The US Military has a strong fleet of fighter jets, many of which have been in service for decades. Simple Flying looks at the top 5 US fighter jets with the longest service life.

5

F/A-18 Hornet

Entered service in 1983

The Hornet completed its first flight in 1978, and five years later, in 1983, it entered operational service with the Marine Corps and, in 1984, with the U.S. Navy. Its entry into military service initiated the process of fleet replacement for the F-4 Phantom and the A-7 Corsair.

FA-18 Super Hornet taking off from an aircraft carrier.

Photo: U.S. Navy

The F/A-18 Hornet was designed to fulfill mission requirements for air-to-air and air-to-ground missions. Covering the tactical spectrum, the Hornet can perform such roles as air superiority, fighter escort, maritime strike, reconnaissance, forward air control, and more.

The F/A-18 Hornet is the primary workhorse of Marine Corps tactical aviation. It supports the Corps’ global missions. This aircraft is lighter and more maneuverable than the Super Hornet, which is oriented towards carrier operations.

Specifications for the F/A-18 Hornet

Technical Specifications

Numerical Data

Crew

1 or 2 depending on the variant

Length

60.7 ft

Width

44.9 ft

Height

16 ft

Empty Weight

22,928 lb.

Maximum Takeoff Weight

51,809 lb.

Maximum Speed

1,190 mph

Service Ceiling

50,033 ft

Operational Range

1,243 miles

Rate of Climb

50,000 ft/min

Onboard weapon systems

1 x 20mm M61 rotary cannon (six barrels)

Powerplant

2 x General Electric F404-GE-402 afterburning engines. Each unit produce’s 17,750 lb. of thrust.

4

F-16 Fighting Falcon

Entered service in 1978

The F-16 Fighting Falcon’s story begins in the 1970s with a small group of engineers and defense analysts known as “The lightweight mafia.” This motley crew sought to design an alternative to fighters of the time that had become increasingly heavy and had decreased maneuverability.

F-16 with red, white and blue paint flying over a desert.

Photo: U.S. Air Force

This team aimed to substitute excess weight and heavy payloads for greater speed and enhanced maneuverability. The desired end product was an affordable fighter that could easily outmaneuver enemy aircraft and strike with missiles or autocannon fire.

This combat aircraft has been so successful that, since entering production in 1975, more than 4,500 F-16s have been manufactured for 26 nations. With 300 potential future sales in the near future (with the Block 70/72 variant), Lockheed Martin still sees a bright future for this fighter jet.

Even Vietnam could be a future customer of the F-16, as it sees the deterrent value in this aircraft during heightened tensions in the South China Sea region.

Specifications for the F-16 Fighting Falcon

Technical Specifications

Numerical Data

Crew

1

Length

49.2 ft

Width

32.8 ft

Height

15.7 ft.

Empty Weight

18,960 lb.

Maximum Takeoff Weight

42,329 lb.

Maximum Speed

1,317mph

Cruise Speed

856 mph

Service Ceiling

50,000 ft

Operational Range

2,622 miles

Rate of Climb

50,000 ft/min

Onboard weapon systems

1 x 20mm M61A1 rotary cannon (six barrels)

Powerplant

1 x General Electric F110-GE-100 Afterburning engine. This unit produces 28,600 lb. of thrust.

3

A-10 Thunderbolt II

Entered service in 1977

It’s not fast, it’s not sleek, and it’s definitely not sexy…but it can eat tanks with great ease, and that was the primary reason for this monster’s birth.

During the Cold War, which lasted essentially from 1949 to 1991, there was a well-founded fear that a Soviet ground invasion would overrun Western Europe. The Soviets had a veritable sea of soldiers and tanks that they could throw into a potential invasion. US military planners needed an airpower component to peel back the Soviet armored formations and provide reliable close-air support.

A-10 flying against a grey cloudy background firing its rotary cannon.

Photo: U.S. Air Force

The answer was the A-10 Thunderbolt II, with planning beginning in the 1960s and the first delivery in 1975. The airframe was designed with pilot survivability as a top priority. Additionally, critical systems redundancy enabled the A-10 to continue operating even after taking significant damage. With its excellent maneuverability at low air speeds and altitude, it could and can loiter near a battlefield for extended periods of time, providing ground forces with tier-one support.

