Turbay T-3

{{Infobox Aircraft Begin

| name=T-3

| image=Turbay T-3 (LV-X24).jpg

| caption=Turbay T-3A

}}{{Infobox Aircraft Type

| type=seven-seater light transport

| national origin= Argentina

| manufacturer=Turbay S.A.

| designer=Alfredo Turbay

| first flight=8 December 1964

| introduced=

| retired=

| status=

| primary user=

| number built=1

| developed from=

| variants with their own articles=

}}

The Turbay T-3A was an Argentine twin-engined seven-seater light transport of the 1960s. A single example was built, but no production followed.

Development and design

In 1957, the Argentine aircraft designer Alfredo Turbay began work on a twin-engined STOL light transport, the Turbay T-3A, with Turbay S.A. formed at Buenos Aires in January 1961 to build the new design.{{cite book|last=Gunston|first=Bill|title=World Encyclopedia of Aircraft Manufacturers|year=2005|publisher=Sutton Publishing|location=Stroud, UK|isbn=0-7509-3981-8|edition=2nd|author-link=Bill Gunston |page=466}} The T-3A was a low-wing cantilever monoplane of all metal construction. It was powered by two {{convert|180|hp|kW|abbr=on|order=flip|lk=in}} Lycoming O-360-A1D air-cooled four-cylinder horizontally-opposed engines driving two-bladed propellers, and was fitted with a retractable nosewheel undercarriage.

Alfredo Turbay piloted the T-3A on its first flight on 8 December 1964. Production was planned of the T-3B, which was to be fitted with {{convert|250|-|350|hp|kW|order=flip|abbr=on}} Lycoming or Continental engines, giving improved performance.{{cite book|last=Taylor|first=John W. R.|title=Jane's All The World's Aircraft 1967–68|year=1967|publisher=Sampson Low, Marston & Company|location=London|author-link=John W. R. Taylor |page=5}} These plans did not come to fruition, with the prototype T-3B never completed, and no production occurring.{{cite web|title=Alfredo Turbay|url=http://www.aracuan.com.ar/turbay.htm|work=GRUPO ARACUAN|access-date=25 August 2012|language=es|url-status=dead|archive-url=https://web.archive.org/web/20150923172841/http://www.aracuan.com.ar/turbay.htm|archive-date=23 September 2015}}

Specifications

{{Aircraft specs

|ref=Jane's All The World's Aircraft 1966–67,{{cite book |title=Jane's All the World's Aircraft 1966-67 |editor1-last=Taylor |editor1-first=John W.R. |year=1966 |publisher=Sampson Low, Marston & Co. Ltd |location=London |edition=57th |pages=6–7}} Jane's All the World's Aircraft 1962-63{{cite book |title=Jane's All the World's Aircraft 1962-63 |editor1-last=Taylor |editor1-first=John W.R. |year=1962 |publisher=Sampson Low, Marston & Co |location=London |page=7}}

|prime units?=met

|genhide=

|crew=1

|capacity=6 passengers / {{cvt|522|kg|0}} max. payload / tanks for {{cvt|800|L|USgal impgal|0}} chemicals for spraying

|length m=9.40

|span m=13.52

|height m=3.60

|wing area sqm=24.08

|aspect ratio=7.5:1

|airfoil=NACA 23024 at root, NACA 4412 at tip

|empty weight kg=1034

|empty weight note=equipped

  • Max. zero-fuel weight: {{cvt|1725|kg|0}}

|max takeoff weight kg=1860

|max takeoff weight note=(MTOW and MLW)

|fuel capacity={{cvt|360|L|USgal impgal|0}} in four wing tanks, with provision for 2x {{cvt|80|L|USgal impgal|0}} external tanks ; {{cvt|24|L|USgal impgal|0}} oil

|eng1 number=2

|eng1 name=Lycoming O-360-A1D

|eng1 type=4-cylinder air-cooled horizontally-opposed piston engines

|eng1 kw=

|eng1 hp=180

|prop blade number=2

|prop name=Hartzell HC-92 zk-2b/8447-12A metal propellers

|prop dia m=

|prop dia note=

|max speed kmh=318

|cruise speed kmh=230

|cruise speed note=(econ. cruise)

::::{{cvt|255|km/h|mph kn|0}} maximum cruising speed

|never exceed speed kmh=342

|stall speed kmh=85.4

|range km=1380

|range note=with maximum payload, zero wind

::::{{cvt|1840|km|mi nmi|0}} with maximum fuel, zero wind

|ceiling m=7600

|ceiling note=

::::{{cvt|3500|m|0}} with one engine inoperative

|climb rate ms=

|climb rate ftmin=1300

|wing loading kg/m2=77

|wing loading note=

|power/mass={{cvt|0.0877|hp/lb|order=flip}}

|more performance=

  • Take-off run: {{cvt|118|m|0}}
  • Take-off distance to {{cvt|15.25|m|0}}: {{cvt|225|m|0}}
  • Landing run: {{cvt|100|m|0}}
  • Landing distance from {{cvt|15|m|0}}: {{cvt|180|m|0}}

|avionics=

  • Motorola VHF radio
  • ADF
  • Blind flying instrumantation

}}

See also

References

{{reflist}}