Antonov An-148

Antonov

ICAOA148
Antonov An-148 aircraft
AntonovAntonov An-148
Photo: Зимин Василий · Public domain · Modified

About

A high-wing regional jet designed to work from rough and unpaved strips, with its engines mounted above the wing where debris cannot reach them. Production ended when the Ukrainian and Russian industries stopped co-operating. The weights, limits, crew, seating and engine rating are certificated figures for the An-148-100E from the Aviation Register of the Interstate Aviation Committee, type certificate data sheet № СТ264-Ан-148, issue 30: maximum ramp 43,850 kg, take-off 43,700 kg, landing 37,800 kg, zero fuel 34,420 kg, payload 9,000 kg, MMO 0.80, maximum operating altitude 12,200 m, two pilots, 83 seats, and two Ivchenko-Progress D-436-148 rated at 6,730 kgf (66.0 kN) for take-off. The fuel volume is the certificated 11,680 kg at 0.775 g/cm³, which agrees with the sheet's second pair, 12,200 kg at 0.81, to within 0.06%.

Weightscompared to Airbus A318

MRW (Maximum Ramp Weight)

43,850kg
0
25k
50k
68k

MTOW (Maximum Takeoff Weight)

43,700kg
0
25k
50k
68k

MLW (Maximum Landing Weight)

37,800kg
0
25k
50k
56k

MZFW (Maximum Zero Fuel Weight)

34,420kg
0
25k
53k

Capacitycompared to Airbus A318

Passenger Capacity

83passengers
0
100
132

63% of A318 maximum capacity

Crew

Total
2
Cockpit
2

Engine Specifications

Engine Count

2×

Engine Model

Ivchenko-Progress D-436-148

Thrust per Engine

66.0 kN(14837 lbf)

Fuel & Cargo

Fuel Capacity

15,070 L

Production & History

Production Status

Out of production

First Flight

December 17, 2004

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