# Service difficulty reports: N633VA A list on [N633VA](https://openairdocs.org/aircraft/N633VA.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR ASAA2022042139652](https://openairdocs.org/sdr/ASAA2022042139652.md): Skin · corroded · Apr 21, 2022 · N633VA · Airbus A320214 · Wing Miscellaneous Structure > CORROSION ON RIGHT WING UPPER TRAILING EDGE SKIN LOWER SURFACE 5" IINBOARD OF RIB 8 GROUNDED - YES. CORROSION ON RIGHT WING UPPER TRAILING EDGE SKIN LOWER SURFACE 5" IINBOARD OF RIB 8 REPAIRED PER EA A320-57EA-01458 REV 00 DATED 8/22/2022 - [SDR ASAA2022042139609](https://openairdocs.org/sdr/ASAA2022042139609.md): Skin · corroded · Apr 21, 2022 · N633VA · Airbus A320214 · Wing Miscellaneous Structure > CORROSION ON RIGHT WING UPPER TRAILING EDGE SKIN LOWER SURFACE 12 INCHES I/B OF RIB 7 GROUNDED - YES. CORROSION ON RIGHT WING UPPER TRAILING EDGE SKIN LOWER SURFACE 12 INCHES I/B OF RIB 7 REPAIRED PER EA # A320-57EA-01458 REV 00, DATED 08/22/2022 - [SDR ASAA2022022439662](https://openairdocs.org/sdr/ASAA2022022439662.md): Skin · corroded · Feb 24, 2022 · N633VA · Airbus A320214 · Wing Miscellaneous Structure > CORROSION ON RIGHT WING UPPER TRAILING EDGE SKIN LOWER SURFACE 3" I/B OF RIB 18 GROUNDED - YES. CORROSION ON RIGHT WING UPPER TRAILING EDGE SKIN UPPER SURFACE 3" I/B OF RIB 18 REPAIRED PER EA A320-57EA-01458 REV 00 DATED 8/22/2022 - [SDR ASAA2022022439656](https://openairdocs.org/sdr/ASAA2022022439656.md): Skin · corroded · Feb 24, 2022 · N633VA · Airbus A320214 · Wing Miscellaneous Structure > CORROSION ON RIGHT WING UPPER TRAILING EDGE SKIN UPPER SURFACE 2" I/B OF RIB 13 GROUNDED - YES. CORROSION ON RIGHT WING UPPER TRAILING EDGE SKIN UPPER SURFACE 2" I/B OF RIB 13 REPAIRED PER EA A320-57EA-01458 REV 00 DATED 8/22/2022 - [SDR ASAA2022022439655](https://openairdocs.org/sdr/ASAA2022022439655.md): Skin · corroded · Feb 24, 2022 · N633VA · Airbus A320214 · Wing Miscellaneous Structure > CORROSION ON RIGHT WING UPPER TRAILING EDGE SKIN LOWER SURFACE 6" I/B OF RIB 14 GROUNDED - YES. CORROSION ON RIGHT WING UPPER TRAILING EDGE SKIN LOWER SURFACE 6" I/B OF RIB 14 REPAIRED PER EA A320-57EA-01458 REV 00 DATED 8/22/2022 - [SDR ASAA2022022439654](https://openairdocs.org/sdr/ASAA2022022439654.md): Skin · corroded · Feb 24, 2022 · N633VA · Airbus A320214 · Wing Miscellaneous Structure > CORROSION ON RIGHT WING UPPER TRAILING EDGE SKIN LOWER SURFACE 12" O/B OF RIB 21 GROUNDED - YES. CORROSION ON RIGHT WING UPPER TRAILING EDGE SKIN LOWER SURFACE 12" O/B OF RIB 21 REPAIRED PER EA A320-57EA-01458 REV 00 DATED 8/22/2022 - [SDR ASAA2022011039661](https://openairdocs.org/sdr/ASAA2022011039661.md): Skin · corroded · Jan 10, 2022 · N633VA · Airbus A320214 · Wing Miscellaneous