Aside from guided munitions, the A-10 could spew out up to 4,200 rounds per minute if it faced off against enemy tanks. Their PGU-14/B Incendiary rounds with a depleted uranium core could turn a perfectly good tank into a smoldering hulk in seconds.

The future of the A-10 is still up in the air (no pun intended), and this is a contentious topic for many aviators and aviation enthusiasts.

Specifications for the A-10 Thunderbolt II

Technical Specifications

Numerical Data

Crew

1

Length

53.3 ft

Width

57.7 ft

Height

14.7 ft

Empty Weight

27,999 lb.

Maximum Takeoff Weight

51,998 lb.

Maximum Speed

439 mph

Service Ceiling

34,695 ft

Operational Range

474 miles

Rate of Climb

6,000 ft/min

Onboard weapon systems

1 x 30mm, General Electric, GAU-8/A rotary cannon (seven barrels)

Powerplant

2 x General Electric TF34-GE-100 non-afterburning turbofan engines. These units produce 9,065 lb. of trust each.

2

F-15 Eagle

Entered service in 1976

The F-15 Eagle is an all-weather, highly maneuverable tactical fighter designed to smash into enemy airspace and gain and maintain air supremacy over a battlefield. The story of the F-15 began in the 1960s due to the F-4 Phantom’s poor close air combat performance.

F-15 flying soaring above the clouds.

Photo: U.S.Air Force

McDonnell Douglas

was selected to design and produce this future aircraft, and on June 26, 1972, the first F-15 prototype rolled out of their factory. The first flight of the F-15A was made in July 1972, and by November 1974, the first F-15 was delivered to the 58th Tactical Fighter Training Wing located at Luke Air Force Base in Arizona. At this location, training began with both the F-15A and B variants.

This rugged aircraft continues to serve, and the program’s future lies with the

F-15EX

. This latest iteration has numerous improvements, and the Air Force is keen to purchase as many as 200 of them.

Specifications for the F-15 Eagle

Technical Specifications

Numerical Data

Crew

2 (Pilot & Weapon systems officer)

Length

63.8 ft

Width

42.8 ft

Height

18.5 ft

Empty Weight

27,000 lb.

Maximum Takeoff Weight

56,000 lb.

Maximum Speed

1,875mph

Service Ceiling

65,010 ft

Operational Range

2,402 miles

Rate of Climb

50,000 ft/min

Onboard weapon systems

1 x 20mm M6A1 rotary cannon (six barrels)

Powerplant

2 x Pratt & Whitney F100-PW-100 afterburning turbofan engines. These units produce 25,000 lb. of thrust each

1

F-5 Tiger

Entered service in 1964

The development of the F-5 Tiger began in 1954 when a team from Northrop Grumman toured Europe and Asia to assess the defense needs of NATO and SEATO countries.

As a result of this tour, the team initiated a design study for a lightweight, supersonic jet fighter that would be affordable, easy to maintain, and capable of operating from short runways. By 1956, the US Air Force did not show interest in operating it in large numbers, but it did maintain small numbers of its trainer version, the T-38 Talon.

F-5 Tiger flying with a mountain range in the background.

On April 25, 1962, the Department of Defense announced that it would offer the F-5 for export within the Military Assistance Program. In total, more than 2,600 were built by Northrop Grumman, including those under co-production and licensing agreements with Canada, Taiwan, South Korea, Spain, and Switzerland.

According to Northrop Grumman:

“From the F-5’s first delivery in 1964…every aircraft was delivered on schedule, at or below the contract price, and with performance as promised. Approximately two-thirds of the original production F-5’s remain operational in 26 countries, including the United States.”

Presently, the US Navy operates the F-5 in its adversary squadrons, which simulate enemy aircraft during training missions. The Air Force uses these aircraft for a similar training role.

Specifications for the F-5 Tiger

Technical Specifications

Numerical Data

Crew

1

Length

47.4 ft

Width

26.7 ft

Height

13.3 ft

Empty Weight

9,722 lb.

Maximum Takeoff Weight

24,723 lb.

Maximum Speed

1,077 mph

Service Ceiling

51,804 ft

Operational Range

1,543 miles

Rate of Climb

28,700 ft/min

Onboard weapon systems

2 x 20mm M39A2 automatic cannons

Powerplant

2 x General Electric J85-GE21 afterburning turbojet engines. These units produce 5,000 lb. of thrust each.

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