N361VA
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.
22 reports on file, 2015-03-20 – 2024-08-01.
Part: REVEAL — CORRODED (ZONE 800) · corrosion level 2 · airframe 31,288 hrs · 10,866 cycles
L2 DOOR SHAPE P/N: D53480048220200 IS EXFOLIATED. GROUNDED - YES. EVALUATED AREA AND FOUND 2 AREA'S OF CORROSION MEASURING .5"X.2" & .3"X.4" NO ALLOWABLE LIMIT'S EXIST FOR SHAPE P/N-D5348004820200 IAW A320 SRM 53-41-79-02-A REV 149-01MAY2024 REPLACEMENT REQUIRED, REMOVED AND REPLACED L-2 DOOR SHAPE IAW A320 SRM 51-72-11-911-001 REV 149 01MAY2024 AND AIRBUS DWG# D53480048 ISSUE A, REPLACEMENT OF PART CONSIDERED CATEGORY A FH: 31288:17 FC: 10866 MSN: 0551 WV015
Part: DUMMY RAIL — CORRODED (ZONE 200) · corrosion level 2 · airframe 31,288 hrs · 10,866 cycles
CABIN FLOORBEAM CORRODED FWD WET AREA FR 16 - Y81 GROUNDED - YES. EVALUATED AREA AND FOUND AN AREA OF CORROSION MEASURING .5"X.5" ON THE AFT END OF THE PART, IAW A320 SRM 51-11-00 / 001 REV 149 01MAY2024. NO ALLOWABLE DAMAGE LIMITS EXIST FOR RAIL P/N D5311411820001 IAW A320 SRM 53-11-14-10-B. RAIL REQUIRES REPLACEMENT. REMOVED + REPLACED RAIL P/N D5311411820001 P.O.# 1097891.2 IAW A320 SRM 51-72-11-911-001 REV 149 01 MAY 2024 AND AIRBUS DRAWING D53114116 ISSUE A. FH: 31288:17 FC: 10866 MSN: 5515 WV015. REPLACEMENT OF PART IS CONSIDERED CATEGORY A
Part: RIB — CORRODED (ZONE 300) · corrosion level 2 · airframe 31,288 hrs · 10,866 cycles
L/H ELEVATOR O/B LOWER L/E CORROSION GROUNDED - YES. REMOVED RIB #10 IAW A320 SRM 55-21-12-300-002 AND A320 SRM 51-42-11/001. ACCOMPLISHED A UT INSPECTION OF THE UPPER AND LOWER SKIN IAW A320 NTM 51-10-06 USING T8270B DUE 21MAR2025. NO RELEVANT INIDICATIONS WERE NOTED OF THIS TIME. RECEIVED PART PN: D5528154620451 PO: 1098255.3 IAW A320 SRM 55-21-12-04-A. LOCATED, DRILLED AND INSTALLED RIB IAW A320 SRM 55-21-12-300-002, PRIMED AREA IAW A320 SRM 51-21-11/001 AND TOP COAT AREA IAW A320 SRM 51-75-12-911-002. REMOVED CORROSION IAW A320 SRM 51-24-00/001/ ORIGINAL THICKNESS IS .063, REMAINING THICKNESS IS .045, FOUND TO BE BEYOND LIMITS IAW A320 SRM 55-20-00-283-001 REV 149 01MAY2024
Part: SHEAR PLATE — CRACKED (ZONE 200) · airframe 31,288 hrs · 10,866 cycles
CABIN FLOOR AFT FR-69 R/H SHEAR PLATE IS CRACKED GROUNDED - YES. REMOVED AND REPLACED P/N-D537112420300, PO# 1095838.3 SHEAR PLATE IAW A320-200 SRM 51-72-11-911-001 REV 149- 01 MAY 2024
Part: THRESHOLD — CORRODED (ZONE 200) · corrosion level 2 · airframe 31,288 hrs · 10,866 cycles
