# Service difficulty reports: N316FR A list on [N316FR](https://openairdocs.org/aircraft/N316FR.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR F3LA2023091900171](https://openairdocs.org/sdr/F3LA2023091900171.md): Computer · inoperative · Sep 15, 2023 · N316FR · Airbus A320251N · Cabin Cooling System > THE AC WAS GROUNDED DUE TO AN SDR REPORTABLE EVENT. DEFECT FOR VENT SKIN VALVE FAULT. PER TSM 21-26-00-810-844-0-A, REMOVED AND REPLACED AEVC IAW AMM 21-26-34-000-001-A. OPS CHECK GOOD. NO FAULTS ON ECAM AT THIS TIME. AC OK FOR SERVICE. ORIGINAL SUBMISSION - [SDR F3LA2023052200060](https://openairdocs.org/sdr/F3LA2023052200060.md): Battery · failed · May 22, 2023 · N316FR · Airbus A320251N · Emergency Lighting > DISCREPANCY: REFERENCE LOG PAGE LP264465 ITEM #1, AIRCRAFT WAS NOT GROUNDED AND WAS AN OVERNIGHT LINE MX CHECK. EPSU TEST FAULT. CORRECTIVE ACTION: REMOVED AND REPLACED 10WL EPSU BATTERY PER AMM 33-51-38-000-002-A AND 33-51-38-400-002-A. OPS TEST GOOD PER AMM - [SDR F3LA2023040700038](https://openairdocs.org/sdr/F3LA2023040700038.md): Threshold · corroded · Mar 21, 2023 · N316FR · Airbus A320251N · Fuselage Floor Panel > DISCREPANCY: REFERENCE NR 5001226088-0020 UPON REMOVAL FOR ACCESS ON INSPECTION FOUND 261LG PANEL CORRODED AND REQUIRES REPLACEMENT. CORRECTIVE ACTION: REPAIRED 261LG PANEL AS PER EA# N2-53R-37571 REV. ORIG REV DATE. N/A TASK SUBJECT TO RII. THE EMBODIED REP - [SDR F3LA2023040700037](https://openairdocs.org/sdr/F3LA2023040700037.md): Beam · corroded · Mar 21, 2023 · N316FR · Airbus A320251N · Fuselage Main, Floor Beam > DISCREPANCY: REFERENCE NR 5001226012-0010 CORROSION ON BEAM Y-254 BETWEEN FR12-FR24 AT FR15 MEASUREMENTS REWORK #1L-31.31MM W=22.56MM D=1.08MM REWORK#2 L-21MM W=2.96MM D=100% OF MATERIAL LOSS AREA FOUND OUT OFF LIMITS NO ALLOWABLE LIMITS IN SRM. CORRECTIVE - [SDR F3LA2023040600036](https://openairdocs.org/sdr/F3LA2023040600036.md): Door Seal · corroded · Mar 20, 2023 · N316FR · Airbus A320251N · Fuselage Miscellaneous Structure > DISCREPANCY: REFERENCE NR: 5001225799-0010 CORRODED ANCHOR NUT HOLE ON LH AFT PASSENGER DOOR SILL AT FRAME 68. CORRECTIVE ACTION: PERFORMED REPAIR PER A320 NEO SRM 53-41-14-300-001 REV. 35//END// - [SDR F3LA2023040600035](https://openairdocs.org/sdr/F3LA2023040600035.md): Beam · corroded · Mar 20, 2023 · N316FR · Airbus A320251N · Fuselage Main, Floor Beam > DISCREPANCY: REFERENCE NR 5001225807-0010 FOUND CORROSION ON BEAM Y-1162.5 FR 68-69 MEASUREMENTS: L=109MM W= 80.6MM D=0.43MM AREA FOUND OUT OF LIMITS AS PER SRM TASK 53-41-14-283-009 REV. 35. CORRECTIVE ACTION: REPLACED BEAM Y-1162.5 FR 68-69 AS PER SRM 51- - [SDR F3LA2023040600034](https://openairdocs.org/sdr/F3LA2023040600034.md): Seat Track · corroded · Mar 20, 2023 · N316FR · Airbus A320251N · Fuselage, Seat/Cargo Attach Fittings > DISCREPANCY: REFERENCE NR 5001225819-0010 FOUND CORROSION ON SEAT TRACK Y1292 AT FR16-17 MEASUREMENTS L-50MM W=20MM D=0.88MM AREA FOUND OUT OFF LIMITS AS PER SRM TASK 53-11-14-283-007 REV. 35 CORRECTIVE ACTION: REPLACED SEAT TRACK Y1292 AT FR16-17 AS PER SRM - [SDR F3LA2023013010016](https://openairdocs.org/sdr/F3LA2023013010016.md): Fmu · defective · Jan 24, 2023 · N316FR · Airbus A320251N · Fuel Controlling System > ENGINE 2 STALL ECAM. STALL WAS HEARD AND FELTED, 14,000 FEET 340 KNOTS, ECAM WANT AWAY IMMEDIATELY AND ENGINE PARAMETERS NORMAL. REMOVED & REPLACED ENG #2 FMU PER STEP 4.B.(5).(A). OPS CHECK AND LEAK CHECK GOOD.