In 2019, DRDO and ADA projected that the AMCA would be ready for operational induction by 2035.
It is now mid-2026. DRDO and ADA have yet to achieve a major programme milestone on the path from the design board to operational induction. Nevertheless, both organisations continue to adhere to the original timeline.
The projected timeline was viewed with considerable scepticism within sections of the IAF when it was first presented. Whether that scepticism has diminished, with only nine years remaining to the planned induction date, is difficult to judge.
Rather than speculate, I will confine myself to the available facts.
According to the current timeline, AMCA's maiden flight is projected to take place in the middle of 2029. That gives ADA and its private sector development partner just 6 years of test flying to qualify the aircraft for initial operational clearance.
By comparison, the F-22 required approximately eight years from first flight to operational service, the F-35 around nine years, and the Su-57 roughly ten years. China, however, fielded the J-20 in about six years.
One important distinction is that China was not attempting to field the aircraft with an interim foreign engine while simultaneously planning an indigenous replacement.
We will talk about the "interim" engine later. Let's first remind ourselves that the J-20 was developed by China’s Chengdu Aircraft Corporation (CAC), part of AVIC.
Before developing the J-20, CAC had designed and produced the J-7 (a MiG-21 derivative) and, crucially, the J-10 — China’s first indigenous fourth-generation multirole fighter (first flight 1998, entered service around 2005).
ADA and its private sector partner will not have the experience of CAC when they start building the AMCA.
The GE F414 Engine Issue
The AMCA has been designed around the General Electric F414 engine. The F414 is a 98 kN thrust class engine. The IAF wants the AMCA to be powered by a 110-kN class engine. Consequently, F414 has been publicly described as an interim AMCA powerplant. The long-term intention is to replace it with a more powerful indigenous engine that is yet to be developed. The follow-up variant with the more powerful indigenous engine is to be called AMCA Mk.2
India, which currently does not have the technology to build a 110-kN class turbofan engine, intends to develop the engine in partnership with Safran or Rolls-Royce.
India intends to procure GE F414 engines not just as an interim powerplant for the AMCA but also as the powerplant for the under development LCA Mk.2 and the Twin Engine Deck Based Fighter (TEDBF) which is still at an early stage of development.
Negotiations for the F414 have reportedly slowed amid disagreements over pricing. Some reports place the cost at over ₹200 crore per engine—nearly three times earlier estimates of ₹70–80 crore—with additional discussions concerning the approximately ₹6,000 crore cost of establishing a dedicated manufacturing line.
The Risks of an Interim Engine Strategy
Designing an airframe around an engine that is acknowledged to be below the aircraft's intended long-term thrust requirement introduces significant technical and programme risk. HAL did this in the past with the Marut HF-24 and the outcome was very disappointing for the IAF. HAL could neither develop nor acquire an aeroengine powerful enough to achieve the airframe's Mach 2 capability that the IAF so desperately coveted. Three squadrons of the Marut were operationally inducted and then prematurely phased out. The author has the dubious distinction of having flown his last sortie on the Marut ferrying an aircraft, with just 60 airframe hours, into retirement storage.
The AMCA programme appears to risk repeating a development approach that produced disappointing results with the HF-24 Marut some six decades ago.
The central concern discussed here is not whether India should develop the AMCA—there is broad agreement that it should—but whether the present development strategy is technically sound and likely to achieve its objectives within a realistic timeframe.
Traditionally, combat aircraft are designed around their engines. The engine is not merely a source of thrust; it is the heart of the aircraft, determining numerous aspects of the overall design. It influences weight distribution, intake and exhaust geometry, cooling requirements, hydraulic capacity, electrical power generation, fuel consumption, centre of gravity, and maintenance philosophy. The engine also determines how much electrical power is available for sophisticated systems such as active electronically scanned array (AESA) radar, electronic warfare equipment, sensors, and future directed-energy or high-power electronic systems.
With the AMCA program India proposes to design and certify an aircraft around one engine and subsequently redesign significant portions of the aircraft to accommodate another. Such an approach introduces substantial technical and programme risks.
Engine Replacement Challenges
ADA has stated that the AMCA airframe incorporates provisions for a future 110-kN-class engine. (The Marut airframe similarly provisioned for a higher thrust reheated engine.)
The question is whether designing and certifying an aircraft around one engine before integrating another introduces unnecessary technical and programme risk.
Replacing an engine is not simply a matter of installing a more powerful unit. Changes in airflow requirements, mounting arrangements, cooling systems, hydraulic pumps, electrical generators, fuel systems, engine controls, software integration, and flight characteristics may all require redesign. Even relatively small differences in engine dimensions, mass flow, or power extraction can affect the aircraft’s overall performance and certification.
From an engineering perspective, developing a new engine to suit an already frozen airframe can also be highly restrictive. Engine designers may find themselves forced to meet constraints imposed by an existing aircraft rather than optimising the engine for performance, reliability, maintainability, and future growth. This creates risks for both the engine programme and the aircraft programme simultaneously.
Alternative Strategy
Rather than committing to an interim airframe, an alternative strategy may reduce technical risk while preserving India’s significant technological gains.
ADA and DRDO have invested heavily in developing many of the enabling technologies that define a fifth-generation fighter. These include radar-absorbent materials, stealth shaping techniques, sensor fusion, avionics architecture, flight-control software, advanced mission computers, and low-observable manufacturing processes. These achievements represent valuable national capabilities irrespective of the final aircraft configuration.
Instead of finalizing an aircraft design around an interim engine, these technologies could continue to mature through incremental integration into existing and developmental platforms.
For example, stealth technologies, autonomous mission systems, and sensor fusion could be demonstrated aboard unmanned combat aircraft such as the Ghatak UCAV currently under development. Other technologies could be progressively integrated into operational platforms such as the Su-30MKI, Mirage 2000, or the LCA Tejas, allowing engineers to validate hardware, software, reliability, and operational concepts under real flying conditions.
Such an incremental approach would continue to advance India’s technological competence while reducing programme risk. Each successful demonstration would increase confidence in individual technologies before integrating them into a completely new aircraft.
Meanwhile, efforts could focus on developing the indigenous engine to the maturity required for operational service. Once that engine is available and its characteristics are fully understood, engineers could design the AMCA airframe around its actual capabilities rather than estimated future specifications.
By that stage, most of the enabling technologies would already have been demonstrated and refined, allowing designers to concentrate on optimising the airframe itself. This could produce a more coherent, better-integrated fighter while avoiding extensive redesign after the aircraft enters development.
Conclusion
This proposal does not advocate slowing India’s fifth-generation ambitions. Rather, it recommends sequencing development in a manner that aligns more closely with established aerospace engineering practice. The objective would be to reduce technical risk, improve system integration, and ultimately produce a more capable aircraft with fewer compromises.
India has already made substantial investments in the technologies required for a fifth-generation fighter. Allowing these technologies to mature independently while bringing the indigenous engine to operational readiness before finalising the aircraft design may provide a more robust path to achieving the AMCA's long-term objectives.




