N928VA

Part: FLOORBEAM — CORRODED (FRM 68) · corrosion level 2 · airframe 17,255 hrs · 4,422 cycles

AFT CABIN FLOOR SUPORT BEAM AT L4 DOOR AT FR 68 HAS CORROSION T NUTPLATE LOCATION GROUNDED - YES. REMOVED CORROSION IAW A321 SRM 53-41-14-283-002. ORIG MAT .071, REMAINING MAT .031. MAT LOSS OF .040 IS BEYOND ALLOWABLE LIMITS. ALLOWED 25% MAT. LOSS REPAIRED AREA IAW A321 SRM 53-41-14-300-001 REPAIR PRINCIPLE 5. THIS IS A CAT. A REPAIR

Part: SHEAR PLATE — CORRODED (UNKNOWN) · corrosion level 2 · airframe 17,255 hrs · 4,422 cycles

AFT CABIN RH SHEAR PLATE AT FR 69-70 HAS CORROSION ON UPPER SURFACE GROUNDED - YES. CORROSION ON SHEAR PLATE HAS EXFOLIATED AROUND FASTNER HOLE - OUT OF LIMITS - RECEIVED NEW SHEAR PLATE P.N. D5347112420800 P.O.1055897.8. AND INSTALLED NEW SHEAR PLATE IAW DWG 18 053474180 AND A321 SRM 51-42-11

Part: SUPPORT BEAM — CORRODED (UNKNOWN) · corrosion level 2 · airframe 17,255 hrs · 4,422 cycles

AFT CABIN SUPPORT BEAM AT R4 DOOR HAS CORROSION ON UPPER SURFACE AT FR 68 GROUNDED - YES. REMOVED CORROSION FROM SILL BEAM, REMOVED 0.080 FROM EDGE. DAMAGE HAS NO LIMITS AND IS CONSIDERED 100% MATERIAL LOSS.REMOVED DAMAGED AREA IAW A321 SRM 53-41-14-300-001 PRINCIPLE 7. FABRICATED REPAIR ANGLE AND FILLER IAW A321 SRM 53-41-14-300-001 PRINCIPLE 7. INSTALLED REPAIR IAW A321-SRM 53-41-14-300-001

Part: SKIN — DENTED · airframe 11,450 hrs · 3,034 cycles

FOUND DENT ON LOWER AFT CORNER OF R1 DOOR GROUNDED - YES. ACCOMPLISHED EXTERNAL SKIN REPAIR ON AFT LOWER CORNER OF R1 DOOR IAW AIRBUS A321-200N SRM 52-10-00-300-003CATEGORY B REPAIR,REINSPECT EVERY 60,000 FLIGHT CYCLES, FLIGHT HOURS OT RELEVANT IAW AIRBUS A321-200N SRM 52-10-00-205-022SEAMC FELIX NOTIFIED

Part: WARNING MESSAGE — FALSE ACTIVATION (ANTI-ICE SYSTEM) · airframe 5,213 hrs · 1,422 cycles

ENGINE 1 ANTI-ICE STATUS MESSAGE AFTER ENGINE SHUTDOWN GROUNDED - YES. CONFIRMED IDLE TEST PERFORMED IAW TSM 30-21-00-810-893-A, NO FAULTS NOTED AFTER OR DURING OPERATION. NO FURTHER ACTION REQUIRED.

Part: LINE — DAMAGED (SENSE) · airframe 4,930 hrs · 1,348 cycles

MAINT AIR BLEED MSG ON STATUS PAGE WORK WITH RMA 3539: AIR BLEED MSG FAULTING SENSE LINE/ 7HA2 XDCR. (SENSE LINE WAS REPLACED ON 6/28/2019) DO NOT REPLACE BMC COMPUTER PER TSM 36-11-00-810-A61-A CHECK SENSE LINE LEAKAGE AROUND THE BRAIDED AREA. (IPC 36-11-49-06) GROUNDED - YES. ON DEFERRAL.