R2 DOOR THRESHOLD CORROSION MARKE IN RED GROUNDED - YES. REMOVED CORROSION IAW A320 SRM 51-74-00/001 REV. 149-01 MAY 2024 AND FOUND TO BE OUT OF LIMITS IAW A320 SRM 53-41-14-283-002 REV. 149-01 MAY 2024. ORIGINAL THICKNESS BEFORE RE-WORK .071 REMOVED .045. REMAINING THICKNESS AFTER RE-WORK .026 IN AN AREA MEASURING 3ÿ½ X .90ÿ½ TOOL # T8492H. ACCOMPLISHED DVI OF AREA WITH NO FURTHER DEFECTS FOUND. PERFORMED SURFACE HFEC AND OPEN HOLE HFEC IAW A320 NTM 51-10-01 & 51-10-08 TOOL # T8257K, NO DEFECTS NOTED. REPAIRED AFT END OF SILL P/N: D5348004320700 AT FR68-Y1732 STR 23R IAW A320 SRM 53-41-14-300-001 REV. 149-01 MAY 2024 USING REPAIR PRINCIPLE 7 FIG.1 SHEET 4 STEPS 1 THRU 37. SEE ATTACHED PHOTO/MAP-OUT FOR REPAIR LOCATION & DIMENSIONS. REPAIR IS A CATEGORY A WITH NO SUPPLEMENTAL INSPECTIONS, FH: 31288:17 FC: 10866 WV015 MSN: 5515
Part: WEB — CRACKED (ZOEN 200) · airframe 31,288 hrs · 10,866 cycles
CABIN FLOOR AFT FR-69 L/H SHEAR PLATE CRACKED GROUNDED - YES. A REPAIR IS NOT PRACTICAL OR ECONOMICAL ON SHEAR PLATE IAW A320 SRM 51-72-11-911-001 REV 149- 01 MAY 2024. REMOVED AND REPLACED SHEAR PLATE P/N D5347112420200 P.O. 1095838.2 IAW A320 SRM 51-72-11-911-001 REV 149- 01 MAY 2024
Part: THRESHOLD — CORRODED (L2) · corrosion level 2 · airframe 31,288 hrs · 10,866 cycles
L2 DOOR THRESHOLD CORROSION MARKED IN RED GROUNDED - YES. REPAIRED AREA AT FR68 STGR 23L Y1732 IAW A320 SRM 53-41-14-300-001 REV 149-01MAY2024 STEPS 1 THRU 36. ORIGINAL THICKNESS BEFORE REWORK .071, REMAINING THICKNESS AFTER REWORK .040 PER A320 SRM 53-41-14-283-002 FIG 2 SHT1 FLAG NOTE 1, INSTALLED PRINCIPLE 4 REPAIR FOR REWORK UP TO 50% OF NOMINAL THICKNESS. FOUND CORROSION IN TWO EACH ATTACHMENTS HOLES, ORIGINAL HOLE DIA .245, REAMED HOLES TO .330 DIA. MAXIUM ALLOWABLE HOLE DIA .354. ATTACHMENT HOLES FOUND TO BE WITHIN LIMITS IAW A320 SRM 53-41-14-283-002 FIG 2 SHT1 FLAGNOTE 7. ACCOMPLISHED DVI OF REWORK AND SURROUNDING AREA AS WELL AS HFEC OF SURFACE AND BFEC OF ALL HOLES IAW A320 NTM PT6 51-10-08, NO DEFECT FOUND TOOL #T8257F. FH: 31288:17, FC: 10866, WV015 MSN 5515 REPAIR CAT A WITH NO SUPPLEMENTAL INSPECTIONS. SEE ATTACH PHOTOS FOR REPAIR/REWORK DIMENSIONS AND LOCATIONS.
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 31,288 hrs · 10,866 cycles
CABIN FLOORBEAM CORROSION FR-16 -Y254 GROUNDED - YES. REMOVED CORROSION IAW A320 SRM 51-74-00/001 REV. 149- 01 MAY 2024 ON RAIL P/N: D5313531220001 FR16, -Y254, Z1955 IN AN AREA MEASURING 1.1" X .5". ORIGINAL THICKNESS BEFORE RE-WORK .087, REMOVED .020, AMOUNT REMAINING AFTER RE-WORK .067 MAXIMUM ALLOWABLE RE-WORK DEPTH .031, FOUND TO BE WITHIN LIMITS IAW A320 SRM 53-11-14-283-007 FIG 9 SHEET 1 FLAGNOTE 1. INSPECTED RE-WORK AREA AND ENSURED NO OTHER PREVIOUS BLEND-OUTS OR REPAIRS EXIST. RESTORED SURFACE PROTECTION IAW A320 SRM 51-75-12 REV 149- 01 MAY 2024. THIS TASK IS CATEGORY A WITH NO SUPPLEMENTAL INSPECTIONS. MSN: 5515 FH: 31288:17 FC: 10866 WV: 015. SEE ATTACHED PHOTO/MAP-OUT OF RE-WORK AREA
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 31,288 hrs · 10,866 cycles
