N835VA
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.
40 reports on file, 2011-08-31 – 2022-12-17.
Part: LIGHT — FAILED (MAIN PASSENGER C) · airframe 39,280 hrs · 12,992 cycles
SEVERAL EMERGENCY EXIT LIGHTS INOP. GROUNDED - YES. REMOVED AND REPLACED EXIT SIGN LIGHTS AT L1 DOOR, L2 DOOR, R2 DOOR AND EMERGENCY POWER SUPPLY UNIT (EPSU) ON POSITION 10WL IAW A320 AMM 33-51-13-000-001-A, 33-51-38-000-001-A AND 33-51-38-400-001-A. PERFORMED OPS CHECK OF EMERGENCY LIGHTS IAW A320 AMM 33-51-00-710-805-A. OPS CHECK GOOD.
Part: FITTING — CORRODED (R2 GIRT BAR) · corrosion level 2 · airframe 39,280 hrs · 12,992 cycles
R2 DOOR FWD GIRT BAT FITTING FLOOR PANEL UPPER SKIN IS CORRODED. GROUNDED - YES. REMOVED AND REPLACED R2 DOOR FWD GIRT BAR FITTING FLOOR PANEL IAW SRM 51-42-11 REV. 143.
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 39,280 hrs · 12,992 cycles
FLOOR PANEL 231QF HAS AREA OF DELAMINATION. GROUNDED - YES. REMOVED AND REPLACED CABIN FLOOR PANEL 231QF IAW A320 AMM 53-00-00-000-801-A02 AND AMM 53-00-00-400-801-A02.
Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 39,280 hrs · 12,992 cycles
MAIN CABIN FLOOR PANEL 241JF HAS AREA OF DELAMINATION. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOOR PANEL 241JF PER A320 AMM 53-00-00-801-A02. ORIG SUB DATE: 12/16/2022
Part: FLOOR PANEL — DELAMINATED · airframe 39,280 hrs · 12,992 cycles
MAIN CABIN FLOOR PANEL 241JF HAS AREA OF DELAMINATION. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOOR PANEL 241JF PER A320 AMM 53-00-00-801-A02.
Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 39,280 hrs · 12,992 cycles
MAIN CABIN FLOORBOARD 231AF HAS AREA OF DELAMINATION. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOORBOARD 231AF IAW A320 AMM 53-00-00-000-801-A02 AND AMM 53-00-00-400-801-A02.
Part: FLOOR PANEL — DELAMINATED · airframe 39,280 hrs · 12,992 cycles
MAIN CABIN FLOOR PANEL 231VF HAS AREA OF DELAMINATION. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOOR PANEL 231VF IAW A320 AMM 53-00-00-400-801-A.
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 39,280 hrs · 12,992 cycles
CABIN FLOOR PANEL 231BF HAS AREA OF DELAMINATION. GROUNDED - YES. REMOVED AND REPLACED CABIN FLOOR PANEL 231BF IAW A320 53-00-00-00-801-A02 AND AMM 53-00-00-400-801-A03.
Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 39,280 hrs · 12,992 cycles
MAIN CABIN FLOORBOARD 231KF HAS AREA OF DELAMINATION. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOORBOARD 231KF IAW A320 AMM 53-00-00-000-801-A03 AND AMM 53-00-00-400-801-A02.
Part: FLOOR PANEL — DELAMINATED · airframe 39,280 hrs · 12,992 cycles
MAIN CABIN FLOOR PANEL 221EF HAS SEVERAL AREAS OF DELAM. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOOR PANEL 221EF IAW A320 SRM 53-00-283-00 PG 6.
Part: FLOOR SUPPORT — CORRODED (FRM 68) · corrosion level 2 · airframe 39,280 hrs · 12,992 cycles
MAIN FLOOR "L" BEAM AT FR68 AND -Y1162.5 HAS CORROSION ON TOP OF BEAM. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOOR "L" BEAM AT FR68-69 Y=-1162.5 PAER A320 SRM 53-41-14-01-A REV. 142 AND 51-42-11/001 REV. 142.