Part: CONNECTOR — DIRTY (THRUST REVERSER) · airframe 4,068 hrs · 1,138 cycles

ENGINE 1 REV MINOR FAULT AFTER LANDING. GROUNDED - YES. CLEANED TR TERTIARY LOCK SENSOR CONNECTORS REF TSM 78-30-00-810-902-A. PERFORMED FADEC TEST PER AMM 73-29-00-710-802-A, TEST OK. NO FAULT FOUND. OK FOR SVC.

Part: SENSOR — FAILED (FUEL STRAINER) · airframe 3,732 hrs · 1,045 cycles

ENG 1 CHANNEL B FUEL STRAINER SENSOR FAULT SEEN FOR SMR CHECK T/C 73-0000-L1-1-VAMENG 2 CHANNEL A FUEL STRAINER SENSOR FAULT SEEN FOR SMR CHECK. T/C 73-0000-L1-1-VAM GROUNDED - YES. R&R FUEL STRAINER SENSOR IAW AMM 73-34-10 SYSTEM TESTED & LEAK CHECKED OK.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 3,409 hrs · 957 cycles

ENGINE 2 HP TIP CTL FAULT MESSAGE OPENED, THEN CLOSED ON CLIMB. GROUNDED - YES. PERFORMED TSM TASK 75-31-00-710-081-A STEPS 4.B (1) (A) (B) (C) AND 4.B (2) (A) (B) (C), CLEANED BOTH RECETACLES. NO HELP. VERIFIED FAULT, RELEASED PER MEL 75-21-01, ACCOMPLISHED MAINT PROCEDURES HPTACC VALVE LOCKED CLOSED. MEL LOG UPDATED. PLACARD INSTALLED. SEAMC AUTHORIZED.

Part: UNKNOWN — MALFUNCTIONED (ENGINE) · airframe 3,372 hrs · 949 cycles

ENGINE 2 HP TIP CONTROL FAULT. GROUNDED - YES. ACCOMPLISHED TSM 75-22-810-819A FAULT OF THE LPTCC VALVE (POSITION FAILED OPEN) #2 ENGINE. OPERATIONAL ENGINE IDLE TEST ON CHANNEL A AMM 75-22-810-819A. TEST SHOWED NO FAULTS AND NO MX ACTION REQUIRED.

Part: FAULT MESSAGE — FALSE ACTIVATION (THRUST REVERSER) · airframe 3,271 hrs · 927 cycles

ENGINE 1 REV MINOR FAULT. GROUNDED - YES. PERFORMED THRUST REVERSER CYCLING TEST ON BOTH CHAN FOR BOTH ENGS REF AMM 73-29-00-740-804-A. NO FAULTS NOTED. OPS CHECKS GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (BLEED AIR) · airframe 3,066 hrs · 876 cycles

CLASS II MAINT MSG AIR BLEED. GROUNDED - YES. DEFERRED. RMA PENDING

Part: SENSE LINE — LEAKING (NR 1 ENGINE) · airframe 2,898 hrs · 838 cycles

AIR BLEED CLASS II WHITE STATUS MESSAGEAIR BLEED MSG FAULTING SENSE LINE/ 7HA1 XDCR.(SENSE LINE WAS REPLACED ON 3/26/2019)PER TSM 36-11-00-810-A60-A CHECK SENSE LINE LEAKAGE AROUND THE BRAIDED AREA. HAD SIMILAR ISSUES WITH OTHER AIRCRAFT. (IPC 36-11-49-06 GROUNDED - YES. ACCOMPLISHED BMC 1 BITE TEST SYS BACK TO NORMAL AMM 36-11-00-740-001 FOUND LEAK ON SENSE LINE/ R/R SENSE LINE ENG 1 PER TSM 36-11-00-810-A60. LEAK CHK GOOD AT THIS TIME. THIS CLEARS RMA 2980.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 2,756 hrs · 804 cycles

ENGINE 1 REV MINOR FAULT DISPLAYED ON ECAM GROUNDED - YES. PERFORMED OPERATIONAL THRUST REVERSER CYCLING TEST REF AMM 73-29-00 NO FAULTS NOTED AT THIS TIME. OK FOR SERVICE.