SEAT TRACK CORRODED AT FRAME C21-Y1292 FWD O/B R/H GROUNDED - YES. REMOVED AND REPLACED SEAT TRACK ON D5311278220200 P.O.1095204.3 IAW A320 SRM 51-44-11/001 REV 149 REV 01MAY2024 A320 SRM 51-42-11/001 REV 149 01MAY2024, A320 SRM 51-72-11-911-001 REV 149 01MAY2024 AND AIRBUS DWG D53112812. FH:31288:17 FC:10866 WV015 MSN:5515 FR12-FR24 Y-1292. NO ALLOWABLE DAMAGE LIMITS EXIST DUE TO MODIFICATION 39700
Part: WEDGE — DENTED (ZONE 500 FLAP) · airframe 31,288 hrs · 10,866 cycles
LESSOR ITEM : L/H I/B FLAP DENTS REQUIRE MAPPING AND MEASURE FOR D&B RECORD AND SERVICEABILITY GROUNDED - YES. PERFORMED A CATEGORY A PERMANENT REPAIR OF THE LEFT-HAND INBOARD FLAP DENTS. THIS NON ROUTINE IS ONLY FOR DOCUMENTATION OF THE STRUCTURAL DIFFICULTY REPORT OF THE OUTBOARD REPAIR, LOCATED ON THE FLAP TRAILING EDGE WEDGE LOWER SKIN IN ZONE 2. THE REPAIR IS 81.25ÿ½ FROM THE INBOARD EDGE, 17.5" WIDE, 12.5ÿ½ TALL. FOR REPAIR PROCEDURES, REFER TO LOG PAGE G2003260, SO: 536493, OPS: 21760. A/C TYPE: A320-214, A/C SN: 5515, A/C FLIGHT HOURS: 31, 288: 17 A/C FLIGHT CYCLES: 10,866, A/C WEIGHT VARAINT: WV015, FLAP PART NUMBER: D5757065005200, FLAP SERIAL NUMBER: TB15515.
Part: SKIN — PUNCTURED (ZONE 600 FLAP) · airframe 31,288 hrs · 10,866 cycles
LESSOR ITEM: RH INBD FLAP LOWER AREA WITH SEVERAL DENTS - EVALUATE / REPAIR AND INCLUDE IN D&B (NOTE ONLY: DB #2) GROUNDED - YES. REMOVED 35 EA FASTENERS TO FOM IAW A320 SRM 57-52-00-300-093 REV. 149. FOUND 66 EA. DENTS WITH PUNCTURES AT 2EA. CLUSTERS REQUIRING REPAIR IAW A320 SRM 57-52-00-283-105 REV 149 & A320 SRM 57-52-00-300-093 REV 149. REMOVED SKIN & CORE CLUSTER 1 FROM RIB 1 4T. 375ÿ½ TO 58.25ÿ½ FROM RIB 1 LWR TE WEDGE & CLUSTER 2 83.25ÿ½ FROM RIB 1 TO 94.75ÿ½ FROM RIB 1 ÿ½ CLUSTER 1 11ÿ½ X 10ÿ½ / CLUSTER 2 11.5ÿ½ X 9.25ÿ½ AND REPAIRED IAW A320 SRM 57-52-00-300-093 REV 149. RELOCATED PERSPECTIVE FATENER HOLES AT AFT SPAR OF WEDGE FOR REINSTALLING TE WEDGE REMOVED TO FOM IAW A320 SRM 57-52-00-300-093 REV. 149 ON S/O 536493 OPS 21999 ATTACHED COPY. FH-31288:17, FC-108-66, WV-015.
Part: WEDGE — DENTED (ZONE 500 FLAP) · airframe 31,288 hrs · 10,866 cycles
LESSOR ITEM: LH INBD FLAP LOWER AREA WITH SEVERAL DENTS - EVALUATE / REPAIR AND INCLUDE IN D&B (NOTE ONLY: DB #3) GROUNDED - YES. PERFORMED A CATEGORY A, PERMANENT REPAIR OF THE LEFT-HAND INBOARD FLAP LOWER AREA DENTS IN 2 AREAS. THE INBOARD REPAIR IS LOCATED ON THE INBOARD FLAP TRAILING EDGE WEDGE LOWER SKIN, IN ZONE 2. IT IS 45ÿ½ FROM THE INBOARD EDGE, 17.75ÿ½ WIDE, 12.5ÿ½ TALL. THE OUTBOARD REPAIR IS LOCATED 81.25ÿ½ FROM THE INBOARD EDGE, 17.5" WIDE, 12.5ÿ½ TALL. A/C TYPE: A320-214. A/C SN: 5515, A/C FLIGHT HOURS: 31,288: 17, A/C FLIGHT CYCLES: 10,866, A/C WEIGHT VARIANT: WV 015, FLAP PART NUMBER : D5757065005200, FLAP SERIAL NUMBER: TB15515.
