What was found
AFTER REMOVING OTBD PLANK DOUBLERS AT WS 118 TO 138 OF THE RT WING, FOUND TWO CRACKS IN THE UPPER WING SKIN. ONE .7500 CRACK AT WS 123.5 AND 47 INCHES AFT OF NOSE SPAR AND ONE .5 INCH CRACK AT WS 123.5 AND 43 INCHES AFT OF THE NOSE SPAR. ACCOMPLISHED REPAIRS IAW SRM 57-30-00 FIG 6 PAGES 6 AND 7. ALL SURFACES CLEANED TREATED AND PRIMED IAW 1 GEN-5 CHAPTER 5. PLANK DOUBLERS REINSTALLED IAW RD6-57-618.