title: IPTN N-250
text: # IPTN N-250
  
  The IPTN N-250 was a turboprop regional airliner designed by Indonesian firm IPTN (Industri Pesawat Terbang Nusantara) (now Indonesian Aerospace). This aircraft was IPTN's first major effort to win the market share of the regional turboprop class of 64–68 seat airliners. The aircraft's development was eventually terminated after the Asian financial crisis of 1998.
  
  As of 21 August 2020, the PA-1 prototype is on displayed at Dirgantara Mandala Museum, Yogyakarta, as its 60th collection.
  
  ## Design and development
  
  The N-250 development plan was first revealed by PT IPTN (now PT Dirgantara Indonesia, Indonesian Aerospace) at the Paris Air Show in 1989, but was first introduced in 1986 when the Indonesian Air Show 1986 was held. The N-250 was initially described as a propfan commuter plane, but on 12 July 1990, IPTN selected the Allison GMA 2100 turboprop to power the aircraft.
  
  In early 1994, Indonesia announced that Great Britain and four states in the United States were interested in hosting production lines for the final assembly of the N-250. In January 1995, IPTN added Long Island, New York and Macon, Georgia to the previous list of U.S. semifinalists that included Mobile, Alabama, Phoenix, Arizona, and Portland, Oregon, out of an original list of 26 contender cities. In the following month, IPTN selected Mobile and Macon as the final candidates. On May 19, 1995, Indonesia awarded the U.S. assembly of the N-250 to Mobile. The U.S. assembly site would be run by American Regional Aircraft Industry (AMRAI), in which IPTN would hold a 40-percent stake. Planned production was to be one plane per week from IPTN's home factory in Bandung, West Java and up to two planes per week from the Mobile factory. The flying aircraft was officially unveiled at the Indonesian Air Show '96, and it also performed at the 1997 Paris Air Show and the 1998 Asian Aerospace show.
  
  The first assembled prototype, which had a capacity of 50 passengers, was initially rolled out on 10 November 1994 in Bandung during the run-up to the 1994 Asia-Pacific Economic Cooperation (APEC) summit, which Indonesia was hosting. This prototype, which had a serial number of PA-1, then flew for the first time on 10 August 1995. It was successfully tested to a cruise speed of 727.8 kilometers per hour (452.2 mph; 393.0 kn) at 7,600 meters (25,000 ft) altitude, and 744.5 km/h (462.6 mph; 402.0 kn) at 5,200 m (17,000 ft) altitude. The second prototype was a stretched variant with a capacity of 64–68 passengers, and it was designated as the N250-100. The N250-100 was planned to have its first flight in May 1996, but the PA-2 prototype instead had its initial flight eight months behind schedule on 19 December 1996. The third and fourth prototypes were planned to first fly in July 1996 and September 1996 respectively.
  
  Construction for the additional prototypes was halted because of the effects of the Asian financial crisis. Although the IPTN was about halfway through its 1,400-hour flight test program, the International Monetary Fund (IMF) required the Indonesian government to end support of the N-250 program as part of the IMF's US$43 billion government bailout plan. Because of this event, IPTN postponed the aircraft's certification from March 1999 to the fourth quarter of 2000. Later, IPTN postponed certification indefinitely so that it could recruit a risk-sharing partner to help complete the program.
  
  ### After termination
  
  There has been some consideration concerning the program's revival by the former director of the IPTN and, later, the former Indonesian president B. J. Habibie after having received approval from the incumbent president Susilo Bambang Yudhoyono. However, to reduce production costs and improve price competitiveness in international markets, changes were made which have resulted in reduced performance such as a reduction in engine capacity, and the removal of the fly-by-wire system. The planned reborn plane was planned to be named N250R.
  
  In August 2012, both developing parties, Erry Firmansyah of PT Eagle Cap and PT Regio Aviasi Industri (RAI), led by both of Habibie's sons, agreed to finance N-250. It will use a new name, R-80.
  
  On 26 September 2013, Nam Air signed an order for 50 R-80 with an option for 50 more aircraft, to be delivered in 2018.
  
  On 22 February 2018, RAI signed a memorandum of understanding with Leonardo Aerostructures to help fund and complete the development of the R-80. The company hoped to build four hundred R-80 aircraft over 20 years. It completed a preliminary design and feasibility test of the 80-90 seat aircraft in 2016 and hoped to finish detail designing and prototype manufacturing by 2019. RAI planned to build six prototypes, with flight testing from 2020 to 2022, and targeted issuance of a type certificate from the European Aviation Safety Agency (EASA) in 2025. The price of the R-80 would be USD$25 million.
  
