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Antonov - An-30, 1974
400 000 $
~362 154 €
~33 371 400 i
The Name of the seller:
ANDREJ
Location:
RUSSIA VORONEZH AIRPORT
Show phone
The Name of the seller:
ANDREJ
Location:
RUSSIA VORONEZH AIRPORT
Show phone

Antonov - An-30, 1974

400 000 $
~362 154 €
~33 371 400 i
Remember
Compare
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04 April 2022
1090

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)

Basic information:

Category: Turboprops
Manufacturer: Antonov
Model: An-30
Year: 1974
RAID (hours): 12345
Registration
number:
30024
Serial number: 30024
The Name of the seller:
ANDREJ
Location:
RUSSIA VORONEZH AIRPORT
Show phone