Description of the engines:
2 AI-24VT IN AIRWORTHINESS
1 RU19-Ф300 IN AIRWORTHINESS
PROPELLER AV-72
General characteristics
Crew: 7
Length: 24.26 m (79 ft 7 in)
Wingspan: 29.20 m (95 ft 10 in)
Height: 8.32 m (27 ft 4 in)
Wing area: 74.98 m2 (807.1 sq ft)
Aspect ratio: 11.4:1
Airfoil: root: TsAGI S-5-18; tip: TsAGI S-3-13[26]
Empty weight: 15,590 kg (34,370 lb)
Max takeoff weight: 23,000 kg (50,706 lb)
Fuel capacity: 6,200 L (1,600 US gal; 1,400 imp gal)
Powerplant: 2 × Ivchenko AI-24TVT turboprop engines, 2,090 kW (2,803 shp) each equivalent
Propellers: 4-bladed constant-speed propellers
Performance
Maximum speed: 540 km/h (340 mph, 290 kn)
Cruise speed: 430 km/h (270 mph, 230 kn)
Range: 2,630 km (1,630 mi, 1,420 nmi) (with no reserves)
Service ceiling: 8,300 m (27,200 ft)
Take-off run: 710 m (2,329 ft)
Landing run: 670 m (2,198 ft)
Avionics:
standard
Avionics
Five positions for large cameras. Other survey equipment can be fitted.
General characteristics
Crew: 7
Length: 24.26 m (79 ft 7 in)
Wingspan: 29.20 m (95 ft 10 in)
Height: 8.32 m (27 ft 4 in)
Wing area: 74.98 m2 (807.1 sq ft)
Aspect ratio: 11.4:1
Airfoil: root: TsAGI S-5-18; tip: TsAGI S-3-13[26]
Empty weight: 15,590 kg (34,370 lb)
Max takeoff weight: 23,000 kg (50,706 lb)
Fuel capacity: 6,200 L (1,600 US gal; 1,400 imp gal)
Powerplant: 2 × Ivchenko AI-24TVT turboprop engines, 2,090 kW (2,803 shp) each equivalent
Propellers: 4-bladed constant-speed propellers
Performance
Maximum speed: 540 km/h (340 mph, 290 kn)
Cruise speed: 430 km/h (270 mph, 230 kn)
Range: 2,630 km (1,630 mi, 1,420 nmi) (with no reserves)
Service ceiling: 8,300 m (27,200 ft)
Take-off run: 710 m (2,329 ft)
Landing run: 670 m (2,198 ft)
Equipment:
standard
Five positions for large cameras. Other survey equipment can be fitted.
General characteristics
Crew: 7
Length: 24.26 m (79 ft 7 in)
Wingspan: 29.20 m (95 ft 10 in)
Height: 8.32 m (27 ft 4 in)
Wing area: 74.98 m2 (807.1 sq ft)
Aspect ratio: 11.4:1
Airfoil: root: TsAGI S-5-18; tip: TsAGI S-3-13[26]
Empty weight: 15,590 kg (34,370 lb)
Max takeoff weight: 23,000 kg (50,706 lb)
Fuel capacity: 6,200 L (1,600 US gal; 1,400 imp gal)
Powerplant: 2 × Ivchenko AI-24TVT turboprop engines, 2,090 kW (2,803 shp) each equivalent
Propellers: 4-bladed constant-speed propellers
Performance
Maximum speed: 540 km/h (340 mph, 290 kn)
Cruise speed: 430 km/h (270 mph, 230 kn)
Range: 2,630 km (1,630 mi, 1,420 nmi) (with no reserves)
Service ceiling: 8,300 m (27,200 ft)
Take-off run: 710 m (2,329 ft)
Landing run: 670 m (2,198 ft)
Exterior:
2007 year
General characteristics
Crew: 7
Length: 24.26 m (79 ft 7 in)
Wingspan: 29.20 m (95 ft 10 in)
Height: 8.32 m (27 ft 4 in)
Wing area: 74.98 m2 (807.1 sq ft)
Aspect ratio: 11.4:1
Airfoil: root: TsAGI S-5-18; tip: TsAGI S-3-13[26]
Empty weight: 15,590 kg (34,370 lb)
Max takeoff weight: 23,000 kg (50,706 lb)
Fuel capacity: 6,200 L (1,600 US gal; 1,400 imp gal)
Powerplant: 2 × Ivchenko AI-24TVT turboprop engines, 2,090 kW (2,803 shp) each equivalent
Propellers: 4-bladed constant-speed propellers
Performance
Maximum speed: 540 km/h (340 mph, 290 kn)
Cruise speed: 430 km/h (270 mph, 230 kn)
Range: 2,630 km (1,630 mi, 1,420 nmi) (with no reserves)
