What was found
HFEC INSPECTION FOUND 01EA CRACK APPROX 0.100" IN LENGTH ON THE FUSELAGE SKIN APPROX 0.150" BELOW THE 6TH STRINGER-ATTACH RIVET ALONG S-13AL AFT OF STA 1654.50 AS MARK PER W/C 5330-01229-01A STEP 4. C/A THE FUSELAGE SKIN APPROX 0.150" BELOW THE 6TH STRINGER-ATTACH RIVET ALONG S-13AL AFT OF STA1654.50 CRACKED SKIN REPAIRED AS PER B767-400 SRM 53-80-01 REPAIR 7 RELEASE 59.00 19DEC19. THE IS GATEGOR B REPAIR,INSPECTION THRESHOLD 30000 RLIGHT CYCLES ARTER AIRPLANE DELIVERY OR WITHIN 7500 FLIGHT CYCLES FROM THE REPAIR INSTALLATION,WHICHEVER COMES LAST AS PER B767-400 SRM53-80-01 REPAIR7 STEP 5 TABLE 202,(1437621)