# Service difficulty reports: N322FR A list on [N322FR](https://openairdocs.org/aircraft/N322FR.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR F3LA2023092800175](https://openairdocs.org/sdr/F3LA2023092800175.md): Tube · leaking · Sep 28, 2023 · N322FR · Airbus A320251N · Hydraulic System, Main > REFERENCE LP 369308 HYD Y RSVR LO LVL INFLIGHT. RESERVOIR SHOWS EMPTY. OPEN. - [SDR F3LA2023091800167](https://openairdocs.org/sdr/F3LA2023091800167.md): Battery · failed · Sep 1, 2023 · N322FR · Airbus A320251N · Emergency Lighting > REFERENCE NR 5001260509-0050. AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING EPSU BATTERIES CAPACITY TEST, EPSU 13WL BATTERY FAILED CAPACITY TEST. REPLACEMENT IS REQUIRED IAW AMM 33-51-38-000-002-A/REV 95 AND AMM 33-51-38-400-002-A/REV 95. - [SDR F3LA2023091800166](https://openairdocs.org/sdr/F3LA2023091800166.md): Battery · failed · Sep 1, 2023 · N322FR · Airbus A320251N · Emergency Lighting > REFERENCE NR 5001260509-0040. AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING EPSU BATTERIES CAPACITY TEST, EPSU 12WL BATTERY FAILED CAPACITY TEST. REPLACEMENT IS REQUIRED IAW AMM 33-51-38-000-002-A/REV 95 AND AMM 33-51-38-400-002-A/REV 95. - [SDR F3LA2023091800165](https://openairdocs.org/sdr/F3LA2023091800165.md): Battery · failed · Sep 1, 2023 · N322FR · Airbus A320251N · Emergency Lighting > REFERENCE NR 5001260509-0030. AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING EPSU BATTERIES CAPACITY TEST, EPSU 11WL BATTERY FAILED CAPACITY TEST. REPLACEMENT IS REQUIRED IAW AMM 33-51-38-000-002-A/REV 95 AND AMM 33-51-38-400-002-A/REV 95 - [SDR F3LA2023091800164](https://openairdocs.org/sdr/F3LA2023091800164.md): Battery · failed · Sep 1, 2023 · N322FR · Airbus A320251N · Emergency Lighting > REFERENCE NR 5001260509-0020. AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING EPSU BATTERIES CAPACITY TEST, EPSU 10WL BATTERY FAILED CAPACITY TEST. REPLACEMENT IS REQUIRED IAW AMM 33-51-38-000-002-A/REV 95 AND AMM 33-51-38-400-002-A/REV 95. - [SDR F3LA2023091800170](https://openairdocs.org/sdr/F3LA2023091800170.md): Shear Tie · cracked · Aug 31, 2023 · N322FR · Airbus A320251N · Fuselage Internal Mounting Structure > REFERENCE NR 5001260330-0010. AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INSPECTION FOUND L/H SHEAR PLATE FR69-70 CRAKED. REQUIRES REPLACEMENT AS PER A320NEO SRM 51-72-11-911-001 REV. 37. L/H SHEAR PLATE WAS REPLACED AS PER A320NEO S - [SDR F3LA2023091800169](https://openairdocs.org/sdr/F3LA2023091800169.md): Shear Plate · cracked · Aug 31, 2023 · N322FR · Airbus A320251N · Fuselage Miscellaneous Structure > REFERENCE NR 5001260327-0010. AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INSPECTION FOUND R/H SHEAR PLATE FR69-70 CRAKED. REQUIRES REPLACEMENT AS PER A320NEO SRM 51-72-11-911-001 REV. 37. R/H SHEAR PLATE WAS REPLACED AS PER A320NEO S - [SDR F3LA2023091800168](https://openairdocs.org/sdr/F3LA2023091800168.md): Door Sill · corroded · Aug 31, 2023 · N322FR · Airbus A320251N · Fuselage Miscellaneous Structure > REFERENCE NR 5001260322-0010. AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. CORRODED AFT DOOR SILL BEAM ON LH SIDE REQUIRES REPLACEMENT AS PER A320NEO SRM 51-41-14-283-002 REV. 37. DOOR SILL INSTALLATION HAS BEEN COMPLETED AS PER A320NEO SRM 51 - [SDR F3LA2023091800163](https://openairdocs.org/sdr/F3LA2023091800163.md): Floor Support · corroded · Aug 31, 2023 · N322FR · Airbus A320251N · Fuselage Miscellaneous Structure > REFERENCE NR 5001260332-0010. AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. FOUND FLOOR BEAM Y765 FR67-70 CORRODED REQUIRED REPLACEMENT AS PER A320NEO SRM 51-73-00 AND 51-74-00 REV. 37. FLOOR BEAM Y765 AT FR67-70 HAS BEEN REPLACED AS PER A320N - [SDR F3LA2023092000174](https://openairdocs.org/sdr/F3LA2023092000174.md): Pylon · elongated · Aug 30, 2023 · N322FR · Airbus A320251N · Nacelle/Pylon Structure > REFERENCE NR 5001260074-0040. AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. ELONGATED HOLES ON PYLON #1 CANTILEVER FLOOR REQUIRES FUTHER EVALUATION. REF: A320 NEO SRM 54-52-12 REV. 37. PERFORMED REPAIR LAY OUT AND TRANSFER OF HOLES ON REPAIR D - [SDR F3LA2023092000173](https://openairdocs.org/sdr/F3LA2023092000173.md): Pylon · elongated · Aug 30, 2023 · N322FR · Airbus A320251N · Nacelle/Pylon Structure > REFERENCE NR 5001260074-0010. AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. ELONGATED HOLES ON PYLON #2 CANTILEVER FLOOR REQUIRES FUTHER EVALUATION. REF: A320 NEO SRM 54-52-12 REV. 37. PERFORMED REPAIR LAY OUT AND TRANSFER OF HOLES ON REPAIR DO - [SDR F3LA2023050100006](https://openairdocs.org/sdr/F3LA2023050100006.md): Elt · failed · Dec 27, 2022 · N322FR · Airbus A320251N · Emergency Locator Beacon > AFT FIXED ELT 110MX FAILED OPERATIONAL CHECK AMM 25-65-00-710-001 REF TASK CARD 256535-02-1. REMOVED AND REPLACED FIXED ELT IAW AMM 25-65-35-000-001-A AND 25-65-35-400-001-A. OPS CHECKS GOOD IAW AMM 25-65-00-740-001-A. COMPLIED WITH EA# N2-25R-37366 IN INSTA - [SDR F3LA2021110900082](https://openairdocs.org/sdr/F3LA2021110900082.md): Pipe · leaking · Nov 7, 2021 · N322FR · Airbus A320251N · Hydraulic System, Main > LP178842 ITEM 1 DISCREPENCY -- HYD GREEN SYSTEM LOSS OF FLUID IN FLIGHT --- CORRECTIVE ACTION -- FOUND L/H ENG HYD PRESSURE LINE LEAKING JUST ABOVE FAN COWL UNDER PANEL 413AL. REMOVED AND REPLACED HYD LINE IAW AMM 20-21-12-911-001-A SERVICED GREEN SYS AMM 12-1 - [SDR F3LA2021081600060](https://openairdocs.org/sdr/F3LA2021081600060.md): Line · leaking · Aug 14, 2021 · N322FR · Airbus A320251N · Hydraulic System, Main > GREEN HYDRAULIC SYSTEM FAILURE AND MANUAL GEAR EXTENSION. DURING THE T/S FOUND HYD LINE #1 ENGINE PYLON CRACKED. SVCD GREEN HYD PER REF AMM 12-12-29-611-301-A. R/R ENG 1 PYLON HYD LINE PER AMM 29-11-49-04, LK & OPS CK OK. C/W AMM 32-00-00-860-003-A TO PUT L - [SDR F3LA2021011100002](https://openairdocs.org/sdr/F3LA2021011100002.md): Line · leaking · Jan 9, 2021 · N322FR · Airbus A320251N · Hydraulic System, Main > HYD G RSVR LO LEVEL HYD G ENGINE 1 PUMP LO PR HYD G SYS LO PR. FOUND HYD LINE PART NR D2902083800000 LEAKING IN FORWARD PYLON NR 1 ENGINE. CORRECTIVE ACTION: REPLACED HYD LINE, PER AMM 29-00-00-910-0014-A. LEAK CHECK C/W NO LEAKS NOTED. AIRCRAFT OK FOR SER - [SDR F3LA2019021200016](https://openairdocs.org/sdr/F3LA2019021200016.md): Actuator · failed · Feb 11, 2019 · N322FR · Airbus A320251N · Leading Edge Slat Actuator > FLIGHT CONTROL SLATS FAULT ECAM SLATS AT ZERO, FLAPS WORK. THE PREVIOUS 2 FLIGHTS ALSO HAD THE SAME ECAM. REMOVED AND REPLACED TYPE A SLAT ACTUATOR ASSEMBLY, OPS AND RIG CHECKS GOOD, REFERENCE AMM 27-84-48 PB401 LEFT WING #11 SLAT TRACK 6041CM. ## 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 = 'N322FR' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N322FR/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.