N925VA
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
42 reports on file, 2017-12-21 – 2024-01-20.
Part: SHEAR PLATE — CRACKED (ZONE 100 - FUSE) · airframe 18,450 hrs · 4,723 cycles
AIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23L. REPLACED SHEAR PLATE PER SRM 51-42-11.
Part: SHEAR PLATE — CRACKED (ZONE 100 - FUSE) · airframe 18,450 hrs · 4,723 cycles
AIRCRAFT IN BASE MAINTENANCE: CRACKED / BROKEN AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23R. REPLACED SHEAR PLATE PER SRM 51-42-11.
Earlier reports · 2017–2023 · 40 reports
2023
Part: DOOR SILL — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 18,450 hrs · 4,723 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT AFT PASSENGER / CREW DOOR CUTOUT LOWER SILL AT FR 68 AND S23L. REPAIRED LOWER SILL PER SRM 53-41-14-300-001.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,444 hrs · 4,720 cycles
EMERGENCY DOME LIGHT 209WL IN MAIN CABIN DID NOT ILLUMINATE DURING OPERATIONAL TEST. GROUNDED - YES. REMOVED AND REPLACED EMERGENCY DOME LIGHT IAW A321 AMM 33-51-11-000-001-A.
2020
Part: SENSOR — FALSE INDICATION (NR 1 STARTER) · airframe 6,789 hrs · 1,833 cycles
ENGINE 1 START FAULT STARTER SHAFT SHEAR GROUNDED - YES. R/R ENG 1 N2 SENSOR IAW AMM (CFML) 77-111-10. PERFORMED IDLE TEST IAW AMM 73-29-00. NO FALUTS NOTED OK FOR SVCREMOVED STARTER AIR VALVE FOR INSPECTION.
2019
Part: WARNING MESSAGE — FALSE ACTIVATION (NR 2 ANTI ICE) · airframe 6,053 hrs · 1,670 cycles
CLASS II MESSAGE: "ENG 2 ANTI ICE" GROUNDED - YES. PERFORMED BITE TEST OF NACELLE ANTI-ICE SYSTEM IAW AMM 30-21-00. NO FAULTS SEEN ON EIU. OK FOR SVC. NO FAULT ON ECAM.
Part: HYDRAULIC SYSTEM — LOW · airframe 6,048 hrs · 1,669 cycles
HYD B SYSTEM LO PR @ 34,000 FT. GROUNDED - YES. REMOVED AND REPLACED BLUE HYD PUMP WITH YELLOW HYD PUMP PER AMM 29-12-51 M. ACEVES 29858 -- SERVICED HYD BLUE SYSTEM TO FULL. REF AMM 12-12-29. OPS CHECK OF BLUE HYD SYSTEM PERFORMED. REF AMM 29-12-00. OPS CHECK GOOD.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 5,777 hrs · 1,610 cycles
AIR PACK 2 REGULATOR FAULT. GROUNDED - YES. RESET PACK 2 AND PERFORMED BITE TEST OF PACK 2 TEMP CONTROL. TEST OK. OPERATED PACKS WITH APU BLEED. NO FAULTS OR WARNINGS. REF AMM 21-63-00.
Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 3,530 hrs · 1,019 cycles
JUST PRIOR TO DESCENT, REC'D "CAB PR 2" FAULT ECAM. GROUNDED - YES. RESET CPC AND PERFORMED OPERATIONAL TEST OF THE PRESSURE CONTROL AND MONITORING PER AMM 21-31-00-710-002. OK FOR SVC.
2018
Part: STATUS MESSAGE — FALSE ACTIVATION (FUEL SYSTEM) · airframe 3,090 hrs · 890 cycles
WHITE MAINT FUEL ON STATUS PAGE GROUNDED - YES. PERFORMED FLSS BITE TEST PER A321 AMM 28-46-00, NO FAULTS NOTED, FUEL MSG CLEARED.
