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Thanks MNLiaison, Interesting links. Thx to rb1957 too.

Hello everyone! Does anybody know if exists a similar advisory circular to AC23-13a for large A/C also? Thx.

Actually this has not to do with the proof of any strength analysis. According to our procedures the pressure test is required after the fuselage assembly during production and after big repairs or additional window/viewport cut outs. Unfortunately this test requires special equipment...

Hi everyone, Does anybody have experience in performing a structural pressure test (not a simple leakage test) after fuselage skin repair (500x500 mm doubler)? Shall I really take care of it? Is it sufficient to reach the pressure relief valve setting? Does anybody have guidelines or procedures...

NoJack, ...and RAPID for commuter. Part 5/5 http://files.engineering.com/getfile.aspx?folder=f091c12a-5646-4bef-8486-d8c401dc4fc7&file=vers_2_-_For_Commuter.part5.rar

NoJack, ...and RAPID for commuter. Part 4/5 http://files.engineering.com/getfile.aspx?folder=0d2d3ea9-f6ec-462c-9b0f-5e75bb0b6101&file=vers_2_-_For_Commuter.part4.rar

NoJack, ...and RAPID for commuter. Part 3/5http://files.engineering.com/getfile.aspx?folder=12f12405-0a6d-446d-9b5d-5ddf2182aeb4&file=vers_2_-_For_Commuter.part3.rar

NoJack, ...and RAPID for commuter. Part 2/5http://files.engineering.com/getfile.aspx?folder=bc8f1096-8c8a-4478-b358-e12092e56ccd&file=vers_2_-_For_Commuter.part2.rar

NoJack, ...and RAPID for commuter. Part 1/5http://files.engineering.com/getfile.aspx?folder=d463069c-9fa8-4e4f-9620-ce548a39be22&file=vers_2_-_For_Commuter.part1.rar

NoJack, There you go. Part. 3 end.http://files.engineering.com/getfile.aspx?folder=a42edf18-bdfc-4146-9a8e-0d4f0c787af5&file=vers_3_-_For_Transport.part3.rar

NoJack, There you go. Part. 1http://files.engineering.com/getfile.aspx?folder=f14ae7f7-8510-4c02-bd1f-feb1b3fc273f&file=vers_3_-_For_Transport.part1.rar

NoJack, There you go. Part. 2http://files.engineering.com/getfile.aspx?folder=5155dc39-bd18-4ef3-a8a7-1e7b4a68680b&file=vers_3_-_For_Transport.part2.rar

Hi NotJack, Yes, you are right. FAA is not giving any support to this software anymore. A couple of years ago I was interested in this program too and after a while I was able to contact one of the program developers who provide me the download file. Unfortunately, i.a.w. the forum policy, I...

Thanks rb1957, do you take into account if the part is classified critical (or not) for your evaluation? (Definition of critical part: A critical part is a part, the failure of which could have a catastrophic effect upon the A/C, and for which critical characteristics have been identified which...

Hi guys, Can anybody help me to understand how can I classify a repair? I mean, which variables do I have to consider to come to a major or minor repair for critical or not critical parts. Is a repair on critical parts always a major repair? I appreciate your feedback, Cheers, D.

Dear all, Thanks a lot for your support. Actually I am dealing with a component that is made of magnesium-casting and afterwards milled to the final geometry. The production procedure requires dye penetrant inspection after the milling, but this procedure is not very clear in defining the...

Good day guys, Do you know if there is a std definition of crack? I have heard that in NDT there is a crack when the length of the defect is three times more than its width. Unfortunately I have not found any document stating that. Thanks, D.

At first glance, it would seem logical to spin up the tires prior to touch-down to alleviate tire wear and spin-up loads. Several methods have been devised to do this, and some have been tested with various degrees of success. One method uses an electric motor and another uses fan-like blades on...

Thanks guys! Debodine, what kind of load and entity do you consider for the interiors?

Hi guys, does anyone know something about "abuse loads"? Can you suggest me some references or give me some tips how to quantify them? Thanks!