N201FR

Service difficulty reports · 22

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 = 'N201FR' AND registry_match = 'registration'
  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 F3LA2021080400057Intake · contaminatedDISCREPANCY: STRONG BURNING RUBBER SMELL MID-FLIGHT ROWS 13-14 DURING DESCENT. / PERFORMED TSM 05-50-00-810-831-A DECISION TABLE MOST PROBABLE CAUSE APU. PERFORMED AMM 49-00-00-200-812-A. FOUND OIL ON INTAKE FLAP CLEANED AREA, OPENED APU AND INSPECTED, NO OTHEJul 30, 2021 · N201FR · Airbus A320214 · APU Core EngineSDR F3LA2019013100009Slide · failedDISCREPANCY: REFERENCE LOG PAGE LP1148549 ITEM 3, EPSU TEST FAILURE WITH MULTIPLE MX MESSAGES. AFTER FURTHER TROUBLE SHOOTING L1 DOOR SLIDE FOUND TO BE CAUSE. L1 DOOR SLIDE REQUIRES REPLACEMENT. CORRECTIVE ACTION: REMOVED AND REPLACED L1 DOOR SLIDE REFERENCEJan 28, 2019 · N201FR · Airbus A320214 · Escape SlideSDR F3LA2018101800457Not Reported · malfunctionedABORTED TAKE-OFF FOR RUDDER JAM/DIFFICULT DIRECTIONAL CONTROL. THE AIRCRAFT WAS GROUNDED DUE TO THE EVENT. MX PERFORMED YAW DAMP SYS TEST AMM 22-63-00-710-001-A, ADIRS SYS TEST AMM 34-14-00-740-004-A, AFS TEST AMM 22-91-00-710-001-A, AUTO CHANGEOVER FUNCTION AOct 14, 2018 · N201FR · Airbus A320214 · Rudder Control SystemSDR F3LA2018092500444Door Frame · crackedLT FWD EMERG EXIT DOOR FWD I/B FRAME HAS CRACK INDICATIONS. REPAIRED LT FWD EMERGENCY EXIT DOOR FWD I/B FRAME IAW EA A2-52R-34380.Sep 5, 2018 · N201FR · Airbus A320214 · Emergency ExitsSDR F3LA2018092500443Door Frame · crackedLT AFT EMERG EXIT DOOR FWD I/B FRAME HAS CRACK INDICATIONS. REPAIRED LT AFT EMERGENCY EXIT DOOR FWD I/B FRAME IAW EA A2-52R-34380.Sep 5, 2018 · N201FR · Airbus A320214 · Emergency ExitsSDR F3LA2018092500442Door Frame · crackedRT FWD EMERG EXIT DOOR AFT I/B FRAME HAS CRACK INDICATIONS. REPAIRED RT FWD EMERGENCY EXIT DOOR AFT I/B FRAME IAW EA A2-52R-34380.Sep 5, 2018 · N201FR · Airbus A320214 · Emergency ExitsSDR F3LA2018092400441Door Frame · crackedRT AFT EMERG EXIT DOOR AFT I/B FRAME HAS CRACK INDICATIONS. REPAIRED RT AFT EMERGENCY EXIT DOOR AFT I/B FRAME IAW EA A2-52R-34380.Sep 5, 2018 · N201FR · Airbus A320214 · Emergency ExitsSDR F3LA2018092400440Door Frame · crackedLT FWD EMERG EXIT DOOR AFT I/B FRAME HAS CRACK INDICATIONS. REPAIRED LT FWD EMERGENCY EXIT DOOR AFT I/B FRAME IAW EA A2-52R-34380.Sep 5, 2018 · N201FR · Airbus A320214 · Emergency ExitsSDR F3LA2018092100439Door Frame · crackedLT AFT EMERGENCY EXIT DOOR AFT I/B FRAME HAS CRACK INDICATIONS. REPAIRED LT AFT EMERGENCY EXIT DOOR AFT I/B FRAME IAW EA A2-52R-34380.Sep 5, 2018 · N201FR · Airbus A320214 · Emergency ExitsSDR F3LA2018091700433Dummy Rail · corrodedMAIN CABIN LONGITUDINAL FLOORBEAM TOP CAP CORRODED, Y+503.2, FR16. REMOVED AND EVALUATED CORROSION ON MAIN CABIN LONGITUDINAL FLOORBEAM AT Y+503.2 FR16. MAT REMOVED .082", MAX ALLOWED .047" FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14-283-004 FIG 006 SHEET 1, RESep 4, 2018 · N201FR · Airbus A320214 · Fuselage, Seat/Cargo Attach FittingsSDR F3LA2018091700437Door Sill · corrodedL2 DOOR SILL CORRODED AT THE FWD AND AFT BLANKING PLATE FASTENER HOLES. REMOVED AND REPLACED THE L2 DOOR SILL IAW SRM 53-41-14-300-001, 51-72-11-911-001, 51-42-11 AND AMM 38-30-00.Sep 4, 2018 · N201FR · Airbus A320214 · Fuselage Miscellaneous