01November 2026

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By Leeanna Tolles, General Manager – Maintenance and Integration, MAG.

Leeanna Tolles is General Manager of Maintenance and Integration at MAG Aerospace, bringing more than 25 years of aviation industry experience spanning aircraft maintenance, business operations, and organizational leadership.  Prior to joining MAG, Leeanna spent 17 years helping build and grow a comprehensive aviation services company specializing in aircraft management, pilot services, flight training and aircraft maintenance.  This experience shaped her hands-on approach to leadership, operational excellence and customer services.  Today, she is passionate about developing strong teams, advancing aircraft modification and integration capabilities, and delivering innovative aviation solutions that support mission readiness.  She believes success in aviation is built on technical excellence, strong relationships, and the people behind the mission. 

Head and shoulders portrait of Leeanna Tolles Manager of Maintenance and Integration at MAG smiling in a blazer with a professional badge visible

November 2026

FACILITIES:

  • Titusville, FL – Space Coast Regional Airport (KTIX)
  • 50,000 ft² Technology Integration Area
  • 6,500 ft² Engineering / Design / Lab / SIL
  • 2,500 ft² Research and Development
  • 12,000 ft² Manufacturing / Machining / Kitting
  • 20,000 ft² Aircraft Integration / Training / Maintenance
  • Machining Capability: Water Cutter / CNC System
  • 8,000 ft² Main Office

CERTIFICATIONS:

  • AS9100D & ISO 9001:2015 Quality Management System
  • FAA Part 145 Repair Station
  • FAA Parts Manufacturer Approval (PMA)
  • FAA/MILSTD/AS9100 Design Practices
  • ANSI/IEEE/MIL-rapid prototyping engineering change process Class I & II TD-100 Drawing Practices
  • 36+ active FAA Supplemental Type certificates (STCs)
  • CMMI Level 3 and PMP‑certified methodologies for:
    • Project planning and scheduling.
    • Resource allocation and acquisition support.
    • Quality assurance and risk management.

Introduction: The Strategic Imperative of Airborne Intelligence and Regulatory Compliance

The modernization of military, federal, and civilian aviation for Command, Control, Computers, Communications, Cyber, Intelligence, Surveillance, and Reconnaissance (C5ISR) operations requires an extraordinary convergence of advanced aerospace engineering and rigorous regulatory compliance. The rapid integration of high-definition optical sensors, multi-domain datalinks, and edge-computing processors fundamentally alters an aircraft’s aerodynamic profile, electrical load distribution, and structural integrity. To execute these critical modifications legally and safely within controlled airspace, aviation authorities such as the Federal Aviation Administration (FAA) mandate the acquisition of Supplemental Type Certificates (STCs).

Over the past decade, MAG Aerospace has positioned itself as a dominant, vertically integrated force in the global C5ISR sector, providing manned and unmanned full-spectrum outsourced intelligence services. A core pillar of this dominance is the company’s robust proprietary portfolio of over 36 active FAA STCs, which authorize sweeping modifications across diverse aircraft platforms. These certifications cover the full spectrum of systems engineering—from the installation of heavy-duty 28 VDC mission power busses and complex structural provisions for external sensors to the intricate relocation of essential flight hardware.

An STC is far more than a regulatory administrative requirement; it is a highly valuable intellectual property asset that dictates the speed, safety, and legality with which critical intelligence platforms—ranging from the rugged turboprop MC-208 Guardian to the high-altitude Bombardier Global 6500—can be deployed into active theaters of operation. As missions become faster, more data-intensive, and more reliant on real-time situational awareness, the ability to seamlessly bridge the gap between commercial aircraft frames and military-grade sensor payloads defines operational success.

This comprehensive report explores the engineering, legal, and operational frameworks underpinning MAG’s STC portfolio, detailing the mechanics of 14 CFR Part 21 Subpart E, the physics of sensor integration, and the future of turnkey intelligence aviation.

The Regulatory Bedrock: Demystifying 14 CFR Part 21 Subpart E

To comprehend the magnitude of MAG’s engineering accomplishments, it is essential to first deconstruct the dense regulatory framework governing aircraft modifications. Under Title 14 of the Code of Federal Regulations (CFR), Part 21, Subpart E prescribes the rigid procedural requirements for the issuance of Supplemental Type Certificates.

