Просмотр кода страницы Английская Википедия:De Havilland Heron

{{Английская Википедия/Панель перехода}}
{{Short description|Small propeller-driven British airliner, 1950}}
{{Use dmy dates|date=May 2019}}
{{EngvarB|date=May 2019}}
{{lowercase title|de Havilland Heron}}
{|{{Infobox aircraft begin
 |name= DH.114 Heron
 |image= File:G-AOXL DH114 Heron 1 BUIA LGW 29APR69 (6812537759).jpg
 |caption=De Havilland DH.114 Heron 1 of [[British United Island Airways]] at [[London Gatwick Airport]] in April 1969
}}{{Infobox aircraft type
 |type=[[Airliner]]
 |national origin= United Kingdom
 |manufacturer=[[de Havilland]]
 |designer=
 |first flight=10 May 1950
 |introduced= [[1950 in aviation|1950]]
 |retired=
 |status= Retired
 |primary user=[[Garuda Indonesian Airways]]
 |more users= See Operators
 |produced=
 |number built=149<ref name = "Bae history"/>
 |developed from=[[de Havilland Dove]]
 |variants with their own articles= [[Saunders ST-27]]
}}
|}
[[File:Heron 1.jpg|thumb|right|DH.114 Heron 2 restored in the United States]]

The '''de Havilland DH.114 Heron''' is a small [[Propeller (aircraft)|propeller]]-driven British [[airliner]] that first flew on 10 May 1950. It was a development of the twin-engine [[de Havilland Dove]], with a stretched [[fuselage]] and two more [[Reciprocating engine|engines]]. It was designed as a rugged, conventional low-wing monoplane with [[tricycle undercarriage]] that could be used on regional and commuter routes. A total of 149 were built;<ref name = "Bae history">{{Cite web|url=https://www.baesystems.com/en/heritage/de-havilland-dh114-heron|title=De Havilland DH114 Heron}}</ref> it was also exported to about 30 countries. Herons later formed the basis for various conversions, such as the [[Advanced Aircraft|Riley]] '''Turbo Skyliner''' and the [[Saunders ST-27|Saunders ST-27 and ST-28]].

==Design and development==
In the closing stages of the [[World War II|Second World War]], the aircraft manufacturer [[de Havilland]] began development of a new small twin-engined passenger aircraft, the DH 104 Dove, intended as a replacement for the earlier [[de Havilland Dragon Rapide|Dragon Rapide]] and which soon proved to be successful. As a further development, the company basically enlarged the Dove; the fuselage was lengthened to make room for more passengers or freight, and the wingspan was increased to make room for two more engines. The Heron was of all-metal construction, and was laid out as a conventional design; the resulting aircraft could use many of the parts originally designed for the Dove, thus simplifying logistics for airlines using both types.

The emphasis was on rugged simplicity to produce an economical aircraft for short- to medium-stage routes in isolated and remote areas which did not possess modern airports. The Heron was designed with a fixed undercarriage and [[de Havilland Gipsy Queen|Gipsy Queen 30]] engines, which lacked potentially unreliable [[reduction gearbox]]es and [[supercharger]]s.

The Heron prototype registered to the de Havilland Aircraft Company, [[Hatfield, Hertfordshire|Hatfield]], UK, as ''[[Aircraft registration|G-ALZL]]'' undertook its first flight with Geoffrey Pike at the controls on 10 May 1950.<ref name = "Jacksonv2">Jackson, A.J. ''British Civil Aircraft Since 1919, Volume 2''. London: Putnam & Company, 1973. {{ISBN|0-370-10010-7}}.</ref> The aircraft was unpainted at the time, and after 100 hours of testing was introduced to the public on 8 September 1950 at the [[Farnborough Airshow]], still glistening in its polished metal state. By November, the prototype had received its formal British Certificate of Airworthiness and had flown to [[Khartoum]] and [[Nairobi]] for tropical trials.

