Trainer aircraft.
T-7A Red Hawk Boeing – Technical Data, Specifications & Performance.
The Boeing T-7A Red Hawk is a next-generation, supersonic advanced jet trainer aircraft jointly developed by Boeing Defense, Space & Security (United States) and Saab AB (Sweden). Designed under the United States Air Force’s T-X program, the T-7A was selected to replace the aging Northrop T-38 Talon, and to serve as the primary fast-jet trainer for pilots transitioning to aircraft such as the F-22 Raptor and F-35 Lightning II. Featuring digital engineering, open-system architecture, and embedded simulation capabilities, the T-7A is engineered to support modern multi-domain training requirements.
Country users: United States
Description
The Boeing T-7A is classified as a supersonic advanced jet trainer, specifically designed to meet the U.S. Air Force’s requirements for a next-generation pilot training aircraft. With a tandem two-seat configuration, the T-7A is engineered to facilitate an advanced training curriculum, preparing student pilots for transition to frontline 4th- and 5th-generation fighters such as the F-15EX, F-22 Raptor, and F-35 Lightning II. The aircraft supports a wide range of mission profiles, including tactical formation flying, aerial refueling training, basic fighter maneuvers (BFM), air-to-air and air-to-ground weapon simulation, and advanced systems management under high-stress conditions.
The program is the product of a collaborative effort between Boeing Defense, Space & Security (United States) and Saab AB (Sweden). Saab was responsible for designing and manufacturing the aft fuselage and various structural components, leveraging its advanced aerostructures expertise. Boeing led the program’s systems integration, final assembly, and mission software development. One of the most revolutionary aspects of the T-7A program is its adoption of a model-based systems engineering (MBSE) and digital twin development process. This allowed engineers to simulate thousands of flight scenarios virtually, greatly reducing time between design and first flight, while enhancing production scalability.
The aircraft was originally developed under the USAF T-X program, which sought to replace the Northrop T-38 Talon, a jet trainer that had been in service since the early 1960s. In September 2018, the U.S. Air Force awarded Boeing a 9.2 billion USD contract to supply 351 T-7A aircraft, along with 46 ground-based training systems and associated support infrastructure. The T-7A was officially named the "Red Hawk" to honor the legacy of the Tuskegee Airmen, whose aircraft featured distinctive red tails during World War II.
Following its selection, the T-7A underwent a rigorous multi-phase test campaign. The aircraft completed its first flight on December 20, 2016, under the internal Boeing-Saab T-X designation. After being selected by the Air Force, it proceeded through Engineering and Manufacturing Development (EMD), where several EMD-configured prototypes underwent extensive flight testing at Boeing’s facilities in St. Louis, Missouri, and at Edwards Air Force Base, California.
During the Initial Flight Test and Evaluation (IFT&E) phase, starting in 2021, the T-7A demonstrated critical capabilities such as high angle-of-attack performance, rapid roll rates, and digital flight control responsiveness. These flight trials validated the performance of the General Electric F404-GE-103 engine and the digital fly-by-wire system, as well as aerodynamic performance at transonic and supersonic speeds.
A significant milestone was reached in September 2023, when the first production-representative T-7A Red Hawk, designated as Tail #21-7002, successfully completed its maiden flight at St. Louis Lambert International Airport. This paved the way for formal acceptance testing by the USAF.
The first T-7A was officially delivered to the United States Air Force in December 2023, arriving at Scott Air Force Base, Illinois, for military acceptance and pre-operational assessments. This marked the beginning of the aircraft's integration under Air Education and Training Command (AETC), with plans to gradually introduce it across Undergraduate Pilot Training (UPT) units.
An important operational milestone was achieved on January 10, 2026, when Boeing Defense announced via its official X (formerly Twitter) account that the first T-7A Red Hawk advanced trainer had been formally inducted into active service in San Antonio, Texas. Delivered in December to Air Education and Training Command (AETC), this induction ceremony officially marked the start of a new era in pilot training for all U.S. Air Force fighter and bomber crews, emphasizing the transition into the digital age of aviation training.
The T-7A is designed to emulate many of the mission system complexities found in modern combat aircraft. Its embedded training architecture, real-time data link capabilities, and scalability for future avionics upgrades make it a highly adaptable platform for evolving air combat doctrine. In addition to its training role, Boeing has also proposed a light attack and aggressor variant, offering a cost-effective solution for air forces seeking multi-role capabilities on a common training airframe.
T-7A Red Hawk variants:
- T-7A Red Hawk: Baseline USAF advanced trainer variant.
- T-7B (Unofficial/Projected): Hypothetical light attack or aggressor variant under consideration.
- T-7 Export Variant: Boeing is actively marketing tailored configurations for foreign air forces under different avionics and weapon systems.
- Red Hawk FMS Configurations: Configurable baseline tailored to international military pilot training requirements.