Structure > CORROSION NOTED DURING NDI INSPECTION CUSTOMER CARD 572127-01-1A-2R-C007 AT THE UPPER R/W SKIN LOWER SURFACE LOCATED 3" O/B OF RIB 10 COMMON TO THE UPPER REAR SPAR GROUNDED - YES. CORROSION NOTED DURING NDI INSPECTION CUSTOMER CARD 572127-01-1A-2R-C007 AT THE - [SDR ASAA2022011039660](https://openairdocs.org/sdr/ASAA2022011039660.md): Skin · corroded · Jan 10, 2022 · N633VA · Airbus A320214 · Wing Miscellaneous Structure > CORROSION NOTED DURING NDI INSPECTION CUSTOMER CARD 572127-01-1A-2R-C007 AT THE UPPER R/W SKIN LOWER SURFACE LOCATED 5" O/B OF RIB 14 COMMON TO THE UPPER REAR SPAR GROUNDED - YES. CORROSION NOTED DURING NDI INSPECTION CUSTOMER CARD 572127-01-1A-2R-C007 AT THE - [SDR ASAA2022011039659](https://openairdocs.org/sdr/ASAA2022011039659.md): Skin · corroded · Jan 10, 2022 · N633VA · Airbus A320214 · Wing Miscellaneous Structure > CORROSION NOTED DURING NDI INSPECTION CUSTOMER CARD 572127-01-1A-2R-C007 AT THE UPPER R/W SKIN LOWER SURFACE LOCATED 5" O/B OF RIB 19 COMMON TO THE UPPER REAR SPAR GROUNDED - YES. CORROSION NOTED DURING NDI INSPECTION CUSTOMER CARD 572127-01-1A-2R-C007 AT THE - [SDR ASAA2022011039658](https://openairdocs.org/sdr/ASAA2022011039658.md): Skin · corroded · Jan 10, 2022 · N633VA · Airbus A320214 · Wing Miscellaneous Structure > CORROSION RIGHT WING UPPER SKIN AT RIB 19 T/E BETWEEN SPOILERS 4/5 HAS CORROSION AT FASTENERS GROUNDED - YES. CORROSION RIGHT WING UPPER SKIN AT RIB 19 T/E BETWEEN SPOILERS 4/5 HAS CORROSION AT FASTENERS INSP AND REPAIRED PER EA A320-57EA-01458 REV 00 DATED 8/ - [SDR ASAA2022011039657](https://openairdocs.org/sdr/ASAA2022011039657.md): Skin · corroded · Jan 10, 2022 · N633VA · Airbus A320214 · Wing Miscellaneous Structure > CORROSION NOTED DURING NDI INSPECTION CUSTOMER CARD 572127-01-1A-2R-C007 AT THE UPPER R/W SKIN LOWER SURFACE LOCATED 5" O/B OF RIB 11 COMMON TO THE UPPER REAR SPAR GROUNDED - YES. CORROSION NOTED DURING NDI INSPECTION CUSTOMER CARD 572127-01-1A-2R-C007 AT THE - [SDR ASAA2022011039653](https://openairdocs.org/sdr/ASAA2022011039653.md): Skin · corroded · Jan 10, 2022 · N633VA · Airbus A320214 · Wing Miscellaneous Structure > CORROSION RH WING UPPER SKIN AT RIB 5 T/E JUST FWD OF #1 SPOILER I/B HINGE HAS CORROSION AT FASTENERS GROUNDED - YES. CORROSION RH WING UPPER SKIN AT RIB 5 T/E JUST FWD OF #1 SPOILER I/B HINGE HAS CORROSION AT FASTENERS INSP AND REPAIRED PER EA A320-57EA-01458 - [SDR ASAA2022011039651](https://openairdocs.org/sdr/ASAA2022011039651.md): Skin · corroded · Jan 10, 2022 · N633VA · Airbus A320214 · Wing Miscellaneous Structure > CORROSION RIGHT WING UPPER SKIN AT RIB 8 TO 10" HAS CORROSION AT FASTENERS GROUNDED - YES. CORROSION RIGHT WING UPPER SKIN AT RIB 