N407SW
Service difficulty reports · 156
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 = 'N407SW' 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 = 'N407SW' 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 SWIA200413479Control Lever · malfunctionedFLIGHT SPOILER FAULT (AMBER MESS) CAME ON AT SHORT FINAL. REMOVED AND REPLACED FLIGHT SPOILER CONTROL LEVER IAW 27-61-01. OPERATIONAL CHECK GOOD.SDR SWIA200413095Wire · damagedFIRST OFFICER'S STAB TRIM SWITCH WILL NOT TRIM NOSE UP. TAXI BACK TO GATE. REPAIRED WIRE IAW WM 20-00-00. OPS CHECK GOOD IAW MM 27-40-00.SDR SWIA200413072Position Sensor · malfunctionedRECEIVED FLAPS FAIL, DID QRH. LANDED SLC 0 DEGREES FLAPS. REMOVED AND REPLACED LEFT BPSU IAW AMM 27-51-10 AND RIGGED FLAPS. OPS CHECKS GOOD.SDR SWIA200412825Computer · malfunctionedAUTOPILOT DISCONNECTED INFLIGHT, HAD FD2 INOPERATIVE STATUS MESSAGE. REMOVED AND REPLACED FCC 2 WITH A SERVICEALBLE UNIT IAW MM 22-12-14. OPS CHECK.SDR SWIA200412824Warning Light · illuminatedON APPROACH, FLAP FAIL CAUTION MESSAGE AFTER SELECT FLAPS 30. PERFORMED QRH PROCEDURE AND LANDED OK. PERFORMED OPS CHECK OF FLAPS SYTSEM (FECU) IAW 27-51-10. ALL SYSTEM CHECKS GOOD, NO FAULTS, OPERATED FLAP IN ALL POSITIONS.SDR SWIA200312600Lever · malfunctionedAFTER LANDING, WHEN SELECTING FLAPS FROM 45 DEGREES TO 30 DEGREES, FLAPS STAYED AT 30 DEGREES AND ECI SHOWED A FLAPS FAIL CAUTION MESSAGE. REMOVED AND REPLACED FLAP CONTROL LEVER IAW MM 27-51-01. OPS CHECK GOOD.SDR SWIA200312354Pump · malfunctionedNR 2 HYD SYSTEM LOST QUANTITY WITH PRESSURE AT 33,000 FT. NR 2 ENGINE DRIVEN PUMP RAN DRY FOR 33 MINS. REMOVED AND REPLACED NR 2 ENGINE HYD PUMP AND PRESSURE STEEL LINE AND PRESSURE RETURN LINE AND SERVICED NR 2 HYD SYSTEM. OPS CHECKS AND LEAK CHECKS GOOD ISDR SWIA200312225Angle · crackedREINFORCEMENT ANGLE AND FRAME ON RIGHT SIDE OF FS 640.00 BETWEEN STR 9 AND STR 12 IS CRACKED NEAR TOP OF BOX BEAM. DISCOVERED DURING A CHECK INSPECTION. REPLACED RIGHT QUARTER FRAME AT FS 640 WITH SERVICEABLE UNIT IAW SRM 51-42-06 AND 51-42-20.SDR SWIA200312224Angle · crackedREINFORCEMENT ANGLE AND FRAME ON LEFT SIDE OF FS 640.00 BETWEEN STR 9 AND STR 12 IS CRACKED NEAR TOP OF BOX BEAM. DISCOVERED DURING A CHECK INSPECTION. REPLACED LEFT QUARTER FRAME AT FS 640 WITH SERVICEABLE UNIT IAW SRM 51-42-06 AND 51-42-20.SDR SWIA200312135Inverter · failedONE SECTION OF