N921VA

Part: BLEED VALVE — FAILED (NR 1 ENGINE) · airframe 9,489 hrs · 2,424 cycles

ENGINE 1 HP VALVE FAULT GROUNDED - YES. PFR FAULTS #1 HP BLEED VALVE(4000H1A), CREW RAN #1 ENGINE, HP VALVE OPS NORMAL. REF AMM 36-11-51-400-803A. 35534. 3/17/2020REF ITEM 2 FOR REPAIR. RAN #1 ENGINE. NO FAULTS. EBAS BITE CK GOOD. REF AMM 36-11-00-740-804.R/R ENG1 HP BLEED VALVE IAW AMM 36-11-51. OPS CHECK AND LEAK CHECK OK. NO DEFECTS NOTED AT THIS TIME.

Part: BLEED AIR SYS — LOW PRESSURE (AC BAY) · airframe 9,484 hrs · 2,423 cycles

PACK 1 BLEED AND PRESSURE LAW ON DESCENT INTO JFK GROUNDED - YES. PER TFU 36-11-00-106 ON SOME CASES THE BLEED SYSTEM EXPERIENCED A LAW PRESSURE SENSOR AT TOP OF DESCENT DURING CRUISE. NEW HPV P/N # TARGETED FOR JUNE 2020 PER THIS TFU. A/C OK FOR SER

Part: WARNING MESSAGE — FALSE ACTIVATION (ENGINES) · airframe 9,239 hrs · 2,367 cycles

CLASS II MAINT STATUS MESSAGES ENG 1 E1U ENG 2 E1U ON LOWER ECAM GROUNDED - YES. PERFORMED RESET PER TSM 73-25-00-810-B70-A. FAULT MESSAGES GONE. A/C OK FOR SERVICE

Part: FIRE LOOP — FAULTED (NR 1 ENGINE) · airframe 9,014 hrs · 2,312 cycles

ENGINE 1 FIRE LOOP "A" FAULT GROUNDED - YES. DEFERRED. ETOPS RESTRICTED

Part: CONTROL VALVE — FAILED (WING ANTI ICE) · airframe 8,113 hrs · 2,095 cycles

WING ANTI ICE SYS FAULT ECAM IN DESCENT, IDLE THRUST, AT 10000 FT. CIRCUIT BREAKER C2 (WING ANTI ICE CTL) WAS POPPED. GROUNDED - YES. REMOVED AND REPLACED LH WING ANTI ICING CONTROL VALVE. REF AMM 30-11-51. OPS CHECK GOOD.

Part: WARNING SYSTEM — ACTIVATED (OIL SYSTEM) · airframe 7,985 hrs · 2,064 cycles

ENGINE #2 HIGH OIL PRESS SMR FAULT GROUNDED - YES. DEFERRED - WATCH ITEM.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 7,927 hrs · 2,052 cycles

ENGINE 1 OVERTHROTTLE PROTECTION FAULT DISPLAYED ON ECAM. GROUNDED - YES. PER TSM 73-21-01-810-922-A OPS CK ENGINE IDLE TEST REF AMM 73-29-00-740-803 OPS CK GOOD NO FAULTS FOUND.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 7,258 hrs · 1,896 cycles

ENG #2 CHANNEL A & B SMR FAULT VIB SYSTEM (FAN POS IND) GROUNDED - YES. ITEM PLACED ON WATCH ITEM PER T/C 730000-L1-1-VAM WHEN THIS/THESE SMR FAULT(S) ARE REPAIRED, TASK 730000-L1-1 IS REQUIRED TO BE ASSIGNED AND ACCOMPLISHED BEFORE THE WATCH ITEM IS CLEARED. WATCH ITEM LIST UPDATED. SEAMC WILL NOTIFY.

Part: IGNITION SYS — FAULTED (NR 2 ENGINE) · airframe 7,179 hrs · 1,878 cycles

IGNITION B FAULT ON START UP. #2 ENGINE GROUNDED - YES. DEFERRED. VERIFIED IGNITION B FAULT AND IGNITION A OPERATIONAL, #2 ENG. DEFERRED IGNITION B ENG 2 PER MEL 74-31-01-01-A.SEAMC LAMONT NOTIFIED , PLACARD INSTALLED , MX PROCEDURE C/W .