//END// - [SDR F3LA2022102700140](https://openairdocs.org/sdr/F3LA2022102700140.md): Light · unknown · Oct 26, 2022 · N316FR · Airbus A320251N · Emergency Lighting > FLOOR LEVEL EMERGENCY EXIT LIGHTS AT AT THE FWD & AFT DOOR EXIT DID NOT ILLUMINATE. PERFORMED OPS TEST OF EMERGENCY LIGHTING, OPS TEST GOOD. REF AMM 33-51-16-860-056-A. - [SDR F3LA2022101000128](https://openairdocs.org/sdr/F3LA2022101000128.md): Unknown · odor · Oct 6, 2022 · N316FR · Airbus A320251N · Air Distribution System > FA'S REPORT AN UNUSUAL ODOR IN THE MID-AFT AIRCRAFT. PERFORMED INSPECTION OF CABIN FOR EVIDENSE OF ODOR OR SMOKE OR FUME. POST BORESCOPE INSPECTION OF THE NR 2 ENGINE. NO ODOR OR DEFECTS NOTED AT THIS TIME. TSM 71-00-00-810-892-A. ORIGINAL SUBMISSION DATE: 1 - [SDR F3LA2022100300126](https://openairdocs.org/sdr/F3LA2022100300126.md): Unknown · odor · Oct 2, 2022 · N316FR · Airbus A320251N · Air Distribution System > APPEARED TO BE FUME EVENT ON DOWN WIND SIDE LANDING PERFORMED INSPECTION CABIM FOR ODOR, SMOKE OR FUME. NO SMOKE OR FUME NOTED AT THIS TOME IAW TSM 05-50-00-810-831-A AC OK FOR SERVICE - LP295768#3 ENGINE#1 RUN - PERFORMED ENGINE#1 IDLE RUN NO DEFECTS NOTED - [SDR F3LA2022091500109](https://openairdocs.org/sdr/F3LA2022091500109.md): Pitot Tube · dirty · Sep 13, 2022 · N316FR · Airbus A320251N · Pitot/Static System > RTO FOR STANDBY AIRSPEED INDICATOR 20 KTS LESS THAN PF PRIMARY AIRSPEED INDICATOR. PERFORMED CLEANING OF PITOT PROBES IAW 34-10-00-170-004-A AND BITE TEST IF ISIS AMM 34-22-25-740-001A OCF REQUIRED.//END// - [SDR F3LA2021071200054](https://openairdocs.org/sdr/F3LA2021071200054.md): Fitting · cracked · Jul 9, 2021 · N316FR · Airbus A320251N · Hydraulic System, Main > LP156984 ITEM 1, DISCREPANCY: GREEN HYDRAULIC SYSTEM LO PRESSURE. AIR TURN BACK TO DENVER. CORRECTIVE ACTION: FOUND PRESSURE FITTING LEAKING IN #1 ENGINE PYLON. REPLACED FITTING AND HYD LINE, DUE TO BOTH NEEDING TO BE REPLACED AS A SET PER THE IPC ( - [SDR F3LA2020123000056](https://openairdocs.org/sdr/F3LA2020123000056.md): Battery Pack · no test · Dec 30, 2020 · N316FR · Airbus A320251N · Escape Slide > DEFECT: EPSU TEST FAILURE. CORRECTIVE ACTION: REMOVED AND REPLACED EPSU BATTERY FOR UNIT (10WL) AND UNIT (13WL). EPSU TEST STILL FAILS. SYSTEM REQUIRES FURTHER TROUBLESHOOTING, REFERENCE AMM 33-51-38. REMOVED AND REPLACED R2 DOOR SLIDE, OPERATIONS CHECK GO - [SDR F3LA2020091400037](https://openairdocs.org/sdr/F3LA2020091400037.md): Slide · no test · Sep 12, 2020 · N316FR · Airbus A320251N · Emergency Lighting > DISCREPANCY: L1 DOOR SLIDE FAILED EPSU TEST. DURING OVERNIGHT MAINTENANCE. CORRECTIVE ACTION: REPLACED L1 DOOR SLIDE, REF AMM 25-62-44-000-012-A AND 25-62-44-400-007-A. OPS CHECKS GOOD AT THIS TIME. - [SDR F3LA202006240029](https://openairdocs.org/sdr/F3LA202006240029.md): Fitting · buckled · Jun 23, 2020 · N316FR · Airbus A320251N · Hydraulic System, Main > HYD GREEN RSVR LO LEVEL FOLLOWED BY GREEN PUMP LO PRESSURE, GREEN SYSTEM LO PRESS, PERFORMED QRH PROCEDURES. DECLARED EMERGENCY, NO FURTHER DEFECTS NOTED. UNDER LANDING WEIGHT. - ALSO GRAVITY GEAR EXTENSION PERFORMED W/NO DEFECTS NOTED, ALL 3 GREEN IND. MAINTA - [SDR F3LA202003260024](https://openairdocs.org/sdr/F3LA202003260024.md): Epsu · failed · Mar 26, 2020 · N316FR · Airbus A320251N · Emergency Lighting > DISCREPANCY: LP1241800 ITEM 1: DURING OVERNIGHT MAINTENANCE, EPSU SYS TEST FAILED DUE TO EPSU 11WL FAULT. CORRECTIVE ACTION: REMOVED AND REPLACED EPSU 11WL, DUE TO FAULTING PERFORMED EPSU SYS TEST, TEST PASSED. REF AMM 33-51-38-000-001-A AND AMM 33-51-38-400 ## 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 = 'N316FR' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N316FR/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.