DO-160 vs. MIL-STD-704: The Engineer’s Cheat Sheet for Power Quality Requirements

DO-160 vs. MIL-STD-704: The Engineer’s Cheat Sheet for Power Quality Requirements

Aircraft Power Requirement Tool

DO-160 Section 16 and MIL-STD-704 (Aircraft) Standard Comparison

PARAMETERREQUIREMENT

The 16V Trap: Many 'COTS' (Commercial Off-The-Shelf) power modules are rated for 18V-36V. If you use these in a Category Z environment, they will shut down during Emergency Operation tests at 16V. At Inrush Technology, we specialize in 'Wide-Input' de-risking, ensuring your power stage remains stable down to 16V without triggering an over-current protection or thermal runaway.

Performance Level Operation at 16.0V DC Example Systems
Level A Full Performance. The equipment must operate exactly as specified without any deviation or degradation. Primary Flight Controls, Critical Avionics, Engine FADEC.
Level B Operational. Minor deviation is allowed (e.g., screen flicker or increased noise), but the system must remain functional. Navigation, Communication Radios, Internal Lighting.
Level C Survive & Restart. The equipment can shut down or fail, but it must automatically return to normal operation when power returns to 28V. IFE (Entertainment), Galley Power, Non-Essential Sensors.

Read more

7 Hiring Mistakes to Avoid When Recruiting Aerospace Power & EMI Engineers

7 Hiring Mistakes to Avoid When Recruiting Aerospace Power & EMI Engineers

1️⃣ The Resume Illusion: Keywords ≠ Competence Most aerospace job descriptions contain: * DO-160 * MIL-STD-461 * EMI/EMC * 28V / 270V DC systems * Power conversion (DC/DC, AC/DC) * Thermal analysis * High-reliability layout * The problem? * Candidates know these keywords. But many have: * Supported testing (not owned architecture) * Followed legacy layouts (without understanding current return

By Inrush