When an aircraft is originally designed and manufactured, the FAA issues a Type Certificate (TC) validating that its original design meets all foundational safety, structural, and airworthiness standards. However, special mission and ISR operations inherently require extreme post-production modifications. These modifications often involve penetrating the pressurized fuselage to mount radomes such as the Universal Adapter Plate (UAP), bolting heavy, drag-inducing sensor turrets to the underbelly, or routing high-voltage wiring through bulkheads.

Because these interventions are classified legally as “major changes in type design” that do not warrant a completely new, original aircraft Type Certificate, an applicant must apply for an STC under the provisions of 14 CFR § 21.113.

The STC application and approval process is uncompromising and highly iterative. Under § 21.115, the applicant bears the absolute burden of proving that the altered product continues to meet all applicable airworthiness and environmental requirements specified in the original certification basis, including complex acoustical and emissions standards. This substantiation demands extensive ground testing, flight testing, computational fluid dynamics (CFD) modeling, and structural fatigue analysis. Once the FAA determines that the modification does not adversely affect the safety or operation of the aircraft, the STC is issued under § 21.117. The STC effectively incorporates the original TC by reference, legally binding the new engineering modifications to the original aircraft’s established operating parameters and creating a unified standard of airworthiness.

The FAA STC certification pipeline demands extensive coordination between the applicant’s engineering team and the regulatory body. The historical data and regulatory texts demonstrate a consistent, multi-stage progression from initial concept to operational deployment, culminating in the creation of a proprietary Master Data List (MDL) and ongoing Instructions for Continued Airworthiness (ICA).

STC Lifecycle Stage 14 CFR Reference Engineering and Regulatory Requirements
1. Application & Familiarization § 21.113 The applicant submits a formal application detailing the scope of the major change in type design. The FAA and the applicant hold preliminary Type Certificate Board (TCB) meetings to establish the certification basis and program plan.
2. Engineering Data & Evaluation § 21.115 The applicant submits exhaustive substantiating data, including structural analysis, electrical load mapping, and aerodynamic models, to prove the altered product meets all applicable airworthiness requirements.
3. Ground & Flight Testing § 21.33, § 21.53 The FAA performs conformity inspections, witnesses ground tests, and conducts official certification flight tests to validate the applicant's engineering claims under real-world aerodynamic loads.
4. Documentation Generation § 21.50 The applicant finalizes the Master Data List (MDL), Airplane Flight Manual Supplements (AFMS), and Instructions for Continued Airworthiness (ICA) to ensure long-term safe operation.
5. Issuance & Deployment § 21.117, § 21.119, § 21.120 The FAA issues the STC. The STC holder gains the privilege to market the modification and must provide written permission for any third party attempting to alter an aircraft using the STC design.

The Intellectual Property of Aviation: Master Data Lists (MDL) and Continued Airworthiness

The acquisition of an STC confers specific, highly guarded privileges and heavy responsibilities under 14 CFR § 21.119 and § 21.120. One of the most critical, yet frequently misunderstood, aspects of the STC ecosystem is the concept of intellectual property and design control.

The possession of the physical STC document by an aircraft owner, a third-party maintenance facility, or a competitor does not grant them the legal right to alter an aircraft. An STC holder such as MAG Aerospace retains strict ownership of all underlying design data. If an external aircraft operator wishes to utilize a MAG Aerospace STC to modify their own fleet, MAG Aerospace must provide explicit written licensing agreements or permission acceptable to the FAA. This regulatory moat ensures that the engineering investments made by thought leaders in the aviation and aerospace are protected against unauthorized replication.

This vast repository of technical data is centralized and legally codified within a document known as the Master Data List (MDL). The MDL serves as the foundational blueprint of the STC, comprehensively cataloging every single engineering drawing, wiring schematic, structural analysis report, and flight manual supplement required to execute the modification accurately. For instance, when MAG integrates structural provisions for external sensors, the STC directly references proprietary MDLs, such as Doc. No. 2020010-MDL-101 or 2020006-MDL. Any deviation from the procedures or hardware specified in the MDL invalidates the STC, rendering the aircraft unairworthy and legally grounding it.

Furthermore, the STC holder is legally obligated to develop and issue FAA-accepted Instructions for Continued Airworthiness (ICA). The ICA dictates exactly how the newly integrated components must be inspected, maintained, and eventually replaced over the aircraft’s entire lifecycle. This includes defining non-destructive testing (NDT) intervals for stress fractures around new structural mounts and specifying the replacement cycles for heavy-duty electrical relays. Through the MDL and the ICA, MAG Aerospace ensures that their modifications do not degrade the aircraft’s safety margins decades after the initial installation.

