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What is the Process for Re-certifying Flight Hardware?


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$begingroup$


I was reading about how we reused the water tanks because they were still within their certified life-time and had two questions:




  • When would a certification become VOID?


    • I'd assume if the water tanks accidentally took a fall they'd not be certified still.

    • What are some other examples of events that can void a certification?



  • When an event occurs altering the suitability of flight hardware how is it re-certified?


    • I'd assume there's some sort of inspection, could someone outline what it'd be?

    • You may use the example of the water tanks being dropped, what would NASA do?




You may also consider the toppled NOA satellite as a case study too if you wish. I'd like to know what all they had to do to consider it as "certified" again after the incident.










share|improve this question









$endgroup$

















    3












    $begingroup$


    I was reading about how we reused the water tanks because they were still within their certified life-time and had two questions:




    • When would a certification become VOID?


      • I'd assume if the water tanks accidentally took a fall they'd not be certified still.

      • What are some other examples of events that can void a certification?



    • When an event occurs altering the suitability of flight hardware how is it re-certified?


      • I'd assume there's some sort of inspection, could someone outline what it'd be?

      • You may use the example of the water tanks being dropped, what would NASA do?




    You may also consider the toppled NOA satellite as a case study too if you wish. I'd like to know what all they had to do to consider it as "certified" again after the incident.










    share|improve this question









    $endgroup$















      3












      3








      3





      $begingroup$


      I was reading about how we reused the water tanks because they were still within their certified life-time and had two questions:




      • When would a certification become VOID?


        • I'd assume if the water tanks accidentally took a fall they'd not be certified still.

        • What are some other examples of events that can void a certification?



      • When an event occurs altering the suitability of flight hardware how is it re-certified?


        • I'd assume there's some sort of inspection, could someone outline what it'd be?

        • You may use the example of the water tanks being dropped, what would NASA do?




      You may also consider the toppled NOA satellite as a case study too if you wish. I'd like to know what all they had to do to consider it as "certified" again after the incident.










      share|improve this question









      $endgroup$




      I was reading about how we reused the water tanks because they were still within their certified life-time and had two questions:




      • When would a certification become VOID?


        • I'd assume if the water tanks accidentally took a fall they'd not be certified still.

        • What are some other examples of events that can void a certification?



      • When an event occurs altering the suitability of flight hardware how is it re-certified?


        • I'd assume there's some sort of inspection, could someone outline what it'd be?

        • You may use the example of the water tanks being dropped, what would NASA do?




      You may also consider the toppled NOA satellite as a case study too if you wish. I'd like to know what all they had to do to consider it as "certified" again after the incident.







      reuse testing






      share|improve this question













      share|improve this question











      share|improve this question




      share|improve this question










      asked 9 hours ago









      Magic Octopus UrnMagic Octopus Urn

      3,49011550




      3,49011550






















          1 Answer
          1






          active

          oldest

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          6












          $begingroup$

          From what I've observed, the general process works like this:




          1. A Non-Conformance Report (NCR) is generated. These are applicable for everything from an unexpected scratch or tool mark on a surface to a system-level failure. The NCR identifies the "is" vs. "should be" state of a component.


          2. A Material Review Board (MRB) convenes. This is a group of engineers and managers who make decisions in a structured way regarding NCRs. From here, it's case-dependent. It may involve specific analysis, or it may just be a series of discussions. It all depends on the specific nonconformance.



          3. The NCR is dispositioned. Again, case dependent. The disposition is determined by the MRB. Typical disposition outcomes:





            • Use as is. Analysis shows the nonconformance does not affect safety or mission success -- no corrective action is necessary to certify the part for flight.


            • Rework the part. Case dependent. Could be as simple as redrilling a hole in the right location, buffing out scratches, etc.


            • Use as is, issue drawing rev. In the case of a misdrilled hole, for example, create a drawing rev showing where the hole was drilled so that there is traceability between the drawing and what was manufactured.


