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 aircraft_model_key = '408' 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 aircraft_model_key = '408' 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 FXGA202610140001Skin · crackedFOUND 2 CRACKS ON LT WING UPPER SKIN. 1ST CRACK 2.3" LONG BETWEEN RIBS AT LBL 142.3 & 157.95, APPROXIMATELY 17.5 INCHES FORWARD OF WING TRAILING EDGE. 2ND CRACK 4.5" LONG BETWEEN RIBS AT LBL 157.95 & 173.6, APPROXIMATELY 14.25 INCHES FORWARD OF WING TRAILING ESDR 2026FA0000836Fairing · separatedUPPER VERTICAL TIP CAP FAIRING SEPARATED IN FLIGHT, SUBSEQUENTLY DAMAGING UPPER PORTION OF RUDDER, UPPER VERTICAL SKIN, ELEVATOR PUSH RODS AND ELEVATOR HORNS.SDR FXTA20261016001Rib · cracked3 CRACKED RIBS RIGHT FLAP COVE. RIB P/N: 7822265-10 @ WS 100.5", RIB P/N: 7822265-12 @ WS 116.0", RIB P/N: 7822265-12 @ 131.5"SDR COEA2026101213738Armature · crackedDURING A SCHEDULED INSPECTION, A CRACK WAS DISCOVERED ON THE LT FWD INERTIAL SEPERATOR ARMATURE. REPLACED INERTIAL SEPERATOR FWD TORQUE TUBE IAW C408 MM 30-20-16. OPS CHECK GOOD.SDR COEA2026101212767Skin · crackedDURING A POST FLIGHT INSPECTION, DISCOVERED A CRACK ON THE RT UPPER WING SKIN BETWEEN WS 224.32 AND WS 241.68. OPENSDR COEA2026101211767Skin · crackedDURING A POST FLIGHT INSPECTION, DISCOVERED A CRACK IN THE LT UPPER WING SKIN BETWEEN WS 157.95 AND WS 142.30. OPENSDR COEA2026100109708Skin · crackedEVIDENCE OF A CRACK ON THE R/H WING AFT SIDE TOWARDS THE OUTBOARD PORTION OF THE FLAP. OPENSDR COEA2026100108708Panel · dentedDENT UNDER LT SPONSON PANEL. OPENSDR COEA2026091707734Light · failedFLIGHT 204, GEG - MFR AIR TURNBACK, REMOTE CAB CASS MESSAGE DURING FLIGHT. AIRCRAFT WAS RETURNED TO GEG. REPLACED LT WING TIP LIGHT ASSY. OPS CHKD GOOD.SDR FXTA20260904001Skin · crackedINSPECTION PANEL ON TOP OF THE VERTICAL STABILIZER ATTACHMENT FLANGE CRACKED ALLOWING THE PANEL TO DEPART AIRCRAFT. THIS INSPECTION PANEL IN UNDER THE RUDDER HORN. TOP PANEL P/N: 7831102-23, ONCE ATTACHMENT FAILS HITS RUDDER AND PIECE FOUND IN ELEVATOR CONTROLSDR COEA2026090306783Exhaust Stack · brokenRIGHT INBD EXHAUST STACK PORT FOR THE HEATED INTAKE DUCT BROKEN OFF. RT INBD EXHAUST STACK REPLACED IAW MM 78-10-05. MINOR REPAIR.SDR COEA2026082705738Master Cylinder · failedFLIGHT 7804, PILOT SIDE RIGHT BRAKE PEDAL INEFFECTIVE. REPLACED ALL 4 MASTER CYLINDERS AND RT BRAKE ASSEMBLY. FLUSHED ENTIRE SYSTEM. ALL CHECKS GOOD.SDR COEA2026081904738Brake · contaminatedRIGHT BRAKE INEFFECTIVE DURING ROLLOUT. BLED AIR FROM RT BRAKE ASSY. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.SDR COEA2026100810759Stringer · damagedON SKIN REMOVAL, FOUND OVERSIZED HOLE IN FRAME 3, ON STRINGER 13L. FREEZE BUSHING REPAIR TO OVERSIZED HOLE, FRAME 3, ON STRINGER 13L IAW FR-408-00-15-54161.SDR FXTA20260804001Strut · damagedDURING PREFLIGHT, IT WAS DISCOVERED THAT THE RH UPPER WING STRUT MISSING PART OF METAL FAIRING. APPEARS THAT DURING MANUFACTURE THE SEAMS WERE OFFSET CAUSING A STRESS IN THE SKIN ALLOWING IT TO CRACK.SDR FXTA20260628002Flex Drive · failedRT OUTBOARD FLAP FLEX SHAFT RUBBER CASE FAILING AT THE CRIMP UNDER STAINLESS STEEL OUTER WRAP. THIS SEPARATION ALLOWS THE OUTER CASE TO LENGTHEN AND THE INNER DRIVE SHAFT CAN SLIDE LEFT AND RIGHT TO THE POINT THE DRIVE COMES OUT OF THE JACKSCREW CAUSING THE FLSDR FXTA20260628001Bolt · looseFLAP ACTUATOR ATTACHMENT HARDWARE FOUND LOOSESDR FXTA20260626001Bolt · looseFLAP ACTUATOR ATTACHMENT HARDWARE FOUND LOOSESDR COEA2026101314759Skin · damagedPERMANENT REPAIR OF L/H NOSE SKIN AND L/H DOOR DRIP CAP DAMAGE. PERMANENT REPAIR COMPLETED IAW DQ51100M2.SDR FXTA20260617001Flex Drive · failedLH AND RH OUTBOARD FLAP FLEX SHAFT RUBBER CASE FAILING AT THE CRIMP UNDER STAINLESS STEEL OUTER WRAP. THIS SEPARATION ALLOWS THE OUTER CASE TO LENGTHEN AND THE INNER DRIVE SHAFT CAN SLIDE LEFT AND RIGHT TO THE POINT THE DRIVE COMES OUT OF THE JACKSCREW CAUSINGSDR FXGA202606150001Drive Cable · deformedFLAP FAIL CASS MESSAGE INDICATED WHEN FLAP DEPLOYED FROM FULL UP. UPON INVESTIGATION FOUND THE LT FLAP HAD A SLIGHT TWIST. THE OTBD ACTUATOR HAD NOT ENGAGED TO DRIVE THE FLAP AND THE INBD ACTUATOR DROVE THE INBOARD SIDE DOWN ABOUT 3 DEGREES BEFORE THE SYSTEM DSDR MTNA2026061500002Probe · false indicationON JUNE 12, 2026, DURING DESCENT ON FLIGHT MTN8380 FROM MEM TO DHN, 714FX, EXPERIENCED INTERMITTENT FUEL LEVEL LO R AND FUEL LEVEL LO L AMBER CAS MESSAGES BEGINNING APPROX 15 MINS PRIOR TO LANDING WITH 3,210 LBS INDICATED FOB AT DEPARTURE. THE RIGHT TANK LEVESDR MTNA2026051900001Probe · false indicationWHEN N743FX LANDED IN MCO LAST NIGHT WITH THE LOW FUEL LIGHT ON, WHEN THE PIC WAS PULLING INTO PARK, THEY HAD APPROXIMATELY 700 LBS AND THE NR 2 ENGINE SHUT OFF. THE RT SIDE NR 4 PROBE SEEMS TO BE WAY OFF PER 28-40-00.SDR 2026FA0000312Torque Tube · damagedPERFORMED INSPECTION OF THE RUDDER HINGES INSTALLATION DUE TO THE CUSTOMER REQUEST. ALL FOUND SATISFACTORY. DURING THE INSPECTION TECHNICIAN TOUCH THE ELEVATORS LH & RH SIDE AND FEELS FREE PLAY. WITH THE INSPECTION MIRROR AND TORCH PERFORMED QUICK CHECK AND RESDR 2026FA0000310Torque Tube · excess playPERFORMED INSPECTION OF THE RUDDER HINGES INSTALLATION DUE TO THE