  B. J. Habibie's son, Ilham Akbar Habibie, advocated for the production of the aircraft as one of its competitors, the Fokker 50, was no longer produced by Fokker which went bankrupt in 1996. The remaining two competitors for the N-250 were the ATR 72 and Bombardier Dash 8.
  
  ## Variants
  
  ### N250
  
      The initial prototype with a capacity of 50 passengers. One produced (PA-1) and named "Gatotkaca"
  
  ### N250-100
  
      The second prototype is a stretched version, capable of carrying 68 passengers. One produced (PA-2) and named "Krincingwesi". First flight on 19 December 1996.
  
  ### N270
  
      Further stretched variant, 3 meters longer than N250-100 capable of carrying 72 passengers. Planned to be produced as the third prototype (PA-3) and will be named "Putut Guritno" or "Koco Negoro". Completion was planned for 18 months after N250-100's first flight and some integral parts like the fuselage, center wing and engines were already or almost completed, however development stalled after the Asian financial crisis of 1998. Also known as the N250-200.
  
  ### RAI R-80 RegioProp
  
      Rebuilding program of N-250 by B.J. Habibie under PT Regio Aviasi Industri. Planned for conducting its first flight between 2019 and 2020. When finished, it will be able to carry up to 92 passengers with a range of up to 800 nm (1.481 km). LoIs have been signed by NAM Air for ordering 100 planes consisting of 50 firm orders and 50 optional orders, and Kalstar Aviation for 25 planes. Other airlines that have expressed their interest including Wings Air, Citilink, Sky Aviation and Merpati Nusantara Airlines.
  
  ## Specifications (N250-100)
  
  Data from Jane's all the World's Aircraft 2000–01
  
  General characteristics
  
  * Crew: 2
  * Capacity: 64-68 passengers (PA-2) / 6,200 kg (13,669 lb) payload
  
               N250-50 50 passengers (PA-1) / 6,000 kg (13,228 lb) payload
  * Length: 28.15 m (92 ft 4 in)
  
               N250-50 26.3 m (86 ft)
  * Wingspan: 28 m (91 ft 10 in)
  * Height: 8.79 m (28 ft 10 in)
  * Wing area: 65 $m^2$ (700 sq ft)
  * Aspect ratio: 12:1
  * Airfoil: root: NASA MS(1)-0317 (modified NASA MD2) ; tip: NASA MS(1)-0317 (modified NASA MD3)
  * Empty weight: 15,700 kg (34,613 lb) operating empty weight
  
               N250-50 13,665 kg (30,126 lb)
  * Max takeoff weight: 24,800 kg (54,675 lb)
  
               N250-50 22,000 kg (48,502 lb)
  * Fuel capacity: 4,200 kg (9,259 lb)
  * Powerplant: 2 × Allison AE2100C turboprop engines, 2,439 kW (3,271 hp) each
  * Propellers: 6-bladed Dowty Rotol R384/6123-FX8, 3.81 m (12 ft 6 in) diameter constant=speed fully feathering reversible propellers
  
  Performance
  
  * Cruise speed: 611 km/h (380 mph, 330 kn) maximum at 6,100 m (20,013 ft) N250-50
  * Economical cruise speed: 556 km/h (345 mph; 300 kn) at 6,100 m (20,013 ft) N250-50
  * Stall speed: 195 km/h (121 mph, 105 kn) EAS flaps up, power off
  
               167 km/h (104 mph; 90 kn) 20° flaps N250-50
  * Range: 1,270 km (790 mi, 690 nmi) N250-50 with maximum payload
  
               800–1,100 km (500–680 mi; 430–590 nmi) N250-50 with 50 pax
  * Service ceiling: 9,140 m (29,990 ft)
  
               N250-50 7,620 m (25,000 ft)
  * Rate of climb: 9.4 m/s (1,850 ft/min) N250-50
  * Max rate of climb on one engine: 2.633 m/s (9 ft/s) N250-50
  * Wing loading: 381.5 $kg/m^2$ (78.1 lb/sq ft)
  
               N250-50 338.5 $kg/m^2$ (69 lb/sq ft)
  * Power/mass: 0.1965 kW/kg (0.1195 hp/lb)
  
               N250-50 0.2218 kW/kg (0.1349 hp/lb)
  * Balanced field length: 1,220 m (4,003 ft) N250-50, S/L, +20°C
  