            • Scrap. The component is too far gone. Toss it out and build a new one. Depending on the source of the NCR, it may be a build to print, or there may be a redesign.








          share|improve this answer









          $endgroup$













          • $begingroup$
            +1, A couple of things to add: A) the MRB is usually given total authority over the future of the part and may direct the project office to examine, test, repair etc. B) there is usually a distinction drawn between "re-work" such as your first example and "repair" which is closer to your second example of buffing to remove a scratch. The difference lies in that "re-work" is re-application of the same processes used in the original build whereas "repair" uses additional (authorised) processes that were not needed for an original build.
            $endgroup$
            – Puffin
            5 hours ago












          Your Answer








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          1 Answer
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          active

          oldest

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          active

          oldest

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          6












          $begingroup$

          From what I've observed, the general process works like this:




          1. A Non-Conformance Report (NCR) is generated. These are applicable for everything from an unexpected scratch or tool mark on a surface to a system-level failure. The NCR identifies the "is" vs. "should be" state of a component.


          2. A Material Review Board (MRB) convenes. This is a group of engineers and managers who make decisions in a structured way regarding NCRs. From here, it's case-dependent. It may involve specific analysis, or it may just be a series of discussions. It all depends on the specific nonconformance.



          3. The NCR is dispositioned. Again, case dependent. The disposition is determined by the MRB. Typical disposition outcomes:





            • Use as is. Analysis shows the nonconformance does not affect safety or mission success -- no corrective action is necessary to certify the part for flight.


            • Rework the part. Case dependent. Could be as simple as redrilling a hole in the right location, buffing out scratches, etc.


            • Use as is, issue drawing rev. In the case of a misdrilled hole, for example, create a drawing rev showing where the hole was drilled so that there is traceability between the drawing and what was manufactured.


            • Scrap. The component is too far gone. Toss it out and build a new one. Depending on the source of the NCR, it may be a build to print, or there may be a redesign.








          share|improve this answer









          $endgroup$













          • $begingroup$
            +1, A couple of things to add: A) the MRB is usually given total authority over the future of the part and may direct the project office to examine, test, repair etc. B) there is usually a distinction drawn between "re-work" such as your first example and "repair" which is closer to your second example of buffing to remove a scratch. The difference lies in that "re-work" is re-application of the same processes used in the original build whereas "repair" uses additional (authorised) processes that were not needed for an original build.
            $endgroup$
            – Puffin
            5 hours ago
















          6












          $begingroup$

          From what I've observed, the general process works like this:




          1. A Non-Conformance Report (NCR) is generated. These are applicable for everything from an unexpected scratch or tool mark on a surface to a system-level failure. The NCR identifies the "is" vs. "should be" state of a component.


          2. A Material Review Board (MRB) convenes. This is a group of engineers and managers who make decisions in a structured way regarding NCRs. From here, it's case-dependent. It may involve specific analysis, or it may just be a series of discussions. It all depends on the specific nonconformance.



          3. The NCR is dispositioned. Again, case dependent. The disposition is determined by the MRB. Typical disposition outcomes:





            • Use as is. Analysis shows the nonconformance does not affect safety or mission success -- no corrective action is necessary to certify the part for flight.


            • Rework the part. Case dependent. Could be as simple as redrilling a hole in the right location, buffing out scratches, etc.


            • Use as is, issue drawing rev. In the case of a misdrilled hole, for example, create a drawing rev showing where the hole was drilled so that there is traceability between the drawing and what was manufactured.


            • Scrap. The component is too far gone. Toss it out and build a new one. Depending on the source of the NCR, it may be a build to print, or there may be a redesign.








          share|improve this answer









          $endgroup$













          • $begingroup$
            +1, A couple of things to add: A) the MRB is usually given total authority over the future of the part and may direct the project office to examine, test, repair etc. B) there is usually a distinction drawn between "re-work" such as your first example and "repair" which is closer to your second example of buffing to remove a scratch. The difference lies in that "re-work" is re-application of the same processes used in the original build whereas "repair" uses additional (authorised) processes that were not needed for an original build.
            $endgroup$
            – Puffin
            5 hours ago














          6












          6








          6





          $begingroup$

          From what I've observed, the general process works like this:




          1. A Non-Conformance Report (NCR) is generated. These are applicable for everything from an unexpected scratch or tool mark on a surface to a system-level failure. The NCR identifies the "is" vs. "should be" state of a component.