Technical Data
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Armament
The T-7A Red Hawk is delivered in its baseline configuration as an unarmed aircraft, strictly intended for advanced pilot training. However, the design includes provisions for weaponization in future variants. The airframe is structurally reinforced to accept underwing hardpoints, enabling the integration of external stores such as short-range air-to-air missiles (e.g., AIM-9 Sidewinder), guided bombs (e.g., GBU-12 Paveway II), or gun pods for light-attack or aggressor-training missions.
The T-7A Red Hawk can be modified to support live ordnance for air-to-ground or air-to-air roles, depending on customer requirements. Boeing has presented conceptual configurations that include up to four external stations, compatible with both NATO and non-NATO standard munitions. This latent capability makes the T-7A a viable candidate for multi-role variants in foreign military sales, particularly for air forces seeking dual-use training and strike platforms.
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Design and protection
The hull of the AMX-10P is made of all-welded aluminum armor with the driver's compartment at the front of the vehicle on the left, the engine compartment to the right and the troop compartment at the rear of the hull. The front of the vehicle is sloped to provide additional protection against incoming fire. The AMX-10P's armor provides protection against small arms fire and shell fragments, but it is not designed to withstand heavy armor-piercing rounds or other high-caliber weapons. The vehicle has a crew of three, including a driver, a gunner, and a commander, and can carry up to eight fully-equipped soldiers. The eight infantrymen are seated on individual bucket seats in the troop compartment at the rear. One man is seated forward and right of the turret facing the rear, one man to the right of the turret facing the turret, four men to the rear of the turret (two on each side facing outwards), and one man on each side at the rear facing inwards. They enter and leave by the large electrically operated ramp at the rear.
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Engine
The T-7A Red Hawk is powered by a single General Electric F404-GE-103 afterburning turbofan engine, which delivers approximately 78.7 kilonewtons (17,700 pounds-force) of thrust when operating in full afterburner. This engine is a modernized derivative of the proven F404 series, widely recognized for its reliability, high thrust-to-weight ratio, and ease of maintenance. The F404-GE-103 features a full-authority digital engine control (FADEC) system that ensures precise throttle response and optimal performance across a wide range of flight conditions.
The T-7A Red Hawk is capable of achieving maximum speeds in excess of Mach 1.2, equivalent to approximately 1,482 kilometers per hour (921 miles per hour) at altitude. The aircraft has a service ceiling of over 15,240 meters (50,000 feet), allowing student pilots to operate within the same vertical envelope as frontline operational fighters. Its rate of climb exceeds 76 meters per second (15,000 feet per minute), enabling rapid altitude gain for intercept or combat maneuvering profiles.
The airframe is rated for sustained high-g maneuvers up to +8g, enabling comprehensive air combat maneuver training. The aircraft is equipped with a triple-redundant digital fly-by-wire (DFBW) flight control system that ensures precision handling across the entire flight envelope. The control laws are adjustable, allowing the T-7A to simulate the aerodynamic responses of other fighter aircraft, enhancing its capability as a surrogate trainer for fifth-generation aircraft. The aircraft also exhibits superior low-speed handling and angle-of-attack control, making it suitable for formation flying and touch-and-go landings under varied environmental conditions.
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Avionics
The T-7A Red Hawk is equipped with a fully digital avionics suite based on an open-architecture system design. Its cockpit includes three reconfigurable multifunction displays (MFDs), a wide-angle heads-up display (HUD), and full HOTAS integration for both seats. This design mirrors the interface logic of operational fighters, ensuring familiarity for trainee pilots transitioning to advanced combat aircraft.
The T-7A incorporates a fully integrated embedded training system (ETS) that simulates radar, electronic warfare, data link operations, and weapons deployment. The aircraft supports Live-Virtual-Constructive (LVC) training environments, enabling seamless interaction with ground-based simulators and networked synthetic adversaries. Navigation is handled by an inertial navigation system (INS) with embedded GPS, and the aircraft includes secure VHF/UHF communication systems, data-link capability, and electronic threat-emulation software. The crew is protected by Martin-Baker US18E Mk.16L ejection seats rated for zero-zero operation.
Specifications
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Type
Supersonic advanced jet trainer
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Country users
United States
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Designer Country
United States (Boeing), Sweden (Saab – components and fuselage)
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Armament
Baseline unarmed; provision for AIM-9, GBU-12, gun pods in future variants
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Avionics
Digital glass cockpit, LVC-enabled, open architecture, embedded training suite
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Weight
Empty: ~7,900 kg (17,420 lbs); Max Takeoff: ~12,700 kg (28,000 lbs)
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Engine
1 × F404-GE-103 afterburning turbofan, 78.7 kN (17,700 lbf) thrust
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Speed
Max Speed: Mach 1.2 (~1,482 km/h or 921 mph)
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Range
Ferry Range: ~1,900 km (1,180 mi); Simulated combat radius: ~850 km (528 mi)
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Dimensions
Length: 14.4 m; Wingspan: 9.4 m; Height: 4.0 m