The prototype was then painted and fitted out as a company demonstrator, and was tried by [[British European Airways]] in 1951 on its Scottish routes. Following the successful completion of the prototype trials as a regional airliner, series production of the Heron began. The first deliveries were to NAC, the New Zealand [[National Airways Corporation (New Zealand)|National Airways Corporation]] (later part of [[Air New Zealand]]).

Basic price for a new Heron in 1960 was around £60,000, minus radio.<ref>{{Cite web |url=http://www.flightglobal.com/pdfarchive/view/1960/1960%20-%202684.html |title=Archived copy |access-date=24 July 2012 |archive-date=12 May 2013 |archive-url=https://web.archive.org/web/20130512174522/http://www.flightglobal.com/pdfarchive/view/1960/1960%20-%202684.html |url-status=dead }}</ref>

==Operational service==
{{More citations needed section|date = August 2015}}

The first Heron, '''Series 1A''' suffered deficiencies, as NAC soon discovered. First, the aircraft was generally underpowered. Its quite heavy engines (weighing about {{Convert|220|kg|lb|order=flip}} each), had an output of only {{convert|250|hp|abbr=on}} each. By comparison, later modifications or rebuilt aircraft had as much as 50% more power (in the case of the Saunders ST-27). Unlike the Dove, the Heron came with a fixed undercarriage and no nosewheel steering, which simplified maintenance, but reduced top speed. Secondly, the lightweight aluminium alloy wingspars were prone to constant cracking due to the heavy loading on the wing caused by the overweight engines and rough landings on unpaved runways. NAC resolved this by replacing the aluminium spars with heavier steel spars, reducing the performance of the Heron Series 1A (re-classified 1B) to uneconomic levels for the services required of them in New Zealand. NAC disposed of them in 1957.

After 51 Series 1 aircraft had been built, production switched to the '''Series 2''', featuring retractable landing gear, which reduced drag and fuel consumption, and increased the top speed marginally. The '''2A''' was the equivalent of the 1A, the basic passenger aircraft while the 1B and its successor the '''2B''' had higher maximum takeoff weight, the '''2C''' featured fully feathering propellers, the Heron '''2D''' had an even higher maximum takeoff weight, while the Heron '''2E''' was a [[Very Important Person|VIP]] version.

In service, the Heron was generally well received by flight crews and passengers who appreciated the additional safety factor of the four engines. At a time when smaller airliners were still rare in isolated and remote regions, the DH.114 could provide reliable and comfortable service with seating for 17 passengers, in individual seats on either side of the aisle.

With its larger fuselage, passengers could stand up whilst moving down the aisle and large windows were also provided. Baggage was stored in an aft compartment with an additional smaller area in the nose. A few peculiarities appeared; passengers who filled the aft rows first would find that the Heron gently "sat down" on its rear skid. Pilots and ground crews soon added a tail brace to prevent the aircraft from sitting awkwardly on its tail.

Performance throughout the Heron range was relatively "leisurely", and after production at de Havilland's Chester factory ceased in 1963, several companies, most notably '''Riley Aircraft Corporation''', offered various Heron modification kits, mainly related to replacing the engines, which greatly enhanced takeoff and top speed capabilities. Riley Aircraft replaced the Gipsy Queens with horizontally-opposed [[Lycoming O-540|Lycoming IO-540]] engines. 
[[File:DH.114 Heron 2 mod N574PR Prinair 011273.jpg|thumb|Prinair Heron with greatly lengthened fuselage ({{Convert|17|ft|disp=or}}) and fitted with Continental 520 engines]]

[[File:DH.114 Riley N15FB Fischer edited-2.jpg|thumb|left|DH Riley Heron fitted with Lycoming engines at [[Cleveland Hopkins International Airport|Cleveland Airport]] Ohio in 1982. It is operated by Fischer Brothers for [[Allegheny Commuter]].]]