Part: FLOOR PANEL — CRACKED (CABIN) · airframe 39,280 hrs · 12,992 cycles
MAIN CABIN FLOOR PANEL 131GF HAS A PUNCTURE. GROUNDED - YES. ACCOMPLISHED PERMANENT REPAIR OF MAIN CABIN FLOOR PANEL 131GF IAW A320 SRM 53-02-00-300-004 AND SRM A320 53-02-00-283-001 REV 142-01 AUG 2022.
Part: FLOOR PANEL — PUNCTURED · airframe 39,280 hrs · 12,992 cycles
MAIN CABIN FLOOR 232SF LARGE PUNCTURE THROUGH COMPOSITE CORE AT FR29. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOOR BOARD 232SF AT FR29 IAW A320 AMM 53-00-00-400-801-A-01.
Part: PROFILE — CORRODED (FRM 34) · corrosion level 2 · airframe 39,280 hrs · 12,992 cycles
FORWARD CARGO R/H OUTBOARD FLOOR SUPPORT FRAME UPPER SURFACE HAS CORROSION FR31 TO FR34. GROUNDED - YES. REMOVED AND REPLACED NEW PROFILE PLATE AT FR31 TO FR34 AND Y765 IAW A320 SRM REV 142 53-21-14-03-A ITEM 15 AND SRM 51-72-11-911-001.
Part: FLOORBEAM — CORRODED · corrosion level 2 · airframe 39,177 hrs · 12,951 cycles
MAIN CABIN FLOORBEAM UPPER SURFACE CORRODED BETWEEN FR67 AND FR68 RBL 24. GROUNDED - YES. REMOVED AND REPLACED 1EA FLOORBEAM IN MAIN CABIN AT RBL24 FR67 - FR70 IAW A320 SRM 54-41-14-01-A AND SRM 51-42-11/001 REV. 26 01 AUG 2022.
Part: SHEAR PLATE — CORRODED (MAIN CABIN) · corrosion level 2 · airframe 34,709 hrs · 11,811 cycles
MAIN CABIN LH AFT FLOOR SHEAR PLATE UPPER SURFACE CORRODED AT FR70 GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOOR LH AFT SHEAR PLATE UPPER SURFACE AT FR70 STGR 22L
Part: FITTING — GOUGED (FRM 70) · airframe 34,709 hrs · 11,811 cycles
MAIN CABIN FLOOR RH OUTBD FLOORBOARD FITTING UPPER SURFACE GOUGED AT FR70 GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOOR RH OUTBD FLOORBOARD FITTING AT FR70 IAW A320 SRM 51-72-11-911-002
Part: FLOORBOARD — CORRODED (CABIN) · corrosion level 2 · airframe 39,280 hrs · 12,992 cycles
L2 DOOR FLOORBOARD UPPER SKIN CORRODED BETWEEN FR66 AND FR68. GROUNDED - YES. REMOVED AND REPLACED FLOORBOARD PANEL 261LG BETWEEN FR66 AND FR68 IAW A320 SRM 53-02-00-233-001.
Part: SHEAR TIE — CORRODED (FRM 70 S23R) · corrosion level 2 · airframe 39,177 hrs · 12,951 cycles
MAIN CABIN OUTBD SHEAR PLATE IS CORRODED AT UPPER SURFACE FR70. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN R/H OUTBD SHEAR PLATE AT FR70 IAW SRM 51-42-11 REV. 142 01 AUG 2022.
Part: FLOORBOARD — CORRODED (CABIN) · corrosion level 2 · airframe 39,280 hrs · 12,992 cycles
R2 DOOR FLOORBOARD LOWER SKIN CORRODED AT FR68. GROUNDED - YES. REMOVED AND REPLACED R2 DOOR FLOORBOARD AT FR66 - FR68 IAW A320 SRM 53-02-00-233-001.
Part: FLOORBEAM — CORRODED (FRM 68) · corrosion level 2 · airframe 39,177 hrs · 12,951 cycles
MAIN CABIN OUTBD FLOORBEAM UPPER SURFACE HAS CORROSION IN 2EA PLACES AT FR68 JUST INBD OF GIRT BAR FITTING. GROUNDED - YES. ACCOMPLISHED CATEGORY "A" PERMANENT REPAIR AT MAIN CABIN R/H OUTBD DOOR SILL AT FR68 IAW SRM 53-41-14-80-A AND SRM 53-41-14-300-001 REV. 142 01 AUG 2022.
