13 July 1968

General Dynamics FB-111A 67-0159, the first production aircraft. (U.S. Air Force)

13 July 1968: The first production General Dynamics FB-111A supersonic strategic bomber successfully completed a 30-minute maiden flight at Carswell Air Force Base, Fort Worth, Texas. The FB-111A differed from the F-111A fighter bomber with the substitution of a larger wing, originally designed for the F-111B, giving the bomber a 7 foot (2.134 meter) increase in wingspan. The landing gear was strengthened, the bomb bay enlarged, and it had more powerful engines.

Aardvark (Orycteropus afer)

The airplane’s very long nose earned the nickname “Aardvark,” but this did not become official until 1996.

67-0159 was delivered to the U.S. Air Force 4 September 1968 and assigned to the Air Force Flight Test Center, Edwards Air Force Base, California. (The first six production airplanes were used for flight testing.)

67-0159 was later converted to the F-111G configuration. In 1980 it was sent to the Sacramento Air Logistics Center to test weapons modifications and received a spectacular white and orange paint scheme. It was retired in 1990. 67-0159 is in the collection of the National Museum of the United States Air Force. It is on loan and now on display at the Aerospace Museum of California, Sacramento, California.

General Dynamics FB-111A-CF (F-111G) 67-159

The General Dynamics FB-111A is a two-place, twin-engine, strategic bomber with variable-sweep wings, assigned to the Strategic Air Command. It is 73.54 feet (22.415 meters) long. The wingspan varies from a maximum 70.0 feet (21.336 meters) when fully extended, and a minimum 33.96 feet (10.351 meters) when swept fully aft. Overall height is 17.04 feet (5.194 meters).

The wings of the FB-111A have a total area of 550 square feet (51.10 square meters). When fully extended, the wings’ leading edges are swept aft to 16.0°. The angle of incidence at the root is +1° and -3° at the tip. There is 1.0° dihedral.

The Aardvark’s empty weight is 47,481 pounds (21,537 kilograms). Normal maximum takeoff weight is 116,115 pounds (52,669 kilograms), and the maximum overload takeoff weight is or 119,243 pounds (54,088 kilograms).

The aircraft is powered by two Pratt & Whitney TF30-P-107 engines. This is a two-spool axial-flow turbofan engine with afterburner. It has a 3-stage fan section, 13-stage compressor section (6 low- and 7 high-pressure stages) and 4-stage turbine (1 high- and 3 low-pressure stages). The -107 has a maximum continuous power rating of 10,800 pounds of thrust (48.041 kilonewtons) at 14,150 r.p.m., N2 (static thrust, at Sea Level), and a maximum power rating of 20,350 pounds (90.521 kilonewtons) at 14,550 r.p.m., N2 (45 minute limit) The T30-P-107 is 3 feet, 2.12 inches (0.968 meters) in diameter, 20 feet, 1.4 inches (6.132 meters) long,  and weighs 4,121 pounds (1,869 kilograms).

The FB-111A has an average cruise speed of 415–442 knots (478–509 miles per hour/769-819 kilometers per hour), depending on the mission profile. It’s maximum speed at 50,000 feet (15,240 meters) is 1,262 knots (1,452 miles per hour/2,337 kilometers per hour)—Mach 2.20. The bomber’s service ceiling varies from 50,390 feet to 56,380 feet (15,359–17,185 meters), again, depending on the mission profile. The maximum combat range is 4,920 nautical miles (5,662 statute miles/9,112 kilometers). The airplane can carry as many as six 600 gallon (2,271 liter) external tanks on underwing pylons. This gives the Aardvark a maximum ferry range of 4,313 nautical miles (4,963 statute miles/7,988 kilometers).

General Dynamics FB-111A 67-163, the fifth production airplane, loaded with four AGM-69 SRAM missiles. The dots on the missiles and airplane are for precise tracking from ground stations. (U.S. Air Force)

The FB-111A could carry weapons in an internal bomb bay or on underwing hardpoints. It could be armed with up to 37,500 pounds (17,010 kilograms) of conventional bombs; or six AGM-69A Short Range Attack Missiles (SRAM). The Aardvark could carry maximum of six nuclear weapons (B-43, B-57 or B-61).

General Dynamics YFB-111A 63-9783, the prototype strategic bomber variant. (U.S. Air Force)

In addition to a prototype (63-9783, which was converted from the last production F-111A) General Dynamics built 76 FB-111A strategic bombers. With the introduction of the Rockwell B-1B Lancer, the FB-111As remaining in service were converted to F-111G tactical fighter bombers. They were retired by 2003.

The Royal Australian Air Force bought 15 of the F-111Gs. By 2007, these had also been taken out of service.

Two General Dynamics FB-111As in formation, 1 December 1983. (MSGT Buster Kellum, U.S. Air Force)

© 2018, Bryan R. Swopes

Facebooktwitterredditpinterestlinkedinmailby feather

11 thoughts on “13 July 1968

  1. Nice article. Two edit suggestions though. The FB-111A/F-111G was retired in 1993 rather than 2003. Also, the Aardvark was officially named as such on its retirement in July 1996.

  2. I’m wondering why you didn’t mention the EF-111 Raven. You usually include the variants in your postings.

  3. Interesting, I was at McClellan when they performed depot maintenance on them, saw a bunch coming in and out.

  4. This question probably warrants its own article, but how can ordinance be mounted on variable-sweep wings? The wings must become fixed in one position, and if so, at what angle? Or can the mounts change their angle somehow?
    – Question from a recovering engineer

  5. I had wondered the same thing. After a little investigating…
    Minimum sweep 16 degrees
    Maximum sweep 72.5 degrees
    Each wing had provisions for 4 pylons
    The innermost pair could pivot with wing sweep to keep pylons parallel to the fuselage.
    The outer two were fixed in orientation for optimum alignment during 26 degrees of wing sweep. Based on what I read, it seems like the outermost station was never used on any version. The third station out from the fuselage was occasionally used by FB-111’s for an external fuel tank. If used, the sweep was limited to 26 degrees which corresponded to an initial cruise setting. Take-off was at 16 degrees sweep and shifted to 26 degrees once airborne. Therefore there was 10 degrees of skewed alignment during the take-off phase. Research suggests it was not common practice to fly with a fuel tank on the 3rd Station.

    I remember seeing an F-111 on static display at an air show at Andrews AFB summer 1968. I thought it was so cool. It still is.

  6. Well I went through a lot of material and after hitting ‘send’ I check out another source. I found a photograph of an F-111 with all 4 pylons loaded with bombs.
    https://scholar.afit.edu/cgi/viewcontent.cgi?article=1029&context=docs
    Obviously the sources I read were incorrect on the usage.
    I also forgot to mention that the two outboard pylons could be jettisoned to allow subsequent configuration to full sweep.
    Please pardon my error. Thanks.

Comments are closed.