N228FR, cancelled Jun 24, 2025

Service difficulty reports · 20

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 = 'N228FR' AND deregistration_id = 'N228FR-2025-06-24'
  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 F3LA2024030500028Door Sill · corrodedREFERENCE AIRBORNE/PEMCO N/R 15047.0599 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SHCEDULED MX. R2 DOOR SILL REQUIRES REPLACEMENT. REMOVED & REPLACED R2 DOOR SILL IAW A320 SRM 51-72-11-911-001MX ACTION IS ACCEPTABLE.Feb 22, 2024 · N228FR · Airbus A320214 · Fuselage Miscellaneous StructureSDR F3LA2024030600032Floor Support · corrodedAIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SHCEDULED MX.DURING INSPECTION AT AFT WET AREA WAS FOUND CORROSION ON THE FLOOR LONGITUDINAL SUPPORT BETWEEN FR68 TO FR70 - RBL 45.00. REMOVED AND REPLACED LONGITUDINAL BEAMS SUPPORT BETWEEN FR 68 TO FR70, RBL 45Feb 12, 2024 · N228FR · Airbus A320214 · Fuselage Miscellaneous StructureSDR F3LA2024030600031Shear Plate · corrodedAIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SHCEDULED MX.DURING INSPECTION AT AFT WET AREA WAS FOUND CRACK AND SEVERAL CORROSION ON THE L/H LATERAL SHEAR PLATE BETWEEN FR69 TO FR70. L/H LATERAL SHEAR PLATE BETWEEN FR69 TO FR70 REMOVED AND REPLACED IAW A320Feb 12, 2024 · N228FR · Airbus A320214 · Fuselage Miscellaneous StructureSDR F3LA2024030500030Floor Support · corrodedAIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SHCEDULED MX.DURING INSPECTION AT AFT WET AREA WAS FOUND CORROSION ON TH FLOOR LONGITUDINAL SUPPORT BETWEEN FR68 TO FR70-LBL 45.00 DOT #997-142. REMOVED & REPLACED FLOOR BEAM FROM FR-68 TO FR-70 L/H IAW A320 SRM Feb 12, 2024 · N228FR · Airbus A320214 · Fuselage Miscellaneous StructureSDR F3LA2024030500029Plate · corrodedAIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SHCEDULED MX.DURING INSPECTION AT AFT WET AREA WAS FOUND CRACK AND SEVERAL CORROSION ON THE THE R/H LATERAL SHEAR PLATE BETWEEN FR69 TO FR70. REMOVED SHEAR PLATE FOR REPLACE ON R/H FR69 TO 70 P/N D5347112420300 LFeb 12, 2024 · N228FR · Airbus A320214 · Fuselage Miscellaneous StructureSDR F3LA2023011300012Hmu · failedBTB DUE TO ENGINE 1 SHUTTING DOWN DURING TAXI. PERFORMED TROUBLESHOOTING PER TSM 72-00-00-810-806-A UP TO STEP 4A, PERFORMED FADEC 1A AND 1B TEST, A PASSED AND B FAILED. PERFORMED TROUBLESHOOTING PER FADEC FAULT CODE TSM 73-21-00-810-865-A UP TO STEP 3C.1, RDec 27, 2022 · N228FR · Airbus A320214 · Fuel Controlling SystemSDR F3LA2022091300102Skin · corrodedFOUND CORROSION AFT OF R2 DOOR, BY LAV VACUUM EXHAUST PORT - (AC TO FERRY TO AIRBORNE FOR REPAIRS). REPAIRED LAV VENT HOLE SKIN IAW A320 SRM 53-41-11-300-004. REF PEMCO NR 13027-0010. ORIGINAL SUBMISSION DATE: 09/13/2022Sep 11, 2022 · N228FR · Airbus A320251N · Fuselage Main, Plate/SkinSDR F3LA2022080600079Power Supply · failedDISCREPANCY: REFERENCE LP256110 ITEM 3: EPSU 10WL FAILS EPSU SYS TEST. CORRECTIVE ACTION: REMOVED AND REPLACED EPSU 10WL PER AMM 31-51-38-00-001-A AND AMM 33-51-38-400-001-A. OPS TEST GOOD, NO FAULTS AT THIS TIME.Aug 3, 2022 · N228FR · Airbus A320214 · Emergency LightingSDR F3LA2022063000066Autopilot Sys · faultedDISCREPENCY:MAJOR VIBRATION IN AFT GALLEY WAS "UNDER THE FEET AND FELT VERTICAL. ON DESCANT FA'S REPORTED VIBRATION GOT WORSE. SPEED WAS CONSTANT 280KTS. CORRECTIVE ACTION: MX ACTION REF LP207661 FOR SEC2 MX C/W ELEVATOR & RUDDER FREE PLAY CHECKS GOOD. NO DEJun 27, 2022 · N228FR · Airbus A320214 · Autopilot SystemSDR F3LA2022053100048Servo · inoperativeDISCREPANCY: REFERENCE LP210393 ITEM 1 WRITEUP: FLT CONTROL CHECK FAILED. L AIL. OUT OF LIMITS. CORRECTIVE ACTION: LP210393 ITEM 1 SIGN OFF: REF TSM 27-10-00-810-836-A FOUND LH AILERON SERVO CONTROL (BLUE SYSTEM) TO BE OUT OF LIMITS. REMOVED AND REPLACED OUTMay 26, 2022 · N228FR · Airbus A320214 · Flight Control SystemSDR F3LA2020030970016Valve · defectiveSUPPLEMENT: CORRECTED INFORMATION ON COCK PIT TRIM AIR VALVE SERIAL NUMBER REMOVED. REMOVED PER AMM 21-63-51PB401. REFERENCE LP 1225350 ITEMS 1-3: DIVERT TO MCO, ODER/OIL/COOKING SMELL ON CA SIDE. PER TSM, RH/LH RETICULATIONS FILTERS TO BE CHANGED PER AMM 21-2Mar 7, 2020 · N228FR · Airbus A320214 · Cabin Temperature Control SystemSDR F3LA2019071200451Line · rupturedREFERENCE LOG PAGE LP1178453 ITEM 3: "CAPT O2 MASK LINE RUPTURED". REMOVED AND REPLACED CAPTAINS OXYGEN MASK IN REFERENCE TO AMM 35-12-41-400-002-A OPS CHECK OK.Jul 8, 2019 · N228FR · Airbus A320214 · Crew Oxygen SystemSDR F3LA2018082800411Unknown · unknownPILOT REPORTED AN UNCOMMANDED LATERAL YAW TO THE RIGHT AFTER TAKEOFF ROLL, SPEED OF 10 KTS. MAINTENANCE COMPLETED TROUBLESHOOTING IAW TSM 05-50-00-810-823-A. BOTH NLG TIRES DAMAGED AND REPLACED IAW AMM 32-41-12 PB 401. NR 1 MLG TIRE DAMAGED, REPLACED THE NAug 23, 2018 · N228FR · Airbus A320214 · Flight Control SystemSDR F3LA2018072000368Water Heater · overheatedVISIBLE SMOKE UNDER AFT LEFT LAV SINK IN FLIGHT. WATER HEATER WAS TURNED OFF. CONDITION DID NOT GET WORSE. DEBRIEF CREW IDENTIFIED SOURCE OF SMOKE TO BE WATER HEATER UNDER SINK. PERFORMED TSM 24-00-00-810-823-A. PLACED WATER HEATER ON MEL 38-10-01B. MAINTENANJul 20, 2018 · N228FR · Airbus A320214 · Wash Water SystemSDR F3LA2018052200345Floorbeam · corrodedCORRODED FLOORBEAM AT Y512.5, FRAME 66. FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-14-283-002. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-11, SRM 51-44-11, AND SRM 51-72-11.May 10, 2018 · N228FR · Airbus A320214 · Fuselage Main, Floor BeamSDR F3LA2018052200343Floor Support · corrodedCORROSION FOUND ON THE FLOOR SUPPORT -Y1732, BETWEEN FRAMES 65 - 66 AT TWO FASTENER HOLSE. EVALUATED THE FLOOR SUPPORT AND FOUND IT TO BE OUT OF LIMITS IAW SRM 53-00-14-283-002. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, SRM 51-42-11, SRM 51-4May 10, 2018 · N228FR · Airbus A320214 · Fuselage Miscellaneous StructureSDR F3LA2017122000271Epsu · inoperativeEPSU AT FIN 13WL OPS CHECK INOP - DURING HEAVY CHECK - RON MAINTENANCE, EPSU AT FIN 13WL FAILED OPS CHECK. NO FLIGHT EFFECTED, NO GROUNDING. REMOVED AND REPLACED EPSU AT FIN 13WL AND ALL OPS CHECK OK IAW AMM 33-51-38 PB 401. NO FURTHER MX REQUIRED.Dec 20, 2017 · N228FR · Airbus A320214 · Emergency LightingSDR F3LA2017060500175Fastener · damagedIAW EA A2-53R-33764. AFT LOWER FUSELAGE DAMAGED AREA. REMOVED AND REPLACED ALL FASTENERS ON AFT LOWER FUSELAGE IAW EA A2-53R-33764 AND SRM 51-42-11.May 27, 2017 · N228FR · Airbus A320214 · Fuselage Main, Plate/SkinSDR F3LA2017060500174Shear Web · crackedRIGHT FRAME 69 SHEAR WEB CRACKED. REMOVED AND REPLACED THE SHEAR WEB IAW SRM 51-42-11, SRM 51-72-11, AND SRM 51-21-11. FLUSH MOTOR WIRE HARNESS DISPLACED, ATTCHED AND OPERATIONAL CHECKED GOOD IAW AMM 38-31-00.May 25, 2017 · N228FR · Airbus A320214 · Fuselage Miscellaneous StructureSDR F3LA2017060500173Shear Web · crackedLEFT FRAME 69 SHEAR WEB CRACKED. REMOVED LEFT SHEAR WEB AND INSTALLED A NEW SHEAR WEB IAW SRM 51-72-11-911-001.May 25, 2017 · N228FR · Airbus A320214 · Fuselage Miscellaneous Structure
Back to N228FR, cancelled Jun 24, 2025