Antonov An-148
Specifications
Sources: Antonov Design Bureau, United Aircraft Corporation, flightglobal.com, Aviant.

Antonov An-148

Section Title: Specifications
Table Section Text: Sources: Antonov Design Bureau, United Aircraft Corporation, flightglobal.com, Aviant.

Measurement	148-100A	148-100B	148-100E	158

Cockpit crew	2

Seating capacity	85 (1-class, dense) 75 (1-class, typical) 68 (2-class, typical)	99 (1-class, dense) 90 (1-class, typical) 86 (2-class, typical)

Seat pitch	30 in (1-class, dense) 32 in (1-class, typical) 35 & 32 in (2-class, typical)	30 in (1-class, dense) 32 in (1-class, typical) 34 & 31 in (2-class, typical)

Length	29.13 metres (95 ft 7 in)	30.83 metres (101 ft 2 in)

Wingspan	28.91 metres (94 ft 10 in)	28.56 metres (93 ft 8 in)

Wing area	87.32 square metres (939.9 sq ft)	–

Height	8.19 metres (26 ft 10 in)	8.20 metres (26 ft 11 in)

Cabin Width	3.15 metres (10 ft 4 in)

Cabin Height	2.00 metres (6 ft 7 in)

Maximum take-off weight	38,550 kilograms (84,990 lb)	41,950 kilograms (92,480 lb)	43,700 kilograms (96,300 lb)

Maximum payload	9,000 kilograms (20,000 lb)	5,000 kilograms (11,000 lb)

Cargo capacity	14.60 m3 (516 cu ft)	–

Takeoff run at MTOW	1,560 metres (5,120 ft)	1,800 metres (5,900 ft)	1,885 metres (6,184 ft)	1,900 metres (6,200 ft)

Dry Operating Weight(DOW)	16,800 kilograms (37,000 lb)	19,800 kilograms (43,700 lb)	22,000 kilograms (49,000 lb)	22,000 kilograms (49,000 lb)

Max Zero Fuel Weight	28,850 kilograms (63,600 lb)	31,850 kilograms (70,220 lb)	34,050 kilograms (75,070 lb)	34,050 kilograms (75,070 lb)

Max Landing Weight	30,000 kilograms (66,000 lb)	33,000 kilograms (73,000 lb)	36,050 kilograms (79,480 lb)	36,050 kilograms (79,480 lb)

Max Fuel Weight	12,050 kilograms (26,570 lb)

Normal/Econ Cruise Altitude	11,000 metres (36,000 ft)

Service ceiling	12,200 metres (40,000 ft)

Cruising speed	800 km/h to 870 km/h (497 mph to 541 mph)

Range fully loaded (with 75 pax for 148 variant)	2,100 kilometres (1,300 mi)	3,500 kilometres (2,200 mi)	4,400 kilometres (2,700 mi)	2,500 kilometres (1,600 mi)

Fuel consumption	1,550 kg/h (3,417 lb/h)	1,600 kg/h (3,527 lb/h)	1,650 kg/h (3,638 lb/h)	1,800 kg/h (3,968 lb/h)

Engine (x 2)	Progress D-436-148	D-436

Max. thrust (x 2)	6,400 Kgf 14,080 lbf (63.0 kN)	6,830 Kgf 15,026 lbf (67.0 kN)

Sentence(s)

Antonov An-148 initially used D-436-148 engines.

final_sentence: Antonov An-148 initially used D-436-148 engines.