Part: IGNITER — FAULTED (NR 2 ENGINE) · airframe 7,086 hrs · 1,854 cycles

ENGINE 2 IGNITION B FAULT, GROUNDED - YES. R & R THE NR 2 ENGINGER IGNITION B IGNITER IAW AMM 74-21-10. PERFORM ENG IDLE TEST NO FAULT.

Part: VALVE — FAILED (NR 1 ENGINE) · airframe 7,032 hrs · 1,838 cycles

DURING CLIMB OUT, ECAM ENGINE 1 HP TIP CONTROL FAULT RECCURING HAD TO ENGINE CANCEL. GROUNDED - YES. REMOVED AND REPLACED ENGINE 1 LPTACC VALVE FIN 4186KS . REF AMM 75-22-05PB401 PERFORMED IDLE TEST (MENU MODE) REF 73-29-00-740-803-A . TEST OK. ACCOMPLISHED NO FAULTS FOUND AT 85% N1 FOR 3 MIN IAW 71-00-00-710-816-A

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 6,689 hrs · 1,749 cycles

ENGINE 1(2) EIU MAINT STATUS. GROUNDED - YES. RESET ENG 1(2) EIU C/B'S. FAULT CLEARS, NO OTHER FAULTS NOTED. WORK DONE IAW AMM 71-00-00.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 6,670 hrs · 1,735 cycles

AIR BLEED CLASS II FAULT MESSAGE GROUNDED - YES. RESET PERFORMED FOR CLASS II AIR BLEED MESSAGE PER AMM 36-11-00-710-002-A. OK FOR SERVICE.

Part: IGNITER — DAMAGED (NR 2 ENGINE) · airframe 6,451 hrs · 1,670 cycles

ENGINE 2 IGNITION B FAULT GROUNDED - YES. #2 EXCITER & #2 IGINITION LEAD WERE PREVIOUSLY REPLACED DEFECT 8038515 & 8056845 RESPECTIVELY. HARNESS FOUND FUSED TO IGNITER HARNESS (IGNITER LEAD) & IGNITER REPLACED IAW AMM 71-51-43 & AMM 74-21-10 SYSTEM TEST OK ALSO ENG RUN WAS ACCOMPLISHED . THIS CLOSED MDDR 65235 MCC NOTIFIED MEL LIST UPDATED.

Part: LINE — CRACKED (NR 2 ENG OIL) · airframe 6,441 hrs · 1,668 cycles

DURING VISUAL INSP OF ENG 2 HIGH OIL CONSUMPTION FOUND OIL LINE TO AGB CRACKED. GROUNDED - YES. R & R OIL TUBE REF AMM 79-21-05. OPS CHECK LEAKS, NO LEAKS FOUND. ENG # 2 OK FOR SERVICE.

Part: SENSOR — FAILED (FUEL STRAINER) · airframe 6,441 hrs · 1,668 cycles

ENGINE 1 FUEL SENSOR FAULT, FUEL STRAINER SENSOR. GROUNDED - YES. REMOVED AND REPLACED #1 ENGINE FUEL STRAINER SENSOR 4081 KS PER AMM 73-34-10 PB 401. OPS AND LEAK CHECK GOOD. THIS CLEARS MDDR 65155. WATCH ITEM LOG UPDATED. MCC CARLOS NOTIFIED.

Part: EXCITER — FAILED (APU) · airframe 6,371 hrs · 1,652 cycles

APU AUTO SHUT DOWN GROUNDED - YES. REMOVED AND REPLACED IGNITION EXCITER IAW 49-41-38 OPS CHECK TRANSFER TO LOG PAGE 8038548 ITEM 3.

Part: IGNITION SYS — FAULTED (NR 2 ENGINE) · airframe 6,159 hrs · 1,606 cycles

ENGINE 2 IGNITION B FAULT GROUNDED - YES. ON DEFERRAL.

Part: IGNITION SYS — INOPERATIVE (NR 2 ENGINE) · airframe 6,051 hrs · 1,579 cycles

ENGINE 2 IGNITION B INOP STATUS GROUNDED - YES. DEFERRED PER MEL 74-31-01-B.