One U.S. airline that carried out Riley-type conversions at their [[Opa Locka|Opa Locka Airport]], Florida, engineering facility was [[Prinair]], of Puerto Rico, which replaced the Gipsy Queens with [[Continental Motors Company|Continental]] IO-520 engines.<ref>[http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgstc.nsf/0/FB2A55478F8143EB85256CCB00601865 "FAA Supplemental Type Certificate SA1685WE."] {{Webarchive|url=https://web.archive.org/web/20210624134858/https://rgl.faa.gov/Regulatory_and_Guidance_Library/rgstc.nsf/0/FB2A55478F8143EB85256CCB00601865 |date=24 June 2021 }} ''faa.gov''. Retrieved: 13 August 2008.</ref> Prinair also considerably stretched Heron 2 ''N574PR'' to allow extra passengers to be carried.

[[Connellan Airways]] also converted its Herons, using Riley kits. When available aircraft reached the end of their service lives, the engine conversions gave the elderly airliner a new lease of life as a number of examples were converted in the 1970s and 1980s including ''N415SA'', a Riley Heron still flying in Sweden as of 20 May 2012 and a Riley Turbo Skyliner, tail number ''[https://web.archive.org/web/20071210055426/http://registry.faa.gov/aircraftinquiry/NNumSQL.asp?verified=1&NNumbertxt=600PR N600PR]'' currently registered in the United States (this example appeared in the 1986 movie [[Club Paradise]]<ref>Ebert, Roger.  [http://rogerebert.suntimes.com/apps/pbcs.dll/article?AID=/19860711/REVIEWS/607110301/1023 " 'Club Paradise' Review".] ''Roger Ebert.com''. Retrieved: 1 April 2007. Note: The Riley Heron is integral to the plot as it unloads planeloads of unsuspecting tourists at a ramshackle resort.</ref>).

The most radical modification of the basic Heron airframe was the [[Saunders ST-27|Saunders ST-27/-28]], that changed the configuration as well as the "look" of the whole aircraft with two powerful [[turboprop]] engines replacing the lethargic four-engine arrangement, a stretched fuselage, the shape of the windows changed and the wingtips squared instead of rounded.

==Variants==
[[File:DH.114 Heron 1B Morton 1965.jpg|thumb|right|DH.114 Heron 1B of Morton Air Services in 1965. Note fixed undercarriage of this version]]
* '''Heron 1''': Four-engined light transport aircraft. Fitted with fixed landing gear.
** '''Heron 1B''': This model had an increased takeoff weight of {{Convert|13000|lb|4 = -1}}.
* '''Heron 2''': Four-engined light transport aircraft. Fitted with retractable landing gear.
** '''Heron 2A''': This designation was given to a single Heron 2, which was sold to a civil customer in the US.
** '''Heron 2B''': This model had the same increased takeoff weight as the Heron 1B.
** '''Heron 2C''': Redesignation of the Heron 2Bs, which could be fitted with optional fully feathering propellers.
** '''Heron 2D''': Four-engined light transport aircraft. This model had an increased takeoff weight of {{Convert|13500|lb|4 = -1}}.
** '''Heron 2E''': VIP transport aircraft. One custom-built aircraft.
* '''Heron C.Mk 3''': VIP transport version for the Queen's Flight, [[Royal Air Force]] (RAF). Two built.
* '''Heron C.Mk 4''': VIP transport aircraft for Queen's Flight, RAF. One built.
* '''Sea Heron C.Mk 20''': Transport and communications aircraft for the [[Royal Navy]]. Three ex-civil Heron 2s and two Heron 2Bs were acquired by the Royal Navy in 1961.
* '''Riley Turbo Skyliner''': Re-engined aircraft. A number of Herons were fitted with {{Convert|290|hp|4 = 0|abbr = on}} [[Lycoming O-540|Lycoming IO-540]] flat-six piston engines.<ref>[http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgstc.nsf/0/BDB945FF897C517E85256CC100820FB5 "FAA Supplemental Type Certificate SA1368WE."]{{Dead link|date=November 2023 |bot=InternetArchiveBot |fix-attempted=yes }} ''faa.gov''. Retrieved: 13 August 2008.</ref> The modifications were carried out by the Riley Turbostream Corporation of the USA.
[[File:Tawron03.JPG|thumb|right|Japanese custom model DH.114 Tawron]]
* '''[[Saunders ST-27]]''': The fuselage was lengthened by {{Convert|8|ft|6|in|abbr = on}}, to accommodate up to 23 passengers. It was powered by two {{Convert|750|shp|abbr = on}} [[Pratt & Whitney Canada PT6]]A-34 [[turboprop]] engines. Twelve Herons were modified by the Saunders Aircraft Corporation of [[Gimli, Manitoba]], Canada.
** '''[[Saunders ST-27A]]''' and '''[[Saunders ST-27B]]''': The original designations of the ST-28.
** '''[[Saunders ST-28]]''': Improved version of the ST-27. One prototype built.
* '''Shin Meiwa Tawron''': Conversion by [[Shin Meiwa]] of Japan for [[Toa Airways|Toa AirWays]] (TAW) with 260&nbsp;hp (194&nbsp;kW) [[Continental IO-470]] engines replacing the originals. Its name means "TAW"+He"ron".<ref name="Janes 65 p107">Taylor 1965, p. 107.</ref>

