N206FR
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 = 'N206FR' 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.
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 = 'N206FR' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR ANCF20260422010Computer · abnormalDURING FLAP/SLAP RETRACTION AT TAKEOFF F7CTL SLTAS LOCKED WING TIP BRK IAW AMM 27-51-34-000-001A AND 27-51-34-400-001A REV 76 01/FEB 2026 SFCC 22CV WAS REPLACED IN NORMAL CONDITION BITE TEST SATISFACTORY. IAW AMM 27-80-00-869-004A THE REST OF THE WING TIP BRASDR 2026FA0000231Computer · faultedAFTER TAKE OFF FLAPS LOCKED. IAW AMM 27-51-00-740-002-A BITE TEST SLAT AND FLAP CONTROL COMPUTER, IAW AMM 27-50-00-869-006-A RESET OF WING TIP BRAKE WAS PERFORMED, SATISFACTORY, IAW AMM 31-36-00-000-001-A PCMCIA MEMORY CARD WAS DOWNLOADED. IAW TSM TASK 27SDR F3LA2022080800083Floorbeam · corrodedDISCREPANCY: REFERENCE LP 12197.0534 BEAM Y919 HAS CORROSION AROUND HOLE AT FRAME C66. CORRECTIVE ACTION: EVALUATED, REMOVED AND REPLACED FLOOR BEAM Y919 AT FR 66 IAW A320 SRM 53-00-14-283-002, 51-42-11 AND 51-75-12-911-002//ENDSDR F3LA2022080800082Floorbeam · corrodedDISCREPANCY: REFERENCE NR 12197.0545 AFT WET AREA FR 66 FLOORBEAM-Y1292 CORRODED. CORRECTIVE ACTION REMOVED AND REPLACED FLOORBEAM-Y1292 AT FR66 IAWA320 SRM 51-72-11SDR F3LA2022080800081Floorbeam · corrodedDISCREPANCY: REFERENCE NR 12197.0547 AFT WET AREA FR 68 FLOORBEAM Y765 CORRODED. CORRECTIVE ACTION REMOVED AND REPLACED FLOORBEAM Y765 AT FR68 IAW A320 SRM 51-72-11SDR F3LA2022091400104Retainer · corrodedR1 DOOR AREA BELOW GIRT BAR RETAINERS, CORROSION ON WEB FWD AND AFT RETAINER AREA. EVALUATED AND REPAIRED R1 DOOR SILL WEB FWD AND AFT RETAINER AREAS IAW A320 SRM 53-11-14-283-005SDR F3LA2022091400108Shear Plate · corrodedCORROSION ON MULTIPLE AREAS ON RH LATERAL SHEAR PLATE FROM FRAME C69C70. REMOVED AND REPLACED RH LATERAL SHEAR PLATE FROM FRAME C69 TO C70 IAW SRM 51-42-11.SDR F3LA2022091400107Shear Plate · corrodedCORROSION ON MULTIPLE AREAS ON LH LATERAL SHEAR PLATE FROM FRAME C69C70. REMOVED AND REPLACED LH LATERAL SHEAR PLATE FROM FRAME C69 TO C70 IAW A320 SRM 51-42-11. PERFORMED PERATIONAL TEST OF VOR 1 AND 2 SYSTEMS IAW AMM 34-55-00-740-002-A. BITE TEST GOODSDR F3LA2022091400106Beam · corrodedAFT R2 DOOR SILL BEAM PREVIOUS REPAIR CORRODED. REMOVED AND REPLACED CORRODED R2 DOOR SILL IAW SRM 51-42-11SDR F3LA2022091400103Beam · corrodedL1 DOOR SILL BEAM, FWD AND AFT FASTENER HOLES CORRODED. REMOVED AND REPLACED L2 DOOR SILL IAW A320 SRM 51-42-11SDR F3LA2022091400105Floor Support · corrodedMAIN CABIN L/H FLOOR SUPPORT