N720FR

ATA 7200

Part: ENGINE — OVERTEMP (ZONE 400) · airframe 18,056 hrs · 7,802 cycles

AIRCRAFT GROUNDED DUE TO REQUIRES MANDATORY ENGINE CHANGE PER AMM. REFERENCE LOG PAGE LP274897 ITEM 1, WITH TOGA TAKEOFF RIGHT BEFORE POWER REDUCTION ECAM FOR EGT OVERLIMIT #2 ENG. TEMP AT 955 DEGREES CELCIOUS FOR LESS THAN 1 SEC. ALL OTHER PARAMETERS NORMAL. REMOVED AND REPLACED #2 ENGINE REF. TASKCARD MP71042-01, MP71042-02, NON ROUTINE NR129595, 129596, 129597, 129598, 129599, 129600, 129601, 129602, 129603, 129604, 129595, 129596, 129597, 129598, 129599, 129600, 129601, 129602, LOG PAGE LP1274898 #2. OPS CHECK GOOD, LEAK CHECK GOOD. ORIGINAL SUBMISSION DATE: 10/02/2023.

ATA 7200

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 1,770 hrs · 7,666 cycles

ENG. #2 EGT OVERLIMIT ECAM ON T/O ROLL RWY 08 BQN, RTO BETWEEN 80 AND 100 KTS. LOUD BANG TIME WAS 2042 UTC T/O WEIGHT 13108 AOT 31C WINDS CALM FOB 27.4. ENG #2 VBV INSPECTED AND ADJUSTED IAW A321 TSM 77-00-00-810-849-A. EXCEEDANCE REPORT PULLED PER AMM 72-00-00-200-008-A. FOUND IN AREA A, LOW EGT MARGING. IDLE RUN PERFORMED, NO DEFECT NOTED. OK TO RETURN TO SERVICE.

ATA 5320

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 17,770 hrs · 7,666 cycles

AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. OFFWING ESCAPE SLIDE ENCLOSURE ON DOOR 3L FOUND WITH CORRODED ANGLES ON ALLOWABLE DAMAGE LIMIT FOUND ON SRM, REPLACEMENT IS REQUIRED AS PER A321 SRM 51-72-11 REV. 146. PERFORMED INSTALLATION OF NEW ANGLES ON DOOR 3L OFFWING ESCAPE SLIDE ENCLOSURE AS PER A321 SRM 51-72-11 REV. 146. MX ACTION IS ACCEPTABLE.

ATA 5320

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 17,770 hrs · 7,666 cycles

DISCREPANCY: REFERENCE NR 5001257734-0010. AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. OFFWING ESCAPE SLIDE ENCLOSURE ON DOOR 2R FOUND WITH CORRODED ANGLES ON ALLOWABLE DAMAGE LIMIT FOUND ON SRM, REPLACEMENT IS REQUIRED AS PER A321 SRM 51-72-11 REV. 146 CORRECTIVE ACTION: PERFORMED INSTALLATION OF NEW ANGLES ON DOOR 2R OFFWING ESCAPE SLIDE ENCLOSURE AS PER A321 SRM 51-72-11 REV. 146. MX ACTION IS ACCEPTABLE./END/

ATA 5320

Part: ANGLE — CORRODED (ZONE 100) · airframe 17,770 hrs · 7,666 cycles

AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. OFFWING ESCAPE SLIDE ENCLOSURE ON DOOR 2R FOUND WITH CORRODED ANGLES ON ALLOWABLE DAMAGE LIMIT FOUND ON SRM, REPLACEMENT IS REQUIRED AS PER A321 SRM 51-72-11 REV. 146. PERFORMED INSTALLATION OF NEW ANGLES ON DOOR 2R OFFWING ESCAPE SLIDE ENCLOSURE AS PER A321 SRM 51-72-11 REV. 146. MX ACTION IS ACCEPTABLE./END/

ATA 5320

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 17,770 hrs · 7,666 cycles

DISCREPANCY: REFERENCE NR 5001257734-0010. AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. OFFWING ESCAPE SLIDE ENCLOSURE ON DOOR 2L FOUND WITH CORRODED ANGLES ON ALLOWABLE DAMAGE LIMIT FOUND ON SRM, REPLACEMENT IS REQUIRED AS PER A321 SRM 51-72-11 REV. 146 CORRECTIVE ACTION: PERFORMED INSTALLATION OF NEW ANGLES ON DOOR 2L OFFWING ESCAPE SLIDE ENCLOSURE AS PER A321 SRM 51-72-11 REV. 146 MX ACTION IS ACCEPTABLE./END/