==Operators==
{{See also|List of de Havilland Heron operators}}

===Military operators===
*{{flag|Belgium}}<ref name=Katanga>{{cite web|url=http://www.acig.org/artman/publish/article_182.shtml |title=Congo, Part 1; 1960–1963 |publisher=ACIG |archive-url=https://web.archive.org/web/20150113052328/http://www.acig.org/artman/publish/article_182.shtml|archive-date=13 January 2015|year=2003|author= Tom Cooper}}</ref> 
* {{flag|Biafra}}
*{{flagicon|Sri Lanka}} [[Ceylon]]
*{{GER}}
*{{GHA}}
*{{flag|Iraq|1924}}
*{{JOR}}
*{{flagicon|Katanga}} [[State of Katanga|Katanga]]<ref name=Katanga/>
*{{KEN}}
*{{KUW}}
*{{MAR}}<ref>''Air International'' November 1985, p. 229.</ref>
*{{MYS}}
*{{flag|South Africa|1928}}
*{{UK}}

===Civil operators===
[[File:HeronG-ANXB-3.JPG|thumb|right|Heron 1B at the [[Newark Air Museum]]]]
[[File:OO-BIA DH114 Heron 1 Sabena RTM 10JAN68 (6812669405).jpg|thumb|right|Heron 1 of [[Sabena]]]]

*{{AUS}}
*{{BHR}}
*[[Gulf Aviation]]
*{{BEL}}
*{{BRA}}
*{{CAN}}
*{{CIV}}
*{{COL}}
*{{DNK}}
*{{FIJ}}
*{{FRA}}
*{{GER}}
*{{HON}}
*{{POR}}
*{{IND}}
*{{IDN}}
*{{ISR}}
*{{ITA}}
*{{JAM}}
*{{JPN}}
*{{NLD}}
*{{NZL}}
*{{NGR}}
*{{NOR}}
*{{PRI}}
*{{flag|Rhodesia}}
*{{STP}}
*{{LCA}}
*{{SLE}}
*{{THA}}
*{{TUR}}
*{{UK}}
*{{USA}}
*{{URY}}

