3
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12
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3 Comments
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4
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DO-254 requires Validation in addition to Verification, whereas DO-178 requires just Verification (u...
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58
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1 Comments
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Because of the strict guidelines of chapter 6.2 Verification Process, designers are faced with sever...
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174
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The FHA identifies and classifies potential failure conditions associated with the various aircraft ...
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216
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Requirements verification of the final FPGA design is an important of part of development activity.&...
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175
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Although the guidance specifically provides for strengthening of the exception of CPUs, it does not ...
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124
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In a word -- no. In fact, whenever someone says any programmable part is simple the discu...
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164
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We receive almost daily questions about "What is DO-254 Quality Assurance?" and "What...
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302
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We are often asked "What goes in a PHAC, the DO-254 Plan For Hardware Aspects o...
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201
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0 Comments
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For years we've been asked "Is there a commercial tool or product available which helps me mana...
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185
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The following is an excerpt from Vance Hilderman's Avionics System Safety Assessment whitepaper avai...
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187
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The following is an excerpt from Vance Hilderman's "...
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335
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2 Comments
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•What is the purpose of AC 20-152?
–FAA recognition of RTCA/DO-254 as an acce...
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354
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DO-254 was written under the premise that avionics hardware logic would be custom developed, from th...
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438
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1 Comments
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The attached provides great information on the Simple and Complex Electronic Hardware....
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343
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1 Comments
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The FAA is conducting research on verification coverage analysis for DO-254. Please see the attach...
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1798
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5 Comments
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DO-254: Simple Versus Complex? This is a major issue, as DO-254 is greatly simplified&nb...
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1171
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4 Comments
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We receive many questions about DO-254 Tool Qualification versus that required for DO-178B Tool Qual...
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1184
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No. MCDC coverage (or structural coverage is not required for DO254). However an alternate means nee...
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1392
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1 Comments
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Simply, doing too much work ($), and neglecting key artifacts/steps, cause cost overruns averaging 4...
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2237
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4 Comments
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DO-254 (also known as DO254, D0254 and Eurocae ED-80) is a formal avionics standard which provides g...
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1478
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DO-254 Verification is a key component of DO254 certification. However, there are two main challenge...
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1335
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This HighRely whitepaper describes the 13 most common DO-254 mistakes and how you can avoid each of ...
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1520
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4 Comments
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Certifying hardware to the RTCA DO-254 avionics standard typically increases development costs by 10...
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1346
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1 Comments
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The D0-254 airborne electronic hardware development guidance document is the counterpart to the well...
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1175
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The U.S. and foreign militaries have adopted D0178B and D0254 certifiability and compliance. Some re...
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