Comprehensive Technical Analysis of MAG Aerospace’s STC Portfolio

MAG Aerospace’s public portfolio of recognized FAA STCs underscores a deliberate, highly strategic approach to vertical integration within the C5ISR market. Rather than relying entirely on third-party integrators, holding these STCs internally allows MAG to execute rapid, turnkey aircraft modifications for defense, federal, and civilian clients across the globe. A deep technical analysis of their registered STCs reveals distinct, highly specialized clusters of engineering focus that work in tandem to create cohesive intelligence platforms.

1. Advanced Optical and Sensor Systems Integration

The absolute core of any modern aerial intelligence platform is its primary sensor array. MAG holds critical STCs specifically engineered for the integration of high-end optical and infrared systems, which form the primary data-gathering apparatus for targeting and surveillance.

A premier example is STC No. SA04482CH, which explicitly authorizes the installation of the Teledyne FLIR Star SAFIRE 380-HDc imaging system, complete with an integrated Laser Range Finder (LRF). The integration of the 380-HDc represents a formidable engineering challenge. This specific system provides high-definition, full-motion video in both the visible and mid-wave infrared spectrums. Because the optics must maintain sub-pixel accuracy to compensate for the continuous, high-frequency vibration of the aircraft engines and turbulent airflow, the mechanical integration must be flawless.

The physical implications of mounting such a system are massive. First, the sensor turret itself represents a heavily concentrated mass. Installing this unit far forward on the nose or aft on the fuselage shifts the aircraft’s center of gravity (CG), requiring precise counter-balancing or strict payload management protocols to prevent aerodynamic instability. Second, a spherical turret protruding into the high-velocity slipstream creates significant parasitic drag. This drag reduces the aircraft’s loiter speed, increases fuel burn rates, and alters the wake dynamics over the empennage (tail surfaces). Third, because the payload includes a highly focused Laser Range Finder, the mounting interface must be phenomenally rigid. If the STC-approved mount flexes by even a fraction of a millimeter under the aerodynamic load of a banking turn, the laser will miss its intended target on the ground by hundreds of meters.

Similarly, STC No. SA04444CH provides broad, modular structural and electrical provisions for Forward-Looking Infrared (FLIR) systems under MAG’s Master Data List 2020006-MDL. This STC serves as a flexible, future-proof architecture. By certifying the provisions rather than just a single camera model, it allows for the rapid swapping of various FLIR models depending on the specific operational theater’s requirements, bypassing the need to ground the aircraft and recertify the entire airframe every time sensor technology iterates. Furthermore, STC No. SA00226MC provides overarching approval for Special Mission Equipment encompassing Intelligence, Surveillance, and Reconnaissance modifications, highlighting a comprehensive approach to payload integration.

2. Structural Engineering and External Payload Mounts

High-fidelity sensors cannot simply be bolted to an aircraft’s thin aluminum or composite skin. The skin of an aircraft is primarily designed to hold internal cabin pressure and maintain an aerodynamic shape; it is entirely unsuited to bear the concentrated, multi-directional structural loads generated by heavy external pods.

To solve this critical physical limitation, MAG holds STC No. SA04564CH, which outlines the exhaustive installation of structural provisions to mount fixed external sensors, governed by MDL Doc. No. 2020010-MDL-101. This STC represents the critical “hidden” engineering of airborne ISR. It mandates the precise design and installation of internal metallic doubler plates, stringer reinforcements, and custom-machined bulkheads that capture the aerodynamic and inertial loads of the sensor and distribute them evenly across the aircraft’s primary load-bearing skeleton.

When an aircraft executes a high-G maneuver to track a fast-moving target, the inertial weight of the sensor turret multiplies dynamically. MAG’s STC guarantees to the FAA, through extensive finite element analysis (FEA) and physical load testing, that these structural reinforcements will prevent the sensor from tearing through the fuselage during extreme flight envelopes, severe turbulence, or hard landings.