          2. A Material Review Board (MRB) convenes. This is a group of engineers and managers who make decisions in a structured way regarding NCRs. From here, it's case-dependent. It may involve specific analysis, or it may just be a series of discussions. It all depends on the specific nonconformance.



          3. The NCR is dispositioned. Again, case dependent. The disposition is determined by the MRB. Typical disposition outcomes:





            • Use as is. Analysis shows the nonconformance does not affect safety or mission success -- no corrective action is necessary to certify the part for flight.


            • Rework the part. Case dependent. Could be as simple as redrilling a hole in the right location, buffing out scratches, etc.


            • Use as is, issue drawing rev. In the case of a misdrilled hole, for example, create a drawing rev showing where the hole was drilled so that there is traceability between the drawing and what was manufactured.


            • Scrap. The component is too far gone. Toss it out and build a new one. Depending on the source of the NCR, it may be a build to print, or there may be a redesign.








          share|improve this answer









          $endgroup$



          From what I've observed, the general process works like this:




          1. A Non-Conformance Report (NCR) is generated. These are applicable for everything from an unexpected scratch or tool mark on a surface to a system-level failure. The NCR identifies the "is" vs. "should be" state of a component.


          2. A Material Review Board (MRB) convenes. This is a group of engineers and managers who make decisions in a structured way regarding NCRs. From here, it's case-dependent. It may involve specific analysis, or it may just be a series of discussions. It all depends on the specific nonconformance.



          3. The NCR is dispositioned. Again, case dependent. The disposition is determined by the MRB. Typical disposition outcomes:





            • Use as is. Analysis shows the nonconformance does not affect safety or mission success -- no corrective action is necessary to certify the part for flight.


            • Rework the part. Case dependent. Could be as simple as redrilling a hole in the right location, buffing out scratches, etc.


            • Use as is, issue drawing rev. In the case of a misdrilled hole, for example, create a drawing rev showing where the hole was drilled so that there is traceability between the drawing and what was manufactured.


            • Scrap. The component is too far gone. Toss it out and build a new one. Depending on the source of the NCR, it may be a build to print, or there may be a redesign.









          share|improve this answer












          share|improve this answer



          share|improve this answer










          answered 8 hours ago









          TristanTristan

          11.5k13858




          11.5k13858












          • $begingroup$
            +1, A couple of things to add: A) the MRB is usually given total authority over the future of the part and may direct the project office to examine, test, repair etc. B) there is usually a distinction drawn between "re-work" such as your first example and "repair" which is closer to your second example of buffing to remove a scratch. The difference lies in that "re-work" is re-application of the same processes used in the original build whereas "repair" uses additional (authorised) processes that were not needed for an original build.
            $endgroup$
            – Puffin
            5 hours ago


















          • $begingroup$
            +1, A couple of things to add: A) the MRB is usually given total authority over the future of the part and may direct the project office to examine, test, repair etc. B) there is usually a distinction drawn between "re-work" such as your first example and "repair" which is closer to your second example of buffing to remove a scratch. The difference lies in that "re-work" is re-application of the same processes used in the original build whereas "repair" uses additional (authorised) processes that were not needed for an original build.
            $endgroup$
            – Puffin
            5 hours ago
















          $begingroup$
          +1, A couple of things to add: A) the MRB is usually given total authority over the future of the part and may direct the project office to examine, test, repair etc. B) there is usually a distinction drawn between "re-work" such as your first example and "repair" which is closer to your second example of buffing to remove a scratch. The difference lies in that "re-work" is re-application of the same processes used in the original build whereas "repair" uses additional (authorised) processes that were not needed for an original build.
          $endgroup$
          – Puffin
          5 hours ago




          $begingroup$
          +1, A couple of things to add: A) the MRB is usually given total authority over the future of the part and may direct the project office to examine, test, repair etc. B) there is usually a distinction drawn between "re-work" such as your first example and "repair" which is closer to your second example of buffing to remove a scratch. The difference lies in that "re-work" is re-application of the same processes used in the original build whereas "repair" uses additional (authorised) processes that were not needed for an original build.
          $endgroup$
          – Puffin
          5 hours ago


















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