Part: VALVE — FAILED (FUEL RETURN) · airframe 2,560 hrs · 756 cycles

ENGINE 1 FUEL RETURN VALVE. VALVE NOT CLOSE ECAM AFTER # 1 ENGINE START GROUNDED - YES. R/R FUEL RETURN VALVE ON ENG 1 REF AMM 73-11-35 OPS CHK GOOD DURING ENGINE RUN. OK FOR SVC. PLACARD REMOVED, MEL LIST UPDATED, MCC YARED NOTIFIED. THIS CLEARS MEL 73-11-01-01-B & MDDR 65529

Part: VALVE — FAILED (FUEL RETURN) · airframe 2,483 hrs · 733 cycles

ENGINE 1 FUEL RETURN VALVE. VALVE NOT CLOSED. GROUNDED - YES. PERFORMED ACTUATORS TEST PER AMM 73-29-00-740-802-A. TEST OK. NO FAULTS NOTED AT THE TIME OF THE TEST.

Part: SENSE LINE — LEAKING (BLEED AIR SYS) · airframe 2,404 hrs · 716 cycles

DURING INSPECTION FOUND BLEED AIR LEAK ON SENSE LINE ENG NR 1 (SEE RMA 2811 AND MDDR 64918) GROUNDED - YES. R/R ENG 1 ECS INDICATING TUBE PER AMM 36-11-49-400-831-A. OPS / LEAK CK WILL BE C/W ON LP 8034834 ITEM 1. ( P/N: ER9691PO1 )

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 2,367 hrs · 707 cycles

AIR BLEED CLASS II STS MSG GROUNDED - YES. OPEN RMA. ETOPS RESTRICTED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 2,340 hrs · 699 cycles

ENGINE 1 OVER THROTTLE PROTECTION FAULT GROUNDED - YES. PERFORMED FADEC TEST PER AMM 73-29-00-710-802. NO FAULT FOUND. ACFT OK FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 2,023 hrs · 597 cycles

ENG 1 REV MINOR FAULT ECAM MSG ON LANDING. GROUNDED - YES. PERFORMED TSM 77-11-00-810-839. NO FURTHER MX ACTION NECESSARY.

Part: ENGINE — FAULTED (NR 2) · airframe 1,616 hrs · 482 cycles

ENGINE 2 MINOR FAULT GROUNDED - YES. FAULT DID NOT OCCUR 5 CONSECUTIVE FLIGHTS, NO MAINTENANCE ACTION REQUIRE PER TSM 77-11-00-810-840A. OK FOR SVC.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 1,523 hrs · 454 cycles

ECAM ENG 2 MINOR FAULT GROUNDED - YES. DEFERRED PER MEL 73-30-05.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 1,425 hrs · 417 cycles

ENG 2 MINOR FAULT MESSAGE AFTER SHUTDOWN GROUNDED - YES. PERFORMED ENG NR 2 IDLE TEST PER AMM 73-29-00-740-803-A. NO FAULTS FOUND.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 1,372 hrs · 402 cycles

ON LANDING RECEIVED ECAM ENG 2 MINOR FAULT GROUNDED - YES. PREFORMED FADEC TEST REF AMM 73-29-00-710-802A AND IDCE TEST REF AMM 73-29-00-740-803-A NO FAULTS NOTED AT THIS TIME FOR ENG 2.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 1,250 hrs · 370 cycles

ENG1 FADEC SYS FAULT THR LVR 1 NOT ABOVE IDLE ECAM MESSAGE ON TAXI IN. GROUNDED - YES. PER GENERAL NUISANCE FAULTS AND T/S TIPS ( ISI 73.00.00045 ) MX-ACTION ACCOMPLISHED PER TSM 73-21-01-810-928A NO CONFIRMATION OF FAULT POST ENG 1 IDLE RUN. A/C RELEASED TO SERV.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 1,208 hrs · 356 cycles

CAUTION MSG ENG NR 2 MINOR FAULT GROUNDED - YES. *DEFERRED MEL 73-30-05*

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 1,097 hrs · 326 cycles

PACK 2 REGUL FAULT AFTER ENG START. GROUNDED - YES. PERFORMED RESET TEST GOOD IAW AMM 21-61-00-710-001.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 1,088 hrs · 324 cycles

ENG 1 MINOR FAULT GROUNDED - YES. PERFORMED TSM 77-11-00-810-839-A, FAULT APPEARED PHASE 9, NO MAINTENANCE ACTION NECESSARY.