8 TO 10" HAS CORROSION AT FASTENERS INSPECTED AND REPAIRED PER EA A320-57EA-01458 REV 00 DATED 8/22/2022 - [SDR ASAA2022011039608](https://openairdocs.org/sdr/ASAA2022011039608.md): Skin · corroded · Jan 10, 2022 · N633VA · Airbus A320214 · Wing Miscellaneous Structure > CORROSION ON LEFT WING UPPER TRAILING EDGE SKIN LOWER SURFACE 3 INCHES I/B OF RIB 21 GROUNDED - YES. CORROSION ON LEFT WING UPPER TRAILING EDGE SKIN LOWER SURFACE 3" I/B OF RIB 21 REPAIRED PER EA # A320-57EA-01457 REV 00, DATED 08/11/2022 - [SDR ASAA2022011039607](https://openairdocs.org/sdr/ASAA2022011039607.md): Skin · corroded · Jan 10, 2022 · N633VA · Airbus A320214 · Wing Miscellaneous Structure > L/H WING UPPER SKIN 6" I/B OF RIB 19 LOWER SURFACE HAS AREA OF CORROSION GROUNDED - YES. L/H WING UPPER SKIN 6" I/B OF RIB 19 LOWER SURFACE AREA OF CORROSION REPAIRED PER EA # A320-57EA-01457 REV 00, DATED 08/11/2022 - [SDR ASAA2022011039606](https://openairdocs.org/sdr/ASAA2022011039606.md): Skin · corroded · Jan 10, 2022 · N633VA · Airbus A320214 · Wing Miscellaneous Structure > L/H WING UPPER SKIN 3" I/B OF RIB 18 LOWER SURFACE HAS AREA OF CORROSION GROUNDED - YES. L/H WING UPPER SKIN 3" I/B OF RIB 18 LOWER SURFACE AREA OF CORROSION REPAIRED PER EA # A320-57EA-01457 REV 00, DATED 08/11/2022 - [SDR ASAA2022011039605](https://openairdocs.org/sdr/ASAA2022011039605.md): Skin · corroded · Jan 10, 2022 · N633VA · Airbus A320214 · Wing Miscellaneous Structure > CORROSION ON LEFT WING UPPER TRAILING EDGE SKIN UPPER SURFACE HAS 17 EA CORRODED FASTENERS AT FALSE SPAR RIB 9 GROUNDED - YES. CORROSION ON LEFT WING UPPER TRAILING EDGE SKIN UPPER SURFACE AT 17 EA FASTENERS AT FALSE SPAR RIB 9 REPAIRED PER EA # A320-57EA-0145 - [SDR ASAA2022011039604](https://openairdocs.org/sdr/ASAA2022011039604.md): Skin · corroded · Jan 10, 2022 · N633VA · Airbus A320214 · Wing Miscellaneous Structure > CORROSION ON LEFT WING UPPER TRAILING EDGE SKIN LOWER SURFACE AT FALSE RIB 8 GROUNDED - YES. CORROSION ON L/H WING UPPER TRAILING EDGE SKIN LOWER SURFACE AT FALSE REAR SPAR RIB 8 REPAIRED PER EA # A320-57EA-01457 REV 00, DATED 08/11/2022 - [SDR ASAA2022011039603](https://openairdocs.org/sdr/ASAA2022011039603.md): Skin · corroded · Jan 10, 2022 · N633VA · Airbus A320214 · Wing Miscellaneous Structure > CORROSION ON LEFT WING UPPER TRAILING EDGE SKIN LOWER SURFACE 3" O/B OF RIB 10 GROUNDED - YES. CORROSION ON L/H WING UPPER TRAILING EDGE SKIN LOWER SURFACE 3" O/B OF RIB 10 REPAIRED PER EA # A320-57EA-01457 REV 00, DATED 08/11/2022 - [SDR ASAA2022011039602](https://openairdocs.org/sdr/ASAA2022011039602.md): Skin · corroded · Jan 10, 2022 · N633VA · Airbus A320214 · Wing Miscellaneous Structure > LEFT WING UPPER TRAILING EDGE