מטוס נוסעים של חברת "נתיבי אויר ארץ ישD2-045.jpg
captionPalestine Airways Pobjoy-Short Scion II, 1938
typeLight transport landplane/floatplane
manufacturerShort Brothers
Pobjoy Airmotors Ltd.
designerArthur Gouge
first_flight18 August 1933
number_built22
Scion: 5
Scion II: 17
statusRetired
variantsShort S.22 Scion Senior
::

|name = S.16 Scion/Scion II |image =POBJOY SHORT "SCION" 5 SEATER LANDPLANE OF THE PALESTINE AIRWAYS COMPANY, FOUNDED BY PINHAS RUTHENBERG IN 1934. מטוס נוסעים של חברת "נתיבי אויר ארץ ישD2-045.jpg |caption =Palestine Airways Pobjoy-Short Scion II, 1938 |type = Light transport landplane/floatplane |manufacturer = Short Brothers Pobjoy Airmotors Ltd. |designer = Arthur Gouge |first_flight = 18 August 1933 |introduction = |retired = |produced = |number_built = 22 Scion: 5 Scion II: 17 |status = Retired |unit cost = |primary_user = |more_users = |developed_from = |variants = Short S.22 Scion Senior

The **Short S.16 Scion ** and Scion II were 1930s British two-engine, cantilever monoplanes built by Short Brothers and (under licence) by Pobjoy Airmotors and Aircraft Ltd. in Rochester, Kent between 1933 and 1937. Altogether 22 Scion/Scion II aircraft were built and they provided useful service to operators working from small airstrips/water courses in many parts of the globe, including Europe, the Near and Middle East, Sierra Leone, Papua New Guinea and Australia. Many were impressed into the Royal Air Force during the Second World War, providing pilot ferry services, anti-aircraft co-operation and radar calibration duties. Of the civilian Scions, at least two were still operating in Australia in 1966, one having been re-engined with de Havilland Gipsy Minor engines.

Design

The Scion and the later Scion II version were high wing cantilever monoplanes with fabric-covered metal wings and fuselage, the latter providing an enclosed cabin for the pilot and 5–6 passengers. The tail unit comprised a cantilever tailplane with a single fin and rudder. The prototype aircraft was powered by two 80 hp Pobjoy R radial engines; the production aircraft however were fitted with the 90 hp Pobjoy Niagara III radial engines. The engines in the Scion were mounted with thrust-lines below the chord-line of the wings; in the Scion II they were raised so that the thrust-lines were aligned with the chord-line, to avoid trim changes in pitch with changes in power. Both the Scion and the Scion II were produced as either landplanes or floatplanes, the majority as landplanes (see the table below). On the landplanes the landing gear comprised a single wheel on each side of the fuselage, mounted on a vertical coil-spring and oleo leg inboard of the engine; there was a small castoring tailwheel mounted below the rear end of the fuselage.

History

::figure[src="https://upload.wikimedia.org/wikipedia/commons/5/5e/PASSENGER_PLANE_OF_THE_PALESTINE_AIRWAYS_COMPANY_AT_THE_LOD_AIRPORT.מטוס_נוסעים_של_חברת"נתיבי_אויר_ארץ_ישראל"_חונה_בנמל_התעופה_בלוד.D2-044.jpg" caption="Scion II, VQ-PAB, at the service of Palestine Airways Ltd in 1938"] ::

The Scion was developed as a light transport for 5–6 passengers. The first flight of the prototype aircraft (G-ACJI) took place on 18 August 1933, piloted by Shorts' Chief Test Pilot John Lankester Parker. The first production aircraft (G-ACUV) was flown at the SBAC's airshow at Hendon in 1934. In 1935 the fifth production model was built as the revised model Scion II; the major improvement was the repositioning of the two engines as noted above; other changes included the provision of 6 passenger seats as standard (on the original Scion there was a folding seat for a sixth passenger if needed), an improved windscreen and better cabin windows. During the production of the Scions the company had opened a new factory at Rochester Airport and all Scion IIs were manufactured there, initially by Shorts, later by Pobjoy, first under licence and later under Shorts' ownership.