Earlier reports · 2015–2019 · 10 reports
2019
Part: COFFEEMAKER — FAILED (AFT GALLEY) · airframe 21,773 hrs · 6,822 cycles
AFT COFFEE MAKER WAS TURNED ON SPARKS AND A FLAME WAS OBSERVED AND THEN WAS IMMEDIATELY TURNED OFF. GROUNDED - YES. R/R AFT COFFEE MAKER IAW AMM 25-35-15, OPS CHECK GOOD, THIS CLEARS MDDR 64117, NEF LIST UPDATED, MCC NOTIFIED
2018
Part: AIRBAG — UNWANTED DEPLOY (ROW 3) · airframe 18,476 hrs · 5,725 cycles
ROW 3, RT SIDE, ALL THREE SEAT AIR BAGS DEPLOYED DURING FLIGHT. ACFT GROUNDED. REPLACED THE AIRBAG SYS COMPONENTS IAW CMM 25-21-77.
Part: CONTROL PANEL — ODOR (CABIN) · airframe 17,520 hrs · 5,460 cycles
DETECTED A BURNING PLASTIC ODOR IN FORWARD CABIN. ACFT GROUNDED. R & R THE FORWARD FLIGHT ATTENDANT PANEL IAW AMM 23-73--12, OPS CHECKED GOOD.
2017
Part: GENERATOR — NO TEST (EMERGENCY)
DURING AN OVERNIGHT CHECK, FOUND EMERGENCY GENERATOR TEST FAILED. REPLACED CSM/G 8XE IAW AMM 24245104. LEAK AND OPERATIONS CHECKED GOOD. OK FOR SERVICE.
2016
Part: FAN — FAILED
ACFT EXPERIENCED A VENT BLOWER FAULT MESSAGE ON ECAM, VIBRATION AND ELECTRICAL BURNING ODOR IN THE FLIGHT DECK APPROXIMATELY 20 MINUTES AFTER DEPARTURE. THE FLIGHT CREW ACCOMPLISHED FCOM PROCEDURES AND RETURNED TO DEPARTURE. TECHS FOUND THE AVIONICS BLOWER FAN SEIZED AND THE AVIONICS INLET CHECK VALVE BROKEN. THE FAILED UNITS WERE REPLACED IAW AMM 21-26-51 PB401 & 21-26-56 PB401, NO FURTHER PROBLEMS REPORTED ON SUBSEQUENT FLIGHTS.
Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 5,515 hrs · 3,347 cycles
ACFT EXPERIENCED THE GROUND POWER DROP OFF WITH THE EMERGENCY LIGHT WHICH IN THE ARM POSITION. THE EMERGENCY LIGHT SYSTEM DID NOT ACTIVATE AS EXPECTED. DURING TROUBLESHOOTING IAW TSM 33-51-00-810-812-A IT WAS DETERMINED THAT ALL 4 ESPU BATTERIES WERE AT FAULT AND WERE REPLACED IAW AMM 33-51-38-000-002-A AND AMM 33-51-38-400-002-A. EMERGENCY LIGHT OPS CHECKS GOOD IAW AMM 33-51-00-710-001-A.
2015
Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 8,744 hrs · 2,797 cycles
DURING PREFLIGHT, CREW REPORTED: R1 SLIDE PRESSURE LOW. R & R DOOR SLIDE, 7501 MM, R1 DOOR REF AMM 25-62-44, PB 401. OK FOR SERVICE.
Part: WIRE — CUT (EMERGENCY LIGHTS) · airframe 8,229 hrs · 2,650 cycles
DURING OVERNIGHT INSPECTION, MAINTENANCE DISCOVERED ROWS 20 AND 21 LT SIDE EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE FOUND 1 WIRE CUT AND PERFORMED A SPLICE REPAIR IAW ESPM 20-53-29, OPS NORMAL WITH NO FURTHER DEFECTS NOTED.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 6,993 hrs · 2,269 cycles
ACFT REPORTED EMERGENCY LIGHT OVER L1 AND R1 DOORS AND LT OVERWING EXIT ON INFLIGHT DOOR L2/ R2 AND RT OVERWING EXIT ARE OFF. BATTERY ON EPSU 10WL WAS REPLACED WITH NO FURTHER DEFECTS NOTED. OUTBOUND FLIGHT TOO A 15 MINUTE DELAY.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 6,993 hrs · 2,269 cycles
EMERGENCY LIGHT OVER L1 AND R1 DOORS AND LT OVERWING EXIT ON INFLIGHT DOOR L2 / R2 AND RT OVERWING EXIT ARE OFF. BATTERY ON EPSU 10 WL WAS REPLACED WITH NO FURTHER DEFECTS NOTED. OUTBOUND FLIGHT TOOK A 15 MINUTE DELAY.