Part: FADEC — MALFUNCTIONED (NR 2 ENGINE) · airframe 2,676 hrs · 760 cycles
ENG 2 FADEC SYS FAULT, GROUNDED - YES. RESET ENG NR 2 FADEC AMM 73-29--00-710-040 NO ACTION REQUIRED AMM 77-11-00.
Part: WARNING MESSAGE — ACTIVATED (COCKPIT) · airframe 2,671 hrs · 757 cycles
CLASS 2 MESSAGE ENG 1 FADEC GROUNDED - YES. ON DEFERRAL.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 2,641 hrs · 750 cycles
ENG 2 FADEC FAULT GROUNDED - YES. PERFORMED FADEC TEST & ESN CHANGE PER TSM 73-21-00. TEST OK.
Part: WARNING MESSAGE — FALSE ACTIVATION (NR 2 FADEC) · airframe 2,610 hrs · 744 cycles
ENG 2- MINOR FAULT ONLANDING. GROUNDED - YES. PERFORMED ENG 2 FADEC TEST. TEST OK NO FAULTS AT THIS TIME REF AMM 73-29-00
Part: FAULT MESSAGE — FALSE ACTIVATION (NR 2 ENGINE) · airframe 2,601 hrs · 741 cycles
ENGINE 2 MINOR FAULT GROUNDED - YES. NO FAULTS ON ECAM FADEC TEST IAW LEAP 1A TFU REF 73.20.00.049 MESSAGE CLEARED
Part: FAULT MESSAGE — FALSE ACTIVATION (NR 2 FADEC) · airframe 2,592 hrs · 738 cycles
ENG 2 FADEC SYS FAULT. GROUNDED - YES. PERFORMED FADEC TEST ON ENG 2 CHANNEL A & B REF AMM 73-29-80. TEST OK. PERFORMED TFU REF 73-20-00-049. A/C OK FOR SVC.
Part: FAULT LIGHT — FALSE ACTIVATION (NR 2 ENGINE) · airframe 2,590 hrs · 736 cycles
ENG 2 MINOR FAULTS GROUNDED - YES. PERFORMED FADEC TEST ON #2 ENG TEST OK PER AMM 73-29-00 NO DEFECT NOTED
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 2,580 hrs · 734 cycles
ENG 2 FADEC SYS FAULT. THR LEVER 2 NOT ABOVE IDLE GROUNDED - YES. T/S PER TSM AND FADEC TEST PER AMM 73-29-80-740-803, TEST OK. PERFORMED TFU REF 73.20.00.049. A/C OK FOR SERVICE.
Part: FAULT MESSAGE — FALSE ACTIVATION (NR 2 ENGINE) · airframe 2,590 hrs · 736 cycles
ENG2 FADEC SYS FAULT .THR LEVER 2 NOT ABOVE IDLE GROUNDED - YES. REF LOG PG 8030102 ITEM-1 AND LOG 8030103 ITEM-1 FOR T/S PER TSM AND FADEC TEST PER AMM 73-29-80-740-803, TEST OK. PERFORMED TFU REF 73.20.00.049. A/C OK FOR SERVICE.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 2,570 hrs · 732 cycles
ENGINE 2 MINOR FAULT AFTER LANDING GROUNDED - YES. PERFORMED ENG IDLE TRST TEST OK PER AMM 73-29-00-740-803-A. OPS CK GOOD NO DEFECTS NOTED.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 2,548 hrs · 722 cycles
ENG 2 FADEC SYS FAULT ON TAXI IN. GROUNDED - YES. PERFORMED BITE TEST OF FADEC CHANNELS 2A & 2B. TEST OK PER AMM 73-29-00-740-818.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 2,520 hrs · 713 cycles
ENGINE 2 MINOR FAULT GROUNDED - YES. FOUND CFDS FAULT 771120 ENG 2B-015S-EOS ELECTRIC FAULT. PER TSM 77-11-00-810-840-A. FAULT OCCURED IN PHASE 9 AND NO OCCURANCES IN PAST 5 FLIGHTS. NO MX ACTION REQUIRED.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 2,487 hrs · 697 cycles
ENG 2 MINOR FAULT ECAM MESSAGE. GROUNDED - YES. PER TSM 77-11-00-810-839A PERFORMED ENG 2 IDLE RUN. OPS CHECK GOOD. NO FAULTS NOTED AND NO FAULTS GENERATED IN THE LAST FOUR FLTS PER POST FLT REPORT.
