GlobalMilitary.net Open-source military intelligence Updated daily

An-71 Madcap

Soviet tactical airborne early warning and control aircraft, developed in the 1980s for overland support of tactical air operations.

Origin country
🇷🇺 Ex-USSR
First flight
1985Jul 12
Produced
3units
Antonov An-71 Madcap military special mission aircraft side profile drawing
Side profile · Antonov An-71 Madcap · length 23.5 m
Technical SpecificationsVersion: An-71
Crew6
Length23.5 m (77.1 ft)
Wingspan31.9 m (104.6 ft)
Height9.2 m (30.2 ft)
Empty weight19,760 kg (43,563 lbs)
Max. takeoff weight32,100 kg (70,768 lbs)
Powerplant2 × turbofans Progress D-436K 7,505 kgf each
PerformanceVersion: An-71
Maximum speed650 km/h (404 mph)
Service ceiling10,800 m (35,433 ft)
Operators — 2026
No country is operating the An-71 Madcap in 2026.
Compare This Aircraft
An-71 Madcap vs
All Operators
🇷🇺 Ex-USSR

Description

The Antonov An-71 (NATO reporting name: Madcap) is a Soviet airborne early warning and control (AWACS) aircraft developed from the An-72 transport for the VVS-FA (Frontal Aviation) forces of the Soviet Air Force. Intended to direct tactical air operations overland, the aircraft never entered operational service, and development was terminated after three prototypes were produced. The type is known for its configuration featuring a radar rotodome mounted on top of a broad-chord, forward-swept vertical stabilizer.

Development

The An-71 program was initiated to provide tactical AWACS support specifically for Soviet Frontal Aviation, distinguishing its operational role from the strategic interceptor-support roles of the Tu-126 and A-50. The first prototype completed its maiden flight on 12 July 1985. Development was halted at the prototype stage with three aircraft built, and the program was formally cancelled following the fall of the Soviet Union due to unresolved technical issues with the radar system. In 2010, one surviving prototype was transferred to the Ukraine State Aviation Museum for display.

Design

The aircraft's design modifies the baseline An-72 transport airframe with a redesigned rear fuselage and a forward-swept, broad-chord tail fin supporting the radar rotodome. The interior cargo bay was converted to house internal electronic systems and six operator stations. Power is provided by two Progress D-436K turbofan engines, yielding a cruise speed of 530 km/h, a maximum speed of 650 km/h, and a service ceiling of 10,800 m. The primary sensor is the Vega-M Kvant search radar, which was designed to track up to 400 targets simultaneously at ranges up to 370 km.

Operational History

Due to the cancellation of the project, the An-71 accumulated no operational record or military deployments. In the early 2000s, Ukraine conducted unsuccessful export negotiations to sell an An-71 to India for US$200 million.

Variants

  • An-75: A proposed naval variant modified for aircraft carrier operations featuring underwing-mounted engines and structural redesigns, which was cancelled by Soviet Naval Aviation prior to construction.

Frequently Asked Questions

What type of aircraft is the An-71 Madcap?
The Antonov An-71 Madcap is a military special mission aircraft aircraft developed by Antonov.
What is the maximum speed of the An-71 Madcap?
The Antonov An-71 Madcap has a maximum speed of 650 km/h (403 mph).
When did the An-71 Madcap first fly?
The Antonov An-71 Madcap made its first flight on July 12, 1985.
How many An-71 Madcap have been built?
3 units of the Antonov An-71 Madcap have been produced.
What is the service ceiling of the An-71 Madcap?
The Antonov An-71 Madcap has a service ceiling of 10,800 meters (35,433 feet). This is the maximum altitude at which the aircraft can maintain controlled flight.
Wikipedia (CC BY-SA) and other open sources. Illustrations generated by AI. Last updated on 5 August 2026. Suggest a change