The Il-114-100 is a passenger aircraft for local airlines and is based on Il-114 aircraft.The aircraft is equipped with high-efficiency PW-127Нengines by Pratt & Whitney (Canada) with the capacity of 2 750 hp. Fuel consumption for a standard Il-114-100 aircraft is 500-550 kg per flight hour. The aircraftuses a modernized digital flight navigation complex, the TsPNK-114 Collins, jointly developed by NII AO Federal State Unitary Enterpriseand Rockwell Collins (USA), which complies with ICAO and Eurocontrol navigation requirements for aircraft of this class.
A modern passenger cabin ensures comfortable flight in any weather conditions.
For this aircraft, the system of operation on technical conditionand without capital repairs has been accepted, which ensures maintaining the required level of airworthiness.
Aircraft is operated by Uzbek AirlinesNational Air Line (Republic of Uzbekistan).
First flight took place on January 26, 1999. Test pilot was I.I. Gudkov.
Type Certificate No. ST178 Il-114-100 AR by IAC was granted in December 1999.
Maximum shaft power (МСА, H=0)2х2750kgf
Maximum takeoff weight23,5tons
Maximum flight altitude7 600m
Main technical characteristics
Dimensional characteristics Length, m 26,877 Height, m 9,324 Wingspan, m 30 Wing area, sq. m. 81,9 Fuselage midsection, m 2,86 Power plant parameters
Number x engine type 2 x turbo-propeller engine Engine
PW127H Maximum shaft power (МСА, H=0), kgf. 2 750 Propeller diameter, m 3,93 Compliance with ICAO standards Appendix 16, Chapter 3 Weight parameters
Maximum takeoff weight, tons 23,5 Maximum payload, tons 6,5 Fuel tank capacity, l 8 780 Aircraft performance Cruising speed, km/h up to 500 Flight altitude, m up to 7 600 Flying range with maximum number of passengers, km 1 500 Flying range with maximum fuel reserve, km 4 730 Takeoff distance, m 750 Landing distance, m 550 Number of seats
Crew, persons 2 Passengers, persons 64 Specified life
Calendar operating life, years 30 Number of flights 12 000 Number of flight hours, hr. 18 000