Specifications include, but are not limited to: 1. Cover material must red in color and meet the following specs. a. CCC-A-680a (Federal Standard 191A Test Method 5903) b. FAA Aircraft Upholstery Requirement FAR 25.853 c. Federal Automotive Upholstery Requirement MVSS-302 d. BIFMA (Screen Test-Sec. 3.3.1) Voluntary Std. e. Oil and mildew resistant as per CCC-A-680a f. Anti-static slip finish g. -20° cold crack h. Wyzenbeek abrasion test (Federal Standard 191A, Method 5304) 2. The cover must be form fitted to the engine nacelle. A. Awarded bidder will work with UND aerospace as needed to modify engine cover as needed to ensure proper fit at no additional cost. B. See attached photos for location of snaps on the engine cowling/nacelle
