From: Jeffrey Epstein <[email protected]> Sent: Wednesday, November 27, 2013 3:17 PM To: Larry Cc: Eric Roth; Jay Massar Subject: Re: RE: in addition now that we changed to led cockpit from tubes = the electric draw shoudl be much less. On Wed, Nov 27, 2013 at 11:01 AM, Lar=y «mailto: > wrote: Eric I will=look in my Palm Beach office again, Not every aircraft of this vintage has=its load analysis binder, Green aircraft and Newer Generation builds may h=ve this book. I gave all me wiring books / Log boods to Tom and Jay at the start =f this project, currently the wiring diagrams are in AFt lavatory closet i= the GIV, if the load analysis book exists, I would image its still at =Jl, If this engineer relayed to you that our aircraft is power limited, ho= did he come to this conclusion if he does not possess the Load Analysis o= our GIV? IF he personally located the cabin converters, (24vdc to 110vac)=and made note of their power AMP limits, would be his only way of determin=ng our load limits. Most engineers will provide the load analysis with the=e research when taking on a project., To my knowledge, I have not seen thi= book yet. when i return to Palm beach, I will search harder, I have 10=boxes of records, most history CMP cards,. thx Larry Sent from my iPad On Nov 27, 2013, at =0:07 AM, Eric Roth < Jeffrey- <mailto > wrote: I am waiting for my engineer t= reply back to me as just came back last night from Europe. I will hopeful=y find out today (based upon if he retained his notes from the preliminary=system discussions). You have dedicated 110vAC power =n the aircraft that supports the L/H galley microwave, the R/H galley coff=e maker and various outlets in the main cabin that are generally used for =ow consumption electronics , such as phone chargers, lap tops and other sm=II personal electronic devices. I recognize that you are frustra=ed, but this information is easily identified and found in the aircraft'. Electrical Load