What was found
DURING PERFORMED AGING AIRCRAFT INSPECTION FOUND EXISTING REPAIR DOUBLER LOCATED LOWER FUSELAGE SKING AT FR31 TO FR32 BTW 38L TO STRG 39L. SEE AEROMAN NON ROUTINE 2022-308900 01-E FIGURE 005 VIEW B (SHEET 02) DOUBLER REPAIR MATERIAL: DAMAGE IAW NTM 51-90-00, THIS REPAIR IS CATEGORY B RE-INSPECTION (TBD) IAW A320 SRI 53-21-11-205-073 TABLE 001 (ZONE A); FIGURE (WHICHEVER OCCURS FIRST) PER SRI 53-21-11-205-073 TABLE 1. ALUMINUM SHEET P/N: 2024T3-0.080"; 2024T3-0.071" P.O. IS REQUIRED AT 60,000FC/120,000FH INSPECTION THRESHOLD FROM TIME 001 (SHEET 01) INSTALLED DOT IAW GMM 06-35-05 PERFORMED SCEPTRE #2021.1110491 AND P.O. #20211751671, PERFORMED VISUAL OF ADL/REPAIR EMBODIMENT AND SUBSEQUENT INSPECTION UNTIL60,000FC ENTRY ON LOG PAGE #9608141. INSPECTION OON REPAIR AREA INTERNAL AND EXTERNAL AND NOT FOUND 120,000FH AT INTERVALS OF FC (TBD)/FH (TBD), INSPECTION METHOD THE REPAIR IS CAT B IN ZONE A AND REQUIRES INSPECTION THRESHOLD FROM THE TIME OF ADL/REPAIR EMBODIMENT 60,000 FC/120,000 FH ADD EMP:V939197 PERFORMED PERMANENT REPAIR ON LOWER FUSELAGE SKIN AT FR.31 TO FR.32 AND BTW STR.38L STR.39L IAW A320 SRM 53-21-11-300-093, PARAGRAPH 2.A. FIGURE 001, SHEET 01 (PRINCIPLE 2), NOMINAL SKIN THICKNESS ON REPAIR AREA IS: 0.071 INCH IAW A320 SRM 53-21-11- ADD EMP:V938965 OK TO CARRY PER SRI 53-21-11-205-073, INSPECTION REQUIRED AT TOMC-APPROVAL FROM SC1ELBYC COMMENT 60000 F/C''S OR 120000 F/H''S FROM REPAIR EMBODIMENT, WHICH EVER OCCURS FIRST. SUBSEQUENT INSPECTION TBD Q/C REVIEWED. Q