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08-31-2010 by DO-254 Blogger DO-254 Wish-List
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3 Comments
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08-30-2010 by Tony Baghai HighRely, Inc.
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DO-254 requires Validation in addition to Verification, whereas DO-178 requires just Verification (u...
08-28-2010 by Vance Hilderman HighRely, Inc.
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1 Comments
Because of the strict guidelines of chapter 6.2 Verification Process, designers are faced with sever...
08-06-2010 by Louie De Luna Aldec
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The FHA identifies and classifies potential failure conditions associated with the various aircraft ...
10-25-2009 by Tony Baghai HighRely, Inc.
216
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Requirements verification of the final FPGA design is an important of part of development activity.&...
10-25-2009 by Tony Baghai HighRely, Inc.
175
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Although the guidance specifically provides for strengthening of the exception of CPUs, it does not ...
10-23-2009 by Tony Baghai HighRely, Inc.
124
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In a word -- no.  In fact, whenever someone says any programmable part is simple the discu...
10-23-2009 by Tony Baghai HighRely, Inc.
164
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We receive almost daily questions about "What is DO-254 Quality Assurance?" and "What...
10-21-2009 by Vance Hilderman HighRely, Inc.
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    We are often asked "What goes in a PHAC, the DO-254 Plan For Hardware Aspects o...
07-17-2009 by Vance Hilderman HighRely, Inc.
201
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For years we've been asked "Is there a commercial tool or product available which helps me mana...
07-14-2009 by Vance Hilderman HighRely, Inc.
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The following is an excerpt from Vance Hilderman's Avionics System Safety Assessment whitepaper avai...
07-14-2009 by Vance Hilderman HighRely, Inc.
187
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The following is an excerpt from Vance Hilderman's "...
07-14-2009 by Vance Hilderman HighRely, Inc.
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2 Comments
  •What is the purpose of AC 20-152? –FAA recognition of RTCA/DO-254 as an acce...
02-05-2009 by Tony Baghai HighRely, Inc.
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DO-254 was written under the premise that avionics hardware logic would be custom developed, from th...
01-22-2009 by Vance Hilderman HighRely, Inc.
438
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1 Comments
The attached provides great information on the Simple and Complex Electronic Hardware....
07-22-2008 by Tony Baghai HighRely, Inc.
343
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1 Comments
The FAA is conducting research on verification coverage analysis for DO-254. Please see the attach...
07-18-2008 by Tony Baghai HighRely, Inc.
1798
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5 Comments
DO-254:  Simple Versus Complex?  This is a major issue, as DO-254 is greatly simplified&nb...
05-08-2008 by Vance Hilderman HighRely, Inc.
1171
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4 Comments
We receive many questions about DO-254 Tool Qualification versus that required for DO-178B Tool Qual...
05-08-2008 by Vance Hilderman HighRely, Inc.
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No. MCDC coverage (or structural coverage is not required for DO254). However an alternate means nee...
05-08-2008 by Tony Baghai HighRely, Inc.
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Simply, doing too much work ($), and neglecting key artifacts/steps, cause cost overruns averaging 4...
05-08-2008 by Reza Madjidi HighRely, Inc.
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4 Comments
DO-254 (also known as DO254, D0254 and Eurocae ED-80) is a formal avionics standard which provides g...
05-08-2008 by Reza Madjidi HighRely, Inc.
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DO-254 Verification is a key component of DO254 certification. However, there are two main challenge...
05-08-2008 by Reza Madjidi HighRely, Inc.
1335
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This HighRely whitepaper describes the 13 most common DO-254 mistakes and how you can avoid each of ...
05-08-2008 by Reza Madjidi HighRely, Inc.
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4 Comments
Certifying hardware to the RTCA DO-254 avionics standard typically increases development costs by 10...
05-08-2008 by Reza Madjidi HighRely, Inc.
1346
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1 Comments
The D0-254 airborne electronic hardware development guidance document is the counterpart to the well...
05-08-2008 by Reza Madjidi HighRely, Inc.
1175
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The U.S. and foreign militaries have adopted D0178B and D0254 certifiability and compliance. Some re...
05-08-2008 by Reza Madjidi HighRely, Inc.
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