N213SW, cancelled Nov 14, 2007

Service difficulty reports · 63

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 = 'N213SW' AND deregistration_id = 'N213SW-2007-11-14'
  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 SWIA200718727Window Post · crackedFOUND AT C-CHECK, LEFT WINDSHIELD SIDE ATTACHMENT POST APPEARS TO BE CRACKED. REPLACED LOWER WINDSHIELD STRUCTURE IAW SRM 120 51-10-02 PG 3 SEC 3A. Aug 2, 2007 · N213SW · Emb EMB120ER · Fuselage Main, StructureSDR SWIA200718725Stringer · corrodedFOUND AT C-CHECK, STRINGER CORRODED NEAR PAX DOOR AFT ACTUATOR ATTACH POINT. REPAIRED STRINGER SECTION AT PAX DOOR AREA IAW SRM 120 53-10-03 PG 201. Aug 2, 2007 · N213SW · Emb EMB120ER · Fuselage Main, Longeron/StringerSDR SWIA200718724Floorbeam · corrodedFOUND AT C-CHECK, CORROSION AT PAX DOOR AREA ON FLOORBEAM. REMOVED AND REPLACED OMEGA BEAM AND BUTTSTRAP IAW SRM 51-10-02. Aug 2, 2007 · N213SW · Emb EMB120ER · Fuselage Main, Floor BeamSDR SWIA200718714Seat Track · corrodedFOUND C-CHECK, LEFT SIDEWALL SEAT TRACK HAS CORROSION ON FORWARD SECTION. REPLACED THE LEFT FORWARD SIDEWALL SEAT TRACK SECTION IAW EMB120 AMM 53-01-05.Aug 2, 2007 · N213SW · Emb EMB120ER · Fuselage, Seat/Cargo Attach FittingsSDR SWIA200718713Control Cable · corrodedFOUND AT C-CHECK, LEFT ELEVATOR INBOARD MIDDLE CABLE IS CORRODED. REPLACED THE LEFT INBOARD CABLE IAW MM 27-00-01.Aug 2, 2007 · N213SW · Emb EMB120ER · Elevator Control SystemSDR SWIA200717867Relay · noisyFOUND NOISE FROM RELAY IN RIGHT SIDE ELEC BAY, LAV SMOKE ALARM WENT OFF ALONG WITH OVERHEATED SMELL IN CABIN. REPLACED RELAY K0194, NR 2 SHOCK RELAY. OPERATIONAL CHECKS GOOD.Mar 1, 2007 · N213SW · Emb EMB120ER · AC Power Distribution SystemSDR SWIA200717826Control Module · malfunctionedAT ABOUT 2000' PUT GEAR DOWN, ALL RED IN ADDITION TO A RATTLING OUTSIDE AIRCRAFT. RETRACTED GEAR AND THEN EXTENDED AGAIN. REPLACED LANDING GEAR RELAY BOX IAW 32-31-02 AND MLG CONTROL MODULE ASSY IAW 32-31-03. OPERATIONAL CHECKS GOOD, P/N 1 - (RELAY BOX) - 1Feb 17, 2007 · N213SW · Emb EMB120ER · Landing Gear Retraction/Extension SystemSDR SWIA200717792Battery Pack · dischargedFOUND EXIT ROW LIGHTS INOP. REPLACED CENTER BATTERY PACK IAW EMB MM 33-50-02. OPERATIONAL CHECKS GOOD.Feb 4, 2007 · N213SW · Emb EMB120ER · Emergency LightingSDR SWIA200616294Fan · smokeON THE GROUND WTIH APU RUNNING, ENGINES OFF, RECEIVE SMELL OF SMOKE FROM THE LEFT PACK. REPLACE LEFT PACK GROUND COOLING FAN IAW EMB 120 MM 21-51-03.Feb 16, 2006 · N213SW · Emb EMB120ER · Air Distribution FanSDR SWIA200616134Floor Support · corrodedTHE BUTT STRAP ON THE CENTER OMEGA BEAM JUST AFT OF THE COCKPIT IS CORRODED. REPLACED BUTT STRAP ON THE CENTER OMEGA BEAM JUST AFT OF COCKPIT IAW 51-42-06, 51-42-13, 51-21-11 SRM.Jan 12, 2006 · N213SW · Emb EMB120ER · Fuselage Miscellaneous StructureSDR SWIA200616133Floor Support · corrodedTHE FRAME CAP BETWEEN THE CENTER AND LEFT OMEGA BEAMS, FRAME 16 IS CORRODED IB FWD OF THE GALLEY. REPLACED FRAME CAP BETWEEN THE CENTER OF LEFT OMEGA BEAMS FRAME IAW 51-42-06, 51-42-13, AND 51-21-11 SRM.Jan 12, 2006 · N213SW · Emb EMB120ER · Fuselage Miscellaneous StructureSDR SWIA200515757Smoke Detector · activatedLAV SMOKE DETECTOR GOES OFF. REPLACED LAV SMOKE DETECTOR. OPERATIONAL CHECK GOOD.Oct 28, 2005 · N213SW · Emb EMB120ER · Smoke DetectionSDR SWIA200514548Transducer · inoperativeWHEN SIDE SLIP HEATER SWITCH IS TURNED ON, RECEIVED AN INOP LIGHT WITH A DE-ICE LIGHT