N642VA

Service difficulty reports · 29

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N642VA' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR ASAA2024030449340Floorboard · delaminatedCABIN FLOORBOARD 231VF DELAMINATED GROUNDED - YES. REPAIRED CABIN FLOORBOARD ZONE A PANEL 231VF AFT 3 P/N SB2076-15 S/N:NSN ON A320-214 S/N 3670 FH:41051 FC:14985 WV:012 USING CATEGORY A PERMANENT REPAIR IAW A320-200 SRM 53-02-00-283-001 TABLE 002 REV 147 01 NMar 4, 2024 · N642VA · Airbus A320214 · Fuselage Floor PanelSDR ASAA2024030449338Floorboard · delaminatedCABIN FLOORBOARD 251FF DELAMINATED GROUNDED - YES. REPAIRED PANEL 251FF 1 FWD & 251FF 3 AFT USING CATEGORY A PERMANENT REPAIR IAW A320-214 SRM 53-02-283-001 REV 147-01 NOV 2023, SRM 53-02-00-300-013 REV 147-01 NOV 2023, SRM 51-77-12-911-002 REV 147-01 NOV 2023Mar 4, 2024 · N642VA · Airbus A320214 · Fuselage Floor PanelSDR ASAA2024020249339Floorboard · dentedLESSOR ITEM (19): DENT AND BUCKLE #23. DAMAGE FLOOR PNL IN AFT CARGO: 151MF. NON-ROUTINE PROVIDED WITH DIMENSIONS BUT WITH NO MATERIAL INFORMATION TO PERFORM THE REPAIR. PROVIDE A NON-ROUTINE TO RE-ACCOMPLISH REPAIR FOR THIS DAMAGE AND INSPECT REMAINDER OF PANFeb 2, 2024 · N642VA · Airbus A320214 · Fuselage Floor PanelSDR ASAA2024012549341Floorboard · delaminatedMAIN CABIN L/H FLOOR PANEL #241FF FR40 UPPER SKIN PEELING OFF. GROUNDED - YES. RECIEVED PANEL 241FF PN# E5367193300000 PO# 1080959.0 IAW A320 IPC 53-32-04-025 REV 9-01NOV2023 INSTALLED 241FF IAW A320 AMM 53-00-00-400-801-A02 REV 9-01NOV2023 #T03835-152Jan 25, 2024 · N642VA · Airbus A320214 · Fuselage Floor PanelSDR ASAA2022021637440Reservoir · depletedR/H OVERWING SLIDE ACTUATION CABLE DISCONNECTED IN AFT CARGO. GROUNDED - YES. REMOVED R/H OVERWING SLIDE INFLATION RESERVOIR ASSEMBLY S/N A16313 AND REPLACED WITH SERVICEABLE UNIT IAW AIRBUS A320 AMM 25-62-46.Feb 16, 2022 · N642VA · Airbus A320214 · Emergency EquipmentSDR ASAA2022011237482Hinge Arm · crackedRUDDER ATTACH FITTINGS, #1 HINGE ARM , LOWER LUG, 3RD FASTENER HOLE FROM LEFT HAS CRACK INDICATION AT 7 O'CLOCK POSITION GROUNDED - YES. REMOVED & REPLACED #1 HINGE ARM IAW ASA AIRBUS DWG D55371321 REV. D, ASA AIRBUS A320 SRM 55-36-42 & EA # A32055EA-01311 REVJan 12, 2022 · N642VA · Airbus A320214 · Vertical StabilizerSDR ASAA2021122937077Floor Panel · noneFLOOR PANEL PN SB2076-19 HAS DAMAGE GROUNDED - YES. REPAIRED CABIN FLOOR PNL Z41EF-2 / SB2076-19 UPPER SURFACE PEELING WITH PRE CURED PHENOLIC REPAIR PATCH IAW A320-200 SRM 53-02-00-300-013 REV. 139 01NOV2021, A320-200 NTM 51-10-03 FLT HRS 39265, SLT CYCLES 1Dec 29, 2021 · N642VA · Airbus A320214 · Fuselage Miscellaneous StructureSDR ASAA2021122937076None · noneFLOOR PANEL PN SB2076-17 HAS DAMAGE GROUNDED - YES. REPAIRE CABIN FLOOR PNL 241EF-1 / SB2076-17 UPPER SURFACE PEELING WITH A PRE CURED PHENOLIC REPAIR PATCH IAW A320-200 SRM 53-02-00-300-013, 53-02-00-283-001 REV. 139 01NOV2021, A320 NTM 51-10-03 FLT HRS 392Dec 29, 2021 · N642VA · Airbus A320214 · Fuselage Miscellaneous StructureSDR ASAA2021122337212None · corrodedMAIN CABIN FLOOR PANEL SUPPORT BEAM ON RH SIDE AT APPROX Y-1292 HAS CORROSION ON UPPER SURFACE FROM FR 18- FR 20 (MARKED). DOT:W486 GROUNDED - YES. REMOVED CORROSION ORG .079, REMAINING .034 LOSS OF .045. FOUND OUT OF LIMITS IAW A320 SRM 53-11-14. REMOVE FLODec 23, 2021 · N642VA · Airbus A320214 · Fuselage Main, StructureSDR ASAA2021122237483Hinge Arm · cracked#7 RUDDER HINGE FITTING, UPPER HINGE ARM, FWD R/H FASTENER HOLE HAS CRACK INDICATION GROUNDED - YES. REPLACED #7 HINGE ARM IAW ASA EA#A320-55EA-01269 REV.00, ASA AIRBUS DWG D55371052 SHEET 5, VEIW 5-5 & SRM 55-36-42Dec 22, 2021 · N642VA · Airbus A320214 · Vertical StabilizerSDR ASAA2021122237211None · corrodedR1 DOOR LOWER THRESHOLD BEAM HAS CORROSION AT GIRT BAR FITTING STUDS, FR20 (MARKED) DOT:T544 GROUNDED - YES. BLENDED AREA AND REMOVED CORROSION, LOWEST REMAINING THICKNESS IS .165Ï¿½ FOUND WITHIN LIMITS IAW AIRBUS A320 SRM 53-11-14 DOT REMOVED TOOLING T84Dec 22, 2021 · N642VA · Airbus A320214 · Fuselage Main, StructureSDR ASAA2021122237122None · corrodedL1 DOOR LOWER THRESHOLD BEAM HAS A LIGHT CORROSION AT GIRT BAR FITTING STUD, FR16 (MARKED) DOT:T545 GROUNDED - YES. REMOVED CORROSION ON 2EA AREAS, LOCATION 1 IS 1.93Ï¿½ LENGTH 1.00Ï¿½ WIDTH. AND .173Ï¿½ REMAINING LOCATION 2 IS 1.75Ï¿½ LENGTH, 1.15Ï¿½ WIDTDec 22, 2021 · N642VA · Airbus A320214 · Fuselage Main, StructureSDR ASAA2021122237455Beam · corrodedR1 DOOR LOWER THRESHOLD BEAM HAS CORROSION AT GIRT BAR FITTING STUDS, FR16 (MARKED). DOT:T543 GROUNDED - YES. REMOVED AND REPLACED R1 DOOR LOWER SILL IAW ALASKA EA # A320-53EA-01286 AND AIRBUS A320 SRM 51-42-11. DOT REMOVED TOOLING T8492UDec 22, 2021 · N642VA · Airbus A320214 · Fuselage Main, StructureSDR ASAA2021122237020Panel · delaminatedFLOOR PANEL 261CF DAMAGE GROUNDED - YES. EVALUATED & REPAIRED 1 EA. DELAMINATED AREA ON FLOOR PANEL 261CF, PANEL IS LOCATED BETWEEN FR 64 & FR 66. LOCATION OF DAMAGE IS 28.5Ï¿½ FROM T/E, 10.5Ï¿½ FROM INBD EDGE. DAMAGE SIZE IS 2.4Ï¿½ IN WIDTH, 15.2Ï¿½ IN LENGTHDec 22, 2021 · N642VA · Airbus A300* · Fuselage Miscellaneous StructureSDR ASAA2021122037075None · corrodedMAIN CABIN AFT FLOOR BEAM CORRODED -Y464.8 DOT:W471 GROUNDED - YES. BLENDED AREA FOUND OUT OF LIMITS, LENGTH 1Ï¿½ WIDTH 1Ï¿½ DEPTH .030Ï¿½ PER AIRBUS A320 SRM 53-41-14. REMOVED AND INSTALLED NEW FLOOR BEAM IN -Y464.8 PART#D53472195 IAW AIRUS A320 SRM 51-42-Dec 20, 2021 · N642VA · Airbus A320214 · Fuselage Miscellaneous StructureSDR ASAA2021122037033None · corrodedMAIN CABIN AFT FLOOR BEAM CORRODED -Y969 DOT:W466 GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOOR BEAM IAW AIRBUS A320 SRM 51-42-11 AND DWG # D53472040 REMOVED DOTDec 20, 2021 · N642VA · Airbus A320214 · Fuselage Miscellaneous StructureSDR ASAA2021122037032None · corrodedMAIN CABIN AFT FLOOR BEAM CORRODED +Y160.5 DOT:W465 GROUNDED - YES. REMOVED AND REPLACED AFT CABIN FLOOR BEAM IAW AIRBUS A320 SRM 51-42-11 AND DWG # D53472040 REMOVED DOTDec 20, 2021 · N642VA · Airbus A320214 · Fuselage Miscellaneous StructureSDR ASAA2021122037021Door Sill · corrodedMAIN CABIN AFT SIDE FLOOR STRUCTURE + Y1292 FR 69 HAS CORROSION. DOT:W467 GROUNDED - YES. BLENDED AREA ORIGINAL THICKNESS .071Ï¿½ LOSS .053Ï¿½ REMAINING .018Ï¿½ FOUND TO BE OUT OF LIMITS IAW AIRBUS A320 SRM 53-41-14 TOOL# T8224P. CUTOUT DAMAGE, MATERIAL ID ,Dec 20, 2021 · N642VA · Airbus A300* · Fuselage Miscellaneous StructureSDR ASAA2019083030623Profile · corrodedPROFILE AT FR63 RBL 23.75 HAS CORROSION GROUNDED - YES. REMOVED AND REPLACED PROFILE AT FR 63 TO FR 65 RBL 23.75 PART # D53470480009000, PO: 953700.1 PER REF SRM 53-41-14-08-A AND 51-42-11. NO INTERVAL INSPECTION REQUIRED.Aug 30, 2019 · N642VA · Airbus A320214 · Fuselage Miscellaneous StructureSDR ASAA2019082213438Skin · delaminatedRH RUDDER SHELL HOIST POINT #2 LOWER FORWARD POSITION BETWEEN BR 1 AND BR2 IS DISBONDED GROUNDED - YES. REPAIRED R/H RUDDER SHELL @ LOWER #2 HOIST POINT FORWARD POSITION BY BONDING LOWER SKIN, CYLINDRICAL BLOCK, INNER PLIES, CORE AND UPPER PLIES IAW A320 SRMAug 10, 2019 · N642VA · Airbus A320214 · Rudder, Plate/SkinSDR ASAA2019082631463Skin · dentedRH FUSELAGE SKIN HAS A DENT AT FR19R AND STR30R GROUNDED - YES. DENT FOUND TO BE OUT OF LIMITS PER A320 SRM 53-11-11; CUT OUT DAMAGED AREA PER A320 SRM 53-11-11-300-041; FABRICATED DOUBLER PER SRM 53-11-11-300-041; PERFORMED HFEC (NO CRACKS NOTED) PER NTM Aug 6, 2019 · N642VA · Airbus A320214 · Fuselage Main, Plate/SkinSDR VQI2015F00029Contactor · odorREPORTED ELECTRICAL BURNING ODOR AND ASSOCIATED ECAM AVIONICS SMOKE MESSAGES AT POWER TRANSFER FROM APU TO NR 1 ENGINE. THE ENGINE WAS SHUTDOWN AND THE ODOR DISIPATED. TECHS REPLACED AC ESS BUSS SWITCHING CONTACTOR 3XC AND GAPCU 24XG.Aug 4, 2015 · N642VA · Airbus A320214 · AC