Part: AUTOTHROTTLE SYS — MALFUNCTIONED (COCKPIT) · airframe 6,006 hrs · 1,569 cycles

AUTO THRUST WAS UNABLE TO MAINTAIN AIRSPEED ON APPROACH GROUNDED - YES. PERFORMED AFS AND CATIII TEST REF AMM 22-96-00 AND AMM 22-97-00 OPS CHECK GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 5,986 hrs · 1,565 cycles

ECAM MSG AFTER LND ENG 1 REV 1 MINOR FAULT. (MEL 73-30-05) GROUNDED - YES. PER TSM 78-37-00-810-843-A PERFORMED OPERATIONAL T/R CYCLING TEST IAW AMM 73-29-00-740-804 OPS CHECK OK NO FAULTS ON PFR DURING 3 PRECEDING FLIGHTS THIS CLEAR MDDR 63341 LIST UPDT PLACARD REMOVED MCC NOTIFIED.

Part: SENSOR — FAILED (NR 2 ENG OIL) · airframe 5,651 hrs · 1,481 cycles

ENGINE 2 OIL PRESSURE FUCTUATES FROM 90 - 150 PSI GROUNDED - YES. REPLACED OIL PRESSURE & TEMPERATURE SENSOR (4079KS ) IAW AMM 79-32-05 PB 401. OPS CHECK NORMAL.

Part: STATUS MESSAGE — FALSE ACTIVATION (NR 2 ENGINE) · airframe 5,640 hrs · 1,479 cycles

ENGINE 2 EIU CLASS 2 STATUS MESSAGE GROUNDED - YES. CHECKED EIU 2 FAULT, SHOWN AS IGN 2B. THIS ITEM CURRENTLY DEFERRED PER MDDR 62343. FAULT WILL REMAIN UNTIL (C/B P-42) CLOSE. CONDITION NORMAL. A/C OK FOR SVC. FOLLOW SAFETY PRECAUTIONS REF AMM 73-25-34 PB401 FOR PULLING C/B DISCONNECT CONNECTOR 4601KS2-P2 AT EEC B AND CHECK THE CONDITION OF THE PINS M, L, D, E AWM 71-51-81 PG. 0001 SHEET 2 DISCONNECT CONNECTOR 403VC2-A AT THE PYLON JUNCTION BOX AND INSPECT PIN AND SOCKET 17 AND 18 ON BOTH SIDES AWM 74-31-02 P0027 SHEET 1 REMOVE EIU 2 AMM73-25-34 PB401 AND CHECK PIN 18 ON THE EIU 2 AND THE RACK CONNECTOR AWM 74-31-02 P0027 SHEET 1. IF NO FAULTS FOUND SWAP EIU 1 AND EIU 2 FOR TROUBLESHOOTING ACCOMPLISH ENGINE RUNS TWICE TO TEST THE IGNITION SYSTEM ON BOTH CHANNELS WITH A NEW MX NUMBER INSTALL EIU TO THEIR ORIGINAL LOCATION AND MAKE LOGBOOK ENTRY FOR DISTURBING EIU. ACCOMPLISH RII FOR ALL CONNECTORS THAT WERE REMOVED ENTER THE RESULTS AND CLOSE RMA

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 5,568 hrs · 1,460 cycles

CLASS 2 MESSAGE ENG 1 ANTI-ICE. GROUNDED - YES. DEFERRED. ETOPS RESTRICTED.

Part: WARNING MESSAGE — FALSE INDICATION (CIDS) · airframe 5,326 hrs · 1,385 cycles

CIDS 2 MESSAGE ON ECAM. GROUNDED - YES. PERFORMED RESET IAW AMM 23-73-00-740-005, CHECK GOOD.

Part: CONNECTOR — DIRTY (FIRE LOOP) · airframe 5,237 hrs · 1,353 cycles

#1 ENGINE FIRE LOOP A FAULT.USE TSM TASK 26-12-00-810-803-ALOSS OF DETECTION BY ENGINE-1 LOOP A GROUNDED - YES. CLEANED AND RESECURED CONNECTOR AT 452VC1 (FIN) IAW AMM 26-12-0 PERFORMED OPS CHECK AND ENGINE RUN TO CONFIRM TEST OK FDU TEST OK MDDR 60923 CLEARED MEL LIST UPDATED CONTACTED MOC ROBERT NOTIFIED

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 4,849 hrs · 1,222 cycles

ENG 1 REV MINOR FAULT ON TAXI IN GROUNDED - YES. PERFORMED OPS CHECK ON ENG 1 REV REF AMM 78-30-00. NO FAULT FOUND AT THIS TIME.