Part: EEC — MALFUNCTIONED (NR 2 ENGINE) · airframe 2,487 hrs · 697 cycles
ENG 2 FADEC SYS FAULT ECAM MSG GROUNDED - YES. SWAP EEC CHAN A FROM ENG 1 TO ENG 2. REMOVED ENG NR 2 CHAN A EEC AND REPLACED W/ CHAN A EEC FROM ENG NR 1 REF AMM 73-21-55. PERFORMED ENG IDLE TEST. OPS CHECK GOOD. NO FAULT FOUND.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 2,456 hrs · 685 cycles
ENG 2 FADEC SYS FAULT. GROUNDED - YES. FAULT CLEARED - NO MX ACTION REQUIRED PER TSM 73-21-01. OK FOR SERVICE.
Part: WARNING SYSTEM — ABNORMAL (COCKPIT) · airframe 2,455 hrs · 684 cycles
ENG 2 FADEC SYS FAULT ECAM MESSAGE AFTER LANDING GROUNDED - YES. PERFORMED ENGINE IDLE TEST OF ENG 2 REF AMM 73-29-00-740-803-A. OPS CHECKS GOOD NO FAULTS ATH THIS TIME.
Part: FAULT MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 2,403 hrs · 670 cycles
ECAM ENGINE 2 FADEC SYS FAULT. GROUNDED - YES. PERFORMED ENG2 FADAC SYS TEST IAW AMM 73-29-00-710-004-B02. TEST OK.
Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 2,350 hrs · 655 cycles
ENGINE 2 MINOR FAULT. GROUNDED - YES. *ON DEFERRAL*
Part: FAULT LIGHT — FALSE ACTIVATION (NR 1 ENGINE) · airframe 2,325 hrs · 641 cycles
NR 1 ENGINE MINOR FAULT. AIRCRAFT GROUNDED. PFR INDICATION EIUI-OIL-IGN POWER. PERFORMED AN OPS TEST OF THE EIU IAW TSM 73-25-00-810-B95A, TEST OK. PERFORMED FADEC TEST OF THE NR 1 ENGINE NON - MOTORING IAW AMM 73-29-00. TESTED OK. CAN NOT DUPLICATE THE FAULT. OK FOR SERVICE
Part: VALVE — FAULTED (NR 2 ENGINE) · airframe 2,317 hrs · 634 cycles
NR 2 ENGINE BLEED AIR ABNORMAL. HP VALVE FAULTED. ACFT GROUNDED.
Part: FADEC — UNKNOWN (NR 2 ENGINE) · airframe 2,317 hrs · 634 cycles
NR 2 ENGINE FADEC SYS FAULTED. ACFT GROUNDED. PERFORMED TSM 77-00-00-810-949-A. NO FAULTS FOUND. OK FOR SERVICE.
Part: ENGINE — FAULTED (NR 2) · airframe 2,208 hrs · 604 cycles
NR 2 ENGINE MINOR FAULT ON LANDING. ACFT GROUNDED.
Part: CONNECTOR — NOT SEATED (HYD PUMP) · airframe 2,208 hrs · 604 cycles
DURING DEGRADED HYDRAULIC POWER CHECK, THE PTU INDICATION WAS NOT FUCTIONING PROPERLY WHEN THE NR 2 ENGINE PUMP WAS OFF. ACFT GROUNDED. RESEATED THE CONNECTOR ON THE NR 2 ENGINE HYD PUMP. PERFORMED AN OPS TEST OF THE PTU WITH ENGINE PUMPS IAW AMM 29-23-00-710-004-A. FUNCTIONAL TESTED GOOD.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 2,121 hrs · 561 cycles
MCDU LEG REPORT EIU1017 IGN POWER SUPPLY RELAY FAULT. GROUNDED - YES. PERFORMED BITE TEST ON EIU1 AND FADEC 1A AND 1B REF. AMM 73-29-00. TEST OK. NO FAULT NOTED AT THIS TIME.
