ARMSNET
Military Equipment Database
Initializing 0%

An-124 (Condor) Russian Heavy Transport Aircraft

Heavy Transport Aircraft
Spotted an error? Sign in to suggest an edit.
Basic Information
Name
An-124 (Condor) Russian Heavy Transport Aircraft
Designation
Alternate Designation
Equipment Type
Heavy Transport Aircraft
Manufacturer
Antonov (NKSA)
Date of Introduction
1986
Description

The An-124 Russian Heavy Transport Aircraft is an outsize freighter. The prototype first flew on 24 December 1982 and the first production aircraft was exhibited at the 1985 Paris Air Show. Entered service in January 1986. The service life extension program was begun by Aviastar on the first of 17 Antonov Airlines and Volga-Dnepr aircraft in 2000. First, RA-82078 of Volga-Dnepr, redelivered on 14 March 2000. Life extension of military An-124s began on 6 October 2004 when RA-82032 was delivered to the Aviastar plant. The An-124 (Condor) Russian Heavy Transport Aircraft World's largest production aircraft; upward-hinged visor-type nose and rear fuselage ramp/door for simultaneous front and rear loading/unloading; titanium floor throughout constant-section main hold, which is lightly pressurized, with a fully pressurized cabin for passengers above; landing gear for operation from unprepared fields, hard packed snow and ice-covered swampland; steerable nosewheels and mainwheels permit turns on 45 m (148 ft) wide runway.

Air & Air Defense Specifications
Crew 6
Engine Turbofan (229 hp)
Max Speed 865.0 km/h
Range 3698.0 km
Service Ceiling 12005 m
Variants
An-124-100 Commercial transport. Civil-operated An-124s are this standard. Maximum T-O weight restricted to 392,000 kg and maximum payload to 120,000 kg.
An-124-100M Upgrade developed by Antonov; includes main components of the An-124-100 program: payload increased from 120–150 t; take-off weight increased from 392–402 t; flight range with 120 t cargo increased from 4,750–5,300 km
An-124-100M-150 Antonov announced An-124 production would re-start in 2005 thanks to orders for 10 An-124-100M-150. Specifications as for An-124-100M, but enhanced western navigation aids comprising Jeppesen global database in Leninets A-820M computer and UKRNIIRA SRPPZ-2000 GPWS, allowing aircraft to conform to P-RNAV requirements.
System
Alternate Designation(s) An-124; NATO: Condor
Type Heavy Transport Aircraft
Manufacturer Antonov (NKSA)
Crew 6 ea
Maximum Cargo Capacity 150,000 kg
Dimensions
Length 69.10 m
Fuselage Width 7.28 m
Wing Span 73.30 m
Height 21.08 m
Wheelbase 22.90 m
Cabin Width 3.80 m
Cargo Hold Length 36.48 m [at floor, excl ramps]; 41.54 m [at floor, incl rear ramp]; 42.68 m [max]
Cargo Hold Width 6.40 m [at floor]; 6.63 m [max]; 4.26 m [at ceiling]
Cargo Hold Height 4.40 m
Cargo Hold Floor Area 2,650 m²
Cargo Hold Floor Volume 1,160 m³
Empty Operating Weight 181,000 kg
Maximum Takeoff Weight 402,000 kg
Maximum Landing Weight 330,000 kg
Automotive
Engine Name 4 x ZMKB Progress/Ivchenko D-18T
Engine Type Turbofan
Engine Power 229 kN each ; thrust reversers standard
Maximum Range 3,698 km [max payload]
Maximum Speed 865 km/h
Service Ceiling 12,005 m
Approach Speed 259 km/h
Protection
Stealth Properties None
Heat Signature Reduction No
EW Counter Measures No
Chaffs/Flares No
Details
Country of Origin Russia
Category Fixed Wing Aircraft
Air > Fixed Wing Aircraft
Filter Label
A
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
69.1 m
Width
Height
21.08 m
Weight
402000 kg
Operators (5)
Russia
United Kingdom
Ukraine
Libya
United Arab Emirates
Something went wrong. Please reload the page. Reload