Y1292 HAS CORROSION ON UPPER FLANGE STA 16-STA20. REMOVED AND REPLACED Y1292 FLOOR SUPPORT STA 16-20 IAW A320 SRM 51-72-911-002SDR F3LA2021121300088Clamp · leakingSTRONG ODOR DURING APPROACH TO LANDING. LP172678 APU LEAKING OIL AT FAN ASSY. CLAMP / REMOVED AND REPLACED PACKINGS AND CLAMP IAW AMM 49-52-51-400-002-A, NO LEAKS NOTED AT THIS TIME. A/C OK TO CONTINUESDR F3LA2021100700073Unknown · odorLP177985 DISCREPENCY ITEM 1 -- FUME EVENT IN DESCENT AT 14000' TO LANDING SMELLED LIKE DIRTY SOCKS. FOUND OIL LEAKING FROM APU OIL DRAIN PLUG REPAIR PLUG LEAK CHECK GOOD REF LP177989 FOR ENGINE AND APU RUNS FOR TWO HOURS AMM 05-50-816-831SDR F3LA2021100400072Drain · leakingAFT FA'S REPORTED FEELINGS TINGELS AND SMELLED DIRTY SOCKS . C/W INSPECTION TO ID CAUSE OF FUME EVENT FOUND TO BE TYPE 3 ENG 2 & C/W DECONTAMINATION OF ECS. PER TSM T/S MANUAL 05-50-500-810-831-A. PLACED ENG 2 BLEED AIR SYSTEM ON MEL 36-11-01ACNTL # 11754SDR F3LA2021006010039Unknown · odorDISCREPANCY: FUME EVENT (SMELLED LIKE ACFT OIL) ON APCH TO CUN. C/W QRH, MASKS ON, SWITCHED OFF LH PACK. A4FTER LANDING, FA'S SAID NO ODOR IN CABIN, BUT THEY COULD SMELL IT ON FLIGHT DECK. PLACED #1 PACK ON MEL# 25-52-01F. CORRECTIVE ACTION: REFERENCE MEL 21-5SDR F3LA2017102700242Nut · looseNR 1 ENGINE AFT MOUNT OTBD LINK UPPER SHEAR PIN NUT LOOSE. REMOVED AND REPLACED THE AFT MOUNT NUT IAW AMM 71-22-11-400-043-A.SDR F3LA2017102700241Nut · looseNR 1 ENGINE AFT MOUNT INBD LINK UPPER SHEAR PIN, NUTS ARE LOOSE. REMOVED AND REPLACED THE NR 1 ENGINE AFT MOUNT I/B LINK UPPER SHEAR PIN NUT IAW AMM 71-72-11-400-043-A.SDR F3LA2016103100065Battery Pack · dischargedLEFT EMERGENCY EXIT POWER SUPPLY BATTERY FAULT. REPLACED THE BATTERY PACK, OPS CHECKED OK. IAW AMM 33-51-38 PB 401.SDR F3LA2016030200008Door Sill · corrodedDURING C CHECK INSPECTION NOTED L2 DOOR SILL CORRODED AROUND FASTENER HOLE AT FRAME 68. REPAIRED L2 DOOR SILL AT FRAME 68 IAW SRM 53-41-14 FIGURE 201.SDR F3LA2016030200007Door Sill · corrodedDURING C CHECK INSPECTION, NOTED THE R2 DOOR SILL CORRODED AROUND FASTENER HOLE AT FRAME 68. REPAIRED R2 DOOR SILL AT FRAME 68 IAW SRM 53-41-14 FIGURE 201.SDR F3LA2016021700004Hydraulic Line · burstHYD GREEN RSVR LOW LEVEL ECAM. R & R AFT HYD LINE RT MLG DOOR IAW AMM 32-31-39PB401. NO LEAKS NOTED AT THIS TIME. SERVICED GREEN HYD SYS.SDR F3LA2010043000393Epsu · faultyDISCOVERED DURING OVERNIGHT MX REF LOG PAGE 523605. EMERGENCY POWER SUPPLY UNIT (EPSU) 11WL FAULTS. R & R EMERGENCY POWER SUPPLY UNIT (EPSU) 11WL OPS CHECK GOOD IAW AMM 33-51-38 PB 401.
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