G-ADDR, the fifth Scion II, was retained by Shorts as an experimental testbed aircraft, and it was on this aircraft (temporarily designated M.3) that a scale wooden model of the slender wings (with Gouge flaps) for the later Short Empire boats was tested, the first flight in this configuration being conducted by Lankester Parker on 6 August 1935. With these flaps fitted it was tested at the Royal Aircraft Establishment, which found that the Gouge flap decreased distance to take-off and stalling speed, among other improvements. Further work with standard wings was carried out; one flight from Rochester Airport, with experimental full-span flaps incorporating retractable spoilers instead of ailerons, was made on 22 July 1936; this idea proved unworkable, Lankester Parker having to draw on his considerable experience to coax the aircraft around on a single circuit before landing safely. The standard wing was refitted and the aircraft continued with Shorts in this configuration until it was impressed into military service in 1940, an operational usage experienced by 14 of the 22 Scion/Scion II aircraft.

::figure[src="https://upload.wikimedia.org/wikipedia/commons/4/4b/Short_Scion_G-AEZF_SGT_25.10.48_edited-2.jpg" caption="Pobjoy-built S.16/1 Scion 2 ''G-AEZF'' hangared at [[Blackpool Airport]] in 1948"] ::

G-AEZF, built by Pobjoy and first flown in December 1937, was originally operated as a floatplane by Elders Colonial Airways in Sierra Leone, between Bathurst (Gambia) and Freetown, and was returned to Shorts in 1939 and converted into a landplane in 1941. After operating for the company for another six years it was eventually sold on to Air Couriers Ltd. in 1947, after which it changed hands between private owners several times before finally ending up at Southend airport. The plane is now undergoing restoration by Medway Aircraft Preservation Society (MAPSL), funded in part by a grant from the Rochester Bridge Trust.

A larger 9-passenger enlarged version of Scion was produced as the Short S.22 Scion Senior.

Survivors

;G-AEZF:After a long career, this aircraft stood derelict at Southend Airport. Its frame was rescued and held for long-term restoration by the Medway Aircraft Preservation Society at Rochester Airport. Newly restored, it was exhibited at Rochester Cathedral by the Rochester Bridge Trust in August 2025.

;G-ACUX: one of the 'Australian' Scions still flying in the 1960s, was later returned to the United Kingdom and is held in deep storage at the Ulster Folk and Transport Museum, Cultra, Holywood, Northern Ireland. It is claimed that its condition has been allowed to deteriorate. It was not on public display in April 2012.

;VH-UTV: another 'Australian' Scion. Under restoration at Luskintyre in New South Wales to return to operable condition. Privately owned.

Variants

  • S-16 Scion : Company designation.
  • Scion : Light transport aircraft, powered by two 85 hp Pobjoy Niagara I or II piston engines. Five built, one prototype and four production machines.
  • Scion II : Light transport aircraft, powered by two 90 hp Pobjoy Niagara III piston engines.
  • M.3: Scion II fitted with scaled-down Empire flying-boat wings with Gouge flaps

Scion and Scion II production

::data[format=table title="List of aircraft"]

