Hi All
Recently i had been asked to check the corrosion rate of Aluminium alloys from interaction with a few 'low use' solutions and compounds. While i couldnot find anything in handbooks, i moved on to research papers and books.... the past research (ie generation of corrosion data from these...
Hi All
i v been working on FLUENT for making CFD simulations with the pre-processing being done in Gridgen software.
At present i was using Gridgen V15. Although now the firm has shifted to Pointwise software, i was comfortable with the previous versions so didnot move
recently i had to...
we have an aircraft that is to be preserved for some time in future. it was depainted for inspection. It has presently been primed with MIL-23377 primer.
the aircraft will remain exposed to UVs and sunshine alongwith rest of environmental factors. i do know that a top coat will endure around 4...
hello all
we had to perform a repair onto the wing to fuselage attachment fitting. the repair is also a fitting and a splice, which has been to be machined out of 7075-T651 Aluminium. Post machining, shot-peening with ceramic media is to be performed with AZB-425.
The problem is...
I recently cam across test bench run requirements of t501, commercial equivalent of a famous t56 engine... it had mandated use of 'test club' prop and prop control for bench run of any engine used onto it....
further this 'test club' parts were also not to be used on aircrafts
to me it was...
Hello all.....
I am maintaining a fleet of five aircrafts. recently I have got a study to redefine the life of some of the components, based upon some occurrences we had in past few years... the aircraft has a very mature history and is being maintained under RCM analysis by USAF.
now I do...
does Dinitrol AV 30, CPC, has a life for which coating will remain effective without reapplication?
the publications dealing with preservation of A/Cs give lives of some of these CPCs, but not this one....
does any body has any reference regarding this?
During the refinishing of exterior of the A/C, after PDM (Major overhaul), damaged sealant on the seating of fillet panels was required to be refinished.… From past experience and as a standard practice, old sealant was required to be completely removed first and then new one was applied, since...
During the conduct of overhaul on our Aircraft, the manual asks for applicaton of Cadmium onto a (fowler type flap) track onto which the carriage assembly (supported by te rollers) will move on.... the process specified is MIL-STD-865D..... material of these track (which will be getting coated)...
During the conduct of overhaul on our Aircraft, the manual asks for applicaton of Cadmium onto a (flap) track onto which the carriage assembly (supported by te rollers) will move on.... the process specified is MIL-STD-865D..... material of these track (which will be getting coated) is 4340...
hello.... i have been working on flight lines in military as an aeropsce engineer for 3 1/2 years. now i v been sent to a depot level activity where suddenly the prority has been changed from systems to structures. though manuals give almost every thing to mos of the common solutions...