SKIN LOWER SURFACE AT RIB 16 HAS CORROSION GROUNDED - YES. CORROSION AT LEFT WING UPPER TRAILING EDGE SKIN LOWER SURFACE AT RIB 16 REPAIRED PER EA # A320-57EA-01457, DATED 08/11/2022, REV 00 - [SDR ASAA2022011039590](https://openairdocs.org/sdr/ASAA2022011039590.md): Skin · corroded · Jan 10, 2022 · N633VA · Airbus A320214 · Wing Miscellaneous Structure > L/H WING UPPER SKIN AT RIB 17 T/E JUST FWD OF #4 SPOILER I/B HINGE HAS CORROSION GROUNDED - YES. L/H WING UPPER SKIN AT RIB 17 T/E JUST FWD OF #4 SPOILER I/B HINGE CORROSION AT FASTENERS REPAIRED PER EA # A320-57EA-01457, DATED 08/11/2022, REV 00 - [SDR ASAA2022011039589](https://openairdocs.org/sdr/ASAA2022011039589.md): Skin · corroded · Jan 10, 2022 · N633VA · Airbus A320214 · Wing Miscellaneous Structure > L/H WING UPPER SKIN AT RIB 13 T/E JUST FWD OF #2/3 SPOILERS HAS CORROSION GROUNDED - YES. CORROSION ON L/H WING UPPER SKIN AT RIB 13 T/E FASTENERS JUST FWD OF #2/3 SPOILERS REPAIRED IAW EA # A320-57EA-01457, DATED 08/11/2022 REV 00 - [SDR ASAA2022011039588](https://openairdocs.org/sdr/ASAA2022011039588.md): Skin · corroded · Jan 10, 2022 · N633VA · Airbus A320214 · Wing Miscellaneous Structure > L/H WING UPPER SKIN AT RIB 5 T/E JUST FWD OF #1 SPOILER I/B HINGE HAS CORROSION AT FASTENERS GROUNDED - YES. L/H WING UPPER SKIN AT RIB 5 T/E JUST FWD OF #1 SPOILER I/B HINGE CORROSION AT FASTENERS REPAIRED PER EA # A320-57EA-01457 REV 00, DATED 08/11/2022 - [SDR ASAA2022011039587](https://openairdocs.org/sdr/ASAA2022011039587.md): Skin · corroded · Jan 10, 2022 · N633VA · Airbus A320214 · Wing Miscellaneous Structure > L/H WING UPPER SKIN AT RIB 19 T/E BETWEEN SPOILERS 4/5 HAS CORROSION AT FASTENERS GROUNDED - YES. L/H WING UPPER SKIN AT RIB 19 T/E BETWEEN SPOILERS 4 AND 5 CORROSION AT FASTENERS REPAIRED PER EA # A320-57EA-01457 REV 00, DATED 08/11/2022. - [SDR ASAA2022011039586](https://openairdocs.org/sdr/ASAA2022011039586.md): Skin · corroded · Jan 10, 2022 · N633VA · Airbus A320214 · Wing Miscellaneous Structure > CORROSION NOTED DURING NDI INSPECTION CUSTOMER CARD 572127-01-1A-2L-C007 AT UPPER LEFT WING SKIN LOWER SURFACE LOCATED 3" O/B OF RIB 15 COMMON TO THE UPPER REAR SPAR. GROUNDED - YES. CORROSION ON L/H WING UPPER SKIN LOWER SURFACE 3" O/B OF RIB 15 COMMON TO THE - [SDR ASAA2022011039585](https://openairdocs.org/sdr/ASAA2022011039585.md): Skin · corroded · Jan 10, 2022 · N633VA · Airbus A320214 · Wing Miscellaneous Structure > CORROSION NOTED DURING NDI INSPECTION CUSTOMER CARD 572127-01-1A-2L-C007 AT UPPER LEFT WING SKIN LOWER SURFACE LOCATED 3" O/B OF RIB 14 COMMON TO THE UPPER REAR SPAR. GROUNDED - YES. CORROSION ON L/H WING UPPER SKIN LOWER SURFACE 3" O/B OF RIB 14 COMMON TO THE - [SDR