THE FLOOR EMERGENCY LIGHTS IS INOP. REMOVED AND REPLACED EMERGENCY LIGHTING INVERTER NR 3. OPS CHECK GOOD.SDR SWIA200312105Door Frame · corrodedPAX DOOR CABLE MOUNT ON DOOR FRAME HAS CORROSION. DISCOVERED DURING AVIONICS MODIFICATION. REMOVED CORRODED CABLE MOUNT AND INSTALLED NEW IAW CRJ SRM 51-40-11, 51-42-20. P/N OFF: 444-2439-1.SDR SWIA200312047Sign · brokenEMERGENCY EXIT SIGN (FLOODLIGHT) AT SERVICE DOOR BROKEN. REPLACED EMERGENCY EXIT SIGN BY SERVICE DOOR AND REPLACED THE ELECTRICAL CONNECTOR. DISCOVERED DURING MAINTENANCE INSPECTION.SDR SWIA200312046Pin · wornLEFT AND RIGHT OVERWING EXIT HINGE SUPPORT PINS SHOWING SIGNS OF WEAR AND SURFACE CORROSION. REPLACED PINS IAW STANDARD MAINTENANCE PRACTICES. DISCOVERED DURING MAINTENANCE INSPECTION.SDR SWIA200311988Actuator · failedSTAB CHI INOP ON CLIMB OUT. AGAIN ON DESCENT. REMOVED AND REPLACED MCU AND HSTA . TESTS GOOD.SDR SWIA200211721Fitting · corrodedANTI-ROTATION FITTING HAS CORROSION. FOUND DURING C-CHECK INSPECTION. ANTI-ROTATION FITTING REPLACED IAW SB 601R-55-007. P/N: 600-21073-7.SDR SWIA200211720Frame · crackedFS 718 RHS FRAME CRACKED BETWEEN STR 10-12. FOUND DURING C CHECK INSPECTION. DAMAGED AREA REPAIRED IAW CRJ REO 601R-53-61-193 REV ''A'' . HFEC INSPECTION COMPLIED WITH ON FRAME CUTOUT REPAIR AND AREA AS REQUESTED IAW RJ NDTM 51-20-06. NO CRACKS FOUND.SDR SWIA200211719Rib · crackedLEFT PYLON RIB AT FS 605.00 FOUND CRACKED. FOUND DURING C-CHECK INSPECTION. PYLON RIB INSTALLED AT FS 605.00 IAW CRJ SRM 51-42-20, 51-40-11 & 51-42-06.SDR SWIA200211718Bolt · corrodedMOUNTING BOLTS ON BOTH LT AND RT WINDSCREENS ARE CORRODED. FOUND DURING C-CHECK INSPECTION. REPLACED BOLTS IAW CRJ AMM 20-21-00.SDR SWIA200211717Floorbeam · crackedFS 280 RBL 9.0 FLOORBEAM OUTBOARD, INBOARD AND AFT ANGLES FOUND CRACKED. FOUND DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-13, 51-42-20, & 51-23-00.SDR SWIA200211716Floor Panel · crackedELECTRICAL BAY FLOOR FS 193.0 LEFT AND RIGHT SIDES CRACKED. FOUND DURING C-CHECK INSPECTION. HFEC INSPECTION COMPLIED WITH ON CUTOUT EDGE AND AREA AS REQUESTED IAW RJ NDTM 51-20-06. NO CRACKS FOUND. DAMAGED AREA REPAIRED IAW CRJ REO 601R-53-11-081 REV 'NC'SDR SWIA200211673Computer · malfunctionedBOTH FUEL QUANTITY AND TOTAL FUEL FAILED AFTER TAKEOFF. RETURNED TO SLC. FUEL CHANNEL 1 FAIL STATUS MESSAGE. LEFT QUANTITY CAME BACK ON AFTER 2 