EFTA02010116.pdf

Executive Aircraft Refinishing Inc. At OKEECHOBEE Air tort Proposal For: Treasure Coast Jet Center Att. Mr. Martin Mroczek Exterior Paint Date 4-7-13 1.0 Complete Basic Paint 1.01 Incoming Inspection The aircraft will be inspected upon arrival for evidence of damage. Particular attention will be given to the windows, flight controls and fuselage skin. Discrepancies• Executive Aircraft Refinishing will forward all discrepancies or squawks noted during the incoming inspection and during completion to the customer for direction, disposition, repair, replacement or exchange. On certain aircraft types, fuel leaks present a major problem to the refinishing process, in particular aircraft with wet wings. We recommend that the aircraft arrive with minimal fuel on board due to possible requirement of de fueling prior to new surface application. The de fueling process will be at the expense of the owner with prior approval. All approved work will be accomplished on a customer-approved quotation. When work is approved an estimate adjustment in the contract price and revised date shall be furnished to the customer 1.02 Paint Stripping Protective masking materials will be applied to the aircraft windows, windshield frame, composites and applicable flight controls. All openings will be sealed. The aircraft and controls will be stripped using chemical stripper. The aircraft will be rinsed with fresh water. Masking materials will then be removed. 1.03 Sanding The aircraft will be sanded as required to remove all paint and primer residue that was not removed by the stripper. Composite parts will be sanded as required. EXTERIOR PRICING INCLUDES: Removing not more than two coats of finish and two coats of primer. Additional charges will apply when stripping procedure indicates more than two coats of primer or paint exists. Fiberglass or sheet metal repair may also result in additional charges with customer's prior approval. 1.04 Composites Applicable composites (Fiberglass, Fairings. Inlet ducts, and Radomes) will be painted with anti static primer. A flexible epoxy primer will be applied over the black anti static primer. No warranty on composites because of the nature of parts cracking and manufactures primer not adhering. EFTA_R1_00511248 EFTA02010116 1.05 Flight Controls Prior to the aircraft being sanded the required flight controls and some slip fairings will be removed and processed separately from the aircraft. After final paint is applied controls will be balanced checked, reinstalled and operationally checked. Any worn hardware will be replaced at an additional cost to customer. 1.06 Conversion Coating Protective masking will be applied to proper areas and the aircraft will be wiped with etch, scrubbed, and neutralized with water. Alodine (Chromic Acid) will be applied, to treat skin for corrosion protection. Masking materials will be removed. 1.07 Primer Application Protective masking materials will be used to protect proper areas and the aircraft will be wiped down with a solvent cleaner. Epoxy corrosion protective primer is applied. Fill primer is applied to fuselage and tops of wings as needed for cosmetic appearances. 1.08 Top Coat Application The primer coat will be prepared and protective masking replaced as required. The aircraft will be blown off with high pressure dry air and wiped down with cleaning solvent. Two to three coats of high quality polyurethane aircraft coating will be applied. Note: One base color is included in standard price. 1.09 Landing Gear The landing gear struts, gear doors, and wheels will be prepared and sanded. Paint will be applied to wheels and landing gear unless otherwise specified. Wheel wells will be cleaned. Painting of wheel wells will be additional cost and will be quoted after inspection. 1.10 Design Layout The layout will be done using fine line tape. The layout will be done in accordance with customer supplied drawings and will be inspected by the project manager for final layout approval. 1.11 Anti Static Priming Certain aircraft will be anti static primed per Maintenance Manual Procedures, on bottom of fuselage and applicable areas. 1.12 Placards All operational exterior placards are silk screened and included in this quotation. Corporation LOGOS can be generated on premises and painted on the aircraft at the same time, on a time and material basis. 1.13 Antennas Antennas will be painted only at the customers request and will accept full responsibility for them. EFTA_R1_00511249 EFTA02010117 1.14 Final Detail A strip of black sealer is applied around cabin windows if approved by the customer. This provides a clean crisp edge. Windows will be cleaned and polished. A service manager will complete a final quality inspection prior to delivery. The aircraft will be cleaned, logbook entries completed and all documents will be checked on board. A touch up kit will be supplied. 1.15 Polishing All brite work will be polished to a high shine with high speed polishers after all the painting is complete. Any scratches or corrosion will be removed at an additional cost to customer, if approved, including time and materials. 1.16 Erosion Tape Erosion tape will be applied to the leading edges of antennas and leading edges as needed. Radome erosion boots are included in this quote. 1.17 Pre-flight Inspection Flight controls will be operationally checked, and a weight & balance will be performed if required at an additional cost of: N/A. 1.18 Stainless Steel Hardware Option N/A TOTAL EXTERIOR QUOTION SEE NOTE $129,800.00 A 50% DEPOSIT IS REQUIRED ON ARRIVAL WITH THE BALANCE DUE ON COMPLETION Plus tax if applicable TOTAL DOWNTIME WILL BE: 20 WORKING DAYS EXCLUDING HOLIDAYS Additional paint options are available per customer request. The job includes 8 hours ofcorrosion, fiberglass or body filler work; any additional hours are additional with prior customer approval. Note: Weight and balance not included in quote. This is an option if customer request and then will be quoted. A gear swing is also not included in quote. Note: RVSM mapping not included in quote. Accept: Customer Authorization Signature EFTA_R1_00511250 EFTA02010118