2. Aircraft 2513 was damaged from contact with a ladder. The gouge is estimated to be 0.5in long with a depth of 0.008in and is located directly aft of the external power receptacle, centered in the milled cavity between Stringers 42 & 43 and Stations 424 & 445. A. What is the maximum blend depth as a percentage of material thickness that is allowed at this location? (NOTE: there is no recorded damage within 5ft of this location) B. What is the minimum remaining material thickness dimension that is acceptable for continued service without limitation? 3. What is the reading on the Caliper shown? A. 0.357cm B. 3.57cm C. 3.62cm D. 3.642cm E. 3.67cm Pulanty prop