Part: FAN — FAULTED (EXTRACT) · airframe 4,614 hrs · 1,139 cycles

EXTRACT FAN FAULT. ACFT GROUNDED.

Part: STRAINER — CLOGGED (NR 1 ENG FUEL) · airframe 4,576 hrs · 1,128 cycles

NR 1 ENGINE FUEL STRAINER CLOGGED. ACFT GROUNDED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 4,479 hrs · 1,104 cycles

ENGINE NR 1 ANTI-ICE FAULT. GROUNDED - YES. ACCOMPLISHED ENGINE IDLE TEST IAW AMM 73-29-00-740-803A. NON CURRENT FAULTS NOTED. A/C OK FOR SERVICE.

Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE) · airframe 4,297 hrs · 1,043 cycles

OUTFLOW VALVE CHATTERING (OSCILLATING) IN ALL MODES OF FLT, SYS 1, 2 AND SEMI AUTO ALL SAME. + OR -200 FPM. GROUNDED - YES. R&R OF OUTFLOW VALVE PER AMM 21-31-51 OPS CHECK GOOD. OK FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 4,178 hrs · 1,004 cycles

CABIN PRESS WARNING ECAM CAME UP AFTER CABIN DOORS WERE CLOSED AND PACK WERE ON WITH APU BLEED AIR GROUNDED - YES. REF TSM 24-00-810-818-A, RESET CAB PRESS CTL 1 AND 2 , PERFORMED CPC 1 AND CPC 2 TEST IAW AMM 21-31-00 , TEST OKAY, NO FAULT NOTED. A/C OK FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 4,095 hrs · 977 cycles

ENG 1 SENSOR FAULT-IN CRUISE FLIGHT FL320. ADVISED "AVOID RAPID THRUST CHANGE" ECAM WAS CLEARED AND STATUS WENT AWAY AFTER 3 SEC. ALL OTHER ENGINE INDICATIONS NORMAL. GROUNDED - YES. PERFORMED NR 1 ENGINE TEST PER AMM 77-11-00-810-836-A. IDLE RUN SATIS & NO FAULTS NOTED. OK FOR SERVICE.

Part: WARNING SYSTEM — INTERMITTENT (COCKPIT) · airframe 4,084 hrs · 974 cycles

INTERMITTENT ENG 1 SENSOR FAULT ECAM MESSAGE CLIMBING THROUGH FL 330 FOR FL 340 WITH ENG. ANTI ICE ON, MESSAGES CLEARED 2 MIN. LATER ENG 1 PARAMETERS NORMAL GROUNDED - YES. PERFORMED ENG IDLE TEST ON NR 1 ENG. PER TSM 77-11-00-810-835-A OPS TEST GOOD NO FAULT

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 4,047 hrs · 963 cycles

VENT EXTRACT FAULT GROUNDED - YES. RESET AEVC. PERFORMED OPS TEST OF AVIONICS EQUIPMENT VENTILATION. NO FAULTS NOTED.

Part: WIRE HARNESS — DAMAGED (NR 1 VBV ACT) · airframe 3,918 hrs · 934 cycles

DURING REMOVAL OF THE NR 1 ENGINE THE RIGHT VBV ACTUATOR, FOUND THE ELECTRICAL WIRE HARNESS CONNECTOR TO THE VBV DAMAGED. ACFT GROUNDED. REPLACED THE WIRE HARNESS HJ5B IAW AMM 73-21-60-400-809-A. FADEC TESTED GOOD. NO FAULTS NOTED

Part: FADEC — FAULTED (NR 2) · airframe 3,415 hrs · 803 cycles

NR 2 ENGINE MINOR FAULT. ACFT GROUNDED. PERFORMED A RESET OF THE FADEC IAW AMM 73-29-00. OPS CHECKED GOOD. NO DEFECTS NOTED AT THIS TIME. OK FOR SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (NR 2 START VALVE) · airframe 1,480 hrs · 770 cycles

NR 2 ENGINE START VALVE FAULT, START VALVE NOT OPEN ECAM MESSAGE DURING ENGINE 2 START. ACFT GROUNDED. PERFORMED FOUR ENGINE DRY RUNS AND ONE ENGINE START. NO FAULTS NOTED AND COULD NOT DUPLICATE FAULT.

