DUNCAN AVIATION PROPOSAL Number 2013.00340 -001 3701 Aviation Rd Lincoln, NE 68524 800.228.4277 Fax: 402.475.5541 15745 South Airport Rd Battle Creek, MI 49015 800.525.2376 Fax: 269.969.8489 To: Mr. Larry Visoski Hyperion Air 3800 SOUTHERN BLVD #204 SUITE 204 WEST PALM BEACH, FL 33406 1 (302) 998-0592 Fax: Make, Model. Serial Gulfstream G-IV Registration Date 24 Jan 2013 Quoted By George Bajo - Battle Creek PAINT REFURBISHMENT 1.00 Duncan Aviation Complete Paint Specifications- DIV/SP (2013) Incoming Inspection The aircraft will be inspected upon arrival for evidence of damage or discrepancies. Particular attention will be given to the windows, flight controls, fuselage skin, boots and polished leading edges. If discrepancies are found, the customer will be notified for approval to repair or defer. Paint Stripping Protective masking materials will be applied to the aircraft to protect sensitive areas such as windows, composites, and leading edges. All openings will be sealed. The aircraft will be stripped using an approved Non-Hap's stripper and then rinsed with heated fresh water. Masking materials will be removed. NOTE: A MIL thickness check will be completed upon input of the aircraft into paint. If the existing MIL thickness is greater than 10 MIL's additional labor and stripper will be required to completely strip the aircraft. Any additional labor or stripper required will be submitted via a Change Order for customer approval. Due to new EPA restrictions, stripper materials are limited to Non-HAP (Hazardous Air Pollutant) strippers. Sanding The aircraft will be sanded as required to remove all paint or primer residue not removed by stripping. Composites Applicable composites will be sanded down to the original base primer, painted with a anti-static primer, and then sanded and prepped for top coat application. NOTE: Existing cracks in composite surfaces will eventually transfer through the paint finish. Du