==Accidents and incidents==
* On 18 April 1955, [[Union Aéromaritime de Transport]] F-BGOI, crashed into Kupe Mountain, [[Cameroon]]. 12 out of 14 passengers and crew died in the crash.<ref>{{Cite web |last=Ranter |first=Harro |title=ASN Aircraft accident de Havilland DH-114 Heron 1B F-BGOI Mount Kupe |url=https://aviation-safety.net/database/record.php?id=19550418-0 |access-date=2022-06-03 |website=aviation-safety.net}}</ref>
* On 7 November 1956, [[Braathens SAFE]] LN-SUR, crash-landed in heavy snow on the mountain [[Hummelfjell]] in [[Tolga, Norway|Tolga]], [[Norway]]. The pilot and one passenger were killed, whilst the remaining crew and passengers survived. The [[Hummelfjell Accident|Hummelfjell accident]] was Braathens SAFE's first fatal accident. The probable cause was unusually heavy icing. <ref>{{Cite web |last=Ranter |first=Harro |title=ASN Aircraft accident de Havilland DH-114 Heron 2B LN-SUR Hummelfjell Mountain |url=https://aviation-safety.net/database/record.php?id=19561107-0 |access-date=2022-06-03 |website=aviation-safety.net}}</ref>
* On 28 September 1957, [[British European Airways]] G-AOFY, on an air ambulance flight, crashed on approach to [[Glenegedale Airport]], [[Islay]], in bad weather. The three occupants, two crew and one nurse, were killed. The pilot did not appreciate that the aircraft had rapidly lost height whilst he was making a visual half circuit to land.<ref>{{Cite web |last=Ranter |first=Harro |title=ASN Aircraft accident de Havilland DH-114 Heron 1B G-AOFY Islay-Glenegedale Airport (ILY) |url=https://aviation-safety.net/database/record.php?id=19570928-0 |access-date=2022-06-03 |website=aviation-safety.net}}</ref>
* On 15 November 1957, [[Aviaco]] EC-ANZ crashed into a mountain close to the airport at [[Son Bonet Aerodrome]] in bad weather after the pilot made a navigation error at the end of a flight from [[Barcelona Airport]]. All six people on board were killed.<ref>{{Cite web |last=Ranter |first=Harro |title=ASN Aircraft accident de Havilland DH-114 Heron 2D EC-ANZ Son Bonet Airport Airport |url=https://aviation-safety.net/database/record.php?id=19571115-0 |access-date=2022-06-03 |website=aviation-safety.net}}</ref> 
* On 19 February 1958, [[Gulf Aviation]] G-APJS, on a ferry flight from [[Bahrain]] to [[England]] via [[Athens International Airport]], crashed into a mountain near [[Ciampino–G. B. Pastine International Airport|Rome]] after a navigational error, killing all three people on board.<ref>{{Cite web |last=Ranter |first=Harro |title=ASN Aircraft accident de Havilland DH-114 Heron 1B G-APJS Mount Scifarello |url=https://www.asndata.aviation-safety.net/database/record.php?id=19580219-3 |access-date=2022-06-03 |website=www.asndata.aviation-safety.net |archive-date=2 December 2021 |archive-url=https://web.archive.org/web/20211202095541/https://www.asndata.aviation-safety.net/database/record.php?id=19580219-3 |url-status=dead }}</ref> 
* On 14 April 1958, [[Aviaco]] EC-ANJ, crashed into the sea off the coast of [[Barcelona]] [[Spain]] after it was forced to make a sudden avoidance manoeuvre to prevent a mid-air collision. All 16 passengers and crew were killed in the crash.<ref>{{Cite web |last=Ranter |first=Harro |title=ASN Aircraft accident de Havilland DH-114 Heron 2D EC-ANJ Barcelona Airport (BCN) |url=https://aviation-safety.net/database/record.php?id=19580414-0 |access-date=2022-06-03 |website=aviation-safety.net}}</ref>
* On 14 October 1960, [[Itavia]] I-AOMU crashed on [[Mount Capanne]], [[Italy]] killing all 11 on board. Bad weather may have played a role in the accident.<ref>{{Cite web |last=Ranter |first=Harro |title=ASN Aircraft accident de Havilland DH-114 Heron 2 I-AOMU Mt Capanne |url=https://aviation-safety.net/database/record.php?id=19601014-0 |access-date=2022-06-03 |website=aviation-safety.net}}</ref>