Service ceiling: 8,300 m (27,200 ft)
Take-off run: 710 m (2,329 ft)
Landing run: 670 m (2,198 ft)
Interior:
2007 year
General characteristics
Crew: 7
Length: 24.26 m (79 ft 7 in)
Wingspan: 29.20 m (95 ft 10 in)
Height: 8.32 m (27 ft 4 in)
Wing area: 74.98 m2 (807.1 sq ft)
Aspect ratio: 11.4:1
Airfoil: root: TsAGI S-5-18; tip: TsAGI S-3-13[26]
Empty weight: 15,590 kg (34,370 lb)
Max takeoff weight: 23,000 kg (50,706 lb)
Fuel capacity: 6,200 L (1,600 US gal; 1,400 imp gal)
Powerplant: 2 × Ivchenko AI-24TVT turboprop engines, 2,090 kW (2,803 shp) each equivalent
Propellers: 4-bladed constant-speed propellers
Performance
Maximum speed: 540 km/h (340 mph, 290 kn)
Cruise speed: 430 km/h (270 mph, 230 kn)
Range: 2,630 km (1,630 mi, 1,420 nmi) (with no reserves)
Service ceiling: 8,300 m (27,200 ft)
Take-off run: 710 m (2,329 ft)
Landing run: 670 m (2,198 ft)
Modifications/changes:
AN-30
General characteristics
Crew: 7
Length: 24.26 m (79 ft 7 in)
Wingspan: 29.20 m (95 ft 10 in)
Height: 8.32 m (27 ft 4 in)
Wing area: 74.98 m2 (807.1 sq ft)
Aspect ratio: 11.4:1
Airfoil: root: TsAGI S-5-18; tip: TsAGI S-3-13[26]
Empty weight: 15,590 kg (34,370 lb)
Max takeoff weight: 23,000 kg (50,706 lb)
Fuel capacity: 6,200 L (1,600 US gal; 1,400 imp gal)
Powerplant: 2 × Ivchenko AI-24TVT turboprop engines, 2,090 kW (2,803 shp) each equivalent
Propellers: 4-bladed constant-speed propellers
Performance
Maximum speed: 540 km/h (340 mph, 290 kn)
Cruise speed: 430 km/h (270 mph, 230 kn)
Range: 2,630 km (1,630 mi, 1,420 nmi) (with no reserves)
Service ceiling: 8,300 m (27,200 ft)
Take-off run: 710 m (2,329 ft)
Landing run: 670 m (2,198 ft)
Status of the inspection:'
IN AIRWORTHINESS 2021 year
General characteristics
Crew: 7
Length: 24.26 m (79 ft 7 in)
Wingspan: 29.20 m (95 ft 10 in)
Height: 8.32 m (27 ft 4 in)
Wing area: 74.98 m2 (807.1 sq ft)
Aspect ratio: 11.4:1
Airfoil: root: TsAGI S-5-18; tip: TsAGI S-3-13[26]
Empty weight: 15,590 kg (34,370 lb)
Max takeoff weight: 23,000 kg (50,706 lb)
Fuel capacity: 6,200 L (1,600 US gal; 1,400 imp gal)
Powerplant: 2 × Ivchenko AI-24TVT turboprop engines, 2,090 kW (2,803 shp) each equivalent
Propellers: 4-bladed constant-speed propellers
Performance
Maximum speed: 540 km/h (340 mph, 290 kn)
Cruise speed: 430 km/h (270 mph, 230 kn)
Range: 2,630 km (1,630 mi, 1,420 nmi) (with no reserves)
Service ceiling: 8,300 m (27,200 ft)
Take-off run: 710 m (2,329 ft)
Landing run: 670 m (2,198 ft)
Other comments:
General characteristics
Crew: 7
Length: 24.26 m (79 ft 7 in)
Wingspan: 29.20 m (95 ft 10 in)
Height: 8.32 m (27 ft 4 in)
Wing area: 74.98 m2 (807.1 sq ft)
Aspect ratio: 11.4:1
Airfoil: root: TsAGI S-5-18; tip: TsAGI S-3-13[26]
Empty weight: 15,590 kg (34,370 lb)
Max takeoff weight: 23,000 kg (50,706 lb)
Fuel capacity: 6,200 L (1,600 US gal; 1,400 imp gal)
Powerplant: 2 × Ivchenko AI-24TVT turboprop engines, 2,090 kW (2,803 shp) each equivalent
Propellers: 4-bladed constant-speed propellers
Performance
Maximum speed: 540 km/h (340 mph, 290 kn)
Cruise speed: 430 km/h (270 mph, 230 kn)
Range: 2,630 km (1,630 mi, 1,420 nmi) (with no reserves)
Service ceiling: 8,300 m (27,200 ft)
Take-off run: 710 m (2,329 ft)
Landing run: 670 m (2,198 ft)