StructureSDR F3LA2018091700436Floor Support · corrodedMAIN CABIN LONGITUDINAL FLOORBEAM TOP CAP CORRODED, FR16-FR18 BL 8.5+Y. REMOVED AND EVALUATED CORROSION OF FLOORBEAM AT Y8.5 FR16-18. MAX ALLOWED REMOVAL IS .031" MAT. REMOVED .038 FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14-283-004. REMOVED AND REPLACED FLOORBSep 4, 2018 · N201FR · Airbus A320214 · Fuselage Miscellaneous StructureSDR F3LA2018091700435Floorbeam · corrodedMAIN CABIN FLOORBEAM TOP CAP, CORRODED 1292, FR16. REMOVED CORROSION AND EVALUATED FLOORBEAM 1292 FR16. REMOVED .0185 MATERIAL, FOUND TO BE OUT OF LIMITS IAW A320 SRM 53-11-15. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-42-11, 52-11-15 AND 51-44-11.Sep 4, 2018 · N201FR · Airbus A320214 · Fuselage Main, Floor BeamSDR F3LA2018091700434Door Sill · corrodedR2 DOOR SILL HAS CORROSION AROUND FASTENER HOLE AT FWD SECTION. REMOVED AND REPLACED R2 DOOR SILL IAW SRM 51-72-11-911-001, 53-41-14-283-002, 51-42-11 AMM 38-30-00.Sep 3, 2018 · N201FR · Airbus A320214 · Fuselage Miscellaneous StructureSDR F3LA2018091300430Floorbeam · corrodedFLOORBEAM -Y765 CORRODED FR 68. REMOVED AND REPLACED FLOORBEAM -Y765 FROM FS 67 TO FS 70 IAW SRM 51-72-11, 51-42-11 AND 53-00-14.Sep 3, 2018 · N201FR · Airbus A320214 · Fuselage Main, Floor BeamSDR F3LA2018091300429Floorbeam · corrodedFLOORBEAM -Y765 CORRODED FR66. REMOVED AND REPLACED FLOORBEAM -Y765 FROM FS 64 TO FS 66 IAW SRM 51-72-11, 51-42-11 AND 53-00-14.Sep 3, 2018 · N201FR · Airbus A320214 · Fuselage Main, Floor BeamSDR F3LA2017021500081Skin · corrodedAFT RIGHT FUSELAGE LAVATORY BACKING SYSTEM EXHAUST VENT SKIN CUT-OUT SEPERATING AND CORRODED JUST FORWARD OF FRAME 70. REPAIRED THE SKIN.Jan 27, 2017 · N201FR · Airbus A320214 · Fuselage Main, Plate/SkinSDR F3LA2014122901095Hydraulic Line · failedGREEN SYS HYD LINE FAILED, FLUID LOSS, RETURNED TO THE FIELD. R & R THE LINE ASSEMBLY IAW AMM 32-31-39-400-001-A. OPERATIONS IAW AMM 32-31-00-710-002-A01 & LEAK CHECKED NORMAL. LOG PAGE 911844 2.Dec 24, 2014 · N201FR · Airbus A320214 · Hydraulic System, MainSDR F3LA2013082600903Skin · dentedACFT OUT OF SERVICE DURING C4/S1 CHECK. LT WING L/E NR 1 SLAT DAMAGED OTBD END. REPAIRED IAW SRM 57-40-00, PB201.Aug 16, 2013 · N201FR · Airbus A320214 · Leading Edge DevicesSDR F3LA2013082600902Plate · corrodedDURING C4/S1 CHECK. CABIN RT AFT SHEAR PLATE CORROSION. R & R SHEAR PLATE IAW SRM 51-42-11, PARA 6.B.(1)-(8). ACFT OUT OF SERVICE.Aug 10, 2013 · N201FR · Airbus A320214 · Fuselage Miscellaneous StructureSDR F3LA2010082400486Wire Harness · failedSMOKE REPORTED IN AFT GALLEY. POWER WAS SHUTOFF AND BREAKERS PULLED, PERFORMED VISUAL INSP BEHIND AFT GALLEY UNIT, POWER CONTROL PANEL FOR COFFEE MAKERS, OVEN, INSPECTED WIRING HARNESS NO BURN MARKS, NO BURN MARKS ON PLUMBING LINES, FOUND AFT OVEN VENT FILTERSAug 22, 2010 · N201FR · Airbus A320214 · Equipment/Furnishings WiringSDR F3LA2009052600087Attach Fitting · brokenDURING DAILY CHECK, DEN MAINTENANCE NOTED THE LEFT INBOARD ELEVATOR SERVO CONTROL ATTACH POINT ANTI-ROTATION LUG WAS BROKEN. MAINTENANCE PERFORMED A MAJOR REPAIR BY FABRICATING AND INSTALLING A REPAIR LUG TO THE LEFT HAND ELEVATOR INBOARD SERVO CONTROL FITTINMay 24, 2009 · N201FR · Airbus A320214 · Wing, Control Surface Attach Fittings
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