CUSTOMER REQUEST. ALL FOUND SATISFACTORY. DURING THE INSPECTION TECHNICIAN TOUCH THE ELEVATORS LH & RH SIDE AND FEELS FREE PLAY. WITH THE INSPECTION MIRROR AND TORCH PERFORMED QUICK CHECK AND RESDR MTNA2026061500001Probe · false indicationDURING MTNA'S 800 HR INSPECTION ON 758FX IT WAS IDENTIFIED THAT: LEFT FUEL QTY FOUND TO BE INACURATE, WITH EMPTY LEFT SIDE IS 77OLB OF FUEL MX: SYSTEM T/S PERFORMED, DETERMINED #4 PROBE AT FAULT PER C408 MM CHAPT 28-40-00. REPLACED #4 LEFT FUEL QTY PROBE AND SDR COEA2026041703781Brake · contaminatedFLIGHT 8737, GEG - YKM R/H BRAKE PEDAL SOFT, LITTLE TO NO BRAKING EFFECTIVENESS DURING TAXI. SHUT DOWN AND THE AIRCRAFT WAS TOWED BACK TO THE RAMP. MAINTENANCE PERFORMED INSPECTIONS AND CLEANED DEICE FLUID FROM THE R/H BRAKE. ENGINE RUN AND TAXI CHECKS GOSDR COEA2026010702708Pressure Switch · faultedFLIGHT 8737, ENROUTE GEG - YKM AIR TURNBACK, DURING CRUISE, THE STAB DE-ICE FAIL ILLUMINATED. DUE TO ICING CONDITIONS, THE PILOT DECLARED AN EMERGENCY AND RETURNED TO GEG WITHOUT INCIDENT. MAINTENANCE REMOVED THE EMPENNAGE PRESSURE SWITCH SV001 AND FOUND RSDR COEA2026010601759Lead · faultedFLIGHT 8658, ENROUTE: SMF - CEC AIR TURNBACK, RECURRING AMBER PROP HEAT L CAS MESSAGE MIDWAY TO CEC DURING ICING CONDITIONS. AIRCRAFT RETURNED TO SMF. NO EMERGENCY WAS DECLARED. LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LT NR 3 PROP LEAD. SDR 2026FA0000059Tach Generator · looseON 12/25/25, WE HAD AN INFLIGHT EMERGENCY DECLARED BY THE FLIGHT CREW FOR #1 ENGINE PROP SPEED ERRATIC. THE CREW REPORTED THE #1 ENGINE PROPELLER SPEED WAS JUMPING AROUND BETWEEN 1400 AND 1900 IN CLIMB SHORTLY AFTER TAKEOFF. THE CREW SAID ALL OTHER ENGINE INDISDR K2AA2026010900001Fuel Filter · bypassingPILOT REPORTED FUEL BYPASS CAS MESSAGE ON LH ENGINE DURING FLIGHT.SDR COEA2025110612738Panel · crackedNUMBER 2 ENGINE INBD PLENUM PANEL SKIN CRACKED AT AFT END OF TOP STIFFENER. STOP DRILLED CRACK AND COVERED WITH SPEED TAPE IAW DQ428170M2. REPLACED THE PLENUM PANEL IAW MM 6-40-50 REV. 5 AND IPC 54-10-25-01 REV. 10.SDR COEA2025110611738Panel · crackedWO 272105 NR 6 MINOR REPAIR/DISCREPANCY: #1 ENGINE OUTBOARD PLENUM PANEL SKIN CRACKED AT AFT END OF TOP STIFFENER. STOP DRILLED CRACK AND COVERED WITH SPEED TAPE IAW DQ428170M2. REPLACED THE PLENUM PANEL IAW MM 6-40-50 REV. 5 AND IPC 54-10-25-01 REV. 10.SDR COEA2025110610738Panel · crackedWO 272105 NR 5 MINOR: NR 1 ENGINE INBD PLENUM PANEL SKIN CRACKED AT AFT END OF TOP STIFFENER. REPLACED THE PLENUM PANEL IAW C408MM 6-40-50 REV.11SDR COEA2025110616759Link · corrodedWO 271980 NR 5 MINOR REPAIR/DISCREPANCY: RT ENGINE AFT DOOR LINK ASSY FRETTED AROUND CHAMBERED AREA. REPLACED RT AFT INERTIAL SEPERATOR DOOR LINK ASSY REF IPC 30-20-05 FIG 1-5.SDR COEA2025110615759Link · corrodedWO 271980 NR 3 MINOR REPAIR/DISCREPANCY: LT ENGINE AFT DOOR LINK ASSY FRETTED AROUND CHAMBERED AREA. CORRECTIVE ACTION: REPLACED L/H AFT INERTIAL SEPERATOR DOOR LINK ASSY. REF IPC 30-20-05 FIG 1-5.SDR COEA2025110614759Link · crackedWO 271980 NR 2 MINOR REPAIR/DISCREPANCY: R/H ENGINE FWD DOOR LINK ASSY IS CRACKED. REPLACED FWD INERTIAL SEPERATOR DOOR LINK ASSY REF C408 IPC 30-20-05 FIG 1-5.SDR FXTA20251029001Cylinder · leakingPILOT FELT STRONG LEFT RUDDER PRESSURE ON TWO CONSECUTIVE TAKE OFFSSDR FXTA20251106001Seal · brokenRH MAIN LANDING SCRAPPER SEAL BROKEN AND HANGING FROM BOTTOM OF STRUT.SDR FXTA2025111000001Transducer · failedON TAKE OFF RIGHT ENGINE LOSS TORQUE INDICATION.SDR COEA2025110613778Mechanism · crackedWO 271981 NR 5 MINOR REPAIR/DISCREPANCY: #1 AND #2 ENGINE SEPERATOR FWD DOOR LINK CRACKED. CORRECTIVE ACTION: REPLACED #1 AND #2 ENGINE INERTIAL SEPERATOR CONTROL MECHANISM ASSYS IAW C408 MM 30-20-16.SDR COEA2025091109757Support · damagedLEFT ENGINE INBOARD AFT TRUSS SUPPORT DAMAGE. MAINTENANCE INSPECTED AND APPLIED SURFACE TREATMENT PER SRM.SDR COEA2025091108757Bracket · gougedDAMAGE FOUND ON THE LEFT ENGINE INBOARD AFT FIREWALL BEHIND ICE VANE ACT REAR BRACKET ASSY. MAINTENANCE INSPECTED AND APPLIED SURFACE TREATMENT PER SRM.SDR COEA2025091107757Rod End · shearedLEFT ENGINE ICE VANE ACTUATOR AFT CLEVIS SHEARED OFF. REPLACED BROKEN ROD END AND RE-INSTALLED ICE VANE ACTUATOR IAW C408 MM 30-20-00.SDR COEA2025082106759Seat · crackedCAPTAIN SEAT BROKEN, FOAM UNDER CUSHION CRACKED. REPLACED WITH NEW CREW SEAT REF. MM 25-71-05.SDR MTNA20250815001Access Panel · crackedCRACK FOUND ON RH ENGINE NACELLE..... PERFORMED TEMP REPAIR PER MAC EO # C408-54-0003 AND CESSNA 408 NACELLE CRACKING MINOR REPAIR LETTER DQ42817M3 DATED OCTOBER 16, 2024SDR COEA2025081904734Support · crackedCAPTAIN SEAT L/H BOTTOM SUPPORT CRACKED. REPLACED WITH NEW SEAT REF. C408 MM 25-10-05.SDR COEA2025081903708Pan · crackedCAPTAIN SEAT SUPPORT PAN CRACKED. MAINTENANCE REPLACED THE CREW SEAT IAW 408 MM 25-10-05.SDR COEA2025080702708Fuel Filter · faultedFLT 8737 GEG-YKM AIR TURNBACK NO EMERGENCY DECLARED. FUEL BYPASS LIGHT TURNED ON DURING CLIMB. MAINTENANCE REPLACED BOTH FUEL HEATER FILTERS. LEAK CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.SDR COEA2025081905738Seat · crackedPILOT SEAT CRACKED. MAINTENANCE REPLACED THE PILOT SEAT.
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