MINUTES. REMOVED AND REPLACED FUEL QUANTITY COMPUTER PER MM 28-41-16. OPS CHECK GOOD. P/N: 736643-10 S/N OFFSDR SWIA200211196Selector Valve · malfunctionedNOSE GEAR WOULD NOT EXTEND NORMALLY ON APPROACH OKC. DID QRH PROCEDURE AND A MANUAL EMER GEAR EXT, ALL NORMAL. LOST NWS ON TAXI INTO GATE. COULD NOT RESET. AS ON FIRST EXT AT 180 KIAS, TRIED TWO MORE NORMAL EXTENSIONS (NOTE NW STEERING HAD BEEN FAIRLY SENSSDR SWIA200211175Sensor · malfunctionedLANDING GEAR DISAGREE MESSAGE APPEARED WHEN LANDING GEAR WAS SELECTED DOWN. GEAR CAME DOWN AFTER MANUAL GEAR RELEASE WAS USED. AFTER LANDING, NOSE WHEEL STEERING WAS INOP. ADJUSTED NOSE LANDING GEAR PROX SENSORS UPLOCK, BOTH NR 1 & 2 DOWNLOCK, BOTH GEAR DOOSDR SWIA200211138Display · failedCAPTAIN'S MFD FAILED INFLIGHT. RETURNED TO SLC. INSTALLED SERVICEABLE MFD SCREEN AT CAPTAIN'S POSITION. OPS CHECKS GOOD.SDR SWIA200210963Computer · malfunctionedYAW DAMPER NR 2 FAILED DUE TO NR 2 AHRS FAILURE. INSTALLED SERVICEABLE AHRS COMPUTER AT NR 2 POSITION. AHRS OPS CHECK GOOD. YAW DAMPER NR 2 OPS CHECK GOOD. RETURNED TO CAT II SERVICE.SDR SWIA200210932Light · inoperativePASSENGER DOOR BOARDING LIGHT IS INOP. REMOVED AND REPLACED TOP PASSENGER DOOR STEP LIGHT. OPS CHECK GOOD.SDR SWIA200210790Connector · dirtyEMERGENCY EXIT (RED) LIGHTS, EXIT ROW 8 ON THE FLOOR, ARE INOP. CLEANED CONNECTIONS TO FLOOR EMERGENCY LIGHTING, OPS CHECKS GOOD.SDR SWIA200210535Relay · failedYD 2 WILL NOT ENGAGE. REPLACED 2K2CA RELAY (ARM). OPS CHECK GOOD YAW DAMPER SYSTEM. P/N: MS27400-31X.SDR SWIA200110457Probe · faultyACCELERATING THROUGH 250 KIAS AT 10,000 FT, ALTIMETERS FLAGGED AND HAD 150 FT DIFFERENCE. AIRSPEED INDICATORS HAD A 5 KNOT SPLIT. AFTER REDUCING AIRSPEED BACK TO AROUND 250 KIAS ALTIMETERS CAME BACK WITHIN TOLERANCE. REMOVED AND REPLACED NR 1 PITOT/STATIC PSDR SWIA200110459AdcEFIS COMP MON MESSAGE ''ALT''. RETURNED TO DFW.PURGED PITOT STATIC SYSTEM IAW MM 34-11-00-100-807. REMOVED AND REPLACED #1 AND #2 ADC'S IAW MM 34-13-01. PITOT STATIC CHECK C/W IAW MM 34-13-00-730-001. LEAK CHECK IAW MM 34-11-00-790-801.