MAG Aerospace STC Primary Engineering Function Operational Capability Enabled
SA04482CH Teledyne FLIR Star SAFIRE 380-HDc & LRF Installation High-definition visible/IR full-motion video collection with precision laser targeting.
SA04444CH Universal FLIR System Provisions Rapid, modular swapping of optical payloads without requiring full airframe recertification.
SA04564CH Structural Provisions for External Sensors Load-bearing reinforcement to prevent airframe fatigue and structural failure under high-G maneuvers.
SA04559AT Installation of up to three 28 VDC Mission Power Busses Segregated, high-capacity electrical power for energy-intensive edge computing and datalinks.
SA04566CH Relocation of TKS Ice Protection System Optimizes lower fuselage space for radomes while maintaining critical all-weather operational safety.

As ISR platforms rapidly evolve, the operational shift from high-latency, kilobit-rate satellite communications to low-latency LEO (Low Earth Orbit) broadband networks, coupled with the integration of onboard AI processing, has exponentially increased the electrical power demands of the aircraft. A standard civilian aircraft’s alternators and factory wiring harnesses are entirely insufficient to power a modern, multi-domain C5ISR suite.

MAG directly addresses this severe electrical bottleneck with STC No. SA04559AT, which explicitly provides for the installation of up to three independent 28 VDC mission power busses.

The engineering rationale underpinning this STC is crucial for mission survival. Modern intelligence platforms carry diverse and electrically noisy systems—such as Signals Intelligence (SIGINT) receivers, Synthetic Aperture Radar (SAR), high-power broadband datalinks, and active liquid-cooling systems for server racks. Segregating power across up to three distinct 28 VDC busses ensures that a sudden power surge or a short circuit in a high-draw transmitter does not trip the circuit breakers for the aircraft’s primary flight avionics, thereby protecting the flight crew. Furthermore, pushing high amperage through dense bundles of aircraft wiring generates significant thermal energy. This STC incorporates strict wire-routing guidelines, specialized aviation-grade circuit protection, and thermal mitigation strategies to prevent catastrophic electrical fires within the tightly packed confines of the cabin. Lastly, in tactical environments, maintaining real-time intelligence feeds is mission-critical; multiple power busses allow operators to switch redundant sensor systems to backup power sources instantly in the event of an engine alternator failure.

4. Ancillary Systems and Relocation Engineering

Modifying an aircraft for special missions is often a zero-sum game regarding physical space and weight. Adding a large belly-mounted radome frequently dictates that an existing, critical aircraft system must be moved to accommodate the new payload.

This complex spatial conflict is resolved through highly specialized relocation STCs, such as MAG’s STC No. SA04566CH. This STC meticulously details the relocation of the TKS ice protection system tank and its associated equipment pack, governed by Doc. No. 2020011-MDL-100. TKS is a critical anti-icing system that utilizes a centralized pump to force glycol-based fluid through micro-porous titanium panels on the leading edges of the wings and tail, preventing hazardous ice accretion during flight. The pump, the reservoir tank, and the dense fluid itself are incredibly heavy and are typically located by the original manufacturer in the lower belly of the aircraft—exactly where systems engineers prefer to mount downward-looking SAR arrays or EO/IR turrets.

Relocating the TKS system is an intricate regulatory and physical challenge. The STC must definitively prove to the FAA that the new tank location maintains the aircraft’s proper center of gravity across all phases of flight as the fluid depletes. It must also demonstrate that the relocated fluid lines can reach the wings without suffering dangerous pressure drops, and that the system will still effectively prevent ice accumulation, thereby preserving the aircraft’s critical all-weather operational capability.

The Physics of Systems Integration: EMI, EMC, and RF De-confliction

Beyond the physical challenges of weight, balance, and raw power draw, integrating dense C5ISR packages into a highly confined metallic aircraft cabin introduces severe, invisible threats: Electromagnetic Interference (EMI) and the absolute necessity of Electromagnetic Compatibility (EMC).

An aircraft is a highly sensitive, enclosed ecosystem of radio frequencies. The navigation radios, GPS receivers, transponders, radar altimeters, and modern fly-by-wire control systems all rely on specific, uncontaminated RF bands to function.

When an integrator like MAG Aerospace installs high-wattage SIGINT packages, SATCOM uplinks, and tactical radios via their STC processes, they must rigorously test for EMC to prevent catastrophic signal fratricide.

Under the stringent testing requirements of 14 CFR Part 23 (for smaller commuter aircraft) or Part 25 (for transport category aircraft), the equipment under test (EUT) must conclusively prove that it can operate seamlessly in its electromagnetic environment without creating emissions that degrade the aircraft’s primary flight systems, while also proving it is not susceptible to interference from the aircraft’s own transmitters. To achieve this, aerospace engineers establish strict “RF keep-out zones,” utilize heavily shielded, mil-spec cabling, and conduct exhaustive ground testing in anechoic chambers to meticulously map the electromagnetic spectrum of the modified aircraft.