Part: RELAY — FAULTY (NR 2 ENGINE) · airframe 1,033 hrs · 307 cycles

FADEC 2 FAULT MESSAGE ON UPPER ECAM. GROUNDED - YES. IDLE RUN NR 2 ENG PER AMM 71-00-00. NO FAULTS COUND NOT ACCESS FADEC 2 THRU MCDU. FOUND FAULTY RELAY 11KS2 REF AWM 73-25-06 P 0029 SHEET 1 REPLACED RELAY 11KS2 FADEC 2 TEST PER AMM 73-29-00 PB 501.

Part: FAULT MESSAGE — FALSE ACTIVATION (NR 2 ENGINE) · airframe 923 hrs · 276 cycles

ENGINE 2 FADEC CLASS II STATUS MESSAGEENGINE 1,2 MINOR FAULT GROUNDED - YES. ITEM 1 DEFERREDPERFORMED ENG 1 AND 2 FADEC TEST OPS CK SATISFATCTORY PER TSM 71-00-00-810

Part: WARNING SWITCH — FALSE ACTIVATION (COCKPIT) · airframe 879 hrs · 261 cycles

FADEC 1 & 2 FAULT ON TAXI IN. GROUNDED - YES. PERFORMED NON MOTORING TEST OF FADEC 1& 2:OK REF AMM 73-29-00.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 870 hrs · 258 cycles

ENGINE 1 MINOR FAULT DISPLAYED ON ECAM. GROUNDED - YES. PERFORMED ENG 1 IDLE TEST PER AMM 73-29-00-740-803. NO FAULTS FOUND.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 866 hrs · 257 cycles

AIR ENG 1 BLEED HI TEMP, ENG 1 MINOR FAULT, ENG 2 MINOR FAULT, ENG 2 FADEC SYS FAULT. GROUNDED - YES. PER TSM 77-11-00-810-839A FAULT DID NOT OCCUR ON FIVE CONSECUTIVE FLIGHTS, NO MAINT ACTION REQ'D. AS A PRECAUTION FADEC TEST C/OUT, NO FAULTS NOTED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 842 hrs · 250 cycles

ENGINE 1 BLEED HI TEMP ECAM ANUNCIATED AFTER BOTH PACKS SELECTED ON GROUNDED - YES. PERFORMED OPS TEST OF ENG 1 BLEED SYS PER TSM 73-25-00-810-C70-A & 36-11-00-810-B31-A. NO FAULT FOUND UNABLE TO DUPLICATE FAOUND.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 842 hrs · 250 cycles

ENGINE 1 & ENGINE 2 FADEC SYS FAULT ON ECAM AFTER TOUCHDOWN. ( THRUST LEVER NOT TO BE MOVED ABOVE IDLE) GROUNDED - YES. PERFORMED ENG IDLE TEST IAW TSM 73-25-00. NO FAULT FOUND. REF TFU 73-20-00-049. NO FURTHER ACTION REQUIRED. A/C OK FOR SVC.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 840 hrs · 248 cycles

ENG 2 FADEC SYSTEM FAULT. GROUNDED - YES. INTEROGATED CFDS/ENG2/FADEC2B; RECOVERED FAULT MESSAGE" "ENG OVSP DETECTION". PER TSM 77-11-00-810-839-A NO MX ACTION REQ. ALSO PERF FADEC TST IAW AMM 73-29-00-710-802A. TEST OK.

Part: UNKNOWN — MALFUNCTIONED (AC PACK) · airframe 829 hrs · 245 cycles

PACK 2 PSI PULSING FROM 4 TO 38 PSI. GROUNDED - YES. PERFORMED TEMP CONTROL TEST PER AMM 21-60-00. TEST OK. INDICATIONS NORMAL PER TSM 36-11-00-710-578-A. OK FOR SERVICE.

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 283 hrs · 75 cycles

WEATHER RADAR FAULT WXR RT GROUNDED - YES. RESET RADAR 1 AND TEST REF AMM 34-41-00 NO FAULTS