# Service difficulty reports: N228FR, cancelled Jun 24, 2025 A list on [N228FR, cancelled Jun 24, 2025](https://openairdocs.org/deregistered/N228FR-2025-06-24.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR F3LA2024030500028](https://openairdocs.org/sdr/F3LA2024030500028.md): Door Sill · corroded · Feb 22, 2024 · N228FR · Airbus A320214 · Fuselage Miscellaneous Structure > REFERENCE 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. - [SDR F3LA2024030600032](https://openairdocs.org/sdr/F3LA2024030600032.md): Floor Support · corroded · Feb 12, 2024 · N228FR · Airbus A320214 · Fuselage Miscellaneous Structure > AIRCRAFT 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 45 - [SDR F3LA2024030600031](https://openairdocs.org/sdr/F3LA2024030600031.md): Shear Plate · corroded · Feb 12, 2024 · N228FR · Airbus A320214 · Fuselage Miscellaneous Structure > AIRCRAFT 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 A320 - [SDR F3LA2024030500030](https://openairdocs.org/sdr/F3LA2024030500030.md): Floor Support · corroded · Feb 12, 2024 · N228FR · Airbus A320214 · Fuselage Miscellaneous Structure > AIRCRAFT 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 - [SDR F3LA2024030500029](https://openairdocs.org/sdr/F3LA2024030500029.md): Plate · corroded · Feb 12, 2024 · N228FR · Airbus A320214 · Fuselage Miscellaneous Structure > AIRCRAFT 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 L - [SDR F3LA2023011300012](https://openairdocs.org/sdr/F3LA2023011300012.md): Hmu · failed · Dec 27, 2022 · N228FR · Airbus A320214 · Fuel Controlling System > BTB 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, R - [SDR F3LA2022091300102](https://openairdocs.org/sdr/F3LA2022091300102.md): Skin · corroded · Sep 11, 2022 · N228FR · Airbus A320251N · Fuselage Main, Plate/Skin > FOUND 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: 09/13/2022 - [SDR F3LA2022080600079](https://openairdocs.org/sdr/F3LA2022080600079.md): Power Supply · failed · Aug 3, 2022 · N228FR · Airbus A320214 · Emergency Lighting > DISCREPANCY: 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. - [SDR F3LA2022063000066](https://openairdocs.org/sdr/F3LA2022063000066.md): Autopilot Sys · faulted · Jun 27, 2022 · N228FR · Airbus A320214 · Autopilot System > DISCREPENCY: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 DE - [SDR F3LA2022053100048](https://openairdocs.org/sdr/F3LA2022053100048.md): Servo · inoperative · May 26, 2022 · N228FR · Airbus A320214 · Flight Control System > DISCREPANCY: 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 OUT - [SDR F3LA2020030970016](https://openairdocs.org/sdr/F3LA2020030970016.md): Valve · defective · Mar 7, 2020 · N228FR · Airbus A320214 · Cabin Temperature Control System > SUPPLEMENT: 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 21-2 - [SDR F3LA2019071200451](https://openairdocs.org/sdr/F3LA2019071200451.md): Line · ruptured · Jul 8, 2019 · N228FR · Airbus A320214 · Crew Oxygen System > REFERENCE 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. - [SDR F3LA2018082800411](https://openairdocs.org/sdr/F3LA2018082800411.md): Unknown · unknown · Aug 23, 2018 · N228FR · Airbus A320214 · Flight Control System > PILOT 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 N - [SDR F3LA2018072000368](https://openairdocs.org/sdr/F3LA2018072000368.md): Water Heater · overheated · Jul 20, 2018 · N228FR · Airbus A320214 · Wash Water System > VISIBLE 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. MAINTENAN - [SDR F3LA2018052200345](https://openairdocs.org/sdr/F3LA2018052200345.md): Floorbeam · corroded · May 10, 2018 · N228FR · Airbus A320214 · Fuselage Main, Floor Beam > CORRODED 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. - [SDR F3LA2018052200343](https://openairdocs.org/sdr/F3LA2018052200343.md): Floor Support · corroded · May 10, 2018 · N228FR · Airbus A320214 · Fuselage Miscellaneous Structure > CORROSION 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 51-4 - [SDR F3LA2017122000271](https://openairdocs.org/sdr/F3LA2017122000271.md): Epsu · inoperative · Dec 20, 2017 · N228FR · Airbus A320214 · Emergency Lighting > EPSU 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. - [SDR F3LA2017060500175](https://openairdocs.org/sdr/F3LA2017060500175.md): Fastener · damaged · May 27, 2017 · N228FR · Airbus A320214 · Fuselage Main, Plate/Skin > IAW 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. - [SDR F3LA2017060500174](https://openairdocs.org/sdr/F3LA2017060500174.md): Shear Web · cracked · May 25, 2017 · N228FR · Airbus A320214 · Fuselage Miscellaneous Structure > RIGHT 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. - [SDR F3LA2017060500173](https://openairdocs.org/sdr/F3LA2017060500173.md): Shear Web · cracked · May 25, 2017 · N228FR · Airbus A320214 · Fuselage Miscellaneous Structure > LEFT FRAME 69 SHEAR WEB CRACKED. REMOVED LEFT SHEAR WEB AND INSTALLED A NEW SHEAR WEB IAW SRM 51-72-11-911-001. ## 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 = 'N228FR' AND deregistration_id = 'N228FR-2025-06-24' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N228FR-2025-06-24/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.