ASAA2022011039584](https://openairdocs.org/sdr/ASAA2022011039584.md): Skin · corroded · Jan 10, 2022 · N633VA · Airbus A320214 · Wing Miscellaneous Structure > CORROSION NOTED DURING NDI INSPECTION CUSTOMER CARD 572127-01-1A-2L-C007 AT THE UPPER L/H WING SKIN LOWER SURFACE LOCATED 4" O/B OF RIB 11 COMMON TO THE UPPER REAR SPAR. GROUNDED - YES. CORROSION ON L/H WING UPPER SKIN LOWER SURFACE 4" O/B OF RIB 11 COMMON TO - [SDR ASAA2022011039583](https://openairdocs.org/sdr/ASAA2022011039583.md): Skin · corroded · Jan 10, 2022 · N633VA · Airbus A320214 · Wing Miscellaneous Structure > CORROSION NOTED DURING NDI INSPECTION CUSTOMER CARD 572127-01-1A-2L-C007 AT UPPER L/W SKIN LOWER SURFACE LOCATED 6" I/B OF RIB 7 COMMON TO THE UPPER REAR SPAR. GROUNDED - YES. CORROSION ON L/H WING UPPER SKIN LOWER SURFACE 6" I/B OF RIB 7 COMMON TO THE UPPER R - [SDR ASAA2019080523277](https://openairdocs.org/sdr/ASAA2019080523277.md): Seat Track · corroded · Jul 12, 2019 · N633VA · Airbus A320214 · Fuselage, Seat/Cargo Attach Fittings > AFT WET AREA FLOOR STRUCTURE BEAM ASSY AT FR68: Y-765 HAS CORROSION GROUNDED - YES. REMOVED AND REPLACED BEAM ASSY IAW A320 SRM 51-72-11 CAT A REPAIR, NO REINSPECT REQUIRED. CORRODED AROUND HARD PAINT. NO DAMAGE ALLOWED IAW A320 SRM 53-41-14 - [SDR ASAA2019062730197](https://openairdocs.org/sdr/ASAA2019062730197.md): Seat Track · corroded · Jun 27, 2019 · N633VA · Airbus A320214 · Fuselage, Seat/Cargo Attach Fittings > SEAT TRACK CORRODED AT FRAME 18 -Y1292 GROUNDED - YES. REMOVED AND REPLACED FLOORBEAM PER SRM 51-42-11 AND DWG # D53112814. CAT A REPAIR NO REINSPECT REQUIRED DAMAGE FOUND TO BEW OUT OF LIMITS PER SRM 53-11-15-287-005. - [SDR ASAA2019062630196](https://openairdocs.org/sdr/ASAA2019062630196.md): Floor Support · corroded · Jun 26, 2019 · N633VA · Airbus A320214 · Fuselage Miscellaneous Structure > CORROSION 3 PLACES AT R2 DOOR UNDER CABIN FLOOR BOARD 262LG. GROUNDED - YES. REMOVED CORROSION, CORRODED AREA EXTENDS COMPLETELY THREW FLOOR SUPPORT - EXFOLIATED- AREA OUT OF LIMITS IAW SRM 53-41-14-283-002, FABRICATED REPAIR IAW SRM 53-41-14-300-001 FIG 001 - [SDR ASAA2019062630195](https://openairdocs.org/sdr/ASAA2019062630195.md): Seat Track · corroded · Jun 26, 2019 · N633VA · Airbus A320214 · Fuselage, Seat/Cargo Attach Fittings > CORROSION CABIN FLOOR SUPPORT, AT FR15 UNDER FLOOR PANEL 221EF GROUNDED - YES. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-72-11. DAMAGE REMOVED. ORIG THICKNESS.087, REMOVED.055, REMAINING.032, FOUND TO BE OUT OF LIMITS IAW SRM 53-11-15-283-005. CAT A REPAIR - [SDR VQI2017F00001](https://openairdocs.org/sdr/VQI2017F00001.md): Sump · leaking · Apr 6, 2017 · N633VA · Airbus A320214 · Aircraft Fuel Distribution System > ON ARRIVAL AT ACFT FOR FIRST FLIGHT, CREW DETECTED A STRONG FUEL ODOR IN THE COCKPIT AND THROUGHOUT CABIN. ODOR DISSIPATED WITH APU BLEED ON. DURING INSPECTION, IAW TSM 055000810831A, FOUND RT CENTER TANK FUEL SUMP LEAKING. RESEATED SUMP DRAIN AND CLEANED A - [SDR VQI2015F00035](https://openairdocs.org/sdr/VQI2015F00035.md): Oven · odor · Oct 24, 2015 · N633VA · Airbus A320214 · Emergency Equipment > FLIGHT CREW REPORTED A BURNING ODOR IN THE FORWARD GALLEY DURING CLIMBOUT. THE FLIGHT CREW DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. UPON ARRIVAL, TECH OPS ACCOMPLISHED TROUBLESHOOTING IAW AMM 05-50-00-810-831-A. NO ODORS OR ABNORMAL OIL CONSUMPTION - [SDR VQI2014F00031](https://openairdocs.org/sdr/VQI2014F00031.md): Connector · burned · Oct 20, 2014 · N633VA · Airbus A320214 · Equipment/Furnishings Wiring > ODOR OF MELTED PLASTIC IN LAVATORY F. COMPLIED WITH AMM 05-5000-810-831, CAUSE OF ODOR, FOUND RAZOR SOCKET ON AFT LAVATORY F BROKEN AND ODOR OF ELECTRICAL BURN ON THE SOCKET. R & R AFT LAV RAZOR SOCKET LAV "F", OPS CHECK SATISFACTORY. REF 25-44-41. THIS RE - [SDR XE4R2013FA0000564](https://openairdocs.org/sdr/XE4R2013FA0000564.md): Support · corroded · Aug 9, 2013 · N633VA · Airbus A320214 · Fuselage Miscellaneous Structure > LEFT AFT SHEAR PLATE SUPPORT FRAMES 69-70, S23-24L HAS CORROSION BEYOND LIMITS. EXTENT OF DAMAGE 1" LENGTH X 1" WIDTH X.030" DEPTH. SUPPORT BELOW SHEAR PLATE WAS R & R IAW SRM 51-40-00 AND 51-42-11. - [SDR XE4R2013FA0000563](https://openairdocs.org/sdr/XE4R2013FA0000563.md): Shear Plate · corroded · Aug 9, 2013 · N633VA · Airbus A320214 · Fuselage Miscellaneous Structure > LEFT AFT SHEAR PLATE FRAMES 69-70, S23-24L HAS CORROSION BEYOND LIMITS. EXTENT OF DAMAGE 2" LENGTH X 2" WIDTH X.032" DEPTH. SHEAR PLATE WAS R & R IAW SRM 51-40-00 AND 51-42-11. - [SDR XE4R2013FA0000562](https://openairdocs.org/sdr/XE4R2013FA0000562.md): Support · corroded · Aug 9, 2013 · N633VA · Airbus A320214 · Fuselage Miscellaneous Structure > RIGHT AFT SHEAR PLATE SUPPORT FR 69-70, S23-24R HAS CORROSION BEYOND LIMITS. EXTENT OF DAMAGE 1" LENGTH X 1" WIDTH X.025" DEPTH. SUPPORT BELOW SHEAR PLATE WAS R & R IAW SRM 51-40-00 AND 51-42-11. - [SDR XE4R2013FA0000561](https://openairdocs.org/sdr/XE4R2013FA0000561.md): Shear Plate · corroded · Aug 9, 2013 · N633VA · Airbus A320214 · Fuselage Miscellaneous Structure > RIGHT AFT SHEAR PLATE FR 69-70, ST23R-24R HAS CORROSION BEYOND LIMITS. EXTENT OF DAMAGE 2" LENGTH X 2" WIDTH X.030" DEPTH. SHEAR PLATE WAS R & R IAW SRM 51-40-00 AND 51-42-11. ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 = 'N633VA' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N633VA/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.