AircraftTypeFirst flightTypeManufacturerBuiltNotes12345678910111213141516171819202122
G-ACJILandplane18 August 1933Scion (prototype)ShortsSeaplane Worksto RAF in 1940
G-ACUVLandplane18 August 1933ScionShortsSeaplane Works
G-ACUWLandplane18 August 1933ScionShortsSeaplane Worksto RAF in 1940
G-ACUXFloatplane18 August 1933ScionShortsSeaplane Works
G-ACUYLandplane10 December 1934ScionShortsSeaplane Worksto RAF in 1940
G-ACUZLandplane13 February 1935Scion IIShortsRochester Airport
G-ADDNLandplane9 June 1935Scion IIShortsRochester Airportto RAF in 1940
G-ADDOLandplane10 July 1935Scion IIShortsRochester Airportto RAF in 1940
G-ADDPLandplane10 July 1935Scion IIShortsRochester Airportto RAF in 1940
G-ADDRLandplane6 August 1935Scion IIShortsRochester Airportto RAF in 1940
VH-UUTLandplane23 August 1935Scion IIShortsRochester Airport
G-ADDTLandplaneScion IIShortsRochester Airport
VH-UVQLandplane-Scion IIShortsRochester Airport
G-ADDVLandplaneScion IIShortsRochester Airportto RAF in 1940
VH-UTVLandplaneScion IIShortsRochester Airport
G-ADDXLandplaneScion IIShortsRochester Airportto RAF in 1940
VQ-PAALandplaneScion IIPobjoyRochester Airportto RAF in 1941
VQ-PABLandplaneScion IIPobjoyRochester Airportto RAF in 1941
G-AEILLandplane1936Scion IIPobjoyRochester Airportto RAF in 1940
G-AEJNLandplaneSeptember 1936Scion IIPobjoyRochester Airportto RAF in 1940
G-AETTLandplaneApril 1937Scion IIPobjoyRochester Airportto RAF in 1940
G-AEZFFloatplane9 December 1937Scion IIPobjoyRochester Airportpreserved
::

Operators

Floatplanes ;Australia

  • Papuan Concessions Ltd (VH-UUP the former G-ACUX) ;Sierra Leone
  • Elders Colonial Airways Ltd (Bathurst-Freetown) (G-AEZF)

Landplanes ;Aden

Specifications (Scion II landplane)

|ref=British Civil Aircraft 1919–1972: Volume III |prime units?=imp General characteristics

|genhide=

|crew=1 |capacity=6 passengers |span m= |span ft=42 |span in=0 |length m= |length ft=31 |length in=6 |height m= |height ft=10 |height in=4+1/2 |wing area sqm= |wing area sqft=255.3 |empty weight kg= |empty weight lb=1770 |gross weight kg= |gross weight lb=3200 |fuel capacity=31 impgal Powerplant

|eng1 number=2 |eng1 name=Pobjoy Niagara III |eng1 type=7-cylinder geared radial engines |eng1 hp=90

|prop blade number=2 |prop name=wooden fixed-pitch propellers |prop dia m= |prop dia ft= |prop dia in=

Performance

|max speed mph=128 |cruise speed mph=116 |range miles=390 |ceiling ft=13000 |climb rate ftmin=625 |more performance=*Take-off run: 420 ft

  • Landing run: 420 ft

|avionics=

References

Bibliography

  • {{cite journal | last =Cohen, B.A., B.Sc. | first =J. | title =Full Scale Trials on Scion M.3 with a Gouge Flap | journal = Reports & Memoranda | issue = 1753 | publisher = Aeronautical Research Committee, Air Ministry | year = 1936 | url =http://naca.central.cranfield.ac.uk/reports/arc/rm/1753.pdf
  • Green, William. Flying Boats Vol.5 (Warplanes of the Second World War). London: Macdonald & Co., 1962.
  • The Illustrated Encyclopedia of Aircraft (part: 1982–1985). London: Orbis Publishing.
  • Jackson, A.J. British Civil Aircraft since 1919. London: Putnam & Sons, Ltd., 1974. .

References

  1. Barnes and James, p.294.
  2. Barnes and James, p.287.
  3. Cohen, 1936, R&M 1753, p.3.
  4. Barnes and James, p.293.
  5. "Home".
  6. https://www.rochestercathedral.org/floatplane
  7. (2025-08-01). "Rochester Cathedral welcomes restored WW2 plane for exhibition".
  8. [http://www.ibiblio.org/pub/academic/history/marshall/military/airforce/museum.txt ibiblio.org]
  9. Jackson 1988, pp. 143–144.
  10. ''Flight'' 28 February 1935, p. 220.

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1930s-british-airlinersshort-brothers-aircrafthigh-wing-aircraftaircraft-first-flown-in-1933twin-piston-engined-tractor-aircraft