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Please, can someone forward me here the Lockheed SB 82-788 regarding EBH (Equivalent Base Hours)?, or explain me how is it calculated? Thank you a lot.

You are guessing right rb1957, and I agree with you about the permanent deformation. It would be towed with a Hobart. Thank you for your advices.

I´m asking about the Fokker F28 cargo. Meanwhile I´m waiting for the maintenance manuals I forward my question. Is there any limitation to move the aircraft with the large left forward cargo door removed? Thank you in advance.

In our case, talking about some years ago, the dimensionless drawings were used without specific tolerances, we used 0,2 mm as general tolerance. The drawings were on Mylar, and had two crosses that were supposed to be inside a tolerance of +- 0,1 mm for a 1000 mm distance. These mylars were...

johnSchwaner, thank you for your priceless information.

"best before date" - Shelf life (acceptance life) is 8 years per AS 1933 revision A. (replaces MIL-STD-1523). Your aerospace supplier will not ship hose product beyond this date. Thank you for your kind answer johnSchwaner! So if I have those 303-6 new hoses kept in good closed conditions, but...

Hi all. I will paint the scene. Always the same issue with those hoses. Assume I have a hose ( Aeroquip 303) continously submerged in aircraft 100-130 fuel tank, no pressure. Many aircrafts. The access to it is fairly tricky. During an overhaul I change it with a new one, normal. Which should be...

see thishttp://files.engineering.com/getfile.aspx?folder=296be09e-204b-4b91-8cf8-2a23d5228167&file=19930082303_1993082303_airfoil66_TN1633.pdf

Don´t know what happpens, I couldn´t post the installer, the uploading is interrupted even whith Rapidshare. I´m sorry. I hope you can do it with the other address you mention.

this is a trial, I hope it works.http://files.engineering.com/getfile.aspx?folder=d3f6974a-4f54-4448-b5de-51d1752045dd&file=Rapid.exe

PolySim, Don´t think I´m didn´t pay attention to your request. I have RapidC and trying to find the way to send it to you.

Last year there was a code named RAPID, and RAPID 2besides other things, to do some works with antena holes in fuselages. I found it in FAA web page, don´t know if it´s still there.

you are right rb1957 about the other side. I was worried about the front rear lower spar cap and didn´t realize about the other hand spar. Thank you very much.

The stressed area is close to the rear landing gear fitting and it is "common" to this type of aircraft. I will try also opinions from the OEM. We are performing a SB from the manufacturer, but it doesn´t make mention about the other parts or the other side undamaged spar. This lighted on my...

thank you all for your answers. rb1957: if I do understand correctly, I should change the rear spar cap of both wings, that´s right?, it has sense. The manufacturer says change the complete spar assembly, where you find damage. The lower skin shows no damage but the reinforcement union band...

Suppose during maintenance tasks you find the rear lower spar cap angle with a crack due to fatigue. Is it normal practice to change both, front and rear lower cap angles, or change only the rear damaged angle?. Thank you

Thank´s to all of you for the great info. der8110, you actually gave me the information I was looking for!!

Can anyone out there explain me please how you use the SMF (Spectrum or Stress Magnification Factor) of Afgrow?. I´m new about this subject and don´t know how to use it and what value to assign to any model. Thanks a lot in advance.