Power Distribution SystemSDR VQIA201505290019Proximity Switch · failedAIRCRAFT WAS READY TO OPERATE WHEN AT DEPARTURE, CREW NOTED DEFECT OF DOOR R2 OPEN INDICATION ON ECAM WHEN ALL DOORS CLOSED. ACFT DEFECT WAS CLEARED BY R & R R2 PAX CREW DOOR PROXIMITY SWITCH AT 17WV2 IAW AMM 52-71-11. OPS CHECK OK. NO FURTHER DEFECTS NOMay 16, 2015 · N642VA · Airbus A320214 · Door Warning SystemSDR VQI2015F00018Outflow Valve · failedACFT RETURNED TO DEPARTURE. VENT SKIN VALVE FAULT ECAM IN FLIGHT AVIONICS SKIN AIR OUTLET VALVE WAS DISCOVERED IN THE OPEN POSITION BY MAINTENANCE AND PROCEEDED TO DEACTIVATE IAW MEL 21-26-04. VALVE WILL BE REPLACED AT NEXT MAINTENANCE OPPORTUNITY. ON 4/26/Apr 23, 2015 · N642VA · Airbus A320214 · Pressure Regulator/Outflow ValveSDR VQI2015F00012Blade · damagedENGINE 2 COMPRESSOR STALL ON DESCENT AND ACCOMPLISHED IFSD IAW QRH. CREW DECLARED AN EMERGENCY AND LANDED SAFELY. MAINTENANCE PERFORMED BOROSCOPE AND FOUND DAMAGED TO STAGE 3 AND 6 BLADES. ENGINE REMOVED AND REPLACED. THE ROOT CAUSE OF FAILURE IS NOT KNMar 23, 2015 · N642VA · Airbus A320214 · Engine (Turbine/Turboprop)SDR VQI2014F00032Engine · failedAIRCRAFT DEPARTED, REPORTED VIA ACARS THAT THEY HAD NR 1 ENGINE FAILURE WITH IFSD ON TAKEOFF AND WERE DECLARING AND EMERGENCY AND RTF, ACFT LANDED WITHOUT INCIDENT AND BLOCKED. ON ARRIVAL FOUND DAMAGE TO RADIAL DRIVE SHAFT ASSY WITH DAMAGE NOTED TO FAN FRAMEOct 24, 2014 · N642VA · Airbus A320214 · Engine (Turbine/Turboprop)SDR VQI2014F00015Line · chafedCREW RECEIVED AN ECAM GREEN SYS LOW QUANTITY. FLIGHT CREW FOLLOWED FCOM PROCEDURES AND DECISION WAS MADE TO DIVERT AND DECLARED AN EMERGENCY. ACFT LANDED WITHOUT INCIDENT AND TAXIED TO THE GATE UNDER POWER. MAINTENANCE TROUBLESHOT LEAK TO NR 1 ENGINE PYLONMay 28, 2014 · N642VA · Airbus A320214 · Hydraulic System, MainSDR VQIA2012F00033Unknown · unknownWHILE PREPARING TO PUSH BACK, F/A ARMED R2 DOOR, THE OVERHEAD "ARMED" LIGHT WOULD NOT ILLUMINATE. MX INSPECTED AND ATTEMPTED TO ARM THE DOOR AND CONFIRMED THE FAULT . THE DOOR ARMING MECHANISM OPERATED NORMALLY IAW AMM 52-10-00-05. THE ACFT PUSHED BACK Sep 6, 2012 · N642VA · Airbus A320214 · Passenger/Crew DoorsSDR VQI2012F00010Plug · looseAPPROX 2 HRS OUTSIDE, CREW REPORTED ENGINE NR 1, SN 697983, OIL QTY DECREASING IN CRUISE WITH STEADY OIL PRESSURE OF 40 PSI AND OIL TEMP 85 DEGREES. CREW MADE DECISION TO DIVERT, NR 1 ENGINE WAS NOT SHUTDOWN UNTIL ON THE GROUND AND NO EMERGENCY DECLARED AND AApr 19, 2012 · N642VA · Airbus A320214 · Engine Oil Distribution (Airframe Furnished)
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