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  2. DO-160 Display Qualification: Components, Systems and Installation
  3. 16 — Electrostatic discharge and accessible display surfaces
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Home └DO-160 Display Qualification: Components, Systems and Installation └16 — Electrostatic discharge and accessible display surfaces
DO-160 Display Qualification: Components, Systems and Installation
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Course content
  • 01 — Public foundations and selected preview chapters
    • 00 — Start here: build a defensible display qualification plan
    • 01 — Public chapter: component, system and installed boundaries
    • 02 — Public chapter: read a qualification claim critically
    • 03 — Public chapter: the complete environmental test suite
    • 04 — Public chapter: temperature limits, ramp rates and decompression
  • 02 — Requirements and climatic exposures
    • 05 — Turn display functions into measurable acceptance criteria
    • 06 — Temperature and altitude: construct the procedure
    • 07 — Temperature variation: 5 and 10 °C per minute in practice
    • 08 — Pressure, altitude and rapid decompression
    • 09 — Humidity, water and fluids: qualify the exposed assembly
    • 10 — Salt spray, fungus, sand and dust
  • 03 — Mechanical and special environments
    • 11 — Shock and vibration: the fixture is part of the argument
    • 12 — Explosion proofness, icing and fire applicability
  • 04 — Power, EMC, lightning and ESD
    • 13 — Aircraft power: qualify the complete input path
    • 14 — EMC: emissions and susceptibility are different evidence
    • 15 — Lightning: connect equipment levels to the aircraft installation
    • 16 — Electrostatic discharge and accessible display surfaces
  • 05 — Installation and qualification planning
    • 17 — Installed display verification and human viewing conditions
    • 18 — Build the environmental qualification matrix
  • 06 — Contracts, changes and lifecycle
    • 19 — Specify the testing contract and supplier deliverables
    • 20 — Changes, anomalies, retests and qualification credit
    • 21 — Tests beyond DO-160 and the production boundary
  • 07 — Capstone, references and assessment
    • 22 — Capstone: plan qualification for a complete aircraft display
    • 23 — Reference shelf and practical worksheets
    • 24 — Knowledge check: apply the qualification principles 10 xp

16 — Electrostatic discharge and accessible display surfaces

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DO-160 Display Qualification | A-P02 — Draft / Not Released

Learning objective: Define Section 25 locations and monitor display and control responses.

Handheld ESD simulator beside a set-top box with accessible connectors.
An ESD simulator and a set-top box under test illustrate discharge equipment and an equipment interface. For an aircraft display, the specified procedure governs discharge points, method, voltage and repetition, while the team monitors image integrity and recovery. This photograph does not establish a DO-160 test configuration.
Image: Eeroalk · Baytems ESDzap and EUT · CC BY-SA 3.0. Source image retained unchanged; displayed at reduced size.

Start with what a person can touch

The display bezel, glass, controls and exposed conductive features can provide discharge paths. Define accessible locations under the installation assumptions. Touch sensing adds a second concern: the display may continue to show an image while issuing a false command or losing touch function. Monitor both the visual output and control outputs.

DO-160G Section 25 uses 15 kV air discharge, with ten positive and ten negative discharges at the selected accessible locations under its procedure. This is not a connector-pin injection test. The full method defines the setup, application and performance evaluation; use it for qualification rather than substituting an IEC contact-discharge procedure based on a similar headline voltage.

Representative construction

Include the production optical stack, coatings, bezel bonding, seals, cable interfaces and touch-controller firmware. A temporary grounded foil or bench earth lead may create a discharge path absent from the aircraft. Conversely, a fixture without the prescribed bond can create an artificial failure. Document both and assess their effects.

Define allowed consequences

If the required function must remain uninterrupted, a reset is not made acceptable by automatic recovery. If a requirement allows a defined temporary degradation, state its maximum duration, indication and recovery condition. Record image artifacts, false controls, link errors and latent effects as well as obvious resets.

Exercise

A display remains bright after discharge, but the touch output issues one unintended activation. Worked response: compare against the control-output and system-function criteria. The visual observation alone is insufficient. Preserve the stimulus timing and output event, investigate the path and retain both the original failure and any retest evidence.

Practical monitoring record

Map discharge locations to photographs or an identified drawing, record polarity and count, log operating mode, and retain functional observations with timing resolution. Document any location inaccessible in the installed state and the rationale for its treatment. Do not turn a test-location omission into an unstated limitation after the test.

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