Humidity – RTCA DO-160

What Is Humidity — RTCA DO-160?

This test is carried out to evaluate the equipment in high relative humidity conditions within the scope of Chapter 6 (“Humidity”) of the RTCA DO-160 “Environmental Conditions and Test Procedures for Airborne Equipment” standard. DO-160 is the exact same text as EUROCAE ED-14 and is recognized by ISO as ISO 7137.

Purpose of Humidity — RTCA DO-160

The aim is to certify that aviation equipment meets the requirements for evaluation of equipment in high relative humidity conditions in flight and ground conditions and to complete equipment qualification.

Which Products Is Humidity — RTCA DO-160 Applied To?

Avionics units and displays
In-flight electronic equipment
Communication and navigation devices
Cabin and cargo compartment equipment
Sensors and actuators

In Which Sectors Is Humidity — RTCA DO-160 Used?

AutomotiveElectric VehicleBatteryPlasticsRubber

Standards Related to Humidity — RTCA DO-160

RTCA DO-160Environmental conditions and test methods in aviation equipment test

Humidity — RTCA DO-160 Conditions

Kategoriler: A (standard humidity), B (severe humidity), C
Cycle: Temperature and humidity cycles; number of days by category
Relative humidity: High humidity levels defined in the standard
Function check: At the end of the cycle and, if necessary, in the cycle

Equipment for Humidity — RTCA DO-160

Temperature-humidity chamber
Insulation resistance measuring instrument
Function monitoring

Sample Requirements for Humidity — RTCA DO-160

Category must be defined
Initial insulation resistance should be measured
Condensation management should be planned

Duration of Humidity — RTCA DO-160

It depends on the category; The severe humidity category may exceed ten days.

Humidity — RTCA DO-160 Procedure

1The category and cycle program are determined.
2The specimen is placed in the chamber.
3Temperature-humidity cycles are applied.
4At the end of the cycle, function and insulation are measured.
5A visual inspection is performed.

Humidity — RTCA DO-160 Acceptance Criteria

The acceptance criteria are that the function continues, the insulation resistance meets the limit and there is no corrosion.

Evaluation of Results

Moisture ingress usually occurs at connector and housing junctions.

Humidity — RTCA DO-160 Report

Applied standard, revision and Chapter 6
Selected equipment category and justification
Applied conditions and measurement results
Function monitoring method and observations
Environmental Qualification Form (DO-160 Environmental Qualification Form) entry

Accreditation

EUROLAB holds internationally recognised accreditation obtained from accreditation bodies party to the IAF and ILAC multilateral recognition arrangements, under ISO/IEC 17025 for laboratory testing, ISO/IEC 17020 for inspection and surveillance, and ISO/IEC 17021-1 and ISO/IEC 17065 for system and product certification. This chain ensures the reports and certificates issued are accepted worldwide.

Whether this test can be offered within accredited scope depends on your product and the standard applied; since accreditation is method-based, the scope is confirmed in writing at the quotation stage.

Scope and authorisations

Related Regulations

Aviation equipment qualification requirements
EASA/FAA certification principles

Otomotiv Testleri — What Does This Testing Field Cover?

The section below describes the field that the Humidity test belongs to; the conditions and acceptance criteria of this particular test are given in the sections above. The scope specific to your product is confirmed in writing at the quotation stage.

Automotive testing shows that a component keeps working under conditions representing the loads it will meet over the life of the vehicle. A vehicle is not a single product but an ENVIRONMENT: vibration, temperature cycling, salt water, stone impact, electrical transients and electromagnetic noise are all present at the same time and for years.

What distinguishes this family is that VEHICLE MANUFACTURER SPECIFICATIONS sit on top of the standards. ISO and SAE publications establish the common ground; but Volkswagen, BMW, Ford, Stellantis, Toyota and Renault define different severity levels, additional tests and different acceptance criteria in their own specifications. For a component, the phrase "complies with automotive standards" is not sufficient on its own; which manufacturer's specification, and which revision of it, must be answered.

The family carries three separate processes together and they are often confused. Homologation covers the type approvals a vehicle needs to enter traffic and runs under state authority. Supplier approval means passing the vehicle manufacturer's own quality and testing requirements and is a commercial relationship. The third is design verification: the engineering team demonstrating that its own design meets its targets.

At component level the test plan is built around the LOCATION OF USE. A module in the engine bay and a module in the boot do not go through the same temperature and vibration profile; a component inside a door and one in the roof console do not see the same water and dust exposure. The ISO 16750 series is the common framework for this location-based approach.

The shift to electric vehicles has reshaped the field. High-voltage safety, insulation coordination, battery safety, charging interface conformity and the electromagnetic behaviour of high-voltage components have been added to the classical automotive test set. In a quiet vehicle, acoustic and vibration expectations have changed too; sounds once masked by the combustion engine are now audible.

The quality system side cannot be separated from testing in this field. A manufacturer under IATF 16949 presents test results in the PPAP file; measurement system analysis, process capability study and the control plan stand around the test report. A single good result is not enough — the process must be shown to be able to repeat it.

Method groups in this field

Environmental and climatic
Temperature cycling, thermal shock, damp heat, salt spray, dust and water ingress (IP), solar radiation. Severity levels vary with the mounting location.
Mechanical
Sine and random vibration, shock, mechanical loads, fastener torque and durability cycles.
Electrical
Supply voltage variations, transients (ISO 7637), reverse polarity, overvoltage, short circuit and sleep current measurements.
EMC
Component emissions (CISPR 25), radiated and conducted immunity (ISO 11452 series), electrostatic discharge (ISO 10605).
Materials and emissions
Odour, fogging and VOC emissions from interior materials; flammability; UV ageing; coating durability and stone impact.
Functional safety and cyber security
Functional safety evidence under ISO 26262 and cyber security engineering under ISO/SAE 21434; these are tied to regulation through UNECE R155 and R156.

Commonly confused in this field

An automotive report without a specification reference is not accepted in the supply chain; which OEM specification and revision was applied must be stated.
Type approval and supplier approval are different processes. A component with E-Mark approval is not thereby considered to have passed the OEM's own acceptance tests.
A result obtained on a prototype does not carry over to series production; PPAP is done with series production parts.
On the EMC side, measuring emissions alone is incomplete; immunity is a separate body of work and is more critical in a vehicle.
On electric vehicle components, high-voltage safety is a distinct competence; classical 12 V test infrastructure is not sufficient.

Which decisions these results support

Supplier component approval and the PPAP file
UNECE type approval and E-Mark marking
Design verification and durability evidence
Root cause analysis of field complaints and warranty returns
Assessing the impact of a design or supplier change

Related Tests

Frequently Asked Questions About Humidity — RTCA DO-160

How is the equipment category determined?

The category is selected based on the equipment's mounting location on the aircraft (pressurized/non-pressurized, heated/unheated area) and aircraft type. Category selection directly determines the test conditions and is declared in the qualification form.

Is there any difference between DO-160 and ED-14?

No. RTCA DO-160 and EUROCAE ED-14 are exactly the same text; the two are considered equivalent.