Part: WARNING MESSAGE — FALSE ACTIVATION (THRUST REVERSERS) · airframe 1,727 hrs · 457 cycles
RETURNED TO THE GATE DUE TO A NR 1 & 2 ENGINES REVERSER MINOR FAULTS. ACFT GROUNDED. RESET THE FADEC 1 & 2 CHANNELS A & B AND PERFORMED BITE TEST THROUGH CFDS. NO FAULTS FOUND IAW AMM 73-22-34.
Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 1,409 hrs · 377 cycles
MAINTENANCE STATUS MESSAGE FOR AIR BLEED DISPLAYED AFTER ENGINE SHUTDOWN. ACFT GROUNDED. BMC TESTS PASSED. ACFT OK FOR SERVICE IAW AMM 36-11-00.
Part: WARNING MESSAGE — FALSE ACTIVATION (BLEED AIR) · airframe 1,352 hrs · 361 cycles
CLASS 2 AIRBLEED WARNING MESSAGE. ACFT GROUNDED. ACCOMPLISHED A CHECK IAW ASM 36-12-01SLH 01-0036, NO FAULTS FOUND.
Part: ACTUATOR — WARNING MESSAGE (NR 1 VBV) · airframe 1,352 hrs · 361 cycles
CLASS 2 NR 1 ENGINE FADEC MESSAGE. ACFT GROUNDED. PERFORMED TSM 75-31-00-810-837-A, 75-31-00-810-107-AD, R & R THE NR 1 ENGINE RIGHT VBV ACTUATOR 4167KS IAW AMM 75-31-05. OPS CHECKED GOOD. ACFT OK FOR SERVICE, NO FAULTS NOTED.
Part: O-RING — LEAKING (OIL CAP) · airframe 726 hrs · 205 cycles
NR 1 ENG OIL CONSUMPTION SHOWS 1.111 QT AN HOUR AFTER SERVICING, EXCEEDING 0.45 QT AN HOUR LIMIT. ACFT GROUNDED. REPLACED THE OIL CAP O-RING IAW AMM 79-11-05. OPS CHECKED NORMAL. TAXIED AIRCRAFT AROUND AIRPORT FOR 20 MINUTES. NO DISCREPANCIES NOTED. NO LEAKS NOTED. OILS ON BOTH ENGINES REMAIN CONSISTENT AND EQUAL THROUGHOUT CHECKS. ACFT OK FOR SERVICE
Part: WARNING MESSAGE — FALSE ACTIVATION (NR 2 BLEED) · airframe 602 hrs · 173 cycles
AIR BLEED CLASS 2 MESSAGE. ACFT GROUNDED. PERFORMED A BITE TEST ON BMC 1 & BMC 2. NO FAULTS, TESTED OK IAW AMM 36-11-00-740-804-A.
Part: TARGET — OUT OF ADJUST (R1 DOOR) · airframe 460 hrs · 133 cycles
R1 DOOR WARNING DURING CLIMB. APPROX 0.8 PSI WARNING WENT OFF ON DESCENT BELOW ABOUT 16,000 FT. ACFT GROUNDED. ADJUSTED THE PROXIMITY SWITCH TARGET IAW AMM 52-71-00. OPS CHECKED GOOD.
2017
Part: UNKNOWN — ODOR (CABIN)
THE FLIGHT CREW REPORTED AN OIL ODOR, MID TO REAR CABIN, ROWS 20 TO 30. PERFORMED TSM 05-50-00-810-831-A. PERFORMED MINIMUM IDLE CHECK ISOLATING THE NR 1 & 2 ENGINES, NO ODOR NOTED IN ANY SECTION OF CABIN.