N197SW, cancelled Feb 24, 2006
Service difficulty reports · 64
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 = 'N197SW' AND deregistration_id = 'N197SW-2006-02-24' 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 = 'N197SW' AND deregistration_id = 'N197SW-2006-02-24' 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 SWIA200515231Battery Pack · dischargedEMERGENCY LIGHTS TOWARD FRONT OF CABIN INOP. REPLACED FORWARD ELBP. OPERATIONAL CHECK GOOD.SDR SWIA200514958Battery · dischargedLAV SMOKE DETECTOR BEEPING INTERMITTENTLY. REPLACED BATTERY. OPERATIONAL CHECK GOOD.SDR SWIA200514897Wire · brokenEMERGENCY LIGHTING STRIP BY GALLEY IS LOOSE AND DOES NOT LIGHT UP. REPAIRED BROKEN WIRE UNDER GALLEY AND REPLACED FORWARD SECTION OF LIGHT TRACK. OPERATIONAL CHECK GOOD.SDR SWIA200414291Bulb · burned outEMERGENCY EXIT LIGHT (OVERHEAD) AT ROW 6C INOPERATIVE. RELAMPED BULB, OPERATIONAL CHECK GOOD.SDR SWIA200414064Roller · dirtyMAIN CABIN DOOR IS HARD TO OPEN/CLOSE. CLEANED MAIN CABIN DOOR ROLLERS AND ACTUATORS. RELUBED ROLLERS AND LOCKING MECHANISM. OPERATIONAL CHECK GOOD IAW 52-00-00.SDR SWIA200413516Annunciator · malfunctionedUPON SELECTING FLAPS 15 DEGREES ON TAXI, WITH THE FLAP SELECTOR IN THE 15 DETENT, NO MOVEMENT ON FLAP COMMAND OR ON INDICATOR. REMOVED AND REPLACED FLAP ANNUNCIATOR ASSEMBLY IAW 27-50-05. OPS CHECKED GOOD.SDR SWIA200413142Annunciator · faultyIN CRUISE FLIGHT, FLAP ADV SWS, AND CONTROL FAULT LIGHTS ILLUMINATED. RESET THE SYSTEM PER QRH, 5 MINUTES LATER, FLAP ADV SWS, CONTROL FAULT, ASYMMETRY, AND FLAP DISAGREEMENT ALL ILLUMINATED. ALSO HAD ERRATIC READINGS ON FLAP INDICATOR. REMOVED AND REPLACEDSDR SWIA200413109Fan · failedLEFT PACK EMITTING SMOKE THROUGH VENTS WHILE ON GROUND. REPLACED LEFT PACK GROUND COOLING FAN. OPS CHECKS GOOD.SDR SWIA200413097Computer · out of adjustCOPILOT'S COMPUTER FLAG CAME ON AUTOPILOT, WOULD NOT ENGAGE. REORIENTED NR 2 AHRS COMPUTER. AUTO PILOT OPS CHECKS GOOD.SDR SWIA200412979Cradle · crackedRIGHT OUTBOARD EXHAUST CRADLE OUTBOARD CORNER IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED EXTERNAL DOUBLER IAW EMB SRM 51-10-02.SDR SWIA200412978Rib · crackedCRACKED RIB AT RIVET OUTBOARD OF SMALL FUEL ACCESS PANEL NR 3 OF LEFT WING. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED LEFT NOSE RIB WEB NR 19 IAW EMBRAER REF 1C2004-120/0414 AND SRM 57-20-07 AND CARD RII 28-301.SDR SWIA200412977Rib · crackedRIGHT FORWARD MOST OUTBOARD SMALL FUEL PANEL, RIB INSIDE WING CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED RIGHT MOST OUTBOARD NOSE RIB WEB IAW SRM 120 57-20-07 PG 210 FIG 203.SDR SWIA200412976Attach Bracket · crackedATTACH BRACKET CRACKED AT LEFT NACELLE OUTBOARD OF WHEEL WELL AT 3RD RIVET FROM BOTTOM (INTERIOR OF WALL). DISCOVERED DURING C-CHECK INSPECTION. REPAIRED BRACKET LOCATED AT LEFT NACELLE OUTBOARD OF WHEEL WELL IAW EMB120 SRM 54-10-03 PAGE 202 FIG 201 SHEET 1.SDR SWIA200412975Bracket · crackedINTERIOR BRACKET CRACKED AT LEFT NACELLE OUTBOARD OF WHEEL WELL SUPPORT. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED IAW SRM 54-10-03 FIG 201. P/N 120-41419-001.SDR SWIA200412974Clip · crackedLEFT WING SHEAR CLIP AT STATION YA-5825 CRACKED OUTBOARD OF FUEL PANEL 4 MIDDLE SECTION. DISCOVERED DURING C-CHECK INSPECTION. REPLACED AND SEALED SHEAR CLIP IAW 120 SRM 51-10-02 AND RII CARD 28-301.SDR SWIA200412973Frame · crackedLEFT ENGINE FRAME NR 1 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED LEFT ENGINE FRAME NR 1 IAW EMB120 SRM 51-10-02 PG 3 SEC 3A AND S/B 120-54-0036 AND RII CARD 54-301.SDR SWIA200412972Frame · crackedLEFT MLG, OUTBOARD LOWER NACELLE FRAME CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED LOWER NACELLE FRAME IAW 120 SRM 51-10-02 PG 3 SEC 3A & RII CARD 54-301.SDR SWIA200412971Frame · crackedRIGHT NACELLE (WHEEL WELL) OUTBOARD UPPER FRAME CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED RIGHT NACELLE (WHEEL WELL) OUTBOARD UPPER AFT FRAME IAW EMB120 SRM 54-10-03 PAGE 202 FIG 201 SHEET 1.SDR SWIA200312586Control Unit · malfunctionedAFTER LANDING NAC FLAPS CONTROL FAULTED AND WOULD NOT RESET. REMOVED FLAP COMPUTER AND INSTALLED A SERVICEABLE UNIT. OPS CHECKS GOOD. P/N: 307500-1007, S/N OFF: 169.SDR SWIA200312538Battery Pack · dischargedCENTER EMERGENCY LIGHTS ARE INOP. REPLACED CENTER ELBP WITH SERVICEABLE UNIT. OPS CHECK GOOD.SDR SWIA200312165Fuse · blownFORWARD SECTION OF EMERGENCY LIGHTS IN CABIN ARE INOPERATIVE. REPLACED BLOWN FUSE. OPS CHECK GOOD. P/N: 1AFUSESDR SWIA200312048Control Unit · failedFLAP CONTROL FAULT DURING FLAP BITE TEST AND WILL NOT RESET. INSTALLED FLAP CONTROL UNIT IAW EMB 120 MM 27-50-06. OPS CHECKS GOOD. S/N OFF: 0230.SDR SWIA200312011Control Panel · malfunctionedBOTH AUTPILOTS TURN RIGHT, UNCOMMANDED, DO NOT FOLLOW COMMAND BARS. REPLACED APP-65. OPS CHECK GOOD IAW AMM 22-00-00.SDR SWIA200311773Bracket · crackedINBOARD FLAP FOLLOWER ROLLER BRACKETS CRACKED ON LEFT SIDE. REMOVED AND REPLACED INBOARD FLAP FOLLOWER ROLLER BRACKETS AT BOTH ENDS IAW SRM 51-10-03 AND 51-40-02. PN: 120-22884-001.SDR SWIA200211432Outflow Valve · malfunctionedAUTO PRESSURIZATION UNABLE TO CONTROL PRESSURE. CONTRACT MAINTENANCE PERFORMED MX PROCEDURE FOR DEFERRAL. NEXT FLIGHT RETURNED TO GJT WITH MANUAL PRESSURIZATION INOPERATIVE REMOVED AND REPLACED ELECTRO OUTFLOW VALVE IAW MM 21-30-03. OPS CHECK GOOD.SDR SWIA200211204Boot · failedINBOARD LEFT AND RIGHT STAB AND INBOARD LEFT AND RIGHT WING LEADING EDGE DEICERS FAILED IN FLIGHT ON BOTH TIMERS. RETURNED TO SLC. REMOVED & REPLACED RIGHT WING OUTBOARD DEICE, LEFT OUTBOARD DEICE BOOT & RIGHT HORIZONTAL STAB DEICE BOOT WITH SERVICEABLE UNITSDR SWIA200210791Receptacle · meltedSMOKE SMELL IN CABIN. FOUND A LIGHT RECEPTACLE MELTED. REPLACED LIGHT RECEPTACLE AT SEAT 5A. OPS CHECK GOOD.SDR SWIA200210725Pressure Switch · defectiveIN CLIMBOUT THROUGH FL20, THE LEFT POWER LEVER WOULD NOT RESPOND TO THROTTLE INPUT. SWITCHED