Part: FLOORBOARD — CORRODED (CABIN) · corrosion level 2 · airframe 39,280 hrs · 12,992 cycles
MAIN CABIN FLOORBOARD AT R1 DOOR HAS CORROSION PANEL 222FF. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOORBOARD AT R1 DOOR PANEL 222FF IAW A320 AMM 53-00-00-400-801-A.
Part: FLOORBOARD — DAMAGED (COCKPIT) · airframe 34,700 hrs · 11,805 cycles
L/H SIDE CAPT SEAT FLOOR PANEL FWD CORNER BROKEN OFF GROUNDED - YES. REMOVED AND REPLACED CAPT SEAT FLOOR PANEL 211HF IAW A320 AMM 53-12-11-400-001.
Part: FLOORBOARD — CORRODED · corrosion level 2 · airframe 39,280 hrs · 12,992 cycles
MAIN CABIN FLOOR BOARD FWD CABIN L1 DOOR ENTRY 221FF HAS CORROSION. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOOR BOARD 221FF AT L1 DOOR ENTRY WAY IAW A320 AMM 53-00-00-000-801-A.
Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 39,280 hrs · 12,992 cycles
FLOORBOARD HAS DELAM FWD CABIN PANEL 221EF. GROUNDED - YES. ACCOMPLISHED PERMANENT REPAIR ON MAIN CABIN FLOORBOARD 221EF IAW A320 SRM 53-02-00-283-001 REV 142 01 AUG 2022 AND SRM 53-02-00-300-001 FIG 001.
Part: FITTING — CORRODED (SCUFF PLATE) · corrosion level 2 · airframe 39,280 hrs · 12,992 cycles
R1 DOOR CUTOUT HAS 3EA AREAS OF CORROSION UNDER LWR SCUFF PLATE GROUNDED - YES. REMOVED AND REPLACED CORRODED FITTING IAW A320 SRM 51-42-11 REV 143 01 NOV 2022
Part: BLANKING PLATE — CORRODED (GIRT BAR) · corrosion level 2 · airframe 39,280 hrs · 12,992 cycles
LH AFT PASSENGER DOOR FLOOR HAS CORROSION AT FWD GIRT BAR GROUNDED - YES. REMOVED AND REPLACED FWD GIRT BAR BLANKING PLATE AT LH AFT PASSSENGER DOOR IAW A320 AMM 53-13-31-400-003-A
Part: WEB — CORRODED (AFT CARGO) · corrosion level 2 · airframe 39,280 hrs · 12,992 cycles
AFT CARGO DOOR SILL BOX UPPER WEB CORRODED AT FR53. GROUNDED - YES. REMOVED AND REPLACED AFT CARGO DOOR SILL UPPER WEB BETWEEN FR52 - FR56 A320 SRM 53-41-49-07-A.
Part: WEB — CORRODED · corrosion level 2 · airframe 39,280 hrs · 12,992 cycles
AFT CARGO DOOR SILL BOX UPPER WEB CORRODED AT FR53. GROUNDED - YES. REMOVED AND REPLACED AFT CARGO SILL UPPER WEB BETWEEN FR52 - FR56 PER A320 SRM 53-51-49-07-A.
Part: SUPPORT FRAME — CORRODED (FRMS 31-34) · corrosion level 2 · airframe 34,493 hrs · 11,723 cycles
FWD CARGO L/H FLOOR SUPPORT FRAME HAS CORROSION ON UPPER SKIN AND RIVET SHEARED FR31 TO FR34 GROUNDED - YES. REMOVED AND REPLACED FWD CARGO L/H OUTBD FLOOR SUPPORT FRAME AT FR31 TO FR34 Y=765 IAW A320 SRM 53-21-41-03-A REV 142 01 AUG 2022 AND SRM 51-42-11 REV 143-2 01 AUG 2022.