A failure in EMC engineering could theoretically result in a high-power intelligence datalink inadvertently jamming the aircraft’s own instrument landing system (ILS) during a crucial low-visibility approach. MAG’s rigorous STC testing regimens guarantee this essential electromagnetic harmony.

Platform Evolution and Strategic Partnerships: From the MC-208 to the Global 6500

MAG Aerospace does not operate in a vacuum; our ability to rapidly design, certify, and deploy STC-approved modifications has positioned us as a highly sought-after prime partner for massive Department of Defense (DoD) fleet modernization contracts.

Historically, MAG has achieved exceptional operational success fielding their proprietary MC-208 Guardian platforms. These heavily modified Cessna turboprops are currently fielded across harsh operational environments in Africa, Asia, and the Middle East, supporting the vital national security interests of the United States and allied foreign militaries. The MC-208 relies heavily on MAG’s foundational STCs to operate as a rugged, low-altitude, long-endurance intelligence gathering asset.

However, the threat landscape is rapidly shifting toward near-peer adversaries, necessitating high-altitude, high-speed platforms.

This strategic pivot is exemplified by the teaming agreement between MAG Aerospace and L3Harris Technologies. Together, we are executing multi-million-dollar contracts to deliver enhanced aerial ISR capabilities for the U.S. Army ATHENA-R program.  MAG serves as the prime contractor, leveraging our deep institutional expertise in aircraft modifications, open systems architecture, and FAA STC certification to rapidly integrate complex, multi-intelligence mission packages.

The Bombardier Global 6500 represents a massive paradigm shift in STC engineering compared to turboprop platforms. The Global 6500 operates at significantly higher altitudes and transonic speeds. Consequently, structural sensor mounts must be engineered to withstand higher mach numbers and extreme sub-zero temperatures, while the mission avionics must interface flawlessly with a highly sophisticated, deeply integrated commercial glass cockpit.

The unique synergy between L3Harris’s cutting-edge sensor payloads and MAG’s modification and STC certification expertise significantly compresses the acquisition timeline from initial prototype to operational deployment, providing the U.S. Army with real-time, low-latency, collaborative decision-making capabilities in the stratosphere.

The Future of Airborne ISR Architectures: LEO Broadband and MOSA

The mission landscape is evolving at a breakneck pace, fundamentally altering what operators demand from an STC. Intelligence cycles that historically took hours to process via ground stations are now executed in seconds, driven by the integration of low-latency LEO broadband arrays and onboard AI processing systems that deliver hundreds of megabits per second of uncompressed imagery.

ISR platforms can no longer be static, single-purpose systems. An aircraft heavily modified today must be structurally and electrically adaptable to accommodate the unknown sensor technologies of 2035. As a thought leader and prime integrator, MAG Aerospace views STC modifications not as isolated, one-off installations, but as long-term capability investments designed for lasting readiness.

Future modifications will increasingly rely on the Modular Open Systems Approach (MOSA). Structural flexibility, highly scalable electrical power, and deeply embedded cybersecurity protocols will define the next generation of FAA certifications. The modern engineering integration challenge is no longer just bolting a camera to a wing strut; it requires bridging highly secure, high-speed Gigabit Ethernet networks with legacy ARINC 429 and 717 avionics data buses, managing massive thermal loads generated by edge-processors, and passing all of this extreme complexity through the unyielding safety scrutiny of the FAA STC process.

Conclusion

The realm of special mission aircraft modification is fraught with immense engineering friction, aerodynamic penalties, and strict regulatory oversight. The Federal Aviation Administration’s uncompromising enforcement of 14 CFR Part 21 Subpart E ensures that only the most meticulous, highly capitalized, and technically sound organizations survive and thrive in the global C5ISR market.

MAG Aerospace has undeniably established itself at the absolute apex of this industry. By strategically developing, certifying, and retaining ownership of a comprehensive portfolio of STCs—ranging from heavy-duty electrical frameworks and deeply integrated structural sensor mounts to the precise, vibration-isolated integration of advanced FLIR optics—MAG provides an unparalleled, turnkey intelligence capability to military and civilian operators worldwide.

