N328FR

Part: SEAL — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 18,043 hrs · 7,979 cycles

REFERENCE NR 5001274441-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. BULK CARGO DOOR SILL BEAM FOUND CORRODED REPAIR REQUIRED AS PER SRM 53-41-49-300-003 REV 38. REPAIRED BULK CARGO DOOR SILL AS PER SRM 53-41-49-300-003 REV 38. MX ACTION IS ACCEPTABLE.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 18,043 hrs · 7,979 cycles

REFERENCE NR 5001273921-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INSPECTION FOUND R/H SHEAR PLATE FR69-70 CRAKED REPLACEMENT REQUIRED AS PER SRM 53-41-14-283-009 REV. 38. REPLACED RH SHEAR PLATE AS PER SRM 51-72-11-911-001 REV 38. MX ACTION IS ACCEPTABLE.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 18,043 hrs · 7,979 cycles

REFERENCE NR 50012739733-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. FOUND FLOOR BEAM Y-1162.5 FR 68-69 CORRODED REPLACEMENT REQUIRED AS PER SRM 53-41-14-283-009 REV. 38. REPLACED FLOOR BEAM Y-1162.5 AT FR68-69 AS PER SRM 51-72-11-911-001 REV 38. MX ACTION IS ACCEPTABLE.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 18,043 hrs · 7,979 cycles

REFERENCE NR 5001273924-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. FOUND CORROSION ON FLOOR BEAM Y1292 FR 66 REPLACEMENT REQUIRED AS PER SRM 51-72-11 REV. 38. REPLACED FLOOR BEAM Y1292 AT FR66 AS PER SRM 51-72-11-911-001 REV 38. MX ACTION IS ACCEPTABLE.

Part: DOOR SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 18,043 hrs · 7,979 cycles

REFERENCE NR 5001273898-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. CORROSION ON LH AFT DOOR SILL BEAM BETWEEN FR 66-68 REPAIR REQUIRED AS PER SRM 53-41-14-283-002 REV. 38 AND SRM 53-41-14-300-003 REV 38 CORRECTIVE ACTION: REPAIRED LH AFT DOOR SILL BEAM AS PER SRM 53-41-14-300-001REV 38 MX ACTION IS ACCEPTABLE.

Part: DOOR SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 18,043 hrs · 7,979 cycles

REFERENCE NR 500127329-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. CORROSION ON RH AFT DOOR SILL BETWEEN FR66-68 REQUIRES REPLACEMENT AS PER SRM 53-41-14 REV 38. REPLACED AFT DOOR SILL AT FR66-68 AS PER SRM 51-72-11REV 38 AND AMM 53-45-15 REV 96. MX ACTION IS ACCEPTABLE./END/

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 18,043 hrs · 7,979 cycles

DISCREPANCY: REFERENCE NR 5001273899-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INSPECTION FOUND L/H SHEAR PLATE FR69-70 CRAKED REPLACEMENT REQUIRED AS PER SRM 53-41-14-283-009 REV. 38. REPLACED LH SHEAR PLATE AS PER SRM 51-72-11-911-001 REV 38. MX ACTION IS ACCEPTABLE.

Part: DOOR SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 18,043 hrs · 7,979 cycles

REFERENCE NR 5001273507-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. CORROSION ON LH AFT DOOR SILL BETWEEN FR66-68 REQUIRES REPLACEMENT AS PER SRM 53-41-14 REV 38. REPLACED AFT DOOR SILL AT FR66-68 AS PER SRM 51-72-11REV 38 AND AMM 53-45-15 REV 96. MX ACTION IS ACCEPTABLE.

Part: ENGINE — STALLED (ZONE 400) · airframe 14,589 hrs · 6,454 cycles

ENG #1 STALL ECAM ON DESCENT LEVELING AT FTL 190 FELT AND HEARD ONE BUMP FROM THE #1ENGINE DID NOT OBSERVE ANY ABNORMALITIES WHEN WE LOOKED AT THE ENGINE PAREMETERS ECAM WENT AWAY BEFORE WE COULD START IT. CORRECTED ACTION: PERFORMED TSM 77-11-11-810-815-A FOUND DAMAGE TO RH VSV ACTUATOR BUSHINGS. INSTALLED NEW BUSHINHG PER EW-AC-75R-37229. PERFORMED OPS TEST PER AMM 71-00-00-710-814 NO REACURRANCE OF STALL T/W JETTPRO JC0123 DUE 12/22

Part: NONE — NONE · airframe 13,759 hrs · 6,048 cycles

DISCREPANCY: REFERENCE LP 210431 ENG 1 STALL CAUTION MSG. ENGINE PARAMETERS NORMAL AFTER CAUTION WENT AWAY. CORRECTIVE ACTION: PERFORMED TSM 77-11-00-810-815-A, THERE WAS NO AUDION EVIDENCE REPORTED AND NO EXCEEDANCE ON EXCEEDANCE REPORT. PERFORMED INSPECTIONS ODF STEP 4.A1(1)(B) NO DISCREPANCIES NOTED. PER THE SAM STEP, NO FURTHER ACTION IS NECESSARY, AC OK FOR SERVICE TSM 77-11-00-810-815-A

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 9,386 hrs · 4,055 cycles

DURING EPSU BATTERY CAPACITY TEST, EPSUS FIN 10WL, 11WL 12WL AND 13WL FAILED TEST. CORRECTIVE ACTION: REMOVED AND REPLACED EPSU BATTERIES FIN 10WL, 11WL, 12WL AND 13WL, TEST OK AT THIS TIME, REF AMM 33-51-00-920-050-A.

Part: UNKNOWN — ODOR (CABIN) · airframe 1,770 hrs · 765 cycles

FA'S REPORTED A STRONG FUEL ODOR IN THE CABIN, DURING TAXI THAT DID NOT DISAPATE. PERFORMED GVI OF EXTERIOR OF AIRCRAFT, APU, AND ENGINES. NO LEAKS OR ISSUES NOTED. PERFORMED ENGINE RUNS AND PACK RUNS SEPERATELY TO ISOLATE ANY ODORS NO ODORS NOTED AFTER 1.5 HOURS OF RUNS. ACFT OK TO CONTINUE SERVICE. IAW AMM TSM 05-50-00-810-831.

Part: FUEL LINE — LEAKING (NR 2 ENGINE) · airframe 1,408 hrs · 607 cycles

FUEL LEAKING OUT OF COWLING OF RIGHT ENGINE. REMOVED AND REPLACE NUMBER 2 ENGINE MAIN FUEL SUPPLY LINE IAW AMM 73-11-46 PAGE BLOCK 401 AND AMM 73-11-49. LEAK CHECK GOOD. AIRCRAFT OK FOR SERVICE.