Part: FLOOR SUPPORT — CRACKED (FRNS 28-31) · airframe 39,280 hrs · 12,992 cycles
FWD CARGO L/H OUTBD FLOOR SUPPORT FRAME IS CRACKED. GROUNDED - YES. REMOVED AND REPLACED FWD CARGO L/H OUTBD FLOOR SUPPORT BETWEEN FR28 - FR31 AND Y = 765 IAW A320-200 SRM REV. 142 DATE 01 AUG 2022 TASK 51-72-11-911-002 AND SRM 53-21-14-03-A ITEM 005.
Part: BLANKING PLATE — CORRODED (RT DOOR) · corrosion level 2 · airframe 39,280 hrs · 12,992 cycles
CORROSION ON AFT R/H PASSENGER DOOR LOWER PLATE BELOW AFT GIRT BAR FITTING. GROUNDED - YES. REMOVED AND REPLACED BLANKING PLATE IAW A320 AMM 52-16-31-400-003-A AND AMM 52-13-00-800-001-A.
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 39,280 hrs · 12,992 cycles
MAIN CABIN FLOOR PANEL 232DF HAS R/H FWD CORNER HAS DELAMINATION. GROUNDED - YES. ACCOMPLISHED PERMANENT REPAIR ON MAIN CABIN FLOOR PANEL 232DF AT FR20 IAW A320 SRM ADL 53-12-00-283-005 FIG 001 AND SRM 53-12-00-300-002 RV 142 01 AUG 2022.
Part: SLIDING WINDOW — SCRATCHED · airframe 38,806 hrs · 12,796 cycles
F/O SLIDING WINDOW HAS MANY SCRATCHES GROUNDED - YES. REMOVED AND REPLACED F/O SLIDING WINDOW IAW A320 AMM 56-12-11-000-002-A. OPS CHECK GOOD.
Part: FITTING — CRACKED · airframe 33,133 hrs · 11,129 cycles
DURING TC 545400-01-1-VAM RH UPPER SPAR FOUND 3 CRACKS IN AREA 4 AND 1 CRACK IN AREA 6 OUTBOARD CORNER FITTING REF STEP 20 & 21 GROUNDED - YES. ACCOMPLISHED PERMANENT REPAIR ON RH PYLON AFT FIXED UPPER SPAR BETWEEN RIB 14-15 PER TC 545400-01-1-VAM RH REPAIRS.
Part: FITTING — CRACKED · airframe 33,133 hrs · 11,129 cycles
WHILE ACCOMPLISHING TC 545400-01-1-VAM LH UPPER SPAR.C001, FOUND OUTBD CORNER FITTING CRACKED AREA 6. GROUNDED - YES. REMOVED AND REPLACED OUTBD CORNER FITTING ON LH PYLON AFT FIXED FAIRING UPPER SPAR RIB 15. ALL WORK ACCOMPLISHED PER TC 545400-01-1-VAM. LH REPAIRS
Earlier reports · 2011–2017 · 4 reports
2017
Part: UNKNOWN — ODOR (CABIN)
SHORTLY AFTER TAKEOFF, FLIGHT CREW REPORTED ODD MUSTY ODOR, AFTER ENGINE SHUTDOWN INFLIGHT CREW REPORTED SAME ODOR. MX EVALUATED CREW REPORTING SHEET AND ODOR DECISION TABLE IAW TSM 0550009910010000A. MX REMOVED AND REPLACED RECIRC FILTER IAW AMM 212141 AND PERFORMED A PACK BURN IAW TSM 055000. NO ODOR PRESENT, NO FURTHER REPORTS OF ODOR.
2015
Part: FAN — FAILED
FLIGHT EXPERIENCED AN ELECTRICAL BURNING ODOR IN THE CABIN AND FLIGHT DECK, REPORTED BY FLIGHT CREW. UPON ARRIVAL, MAINTENANCE ACCOMPLISHED TSM 24-00-00-810-823-A & 21-26-00-810-809. THE EQUIPMENT COOLOING SYS EXTRACT FAN WAS FOUND FAILED AND SUBSEQUENTLY DEFERRED IAW MEL 21-26-02-01. THE FAN WAS REPLACED IAW AMM 21-26-51. DURING OVERNIGHT MAINTENANCE, NO FURTHER PROBLEMS REPORTED.
