Harman Patil (Editor)

Sukhoi Su 80

Updated on
Edit
Like
Comment
Share on FacebookTweet on TwitterShare on LinkedInShare on Reddit
Top speed
  
470 km/h

Range
  
1,300 km

Cruise speed
  
430 km/h

First flight
  
September 4, 2001

Length
  
18 m

Wingspan
  
23 m

Engine type
  
Turboprop

Sukhoi Su-80 FileSukhoi Su80 at MAKS2007 airshowjpg Wikimedia Commons

The Sukhoi Su-80 (formerly known as the Sukhoi S-80) is a Russian twin-turboprop, twin-boom STOL transport aircraft.

Contents

Design and development

Sukhoi Su-80 FileSukhoi Su80 at MAKS2005 airshowjpg Wikimedia Commons

The Su-80 program was supposed to start in the late 1990s, but due to lack of funds, it was postponed for several years. A prototype of the combined Freight/Passenger Su-80GP was built and its first flight was planned for early 1998, but the program was delayed again. The first flight of the prototype was at the 2001 MAKS in Moscow issued Zhukovsky.

Sukhoi Su-80 httpsuploadwikimediaorgwikipediacommonsthu

On the fourth September 2001, Igor Wotinzew started with the prototype, 82911, on his first flight. In early 2006, the Su-80 in the KnAAPO in Komsomolsk-on-Amur went into production.

Sukhoi Su-80 SUKHOI Su80 SKYbrary Aviation Safety

The first model of the turboprop transporter Sukhoi S-80 was shown at the 46th Paris International Air and Space Show, 2005. The plane is being developed by Sukhoi OKB and the aircraft factory in Komsomolsk/Amur under the "konversija" program. The aircraft is intended to replace the An-24/26, An-28 and Yak-40, and to compete with the Antonov An-38 . The design of the machine is very similar to the Scaled Composites ATTT and the Rockwell OV-10. It has three lift-generating surfaces: the primary wings; two fins at the rear of the fuselage which join the booms to the fuselage; and the horizontal stabilizer which joins the two vertical fins at the rear of the booms. Two General Electric CT7-9B turboprop engines are housed in bays at the front of the tail booms.

Sukhoi Su-80 SUKHOI Su80 SKYbrary Aviation Safety

The sleek hull offers space for 30 passengers, and a "beaver-tail" cargo ramp is fitted at the rear of the fuselage, which allows for easy loading and unloading of cargo.

Operational history

Eight aircraft from the second production (first definitive) batch are earmarked for delivery to customers.

Commercial orders

Sukhoi Su-80 Sukhoi Su80 Updated for FSX

Blagoveshchensk Airlines, Chukotavia, Dalavia, the Petropavlovsk-Kamchatski Aviation Enterprise, and Polar Airlines have all signed preliminary agreements for the acquirement of the type. The KnAAPO factory airline is expected to be the Su-80s first operator.

Military orders

Sukhoi Su-80 Sukhoi Su80 Updated for FSX

The Kazakhstan Border Guards have tentatively ordered ten Su-80s, while the Chinese People's Liberation Army Air Force, Jordanian Air Force, Malaysian Air Force and Republic of Korea Air Force have all expressed interest.

Variants

The Su-80 exists in two distinct variants. The initial four pre-series aircraft featured a shorter fuselage, whereas the fifth, sixth, and seventh prototypes underwent a lengthening by 1.4 meters (4 feet 7 inches), accommodating an additional row of seats for passengers.


  • S-80PC (Su-80GP) – Combination Passenger and Freight carrier
  • S-80TC – light military troop transport
  • S-80A – Air Ambulance
  • S-80F – Fishery patrol
  • S-80PT – (patrol transport) for the Russian Border Guards, can be armed with machine guns, light auto-cannon, rockets, bombs, and surveillance devices.
  • S-80GE – Geological support
  • Su-80GP-100 – Transporter
  • Specifications (Su-80GP)

    Data from Sukhoi and KNAAPO

    General characteristics

  • Crew: 2
  • Capacity: 30 Passengers
  • Length: 18.26 m (59 ft 10 in)
  • Wingspan: 23.18 m (76 ft 4 in)
  • Height: 5.74 m (18 ft 8 in)
  • Wing area: 44.36 m² (477 ft)
  • Empty weight: 8,350 kg (18,408 Ib)
  • Useful load: 3,300 kg (2,730 kg)
  • Max. takeoff weight: 14,200 kg (31,305 Ib)
  • Powerplant: 2 × General Electric CT7-9B turboprop, 1,305 kW (1,750 hp) each
  • Performance

  • Never exceed speed: 575 km/h (358 mph, 311 knots)
  • Maximum speed: 470 km/h (292 mph, 254 knots)
  • Cruise speed: 430 km/h (267 mph, 232 knots)
  • Range: 1,300 km (700 nmi) with 30 passengers
  • Service ceiling: 8,000 m (25,000 ft)
  • Takeoff run: 830 m
  • landing: 530 m
  • Armament
    Wing and fuselage hardpoints for bombs, rockets, machine guns, and light autocannon.

    Avionics

  • SSI-80 aerial navigation and indication system
  • SBKV-P strapdown heading and altitude system
  • SVS-80 aerial signals system
  • ARK-M automatic radio compass
  • A-076 radio altitude-sensing and speed-measuring system
  • VIM-95C (VOR/ILS/SP/MRK) navigation and landing systems
  • VND-94S(DME) radio range-finder
  • SO-94R (UVD) radar responder
  • 4205 airborne national identification responder
  • RSBN-85C meteorological short-range navigation system
  • References

    Sukhoi Su-80 Wikipedia