Rtca do - 160c

For system and hardware engineers, the intent is to educate and empower them to develop equipment designs that are compliant with DO by design, and avoid expensive redesigns to correct issues found late in the development cycle during test. This document outlines a set of minimal standard environmental test conditions categories and corresponding test procedures for airborne equipment for the entire spectrum of aircraft from light general aviation aircraft and helicopters through the jumbo jets and supersonic transport categories of aircraft. This page was last edited on 17 October , at This test determines whether the equipment interconnect circuit configuration will accept a level of induced voltages caused by the installation environment.

Uploader: Arashilkree
Date Added: 25 September 2013
File Size: 37.26 Mb
Operating Systems: Windows NT/2000/XP/2003/2003/7/8/10 MacOS 10/X
Downloads: 39386
Price: Free* [*Free Regsitration Required]





This test determines whether the equipment interconnect circuit configuration will accept a level of induced voltages caused by the installation environment. Typically moisture sensitive devices have issues with this test and require conformal coat or other types of protection. Condensation also can be a factor coming from cold temperatures.

Retaliation is also prohibited by university policy. The standard environmental test conditions and test procedures contained within the standard, may be used in conjunction with applicable equipment performance standards, as a minimum specification under environmental conditions, which can ensure an adequate degree of confidence in performance during use aboard an air vehicle. If you do not have a 160 with a password, click "create a profile".

Factors tested include dielectric strengthcooling under low pressure, and resilience to rapid change in air pressure. These tests subject the unit to an environment of blowing sand and dust of specific particle sizes in which the unit must operate at the end of exposures. This fo verifies the test articles ability to survive multiple exposures of salt fog and drying and the environment's ability to cause accelerated corrosion.

All information presented is for general reference and does not represent a professional opinion nor the policy of an author's employer. Think about it- will my inexpensive, low grade monitor render a specific shade of orange exactly the same as your high priced, high definition monitor?

Direct and indirect effects depending on mounting location; includes induced transients into the airframe or wire bundle. Input power conducted emissions and susceptibility, transients, drop-outs and hold-up.

To receive the federal employee discount, you must enter the code FGVT during the checkout process. Due to the variety of aircraft, the equipment are classified in categories.

Purpose,Testing and Design Considerations - online. Send them an e-mail and ask. These tests subject the test article to various scenarios of dripping water or pooled water to verify the unit will fully operate in the given condition.

Info about FED STD and RTCA DO C

The purpose of these tests is to provide a controlled laboratory means of assuring the performance characteristics of airborne equipment in environmental conditions similar of those which may be encountered in di operation of the equipment. This section relates specifically to interfering signals related to the power frequency and its harmonics, audio frequency signals, and electrical transients that are generated by other on-board equipment or systems and coupled to sensitive circuits within the EUT through its interconnecting wiring.

Continue shopping to register for the course and session of your choice. We also provide a high-level, step-by-step guide through the test procedure and design considerations for passing the test.

This aircraft type dependent test checks the effects of mechanical shock. The direct web address is http: This page was last edited on 17 Octoberat The following persons have been designated to handle inquiries regarding the nondiscrimination policies and are the Title IX coordinators for their respective campuses: So if the color standards were published on the web, they would only cause anarchy- for noone could be sure what color Orange was.

Aviation related fluids susceptibility including a variety of fluids ranging from carbonated sugared beverage to various cleaners and solvents. Overland Park, KS kupce ku. The norm defines the different temperature profiles under which the equipment must be tested.

Info about FED STD 595 and RTCA DO 160C

You'll notice they don't seem to offer the old revision, but still you might be able to BUY it from them. The C rev was only current from until In any event, I found out these things with just a couple of words typed into Google, and a few quick clicks. Aircraft type dependent test checks the effects of vibration and the equipment's ability to operate during all vibration scenarios.

These fo components are normally harmonically related to the power source fundamental frequency.

2 thoughts on “Rtca do - 160c”

Leave a Reply

Your email address will not be published. Required fields are marked *