In an era where strategic decision superiority hinges on real-time, low-latency data, the physical foundation of that data is undeniably built upon the structural, electrical, and regulatory guarantees of the Supplemental Type Certificates held by MAG Aerospace.

 

Frequently Asked Questions (FAQ)

 

1. What exactly is an FAA Supplemental Type Certificate (STC)?

A Supplemental Type Certificate (STC) is a formal approval issued by the FAA under 14 CFR Part 21 Subpart E for major changes or modifications to an existing, previously type-certified aircraft, engine, or propeller that do not necessitate a completely new Type Certificate. The STC proves that the modification complies with all applicable safety, airworthiness, and environmental standards.

2. How many FAA Supplemental Type Certificates (STC) does MAG Aerospace hold?

As the Lead Systems Integrator (LSI) and a proven U.S. Government Prime Contractor, MAG holds over 36 active Federal Aviation Authority (FAA) Supplemental Type Certificates (STCs) for a diverse set of airborne platforms including Cessna Caravan C208, Havilland Canada DHC-6-400 Twin Otter, Boeing 737-700, and Airbus H-125.

3. Where does MAG Aerospace do the integration work for FAA Supplemental Type Certificates (STC)?

MAG’s Florida Technology Integration & Interoperability Innovation Center in Titusville, FL – Space Coast Regional Airport (KTIX). This facility is a 50,000-square-foot advanced manufacturing and engineering hub dedicated to airborne ISR modifications and stands out as a pinnacle of innovation, technological advancement, and manufacturing excellence. This state-of-the-art facility with over 15 years of experience supporting the design, modification, integration, testing, and certification of ISR platforms, is prominently located in the heart of the Space Coast, is a testament to MAG’s commitment to pushing the boundaries of what’s possible in technology.

4. If I possess a copy of an STC document, do I have the right to modify my aircraft?

No. Physical possession of the STC document itself by a third party does not constitute the right to use the underlying design data or perform the modification. The STC holder retains all intellectual property rights. If a person or organization wishes to utilize an STC to alter an aircraft, the STC holder must provide them with an explicit written licensing agreement or permission acceptable to the FAA.

5. What is a Master Data List (MDL)?

The Master Data List (MDL) is the foundational, proprietary blueprint of any given STC. It comprehensively lists and catalogs all the specific engineering drawings, wiring schematics, installation instructions, structural analyses, and flight manual supplements required to correctly and legally implement the approved design change.

6. Why is Electromagnetic Compatibility (EMC) testing required for ISR aircraft modifications?

Integrating complex C5ISR equipment (like high-powered sensors and broadband radios) into a confined aircraft cabin introduces the risk of Electromagnetic Interference (EMI). To comply with FAA certification standards under 14 CFR Parts 23 or 25, the equipment must undergo rigorous EMC testing. This ensures the new electronics do not disrupt the aircraft’s critical navigation or flight systems, and concurrently, that the new systems are not disrupted by the aircraft’s pre-existing electrical environment.

 

What Does MAG Aerospace Do?

MAG is a leader in delivering Command, Control, Communication, Computers, Cyber, Intelligence, Surveillance and Reconnaissance (C5ISR) services at the tactical edge with premier engineering and operational solutions around the world.

As the Lead Systems Integrator (LSI) and a proven U.S. Government Prime Contractor, MAG brings operational excellence and technical understanding with program management and systems engineering expertise to manage large, complex DOD systems development and deployment contracts.

MAG’s expertise in “Turnkey C5ISR” services involves taking commercial-off-the-shelf (COTS) technology and “missionizing” it for military use. MAG partners with non-traditional technology providers to accelerate adoption and compliance within the DoW (DoD) markets. By acting as a bridge between the commercial tech sector and the defense establishment, MAG ensures the warfighter has access to the latest defense technology on relevant timelines and across all domains.

MAG’s hybrid, technology and platform-agnostic business model enables us to work with the largest military OEMs, while avoiding vendor lock-in, as well as with small businesses and startups, to deliver large programs while accelerating deployment to the field and maximizing customer mission success. Solutions that require novel and state-of-the-art technologies with niche partners gives MAG the ability to continuously improve solutions with innovation. MAG experts are on the leading edge of technological advances, which enables MAG to rapidly prototype, integrate, and connect joint, next generation capabilities across Air, Land, Maritime, Space and Cyberspace Domains. Focused on making the world smaller and safer, MAG is defined by our core values of Serve. Win. Perform.