Part: FAN — FAILED (E&E BAY) · airframe 3,180 hrs · 746 cycles

VENT EXTRACT FAULT, EXTRACT FAN CB POPPING GROUNDED - YES. ETOPS RESTRICTED. R&R AVIONICS BLOWER FAN REF AMM 21-26-51. OPS CHECK GOOD. THIS CLOSES MDDR 54043. MEL LIST UPDATED. PLACARD REMOVED.

Part: SHUTOFF VALVE — FAULTY (NR 1 ENGINE) · airframe 3,176 hrs · 745 cycles

MULTIPLE ENG 1 ANTI-ICE FAULT AT LOW POWER SETTING. GROUNDED - YES. ETOPS RESTRICTED. R&R ENG NR 1 PRSOV 1 AND 2 IAW AMM 30-21-51. OPS CHECK OK, NO LEAKS NOTED. THIS CLOSES MDDR 54054, MEL LIST UPDATED.

Part: SHUTOFF VALVE — FAILED (NR 1 ENGINE) · airframe 3,176 hrs · 745 cycles

MULTIPLE NR 1 ENGINE ANTI-ICE FAULTS AT LOW POWER SETTING. ACFT GROUNDED. R & R THE NR 1 ENGINE PRSOV 1 AND 2 IAW AMM 30-21-51. OPS CHECKED OK, NO LEAKS NOTED.

Part: WARNING MESSAGE — FALSE ACTIVATION (VENT) · airframe 3,155 hrs · 741 cycles

VENT EXTRACT FAULT ECAM MESSAGE. ACFT GROUNDED. PERFORMED A RESET OF THE CIRCUIT BREAKERS ASSOCIATED OF AVEC IAW TSM 24-00-00-810-818-A, OK.

Part: INDICATION SYS — FALSE INDICATION (WEATHER RADAR) · airframe 3,038 hrs · 713 cycles

"WEATHER AHEAD" WARNING WITH NO WEATHER IN THE AREA GROUNDED - YES. PERFORMED OPERATIONAL CHECK OF THE WEATHER RADAR SYSTEM OPS CHECK GOOD. NO FAULTS FOUND PER AMM 34-41-00-740-050-N.

Part: START VALVE — FAILED (NR 1 ENGINE) · airframe 2,986 hrs · 697 cycles

NR 1 START VALVE WILL NOT OPEN DURING START. ACFT GROUNDED. R & R THE STARTER AIR VALVE FOR THE NR 1 ENGINE, OPS CHECKED GOOD IAW AMM 80-11-15 PB401.

Part: START VALVE — FAILED (NR 2 ENGINE) · airframe 2,963 hrs · 687 cycles

ENG 2 START VALVE FAULT. START VALVE NOT OPEN APPEARED DURING START ATTEMPT. GROUNDED - YES. R&R STARTER VALVE PER A321 AMM 80-11-15. OPS CHECK GOOD. THIS CLEARS MDDR 53489. MEL LIST UPDATED.

Part: START VALVE — INOPERATIVE (NR 1 ENGINE) · airframe 2,936 hrs · 682 cycles

NR 1 ENGINE START VALVE INOPERATIVE. ACFT GROUNDED. OPS TEST OF THE NR 1 ENGINE START VALVE COMPLETED IAW AMM 73-29-00-740-802A. OPS TESTED NORMAL. NO DEFECTS NOTED.

Part: BLADE — DAMAGED (NR 1 ENGINE) · airframe 2,737 hrs · 634 cycles

NR 1 ENGINE FAN BLADE NR 14 TRAILING EDGE BACKSIDE DAMAGED. ACFT GROUNDED. COMPLETED A FULL R & R OF THE ENG FAN BLADES 14 & 5, FRONT SPINNER, FRONT PLATFORM SHROUD AND BLADE 14 & 5 BLADE PLATFORMS IAW AMM 72-21-20. OK FOR SERVICE.

Part: SHUTOFF VALVE — FAILED (ANTI-ICE SYSTEM)

AFTER SHUTDOWN ECAM CLASS II MESSAGE FOR THE NR 2 ENG ANTI-ICE. R & R THE ENG ANTI-ICE PRSOV 2 IAW AMM 30-21-51.