What was found
R/W O/B AFT FLAP I/B END UPPER SURFACE IS DELAMINATED / [01] REMOVED R/W O/B AFT FLAP IAW AMM 27-51-22-000-801 STEPS 2.D.;[02] VERIFIED;[03] ACCOMPLISHED PARTS REMOVAL TABLE;[04] R/W O/B AFT FLAP I/B END UPPER SURFACE DELAMINATED AREA WAS REPAIRED ON ATS WORK ORDER #548603; CUSTOMER PO<BR>#P2796377-1;[05] OK TO INSTALL;[06] VERIFIED CORRECTIVE ACTION 3 AND 4. <BR>OK TO INSTALL;[07] INSTALLED R/W O/B AFT FLAP IAW AMM 27-51-22-420-002 STEP 3.F.(4)(A)-(D)(E)1)-6);[08] VERIFIED;[09] INSTALLED RIGHT WING OUTBOARD AFT FLAP IAW AMM 27-51-22-400-801 STEPS 3. F. (4) (5). TORQUE AND SAFETY VERIFIED<BR>CAL ID ATS2687<BR>S/N 1021903746<BR>CAL DUE 11/2022<BR><BR>CAL ID ATS1731<BR>S/N 1505093<BR>CAL DUE 11/2022;[10] VERIFIED;[11] VERIFIED CORRECTIVE ACTION #9;[12] ADJUSTED RIGHT WING OUTBOARD AFT FLAP IAW AMM 27-51-22-400-801 STEPS 3. G. ADJUSTMENT CHECK GOOD.;[13] VERIFIED;[14] REMOVED RIG PINS AND PUT AIRCRAFT BACK TO USUAL CONDITION IAW AMM 27-51-22-400-801;[15] VERIFIED;[16] VERIFIED CORRECTIVE ACTION 12;[17] VERIFIED CORRECTIVE ACTION 14