Computer Testing Supplement for Inspection Authorization|FAA-CT-8080-8DSection IIIEXHIBITS70 Pages|Pages 3-1–3-70 ContentsRead Citation (on FlightPush)Copy CitationSave to Flight BagShow Page NumbersExhibit 1—Rivet requirement and part number breakdownExhibit 2—Aircraft rivet identificationExhibit 3—Aircraft rivet identification (continued)Exhibit 4—Rivet requirement chart for bare and clad alloysExhibit 5—Rivet requirement chart for ALCLAD alloysExhibit 6—Rivet requirement chart for 5052 alloysExhibit 7—Recommended radii for 90° bends in aluminum alloysExhibit 8—Minimum Bend Radius for Aluminum AlloysExhibit 9—Bend allowance chartExhibit 10—K-chart for determining setback for bends other than 90°Exhibit 11—Empty weight center-of-gravity formulasExhibit 12—Empty weight and empty center-of-gravity—tail-wheel type aircraftExhibit 13—Empty weight and empty center-of-gravity—nose-wheel type aircraftExhibit 14—Example of check of most forward weight and balance extremeExhibit 15—Example of check of most rearward weight and balance extremeExhibit 16—AC 43.13-2A, Chapter 1. Structural dataExhibit 17—Turnbuckle safetying guideExhibit 18—Straight-shank terminal dimensions (cable terminals)Exhibit 19—Minimum bend radii for MIL-H-8794 and MIL-H-8788 hoseExhibit 20—Minimum bend radii for Teflon hoseExhibit 21—AC 43.13-2A, Chapter 11. Adding or Relocating InstrumentsExhibit 22—Electrical Wiring RatingExhibit 23—Minimum Equipment List PageExhibit 24—Bend AllowanceExhibit 25—Circumference Formula Previous PartSection II: Airworthiness DirectivesNext Part TCDS Background Information