ATA 5320

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 17,770 hrs · 7,666 cycles

DISCREPANCY: REFERENCE NR 5001257734-0010. AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. OFFWING ESCAPE SLIDE ENCLOSURE ON DOOR 3R FOUND WITH CORRODED ANGLES ON ALLOWABLE DAMAGE LIMIT FOUND ON SRM, REPLACEMENT IS REQUIRED AS PER A321 SRM 51-72-11 REV. 146. CORRECTIVE ACTION: PERFORMED INSTALLATION OF NEW ANGLES ON DOOR 3R OFFWING ESCAPE SLIDE ENCLOSURE AS PER A321 SRM 51-72-11 REV. 146. MX ACTION IS ACCEPTABLE./END/

ATA 5320

Part: SUPPORT — CORRODED (ZONE 100) · airframe 17,770 hrs · 7,666 cycles

AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. OFFWING ESCAPE SLIDE ENCLOSURE ON DOOR 2L FOUND WITH CORRODED ANGLES ON ALLOWABLE DAMAGE LIMIT FOUND ON SRM, REPLACEMENT IS REQUIRED AS PER A321 SRM 51-72-11 REV. 146. PERFORMED INSTALLATION OF NEW ANGLES ON DOOR 2L OFFWING ESCAPE SLIDE ENCLOSURE AS PER A321 SRM 51-72-11 REV. 146. MX ACTION IS ACCEPTABLE./END/

ATA 5320

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 17,770 hrs · 7,666 cycles

DISCREPANCY: REFERENCE NR 5001257734-0010. AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. OFFWING ESCAPE SLIDE ENCLOSURE ON DOOR 3R FOUND WITH CORRODED ANGLES ON ALLOWABLE DAMAGE LIMIT FOUND ON SRM, REPLACEMENT IS REQUIRED AS PER A321 SRM 51-72-11 REV. 146. CORRECTIVE ACTION: PERFORMED INSTALLATION OF NEW ANGLES ON DOOR 3R OFFWING ESCAPE SLIDE ENCLOSURE AS PER A321 SRM 51-72-11 REV. 146. MX ACTION IS ACCEPTABLE./END/

ATA 5320

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 17,770 hrs · 7,666 cycles

AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. OFFWING ESCAPE SLIDE ENCLOSURE ON DOOR 3R FOUND WITH CORRODED ANGLES ON ALLOWABLE DAMAGE LIMIT FOUND ON SRM, REPLACEMENT IS REQUIRED AS PER A321 SRM 51-72-11 REV. 146. PERFORMED INSTALLATION OF NEW ANGLES ON DOOR 3R OFFWING ESCAPE SLIDE ENCLOSURE AS PER A321 SRM 51-72-11 REV. 146.MX ACTION IS ACCEPTABLE.

ATA 5320

Part: ANGLE — CORRODED (ZONE 100) · airframe 17,770 hrs · 7,666 cycles

AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. OFFWING ESCAPE SLIDE ENCLOSURE ON DOOR 3L FOUND WITH CORRODED ANGLES ON ALLOWABLE DAMAGE LIMIT FOUND ON SRM, REPLACEMENT IS REQUIRED AS PER A321 SRM 51-72-11 REV. 146. PERFORMED INSTALLATION OF NEW ANGLES ON DOOR 3L OFFWING ESCAPE SLIDE ENCLOSURE AS PER A321 SRM 51-72-11 REV. 146. MX ACTION IS ACCEPTABLE./END/

ATA 5320

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 17,770 hrs · 7,666 cycles

DISCREPANCY: REFERENCE NR 5001257734-0010. AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. OFFWING ESCAPE SLIDE ENCLOSURE ON DOOR 2L FOUND WITH CORRODED ANGLES ON ALLOWABLE DAMAGE LIMIT FOUND ON SRM, REPLACEMENT IS REQUIRED AS PER A321 SRM 51-72-11 REV. 146 CORRECTIVE ACTION: PERFORMED INSTALLATION OF NEW ANGLES ON DOOR 2L OFFWING ESCAPE SLIDE ENCLOSURE AS PER A321 SRM 51-72-11 REV. 146. MX ACTION IS ACCEPTABLE./END/

ATA 5320

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 17,770 hrs · 7,666 cycles

DISCREPANCY: REFERENCE NR 5001257734-0010. AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. OFFWING ESCAPE SLIDE ENCLOSURE ON DOOR 3R FOUND WITH CORRODED ANGLES ON ALLOWABLE DAMAGE LIMIT FOUND ON SRM, REPLACEMENT IS REQUIRED AS PER A321 SRM 51-72-11 REV. 146. CORRECTIVE ACTION: PERFORMED INSTALLATION OF NEW ANGLES ON DOOR 3R OFFWING ESCAPE SLIDE ENCLOSURE AS PER A321 SRM 51-72-11 REV. 146. MX ACTION IS ACCEPTABLE.

