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General Dynamics / Grumman EF-111A Raven


The General Dynamics–Grumman EF-111A Raven is an electronic-warfare aircraft designed to replace the EB-66 Destroyer in the United States Air Force.

Its crews and maintainers often called it the “Spark-Vark”, a play on the F-111’s “Aardvark” nickname.

The USAF contracted with Grumman in 1974 to convert some existing General Dynamics F-111As into electronic warfare/electronic countermeasures (ECM) aircraft.

The USAF had considered the Navy / Marine Corps Grumman EA-6B Prowler but desired a penetrating aircraft with supersonic speed.

The EF-111 entered service in 1983 and served until its retirement in 1998.

In the late 1960s, the U.S. Air Force sought to replace its aging EB-66 and EB-57 electronic warfare aircraft.

The Air Force studied the use of Navy EA-6B Prowlers during 1967–1968.

However, the Air Force desired a penetrating electronic jamming aircraft with supersonic speed, and, in 1972, decided to modify F-111As into electronic warfare aircraft as a cost-effective option.

In January 1974, the Air Force awarded electronic warfare study contracts to Grumman and General Dynamics.

Grumman was selected as the EF-111 prime contractor in December 1974, then was awarded a contract to modify two F-111As into EF-111 prototypes in January 1975.

The first fully equipped model, known then as the “Electric Fox”, flew on 10 March 1977.

A total of 42 airframes were converted at a total cost of US$1.5 billion.

The first EF-111s were deployed in November 1981 to the 388th Tactical Electronic Squadron, Mountain Home AFB, Idaho.

The last was delivered in 1985.

The Raven retained the F-111A’s navigation systems, with a revised AN/APQ-160 radar primarily for ground mapping.

The primary feature of the Raven, however, was the AN/ALQ-99E jamming system, developed from the Navy’s ALQ-99 on the Prowler.

The aircraft also utilized the ALR-62 Countermeasures Receiving System (CRS) as a Radar Homing and Warning (RHAW) System, the same system carried by all F-111 fighter/bomber models in the United States and Australia.

The ALQ-99E primary electronics were installed in the weapons bay, with transmitters fitted in a 16 feet (4.9 m) long ventral “canoe” radome; the complete installation weighed some 6,000 pounds (2,700 kg).

Receivers were installed in a fin-tip pod, or “football”, similar to that of the EA-6B.

The aircraft’s electrical and cooling systems had to be extensively upgraded to support this equipment.

The cockpit was also rearranged, with all flight and navigation displays relocated to the pilot’s side, and flight controls except throttles being removed from the other seat, where the electronic warfare officer’s instrumentation and controls were installed.

The EF-111 was unarmed.

Its speed and acceleration were its main means of self-defence.

It was not capable of firing anti-radiation missiles in the Suppression of Enemy Air Defences (SEAD) role, which was a tactical limitation.

The Raven’s engines were upgraded to the more powerful TF30-P-9 of the D-model, with 12,000 pounds-force (53 kN) dry and 19,600 lbf (87 kN) afterburning thrust in 1986. 

From 1987 to 1994 the “Spark ‘Vark” underwent an Avionics Modernization Program (AMP), similar to the Pacer Strike program for the F-model.

This added a dual AN/ASN-41 ring laser gyroscope INS, AN/APN-218 Doppler radar, and an updated AN/APQ-146 terrain-following radar.

Cockpit displays were upgraded with multi-function displays.




68 ft 10 in (20.98 m)


15 ft 9 in (4.80 m)



NACA 64-210.68 


NACA 64-209.80 

Empty weight

46,100 lb (20,910 kg)

Gross weight

79,000 lb (35,800 kg)

Max take-off weight

88,000 lb (39,900 kg)



70 ft (21.3 m)


33 ft 11 in (10.34 m)

Wing area


655.5 ft2 (60.9 m2)


550 ft2 (51.1 m2)


2 × Pratt & Whitney TF30-P-3 turbofans,

10,750 lbf (47.8 kN) thrust each dry,

18,500 lbf (82 kN) with afterburner


Maximum speed

1,450 mph (2,330 km/h, 1,260 kn)

Maximum speed

Mach 2.2


2,100 mi (3,390 km, 1,830 nmi); with 6 AIM-54 missiles and 23,000 lb fuel internal

Ferry range

3,200 mi (5,150 km, 2,780 nmi); with 2 x 450 gal external tanks

Service ceiling

65,000 ft (19,800 m)

Rate of climb

21,300 ft/min (108 m/s)



Wing loading


120 lb/ft2 (586 kg/m2)


144 lb/ft2 (703 kg/m2)



1× M61 Vulcan 20 mm (0.787 in) Gatling cannon (seldom fitted)


6 underwing pylons for ordnance and external fuel tanks


6 x AIM-54 Phoenix long range air-air missiles (four under wings, two in weapons bay)


AN/AWG-9 Pulse-Doppler radar








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