* On 17 August 1963, [[Fujita Airlines]] JA6159 crashed just after takeoff into Mount Hachijō-Fuji, [[Hachijōjima]], [[Japan]]; the accident killed all 19 passengers and crew in the worst disaster suffered by the de Havilland Heron.<ref>{{ASN|HAC}}</ref>
* On 27 January 1968, [[Air Comoros]] F-OCED flight hit the runway at [[Moroni, Comoros|Moroni]], [[Comoros]] and overran the runway then crashed into the sea. 15 passengers and crew died but one person survived the accident.<ref>{{Cite web |last=Ranter |first=Harro |title=ASN Aircraft accident de Havilland DH-114 Heron 1B F-OCED Moroni Airport (HAH) |url=https://aviation-safety.net/database/record.php?id=19680127-2 |access-date=2022-06-03 |website=aviation-safety.net}}</ref>
* On 5 March 1969, [[Prinair Flight 277]] from [[Charlotte-Amalie, United States Virgin Islands]] to [[San Juan, Puerto Rico]] crashed into a mountain in the [[Fajardo, Puerto Rico]] area, killing all 19 on board.<ref>{{Cite web|url=http://aviation-safety.net/database/record.php?id=19690305-0|title=ASN Aircraft accident de Havilland DH-114 Heron 2D N563PR San Juan}}</ref>
* On 26 May 1970, Aero Servicios HR-ASN stalled in turbulent conditions on approach to [[Toncontín International Airport]], killing all six people on board.<ref>{{Cite web |last=Ranter |first=Harro |title=ASN Aircraft accident de Havilland DH-114 Heron 1B HR-ASN Tegucigalpa-Toncontin Airport (TGU) |url=https://aviation-safety.net/database/record.php?id=19700526-1 |access-date=2022-06-03 |website=aviation-safety.net}}</ref>
* On 24 June 1972, [[Prinair Flight 191]] crashed near [[Ponce, Puerto Rico|Ponce]], [[Puerto Rico]] while trying to land, killing five people out of 20 passengers and crew. The cause was pilot error.<ref>{{Cite web |last=Ranter |first=Harro |title=ASN Aircraft accident de Havilland DH-114 Prinair Heron 2B N554PR Ponce-Mercedita Airport (PSE) |url=https://aviation-safety.net/database/record.php?id=19720624-0 |access-date=2022-06-03 |website=aviation-safety.net}}</ref>
* On 23 October 1975, VH-CLS performing Connair Flight CK1263 crashed in a cane field at Holloways Beach after a missed approach to [[Cairns Airport]], [[Queensland]], [[Australia]] during a storm. The three crew and eight passengers were all killed.<ref>{{Cite web |last=Ranter |first=Harro |title=ASN Aircraft accident de Havilland DH-114 Riley Heron 2E/A1 VH-CLS Cairns Airport, QLD (CNS) |url=https://aviation-safety.net/database/record.php?id=19751023-0 |access-date=2022-06-03 |website=aviation-safety.net}}</ref>
* On 24 July 1979 PrinAir crashed on takeoff from Saint Croix-Alexander Hamilton Airport (STX) killing 8 of the 21 onboard including both pilots. The crash was attributed to the aircraft being 1060 pounds over max takeoff weight and significantly out of the rear CG limit. It was reported that the ground crew did not provide proper information to the crew for weight and balance purposes. It was also reported the aircraft was observed with the front nose bouncing up and down off the ground as the aircraft taxied for takeoff.<ref>{{Cite web |last=Ranter |first=Harro |title=ASN Aircraft accident de Havilland DH-114 Heron 2D N575PR Saint Croix-Alexander Hamilton Airport (STX) |url=https://aviation-safety.net/database/record.php?id=19790724-1 |access-date=2022-06-03 |website=aviation-safety.net}}</ref>
* On 27 December 1986, DQ-FEF operated by the Fijian airline [[Sunflower Airlines]] crashed short of runway 21 of [[Nadi International Airport]] after its right flaps jammed in flight. 11 of the 14 people on board were killed.<ref>{{cite web|url=https://aviation-safety.net/database/record.php?id=19861227-0|title=Aviation Safety Network|work=aviation-safety.net|access-date=7 November 2016}}</ref>