2014
Part: AIR DATA MODULE — FAULTED (NR 1)
THE FLIGHT CREW REPORTED AN ADR 1 NAV FAULT DISPLAYED ON ECAM WITH ASSOCIATED FAULT LIGHT AND LOSS OF CAPT AIRSPEED AND ALTITUDE. THE CREW ACCOMPLISHED FCOM PROCEDURES AND CONTINUED TO DESTINATION WITHOUT FURTHER INCIDENT. OUR CONTRACT MAINTENANCE PARTNER MET THE ACFT UPON ARRIVAL AND RESET THE NR 1 ADIRU AND ACCOMPLISHED BITE TEST IAW AMM 34-18-00 WITH NO FAULTS FOUND. DURING THE SUBSEQUENT TAKEOFF ROLL THE CREW EXPERIENCED LOSS OF AIRSPEED INDICATION ON THE CAPT PRIMARY DISPLAY UNIT AND ABORTED THE TAKEOFF. THE ACFT WAS REMOVED FROM SERVICE FOR TROUBLESHOOTING AND A CREW OF TECHS WAS DISPATCHED. DURING TROUBLESHOOTING THE ADM, 19FP1, WAS FOUND FAULTY AND REPLACED, THE NR 1 ADIRU WAS ALSO REPLACED PRECAUTIONARY. ALL REQUIRED OPS TESTS WERE ACCOMPLISHED AND THE ACFT WAS RETURNED TO SERVICE. THE ACFT DEPARTED WITHOUT FURTHER INCIDENT.
2011
Part: UNKNOWN — ODOR (CABIN)
ACFT MADE A NORMAL DEPARTURE AT 2313Z. AT APPROX 1 HR INTO FLIGHT, THE IN-FLIGHT TEAM NOTIFIED THE FLIGHT DECK OF A HOT ELECTRICAL ODOR IN THE VICINITY OF ROWS 19-21. NO SMOKE WAS NOTED. THE CREW CONTACTED THE DISPATCHER AND MX VIA AIRCELL. CHECKLIST ITEMS WERE ACCOMPLISHED. IT WAS DETERMINED TO LAND ASAP AT THE CLOSEST DIVERSION CITY. AN EMERGENCY WAS DECLARED BY THE FLIGHT CREW AND THE ACFT MADE AN UNEVENTFUL LANDING AT 0119Z(31ST). THE FIRE DEPT MET THE ACFT, AND DID A CABIN INSPECTION INCLUDING INFRARED SENSORS THAT REVEALED NO HEAT SIGNATURES. NO ODOR WAS PRESENT AT THAT TIME. MX HAD CONTACTED AND ARRANGED A 1-TIME TECH AUTHORIZATION FOR AN INSP OF THE SOURCE OF THE ODOR. MX PROVIDED REF TSM 24-00-00-810-823 FOR "BURNING SMELL OR FUMES IN THE CABIN" AND 26-15-00-810-804 "ODORS AND MIST IN THE CABIN AND NOT FIRE" INSPECTION. THEY WERE ALSO INSTRUCTED TO DO A VISUAL OF THE UNDER FLOOR WIRING AND IFE BOXES FROM THE AFT PIT THRU THE CEILING PANELS IN THE SUSPECTED AREA. NO DEFECTS WERE NOTED AS WELL AS NO FAULTS OR BURNED OUT LIGHTS IN THE AREA WERE NOTED. THE ACFT WAS DEEMED AIRWORTHY AFTER LOG ENTRIES OF FINDINGS AND PANEL OPEN AND CLOSE UP. IT DEPARTED AS A REPOSITION FLIGHT AFTER A 10 HOUR DELAY. GUEST WERE ACCOMMODATED AND TAKEN ON TO DESTINATION. UPPON ARRIVING, MFG WAS INSTRUCTED TO ACCOMPLISH A FULL CHECK OF THE IFE SYS AFTER REACTIVATION. NO OUTAGES OR FAILURES WERE NOTED ON ANY ROWS. THE ACFT WAS RETURNED TO FULL SERVICE AND FLEW AN UNEVENTFUL SCHEDULE.