DGCA Section 7.1 · Open-Source Firmware Compliance

The compliance gate between your firmware and your Type Certificate.

Section 7.1 can become a significant source of delay in a DGCA Type Certification submission. It requires a verifiable chain across firmware, hardware, and ground-control software, including integrity verification, POST, secure updates, and compliance-critical parameter controls supported by objective evidence. We implement and validate that chain on supported ArduPilot or PX4 platforms—without requiring a hardware replacement or creating unnecessary fork lock-in.

ArduPilot·PX4

Why This Blocks You

Section 7.1 is not an isolated checkbox. Gaps in its firmware, hardware, or ground-control chain can delay the wider Type Certification submission.

It connects hardware, firmware, and ground-control software into one verifiable chain—not a single checkbox. Each control requires an appropriate firmware-side implementation and, where applicable, a matching ground-control interface. If either side is incomplete, the overall evidence chain remains incomplete.

Hardware
Firmware
Ground Control
One connected chain — not a single checkbox
What We Deliver

The full Section 7.1 chain — proven by test.

Each control is implemented in the relevant firmware and ground-control components, mapped to the applicable requirement, and demonstrated through testing rather than assertion alone. The final two are additional security controls beyond the items mapped to Section 7.1.

7.1 (a)Firmware Integrity

Signature verification runs in the bootloader, before any flight code executes. An unsigned image or one altered by a single byte fails the check and the boot halts. The aircraft will not arm when firmware authenticity and integrity cannot be verified.

Checksumming code and data independently means a tampered data partition cannot hide behind a valid code checksum or the other way around. Each segment is verified against its own registered SHA-256 reference.

The reference values the aircraft checks against are themselves protected. They cannot be edited in the field or swapped by an operator; a new set is written only when a manufacturer-signed firmware release is installed.

Validated on every power cycle, not once at the factory. A checksum mismatch prevents arming, and each result is written to an evidence log that can support the Type Certification submission.

Unauthorized modification is blocked by design and backed by a test record: tampered images, unsigned images, and images signed with the wrong key are each shown to be rejected. The resulting test record can be included in the objective-evidence package for assessment.

7.1 (b)Secure Firmware Updates

Every update is verified before it is applied—never afterward and never merely as a dismissible warning. Unsigned, tampered, wrong-key, and unauthorized rollback attempts are rejected and logged. After an authorized upgrade, the registered reference hashes are rewritten securely.

7.1 (c)Parameter Lock

Parameters that define the certified compliance boundaries are controlled by the signed release. Normal mission variables may remain adjustable within those approved boundaries, while changes to the boundaries require an authorized release and the applicable certification-change process.

Beyond 7.1What Most Vendors Skip

Every security-relevant event is written to a cryptographically signed, tamper-evident log. The log can be verified offline without relying solely on the aircraft that generated it, providing an independently checkable record of security-relevant events.

The command link uses per-aircraft MAVLink signing to authenticate messages from the configured ground station. Commands that fail authentication or originate from an unpaired station are rejected according to the configured acceptance policy.

Engagement Process

Four steps. A defined scope, not an indefinite retainer.

01
Step 01

Compliance Assessment

We review your hardware, firmware baseline, and current Type Certification stage to define the applicable Section 7.1 scope.

02
Step 02

Implementation Plan

A defined scope and timeline against the full Section 7.1 control set. No indefinite engagement.

03
Step 03

Integration

We implement the controls mapped to Section 7.1, together with the selected additional security controls, across the relevant firmware and ground-control components.

04
Step 04

Validation and TC Support

We validate POST behaviour, prepare evidence logs, and support the relevant documentation during your Type Certification submission.

Supported Flight Stacks

Two flight stacks. Full Section 7.1 support.

We provide Section 7.1 implementation support for two widely used open-source autopilot platforms. Choose your stack—the implementation, validation, and evidence discipline remain consistent in either case.

Get Started

Get a compliance assessment.

Tell us about your flight controller and current Type Certification stage. We will respond with a defined scope—not a sales pitch.