Skip to Content
FPD.DEV FPD.DEVThe Future of Display & Systems Development
  • Services
  • Products
  • Learning
  • Partners
  • Schedule Free Consultation
  • Sign in
  • 0
  • 0
FPD.DEV FPD.DEVThe Future of Display & Systems Development
  • 0
  • 0
    • Services
    • Products
    • Learning
    • Partners
  • Sign in
  • Schedule Free Consultation
  1. Courses
  2. DO-160 Display Qualification: Components, Systems and Installation
  3. 06 — Temperature and altitude: construct the procedure
Nav
Home └DO-160 Display Qualification: Components, Systems and Installation └06 — Temperature and altitude: construct the procedure
DO-160 Display Qualification: Components, Systems and Installation
0 %

Completed

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

06 — Temperature and altitude: construct the procedure

Prev Next
Fullscreen Share Forum

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

Learning objective: Separate conditioning, stabilization, exposure and functional evidence in Section 4.

Open laboratory heat and cold chamber with a test fixture inside.
An open heat/cold chamber containing a materials-test fixture. For a display test, the fixture, cabling, airflow and temperature measurement points must represent the specified test boundary.
Photo: Cjp24 · Environmental chamber-open · CC BY-SA 3.0. Original image, displayed at reduced size.

Translate the matrix into stages

A temperature procedure needs a chronological sequence and an acceptance matrix. Label unpowered survival, short-time operation and normal operation separately. For each stage specify chamber setpoint, tolerance from the adopted method, power state, required stabilization basis, timing origin, minimum duration, functions and measurements. Time spent approaching a setpoint does not automatically count as stabilized exposure.

In DO-160G the low/high operating tests include at least two hours of operation after equipment temperature stabilization; ground-survival conditions include at least three hours after stabilization. Applicable short-time operation is at least 30 minutes with its prescribed preceding conditioning. Use §§4.5.1–4.5.4 and the full profile to place these intervals correctly. Do not assemble a new sequence merely by joining the three durations.

Instrument the actual boundary

Chamber air, enclosure, LCD glass, backlight heat spreader and processor can have different temperatures. Choose thermocouple points that support the required stabilization and the allocated component limits. Do not let sensors or instrumentation wires alter a seal, cooling path or EMI arrangement without assessing their influence. Preserve raw temperature histories along with summarized dwell times.

Representative heat and cooling

Use installed mounting conduction, airflow and specified cooling interfaces. Establish modes that challenge the thermal design: maximum backlight, high graphics load, heater startup and combinations permitted by the design. A thermostatic heater may dominate a cold startup; a dim mode can still stress processing electronics. Loss-of-cooling subtests apply where required by the selected category and architecture; they are not assumed for every passively cooled display.

Worked discrepancy

The chamber reaches +70 °C at 09:00. The defined equipment stabilization condition is reached at 09:40. The log stops normal high-temperature operation at 11:00. Only 80 minutes follow stabilization, so this record does not demonstrate a two-hour post-stabilization requirement. Investigate the actual method, then extend or repeat as dispositioned. Do not relabel chamber arrival as equipment stabilization.

Procedure output

Prepare a stage table with columns for source paragraph, target, power, stabilization, start trigger, duration, measured functions and stop conditions. At altitude, include absolute pressure and pressure history. Section 4.6.1 requires at least two hours after stabilization, or the duty cycle if longer, under its specified conditions. Check combined temperature/altitude requirements explicitly rather than assuming an ambient-altitude test represents the hottest installation.

Selected A3 and F2 temperature ranges. Original plot of selected factual values; not the full category table. Source: DO-160G Table 4-1 and §4.3.
Selected A3 and F2 temperature ranges. Original plot of selected factual values; not the full category table. Source: DO-160G Table 4-1 and §4.3.
  • About
  • Comments (0)
Rating
0 0

There are no comments for now.

Join this Course
to be the first to leave a comment.

Prev Next

Subscribe to the FPD.DEV newsletter

Get display and embedded engineering articles, Edge AI insights, tool updates and product news by email.

Thanks for registering!

Subscribe

By subscribing, you agree to receive the FPD.DEV newsletter. You can unsubscribe at any time. See our Privacy Policy.


FPD.DEV
The Future of Display & Systems Development

  • Contact Us




  • Privacy Policy

 

 

Get in touch

Operated by Colabmo · Quality, operations & ERP support.


Cookie Policy

Copyright © 2026 Colabmo ​ ​
English (US) Español
Powered by Colabmo
Powered by Colabmo

Essential cookies support website functions. With your permission, Google Analytics measures visits and Microsoft Clarity records masked interactions, heatmaps and session replays on approved public pages. Optional embedded features may also contact their providers. These providers receive usage and device data; Microsoft may use data for its own purposes, including advertising. You can reject optional services and change your choice later. Cookie PolicyPrivacy Policy

Allow all optional cookies Only essential cookiesManage choices