Documents
Boeing
T-7A Red Hawk
Advanced jet trainer developed by Boeing and Saab to replace the T-38 Talon in U.S. Air Force pilot training, designed digitally with a focus on preparing pilots for fifth-generation fighters.
In service since 2023 · 1 operator countries
Compiled from public sources ·primary reference ↗ ·last verified 2026-07-02
💲 ≈ $32,000,000, Approximate unit procurement cost
Procurement snapshot
Availability & export
US ITAR-controlled
Export needs U.S. State Dept (DDTC) approval; end-use & re-transfer restrictions apply.
Channel: Foreign Military Sales (FMS) or Direct Commercial Sale
Fielded & proven
Limited · 1 operator
In service since 2023. Status: active · ~5 built.
Lifecycle cost (est.)
$80M – $112M
Acquisition is only ~30% of lifecycle cost, operating & support dominate over ~25 yrs. Rough 2.5–3.5× the unit price. How we estimate this →
Interoperability
No standardised NATO calibre / datalink detected in public specs.
Derived guidance from public data, export regime by country of origin, lifecycle from the GAO ~30% acquisition rule. Verify eligibility, pricing and offsets with the manufacturer and your acquisition authority.
Powerplant
The T-7A Red Hawk's engine has its own full spec page.
Full specifications
Performance
Speed, range, altitude and engagement capability.
| Max speed (Mach) Maximum speed as a multiple of the speed of sound. Mach 2+ is typical for air-superiority fighters. | 0.97 Mach |
|---|---|
| Service ceiling Maximum operating altitude. Higher gives energy advantage and sensor horizon. | 15,000 m |
Physical
Dimensions, weight and crew.
| Length Overall length including gun/probe where applicable. | 14.2 m |
|---|---|
| Wingspan Wingtip-to-wingtip span. | 9.6 m |
| Height Overall height. Lower profile is harder to spot and hit for ground vehicles. | 4.3 m |
| Crew Personnel required to operate. Fewer reduces exposure; autoloaders trade a loader for mechanical complexity. | 2 |
Propulsion
Engine, power and fuel.
| Engine Powerplant model and type. | General Electric F404-GE-402 turbofan |
|---|---|
| Engines Number of engines. Twin-engine gives redundancy at higher cost. | 1 |
| Propulsion type Turbofan, turboshaft, diesel, gas turbine, solid-fuel rocket, ramjet… | Turbofan |
Program
Cost, production scale and operators.
| Unit cost Approximate flyaway/unit cost where public. Defense pricing varies hugely by contract, offsets and configuration. Lower is cheaper. | $32,000,000 |
|---|---|
| Units built Total production run. Higher means proven manufacturing, mature logistics and spares availability. | 5 |
| Operator countries Number of countries operating the system. More operators means broader support ecosystem. | 1 |
Specifications compiled from public Boeing and reference sources ↗. Published defense figures are approximations, treat comparisons as directional. Last verified 2026-07-02.
Compare with rivals
See how it stacks up
Frequently asked questions
How many crew does the Boeing T-7A Red Hawk require? +
The Boeing T-7A Red Hawk requires a crew of 2.
What engine does the Boeing T-7A Red Hawk use? +
The Boeing T-7A Red Hawk is powered by the General Electric F404-GE-402 turbofan.
How many countries operate the Boeing T-7A Red Hawk? +
The Boeing T-7A Red Hawk is operated by 1 countries.
How much does the Boeing T-7A Red Hawk cost? +
The Boeing T-7A Red Hawk has an approximate unit cost of 32,000,000 USD. Defense pricing varies by contract, offsets and configuration, treat this as directional.
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Related coverage
T-7A Red Hawk in the news
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