#1 S/N ON: 1104 S/SDR SWIA200110301Display · failedEICAS PRIMARY DISPLAY FAILED ON TAKEOFF ROLL ACCOMPANIED WITH AN EICAS COMP INOP MESSAGE. ABORTED TAKEOFF. REMOVED NR 1 PRIMARY EFD AND REPLACED IT WITH A SERVICEABLE ONE IAW CL600 MM 31-41-00. OPS CHECK GOOD. S/N ON: DN4T, S/N OFF: 964.SDR SWIA200110254Ground Wire · looseAPU FAULT LIGHT COMES ON WITH APU BATT OFF LIGHT INTERMITTENT, VARIABLE VOLTS ON THE APU BATTERY DISPLAY AND THE APU CHARGER INDICATION CYCLING ON AND OFF ERRATICALLY. FOUND APU GENERATOR GROUND WIRE LOOSE AT ATTACH POINT. APU CHARGER AND APU OPS CHECK GOOD SDR SWIA200110058Light · inoperativeTHREE STRIPS OF EMERGENCY FLOOR LIGHTING INOP.EMERGENCY TRACK LIGHTING COVER REMOVED. LOOSE CONNECTION PUT TOGETHER AND EMERGENCY TRACK COVER REINSTALLED. EMERGENCY TRACK LIGHTING TESTED SERVICEABLE.SDR 20010411CW010Bearing · lack of lubeTHRUST BEARING FAILURE DUE TO LACK OF LUBRICATION AND POSSIBLE PRELOAD CONDITION.SDR SWIA972383Actuator · failedFLAP FAIL MESSAGE ON APPROACH TO SLC. FLAPS STUCK AT 22 DEGREES. REPLACED LEFT FLAPS NUMBER THREE ACTUATOR IAW 27-53-05. OPS CHECK GOOD. (P/N ON 853P100-17) (S/N ON 0964) (S/N OFF 1272).SDR SWIA972326Controller · failedAIRCRAFT FAILED TO PRESSURIZED. QRH NO EFFECT. RETURNED TO SLC. PRESSURIZED AIRCRAFT ON GROUND USING BOTH AUTO CONTROLLER NUMBER ONE AND NUMBER TWO. ALSO PRESSURIZED AIRCRAFT IN MANUAL MODE. SYSTEM OPERATES NORMAL IAW CRJ MM 21-31-00.SDR SWIA972077Pcu · malfunctionedRIGHT SPOILERON STATUS MESSAGE ON MOST OF THE TIME. REMOVED AND REPLACED INBOARD SPOILERON PCU ON RIGHT SPILOERON IAW MM 27-62-01 WITH SERVICEABLE UNIT. OPS CHECKS AND LEAK CHECKS GOOD AT THIS TIME. P/N ON: 27000-7, S/N: MAL-0537, S/N OFF: MAL-0324.SDR SWIA971972Controller · failedSTALL FAIL CAUTION MESSAGE JUST AFTER TAKEOFF. RETURNED TO SLC. REMOVED AND REPLACED STALL PROTECTION UNIT IAW MM 27-35-01. OPS CHECKS GOOD. (P/N 3995100208) (S/N 206) ON, (S/N 147) OFF.SDR SWIA971942Warning System · malfunctionedSTALL FAIL MESSAGE CAME ON AFTER TAKEOFF AND FLAPS SET TO 8. RETURNED TO SLC. FOUND NO FAILURE IN STALL WARNING SYSTEM IN MDC. OPERATED AOA VANES WHILE IN FCC DIAGNOSTICS, NO FAULTS. OPERATED FLAPS IN FCC DIAGNOSTICS, NO FAULTS. RESET STALL WARNING COMPUTSDR SWIA971915Clamp · looseRIGHT 14TH DUCT MESSAGE AFTER TAKEOFF. RETURNED TO SLC. FOUND LOOSE CLAMP ON 14TH STAGE BLEED VALVE. TIGHTENED CLAMPS AND RAN RIGHT ENGINE. OPS CHECK 14TH BLEED SYSTEM, NO LEAKS AND NO MESSAGES.SDR SWIA971877Fire Loop · malfunctionedRIGHT 14TH STAGE DUCT MESSAGE CAME ON INFLIGHT. FOLLOWED QRH PROCEDURES AND INFLIGHT ENGINE SHUT DOWN PERFORMED. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED RIGHT 14TH DUCT FIRE LOOP IAW MM 362104, OPS CHECKS GOOD. (P/N 356024)SDR SWIA971841Pcu · malfunctionedAFTER FLAPS WERE RETRACTED FOLLOWING TAKEOFF, AC ROLLED RIGHT, AILERON TRIM HAD TO BE DEFLECTED 50 PERCENT OF ITS TRAVEL TO MAKE AC FLY STRAIGHT. NOTE: FUEL WAS BALANCED. REMOVED AND REPLACED THE RIGHT AILERON TO PCU LINKS IAW MM 271415. MX REQUEST AN INFLSDR SWIA971582Bpsu · failedCLIMBING THROUGH 22,000 FEET, FLAPS FAIL MESSAGE ON EICAS. CYCLED CIRCUIT BREAKERS PER MAINTENANCE CONTROL WITH NO CHANGE. RETURNED TO SLC AND LANDED O FLAPS, (FLAPS FAILED AT 0 DID NOT OPERATE FLAP SELECTOR). REMOVED AND REPLACED LEFT BRAKE POSITION SENSORSDR SWIA971516Sensing Element · looseON CLIMB-OUT RIGHT 14TH DUCT MSG ILLUMINATED. FOLLOWED QUICK REFERENCE HANDBOOK AND LIGHT EXTINGUISHED WHEN RIGHT 14TH BLEED VALVE WAS CLOSED. RETURNED TO SLC. TORQUED RIGHT 14TH STAGE DUCT SENSING ELEMENT IAW MM 36-21-00. OPS CHECKS GOOD AT THIS TIME.SDR SWIA971365Sensor · out of adjustGEAR DISAGREE AND NOSE DOOR DISAGREE RED LIGHTS CAME ON AFTER GEAR HANDLE IS SELECTED UP. GEAR WILL NOT GO UP TO LOCKED POSITION. RETURNED TO SLC. ADJUSTED S23 SENSOR ON NOSE GEAR. GEAR EXTENDS AND RETRACTS NORMALLY, OPS CHECKS GOOD.SDR SWIA971339Bpsu · failedFLAPS FAIL MESSAGE AT FL330. RETURNED TO SLC, MADE A NO FLAP LANDING. COMPLIED WITH AD 98-20-01. REMOVED AND REPLACED LEFT BPSU IAW MM 27-51-10.SDR SWIA971315Indication · malfunctionedFLAP FAIL MESSAGE COMES ON IN CRUISE WHILE LEVEL AT 35,000. FLAPS REMAINED AT 0, NO CONTROL PROBLEMS. RETURNED TO SLC. RESET CB1-F4 AND CB2-F4, IAW A/D 98-20-01 PAR B. FLAP SYSTEM RESET TO NORMAL AND NO EVIDENCE OF TWISTING, SKEWING OR ABNORMAL DEFORMATIONSDR SWIA971254Seal · failedDURING CRUISE FLIGHT, LT ENGINE OIL PRESS MSG ILLUMINATED ON EICAS. ALSO, LT ENGINE OIL PRESS WAS FLUCTUATING BETWEEN 20 AND 40 PERCENT. PERFORMED ALL ITEMS ON ALL PERTINENT CHECK LIST AND SHUT DOWN ENGINE. PERFORMED SINGLE ENGINE LANDING. FOUND LT ENGINE SDR SWIA971164Smoke Detector · malfunctionedSMOKE CARGO WARNING CAME ON INFLIGHT. PERFORMED EMERGENCY PROCEDURE AND RETURNED TO SLC. BOTH FIRE BOTTLES WERE FIRED. REPLACED FAULTY SMOKE DETECTOR AND REPLACED CARGO BAY FIRE BOTTLE WITH SERVICEABLE UNIT .SDR SWIA971157Structure · lightning strikeDURING DEPARTURE CLIMB, INCURRED A LIGHTNING STRIKE. RETURNED TO AIRPORT. COMPLIED WITH LIGHTING INSPECTION AT MAINTENANCE BASE.
Back to N407SW