THE LEFT EEC TO MANUAL AND THE ENGINE REQUIRED POWER. SELECTED MANUAL ON THE RIGHT ENGINE EEC AND RETURNED TO DEN. REMOVED AND REPLACED LEFT 14,000 FT PRESSURE SWITSDR SWIA200110399Boot · leakingVERTICAL FIN AND RIGHT OUTBOARD STAB DEICE BOOTS FAIL ON BOTH TIMERS. REMOVED & REPLACED RIGHT HORIZONTAL DEICE BOOT IAW EMB 30-10-00 & FAST BOOT INSTRUCTION. OPS CHECK GOOD.SDR SWIA200110378Boot · leakingLEADING EDGE DEICE BOOTS FAILED (VERTICAL FIN AND RIGHT OB STAB) BOTH TIMERS. INSPECTED HORIZONTAL AND VERTICAL STAB. DEICE BOOTS. FOUND RIGHT OUTBOARD BOOT TO HAVE HOLE AND LEAKY PATCH. REPAIRED RIGHT OUTBOARD BOOT IAW 30-00-00. OPS CHECK GOOD.SDR SWIA200110377Control Cable · faultyRIGHT POWER LEVER WOULD NOT RETARD TO FLIGHT IDLE IN CRUISE FL22.0 OAT-15. PERFORMED PRECAUTIONARY ENGINE SHUTDOWN CHECK. INSPECTED CABLE FROM POWER LEVER AND ENGINE QUADRANT. CYCLED POWER LEVER SEVERAL TIMES. INSPECTED CABLE FROM ENGINE QUADRANT TO HMU. CSDR SWIA20019998Warning Light · illuminatedON TAKEOFF, THE FORWARD DOOR LIGHT ILLUMINATED WITH ASSOCIATED AURAL WARNINGS, THE TAKEOFF WAS ABORTED. THE DOOR WAS CHECKED CLOSED AND THE FORWARD DOOR WARNING INDICATION WAS DEFERRED PER MX CONTROL 52-70-1C, MC 021.INSPECTED WIRING & MICRO SWITCHES FOR SECUSDR SWIA972596Comparator · faultyUPON ADDING TAKEOFF POWER CAPT'S EADI AND EHSI FAILED AND CAME BACK ON LINE. AFTER 100 PERCENT TORQUE AND DOUBLE CHECK OF ALL INSTRUMENTS, TAKEOFF ROLL WAS COMMENCED AND ABORTED AFTER CAPT EHSI CHANGED HDG FROM 250 TO 270 DEGREES. INSTALLED AND REORIENTED SESDR SWIA972475Flap Track · dirtyFLAPS WOULD NOT EXTEND TO 45 DEGREES INBOUND TO CARLSBAD. COMPLIED WITH QRH PROCEDURE FOR FLAP DISAGREEMENT. RETURNED TO LAX. EXAMINED FLAP TRACKS AND ROLLERS FOR OUTBOARD FLAPS AND CLEANED AS NEEDED. OPERATED FLAP SYSTEMS 12 TIMES IAW 27-50-00 AND OPS CHESDR SWIA972476Target · out of adjCARGO DOOR LIGHT ILLUMINATED ON TAKEOFF ROLL. ABORTED TAKEOFF. LIGHT GOES ON AND OFF INTERMITTENTLY. ADJUSTED STRIKER PLATE ON CARGO LIGHT SWITCH. CYCLED DOOR NUMEROUS TIMES. OPS CHECK GOOD.SDR SWIA972359Actuator · seizedRUDDER TRIM FROZE IN ZERO POSITION IN FLIGHT. FLIGHT CONDITIONS VMC AT 7000 FEET. AFTER 10 MINUTES RUDDER TRIM WORKED FINE. INSPECTED RUDDER TRIMMING SYSTEM IAW EMB120 MM 27-23-00. WIPED MOISTURE FROM LINEAR ACTUATOR. RUDDER TRIM SYSTEM OPS CHECK GOOD.SDR SWIA972178Signal Cond Unit · failedRIGHT TORQUE GAUGE WOULD NOT DROP BELOW 76 PERCENT TORQUE. ALL OTHER GAUGES WERE NORMAL. AFTER ABOUT 5 MINUTES, WHEN WE BEGAN DESCENT, LEFT PROP WENT TO FEATHER. TURNED OFF AUTOFEATHER SYSTEM AND EVERYTHING RETURNED TO NORMAL. DIDN'T SEE LEFT TORQUE EXCEEDSDR SWIA972117Actuator · malfunctionedMOMENTARY FLAP LIGHT ON MAP ASSOCIATED WITH FLAP RETRACTION IN AIR/GROUND. REPLACED INLINE HYDRAULIC FILTER FOR INBOARD FLAPS AS REQUIRED. OPS CHECK FAILED. REPLACED LEFT AND RIGHT INBOARD FLAP ACTUATORS IAW MM 27-50-07, EMB 120 MM RII 27-307. OPERATIONS CSDR SWIA972128Control Unit · malfunctionedINBOARD DISAGREEMENT ON FLAP RETRACTION. REPLACED FCU. OPERATED FLAPS SEVERAL TIMES, OPS CHECKS GOOD. P/N 307500-10175-1, S/N ON: 0160, S/N OFF: 0276.SDR SWIA971929Indicator · failedANALOG AND DIGITAL READING ON RIGHT NP GAUGE FAILED. RETURNED TO FAT. REMOVED AND REPLACED RIGHT NP GAUGE. OPS CHECKS GOOD. P/N ON: SEL-OC29DH, S/N: 511, S/N OFF: 123.SDR SWIA971634Flap · malfunctionedFLAP ASYMMETRY LEFT OUTBOARD AFTER TAKEOFF. RETURNED TO PIH. RESET FLAP SYSTEM. CYCLED UP AND DOWN 5 FAULT FREE CYCLES. CHECKED FLAP TRACKS AND ROLLERS, CHECKED GOOD. COULD NOT DUPLICATE DISCREPANCY.SDR SWIA971579Tq Sig Cond · malfunctionedEXPERIENCED PLUS AND MINUS 10 TO 12 PERCENT TORQUE FLUCTUATIONS ON RIGHT ENGINE AT CLIMB POWER SETTINGS. FLUCTUATIONS CAUSED REDUCED POWER SETTINGS. RETURNED TO GJT. FLUCTUATIONS OCCURRED BETWEEN 8,500 FT AND 10,000 FT. REMOVED AND REPLACED THE TORQUE SIGNSDR SWIA971474Actuator · malfunctionedON DEPARTURE OUT OF SLC, RIGHT RUDDER PEDAL STUCK AT APPROX ONE-HALF TRAVEL. RUDDER WOULD CENTER BUT WOULD NOT GO PAST ONE-HALF TRAVEL. FOLLOWED QRH AND UPON SELECTION OF BLUE RUDDER SYSTEM TO OFF, RUDDER TRAVEL WAS NORMAL. RETURNED TO SLC. REMOVED AND REPSDR SWIA971455Ehsi · malfunctionedCAPTAIN'S EHSI WILL NOT INITIALIZE THEN CORRECTED ITS SELF ON THE GROUND, BUT TWICE DISCONNECTED AUTOPILOT IN FLIGHT. WHEN NR 1 GYRO COMPUTER FLAG APPEARED NR 1 HSI LOST HEADING. RETURNED TO SLC. RERACKED NR 1 AHC85 AND REINITIALIZED REORIENTED. PERFORMED SDR SWIA971400Regulator · failedLOW LEVEL AND LOW PRESSURE LIGHT CAME ON GREEN SYSTEM. DECLARED AN EMERGENCY AND LANDED IN SLC WITHOUT INCIDENT. REPLACED HYDRAULIC HEAD PRESSURE REGULATOR AND DRAINED WATER FROM SYSTEM, OPS CHECKS GOOD.SDR SWIA971370Valve · failedLEFT ENGINE INLET DEICER INOP. ANNUNCIATION IN FLIGHT AND RETURNED TO SLC. REMOVED AND REPLACED LEFT ENGINE FLOW CONTROL VALVE IAW EMB 120 MM 30-10-04. OP, CHECK GOOD.SDR SWIA971379Retract Mech · malfunctionedAFTER TAKEOFF FLAPS WOULD NOT RETRACT. CONTROL FAULT ON OVERHEAD ILLUMINATED. FLAP AND ADVANCED STALL WARNING LIGHT ON MAP. FOLLOWED QRH PROCEDURE. RETURNED TO FIELD COULDN'T DUPLICATE PROBLEM. CANNON PLUGS VISUALLY CHECKED GOOD AT OUTBOARD AND INBOARD ACSDR SWIA971219Indicator · malfunctionedLEFT ENGINE NL ON TAKEOFF SHOWED 110 PERCENT TO 115 PERCENT. RETURNED TO SLC. REPLACED LEFT HAND NL/NH INDICATOR. RAN ENGINE, OPS CHECKS GOOD.SDR SWIA971078Actuator · failedSELECTING FLAPS DOWN, NACELLES WOULD NOT EXTEND CAUSING DISAGREEMENT. WHEN FLAPS ARE RETRACTED THE INBOARDS LAG. CYCLED FLAPS SEVERAL TIMES ON GROUND AND UNABLE TO DUPLICATE. OHMED WIRE FROM CONTROL BOX TO ANNUNCIATOR, CHECKS GOOD. OHMED WIRING FROM CONTROSDR SWIA971077Switch · malfunctionedAT 400 FT CALLED FOR FLAPS UP AND GOT FLAP ASYMMETRY INDICATION. RETURNED TO LAX. INSTALLED SERVICEABLE FLAP HANDLE ASSEMBLY. CYCLED FLAPS EXTENSIVELY WITH NO ASYMMETRY NOTED. OPS CHECKS GOOD.
Back to N197SW, cancelled Feb 24, 2006