EFTA02503476.pdf

From: Larry Visoski a Sent: Saturday, March 17, 2018 2:00 AM To: Je vacation Cc: Rich Kahn Subject: Fwd: N120.1E GIV entrance veneer Pete and I had cabin crafters from Teterbor= give a quote in reference to the entrance veneer and Aft side cabin door o= the GIV 1-Plane Perfect interior in PBI quoted $23k for entra=ce Venere forward and aft and aft side of cabin door, new veneer., 2-Cabin craters quoted $20,060.98 for entrance Venere=forward and aft only, they quoted to install a chrome metal plate around th= door handle, they did not quote veneer on the aft side of c=binet door as I requested. 3-need quote from Eric R=th if you elect to have him work the GIV veneer., = week lead time for the veneer according to Cabin Crafters in Teterboro.&nb=p; Sent from my iPhone Begin forwarded message: =b>From: Pete Rawson Date: March 16, 2018 at 9:38:20 PM=EDT To: Subject: Pete Rawson Chief Inspector Meridian Jet Center Begin forwarded message: From: Wendy Date: March 16, 2018 at 2:20:44 PM EDT To: "Pete Rawson Subject: N1201E EFTA_R1_01632285 EFTA02503476  Good afternoon Pete, Please find below estimate; give me a call with any q=estions. FWD and AFT MED Bulkheads =/span> * &nbs=; Remove the FWD and AFT MED bulkheads. * &nbs=; Disassemble the Components, remove all Hardware (Latches, Hinges, and=Tracks etc.) from Woodwork and retain for re-use. All components will=be inspected. Any Hardware Damage will be reported to the Customer prior to repairing o= replacement. All repairs or replacement will be performed on a "Time and Mater=al" basis. * &nbs=; Strip and remove existing veneer and replace with new. Q The veneer will be stained to match existing veneer in a/c using a cu=tomer-approved color. (NOTE: CCI CANNOT guarantee that new veneer will be an e=act match in grain or color to existing veneer. Woodwork is a natural mater=al and has variances in both grain configuration and stain acceptance. = Wood is susceptible to change over time prompted by exposure to light, heat and other elements.) * &nbs=; Re-finish all surfaces using a polyurethane high-build controlled met=od. Final coat will be gloss finish. * &nbs=; Re-assemble all components and re-install all removed hardware. = * &nbs=; Re-install the bulkheads. =o:p> Estimated Labor &nb=p; $ 15,440.00 Estimated Material &=bsp; $ 3,720.96 Certification &n=sp; 4 900.00 TOTAL &n=sp; =nbsp; $ 20,060.96 =o:p> =o:p> 2 EFTA_R1_01632286 EFTA02503477  Cabin Door • &nbs=; Remove the cabin door. • &nbs=; Fabricate and install an aluminum plate to conceal damaged veneer aro=nd door knob. * &nbs=; Re-assemble door and re-install door knob. * &nbs=; Re-install door. =o:p> Estimated Labor and Material &nb=p; $ 902.00 SCHEDULING We will offer a turn t=me to meet your individual needs and will be ready to work around the Aircr=ft Flight Schedule. We estimate a lead-time of "2 WEEKS" will be required to order and receiv= materials, prepare our shops and prepare related documentation at this tin-I.. Final parts lead-time will be confirmed upon our receipt of a signe= proposal. DOWNTIME=/b> We will require a total of "10 Working Days" from the scheduled start dat= to accomplish the work as defined in this proposal. </=pan> =o:p> =/p> Wendy Pimentel Sales Manager 3 EFTA_R1_01632287 EFTA02503478 ISO 9001:2015 and AS9100D Certif=ed 4 EFTA_R1_01632288 EFTA02503479