ATA 5310

Part: DOOR SEAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 17,770 hrs · 7,666 cycles

DISCREPANCY: REFERENCE NR 5001257278-0010. AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX.CORRODED SILL SHAPE ON RH FWD DOOR NO AWOLLABLE DAMAGE FOUND ON SRM REQUIRES REPLACEMENT AS PER A321 SRM 51-72-11 REV.146 CORRECTIVE ACTION: PERFORMED INSTALLATION OF ANCHOR NUTS AND NEW SILL SHAPE AS PER A321 SRM 51-72-11 AND 51-42-11 REV. 146 MX ACTION IS ACCEPTABLE./END/

ATA 5322

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 17,770 hrs · 7,666 cycles

REFERENCE NR 5001257113-0030. AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INSOECTIONS FOUND R/H SHEAR PLATE FR69-70 CRACKED REQUIRES REPLACEMENT AS PER SRM 51-72-11-911-001 REV. 146. R/H SHEAR PLATE WAS REPLACED AS PER SRM 51-72-11-911-001 REV. 146 MX ACTION IS ACCEPTABLE.

ATA 5310

Part: DOOR SEAL — CORRODED (ZONE 200) · corrosion level 2 · airframe 17,770 hrs · 7,666 cycles

REFERENCE NR 5001257125-0010. AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. CORRODED AFT DOOR SILL BEAM ON RH SIDE REQUIRES EVALUATION AS PER A321 SRM TASK 53-41-14-283-002 REV. 146. REPAIRED AFT DOOR SILL BEAM ON RH SIDE AS PER SRM TASK 53-41-14-300-001 REV. 146 MX ACTION IS ACCEPTABLE.

ATA 5322

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 17,770 hrs · 7,666 cycles

REFERENCE NR 5001257113-0010. AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INSOECTIONS FOUND L/H SHEAR PLATE FR69-70 CRACKED REQUIRES REPLACEMENT AS PER SRM 51-72-11-911-001 REV. 146. L/H SHEAR PLATE WAS REPLACED AS PER SRM 51-72-11-911-001 REV. 146 MX ACTION IS ACCEPTABLE.

ATA 5315

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 17,770 hrs · 7,666 cycles

REFERENCE NR 5001257119-0010. AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. FOUND FLOOR BEAM Y-160.5 AT FR68-69 CORRODED IN EXCLUDED AREA REPLACEMENT REQUIRED AS PER SRM TASK 53-41-14-283-009 REV. 146. FLOOR BEAM Y-160.5 AT FR68-69 REPLACED AS PER SRM 51-72-11-911-001 REV. 146 MX ACTION IS ACCEPTABLE.

ATA 3350

Part: NONE — NONE · airframe 16,214 hrs · 6,984 cycles

DISCREPANCY LP293997 ITEM 1; 13WL FAIL DURING EPSU TEST. CORRECTIVE ACTION FOUND L-4 SLIDE EMERGENCY LIGHTS CONNECTOR ON FRONT OF SLIDE NOT SECURED PROPERLY. RECONNECTED SLIDE LIGHTS CONNECTOR AND PERFORMED EPSU BITE TEST PER AMM 33-51-73-00-740-005. OPS CHECKS GOOD. CIOS INTERFACE AND POWER UP TEST GOOD. //END//

ATA 3350

Part: POWER SUPPLY — FAILED (ZONE 100) · airframe 16,214 hrs · 6,984 cycles

DISCREPANCY LP293997 ITEM 2; REPLACE EPSU 13WL DUE TO FAILED TEST. CORRECTIVE ACTION: REMOVED AND REPLACED EPSU 13WL REF AMM 33-51-38-400-001-A. OPS CHECK FAILED. SEE ITEM 1 AND 3 OF THIS LP FOR EPSU SUCCESSFUL TEST. //END//