==Specifications (Heron 2D)==
[[File:Heron flight deck.jpg|thumb|De Havilland Heron instrument panel]]
{{Aircraft specs
|ref=De Havilland Aircraft since 1909 <ref name="Jackson dh p494">Jackson 1987, p. 494.</ref>
|prime units?=imp
<!--
        General characteristics
-->
|genhide=

|crew=Two
|capacity=14 passengers
|length m=
|length ft=48
|length in=6
|span m=
|span ft=71
|span in=6
|height m=
|height ft=15
|height in=7
|wing area sqm=
|wing area sqft=499
|empty weight kg=
|empty weight lb=8150
|max takeoff weight lb=13500
|gross weight lb=
|fuel capacity={{convert|412|impgal|USgal L|abbr=on}}<ref name="jawa58p68">Bridgman 1958, p. 68.</ref>
<!--
        Powerplant
-->
|eng1 number=4
|eng1 name= [[de Havilland Gipsy Queen]] 30 Mk.2
|eng1 type= 6-cylinder inverted inline air-cooled piston engine
|eng1 kw=<!-- prop engines -->
|eng1 hp=250<!-- prop engines -->

|prop blade number=2<!-- propeller aircraft -->
|prop name=[[de Havilland Propellers|D.H.]] 2/1000/2 [[constant-speed propeller]]s
|prop dia m=<!-- propeller aircraft -->
|prop dia ft=7
|prop dia in=0<!-- propeller aircraft -->
|prop dia note=<ref name="jawa58p68"/>

<!--
        Performance
-->
|perfhide=

|max speed kmh=
|max speed mph=
|max speed kts=
|max speed mach=<!-- supersonic aircraft -->
|cruise speed kmh=<!-- if max speed unknown -->
|cruise speed mph=183
|cruise speed kts=
|range km=
|range miles=915
|range nmi=
|ceiling m=
|ceiling ft=18500
|climb rate ms=
|climb rate ftmin=1140
|more performance=* '''Takeoff distance to 50 ft (15 m):''' {{convert|2425|ft|m|abbr=on}}<ref name="jawa58p68"/>
* '''Landing distance from 50 ft (15 m):''' {{convert|2065|ft|m|abbr=on}}<ref name="jawa58p68"/>

|avionics=
}}

==See also==
{{Aircontent
|related=
*[[de Havilland Dove]]
|similar aircraft=
* [[Beechcraft Model 34]]
* [[Cessna 620]]
* [[Potez 840]]
* [[PZL MD-12]]
|lists=
|see also=
}}

==References==
{{Commons category}}

===Notes===
{{Reflist}}

===Bibliography===
* Bain, Gordon. ''De Havilland: A Pictorial Tribute''. London: AirLife, 1992. {{ISBN|1-85648-243-X}}.
* [[Leonard Bridgman|Bridgman, Leonard]]. ''Jane's All the World's Aircraft 1958–59''. London: Sampson Low, Marston & Company, Ltd., 1958.
* Green, William. ''Macdonald Aircraft Handbook''. London: Macdonald & Co. (Publishers) Ltd., 1964.
* Jackson, A.J. ''De Havilland Aircraft since 1909''. London: Putnam, Third edition, 1987.
*[[John W. R. Taylor|Taylor, John W. R.]] (editor). ''Jane's All The World's Aircraft 1965–66''. London: Sampson Low, Marston, 1965.
* "The Royal Moroccan Air Force...A Seasoned Air Arm". ''[[Air International]]'', November 1985, Vol. 29, No. 5. pp.&nbsp;226–232, 250–252. {{ISSN|0306-5634}}.
*Wixey, Ken. ''Heron at Fifty: De Havilland's Beautiful DH.114''. [[Air Enthusiast]] 87, May–June 2000, pp.&nbsp;72–77. {{ISSN|0143-5450}}

<!-- ==External links==-->
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{{Authority control}}

[[Category:De Havilland Heron| ]]
[[Category:1950s British airliners]]
[[Category:De Havilland aircraft|Heron]]
[[Category:Four-engined tractor aircraft]]
[[Category:Low-wing aircraft]]
[[Category:Aircraft first flown in 1950]]
[[Category:Four-engined piston aircraft]]
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