# IAR 14 > Mediated Wiki article. Canonical URL: https://mediated.wiki/source/IAR_14 > Markdown URL: https://mediated.wiki/source/IAR_14.md > Source: https://en.wikipedia.org/wiki/IAR_14 > Source revision: 1339415513 > License: Creative Commons Attribution-ShareAlike 4.0 International (https://creativecommons.org/licenses/by-sa/4.0/) {{Short description|Romanian fighter and trainer aircraft}} {{Infobox aircraft |name = IAR 14 |image = IAR 14.png |caption = |type = Fighter-trainer aircraft |manufacturer = [Industria Aeronautică Română](/source/Industria_Aeronautic%C4%83_Rom%C3%A2n%C4%83) (IAR) |designer = |first_flight = June [1933](/source/1933_in_aviation) |introduction = |retired = |produced = 20 |number_built = |status = |unit cost = |primary_user = [Royal Romanian Air Force](/source/For%C5%A3ele_Aeriene_Regale_ale_Rom%C3%A2niei) |more_users = |developed_from = [IAR 12](/source/IAR_12) |variants = }} The '''IAR 14''' is a [Romania](/source/Romania)n low-wing monoplane fighter-trainer aircraft designed before [World War II](/source/World_War_II). ==Design and development== After rejection of [IAR 12](/source/IAR_12), Romanian officials did not want to discourage eventual national aircraft production. Therefore, in early 1933, an unofficial message was forwarded from top levels to Brasov, essentially indicating that a small number of fighter-trainers would be purchased by the air force. The I.A.R. team immediately began to work on a new type, designated I.A.R. 14, still based on the experience gained with previous designs The airplane was designed by [IAR](/source/Industria_Aeronautic%C4%83_Rom%C3%A2n%C4%83) design bureau in 1933 and was an evolution from the [IAR 12](/source/IAR_12) prototype. It was a cantilever low-winged monoplane with a spatted main undercarriage with V-form legs and a single, open cockpit over the wing. The rectangular section fuselage was of mixed metal-wood configuration, with the front half covered by duralumin sheets and the rear part with pine plywood. The tail had been modified once more and the control surfaces were balanced. The pilot's head rest was not fitted with the anti-crash pylon, typical to the precedent prototypes. The engine was mounted on welded steel bearers attached to a duralumin fireproof bulkhead. The wings were built around twin duralumin spars and pine and plywood ribs and had plywood leading edges. The centre section, let into the fuselage underside was duralumin covered, outer sections and ailerons fabric-covered. The fixed tail was built of pine and plywood-covered, the moving surfaces duralumin with fabric cover. The aircraft was equipped with the [IAR LD 450](/source/IAR_LD_450) powerplant, produced under license by IAR, that also equipped the [IAR 12](/source/IAR_12). The first flight took place in June 1933. In September 1933, an order for 20 aircraft was placed. ==Operators== ;{{flag|Romania}} *[Royal Romanian Air Force](/source/For%C5%A3ele_Aeriene_Regale_ale_Rom%C3%A2niei) ==Specifications (IAR 14)== frameless|right|upright=1.5 {{Aircraft specs |ref=''Jane's all the World's Aircraft 1938'' {{cite book |title=Jane's all the World's Aircraft 1938 |editor1-last=Grey |editor1-first=C.G. |year=1938 |publisher=Sampson Low, Marston & company, ltd |location=London |editor2-last=Bridgman|editor2-first=Leonard |page=230c}} |prime units?=met |crew=1 |length m=7.37 |length note= |span m=11.7 |span note= |height m=2.6 |height note= |wing area sqm=20.3 |wing area note= |aspect ratio= |airfoil= |empty weight kg=1255 |empty weight note= |gross weight kg=1552 |gross weight note= |max takeoff weight kg= |max takeoff weight note= |fuel capacity={{cvt|230|L|USgal impgal}} |more general= |eng1 number=1 |eng1 name=[IAR LD 450](/source/IAR_LD_450) |eng1 type=W-12 water-cooled piston engine |eng1 kw= |eng1 hp=450 |eng1 note=([Lorraine 12Eb](/source/Lorraine_12Eb)) |prop blade number=2 |prop name=[Ratier](/source/Ratier) wooden fixed-pitch propeller |prop dia m= |prop dia note= |max speed kmh=294 |max speed note=at sea level ::::{{cvt|265|km/h|mph kn}} at {{cvt|5000|m}} *'''Minimum speed:''' {{cvt|110|km/h|mph kn}} at sea level |cruise speed kmh= |cruise speed note= |stall speed kmh= |stall speed note= |never exceed speed kmh= |never exceed speed note= |minimum control speed kmh= |minimum control speed note= |range km= |range note= |combat range km= |combat range note= |ferry range km= |ferry range note= |endurance=2 hours 10 minutes |ceiling m=7900 |ceiling note= |g limits= |roll rate= |climb rate ms= |climb rate note= |time to altitude={{cvt|5000|m}} in 10 minutes 27 seconds |wing loading kg/m2=76.5 |wing loading note= |fuel consumption kg/km= |power/mass={{cvt|0.132|hp/lb|kW/kg|order=flip}} |more performance= |guns=2 x 7.7 mm Vickers machine-guns in the nose of the aircraft firing through airscrew. }} ==See also== {{aircontent| |related= *[IAR 12](/source/IAR_12) |similar aircraft= *[Boeing P-26](/source/Boeing_P-26) *[Dewoitine D.500](/source/Dewoitine_D.500) *[Avia BH-3](/source/Avia_BH-3) }} ==References== {{reflist}} ==Bibliography== *{{cite journal |last1=Cortet|first1=Pierre|title=Les chasseurs I.A.R: à la mode "Jockey" des années 30, mais en Roumanie (2)|journal=Le Fana de l'Aviation |date=June 1976 |issue=79 |pages=10–13 |issn=0757-4169 |language=fr|trans-title=The I.A.R Fighters: In the Jockey Style of the Thirties, but in Romania, Part 2}} {{IAR_Aircraft}} Category:1930s Romanian fighter aircraft 14 Category:Low-wing aircraft Category:Single-engined tractor aircraft Category:Aircraft first flown in 1933 Category:Aircraft with fixed conventional landing gear Category:Single-engined piston aircraft --- Adapted from the Wikipedia article [IAR 14](https://en.wikipedia.org/wiki/IAR_14) by Wikipedia contributors ([contributor history](https://en.wikipedia.org/wiki/IAR_14?action=history)). Available under [Creative Commons Attribution-ShareAlike 4.0 International](https://creativecommons.org/licenses/by-sa/4.0/). Changes may have been made.