ON THE MAP. REPLACED TRANSDUCER ASSY PER MM 27-00-00, OPERATIONAL CHECK GOOD.Feb 15, 2005 · N213SW · Emb EMB120ER · Stall Warning SystemSDR SWIA200414269Strut · separatedMAIN CABIN DOOR WOULD NOT OPEN. REATTACHED F/A JUMP SEAT STRUT. DOOR OPERATES NORMAL. OPERATIONAL CHECK GOOD.Dec 8, 2004 · N213SW · Emb EMB120ER · Passenger/Crew DoorsSDR SWIA200414152Seat · out of positionFORWARD DOOR WILL NOT OPEN. FOUND FORWARD DOOR HANDLE HITTING F/A JUMPSEAT, REPOSITIONED F/A SEAT. OPERATIONAL CHECK GOOD.Nov 24, 2004 · N213SW · Emb EMB120ER · Flight Compartment EquipmentSDR SWIA200413713Bolt · out of adjustFORWARD ENTRY DOOR WILL NOT OPEN. ADJUSTED FORWARD DOOR FORWARD ECCENTRIC BOLT IAW MM 52-11-00 PAGE 504. OPERATIONAL CHECK GOOD.Aug 14, 2004 · N213SW · Emb EMB120ER · Passenger/Crew DoorsSDR SWIA200413538Switch · malfunctionedWHEN AUTOPILOT IS TRANSFERRED TO FIRST OFFICER'S SIDE, TRIM FAIL ON MAP AND AUTOPILOT CONTROL PANEL. REPLACED FIRST OFFICER'S TRIM SWITCH IAW MM 22-10-10. OPERATIONAL CHECK GOOD.Jun 30, 2004 · N213SW · Emb EMB120ER · Elevator Tab Control SystemSDR SWIA200413476Computer · malfunctionedAUTOPILOT ON CAPTAIN'S SIDE INFLIGHT WILL GET THE AUTOPILOT WARNING WITH NO DISCONNECT OF THE AUTO PILOT AP LIGHT ON FCP. REMOVED AND REPLACED CAPTAIN'S AUTO PILOT COMPUTER IAW MM 22-10-02 AND AUTO PILOT PANEL IAW MM 22-10-04. OPERATIONAL CHECK GOOD IAW MM 2Jun 16, 2004 · N213SW · Emb EMB120ER · Autopilot SystemSDR SWIA200413256Servo · malfunctionedFEEL A BINDING WHEN MOVING AILERONS. REMOVED AND REPLACED AILERON SERVO WITH SERVICEABLE UNIT IAW EMB 120 MM CHAPTER 22-10-05. OPS CHECK GOOD.Apr 24, 2004 · N213SW · Emb EMB120ER · Autopilot Main ServoSDR SWIA200413070Window Post · crackedANGLE BRACKET UNDER PILOT'S WINDOWSILL IS CRACKED (FRAME 10). (DISCOVERED DURING C-CHECK INSPECTION)REMOVED AND REPLACED ANGLE BRACKET UNDER PILOT'S WINDOW SILL IAW SRM 51-10-02, 51-40-00. SEE RII 53-301.Mar 24, 2004 · N213SW · Emb EMB120ER · Fuselage Main, StructureSDR SWIA200413116Shear Tie · crackedCRACK FOUND ON SHEAR CLIP ON RIGHT SIDE OF CARGO PIT WALL AT FLOOR LEVEL 2ND RIB FORWARD OF AFT BULKHEAD. DISCOVERED DURING C-CHECK INSPECTION. REPLACED SHEAR TIE AT FRAME 46 FLOORBOARD LEVEL RIGHT SIDE PER EMB120 SRM 51-40-02. P/N: 120-04984-002.Mar 2, 2004 · N213SW · Emb EMB120ER · Fuselage Main, StructureSDR SWIA200413115Support Bracket · crackedSUPPORT BRACKET UNDER PILOT WINDOW CRACKED (MARKED). DISCOVERED DURING C-CHECK INSPECTION. REPAIRED SUPPORT BRACKET UNDER PILOT WINDOW IAW SRM 53-00-04.Mar 2, 2004 · N213SW · Emb EMB120ER · Fuselage Miscellaneous StructureSDR SWIA200413114Bracket · crackedLEFT COCKPIT SIDE LATERAL BRACKET IN COCKPIT IS CRACKED AT LIGHTENING HOLE. DISCOVERED DURING C-CHECK INSPECTION. REMOVED CRACKED BRACKET AT LEFT COCKPIT FRAME 12 AFT OF DV WINDOW. INSTALLED SERVICEABLE BRACKET.Mar 2, 2004 · N213SW · Emb EMB120ER · Fuselage Miscellaneous StructureSDR SWIA200312438Mount · malfunctionedAILERON SYSTEM HAS BUMP. MOVEMENT NOT SMOOTH. INSTALLED SERVICEABLE MOUNT, CAPSTAN AND SERVO MOTOR FOR AILERON CONTROL IAW 27-20-00. P/N 622-5734-002 S/N OFF 6176.Sep 17, 2003 · N213SW · Emb EMB120ER · Aileron Control SystemSDR SWIA200312437Computer · malfunctionedFO'S HDG BUG SLEWS ITSELF CLOCKWISE INTERMITTENTLY. SEEMS TO ONLY DO IT WITH AP SELECTOR TO FO'S SIDE WITH OR WITHOUT AP ENGAGED. REMOVED AND REPLACED FO'S AUTOPILOT COMPUTER IAW EMB MM 22-10-00. OPS CHECK GOOD.Sep 12, 2003 · N213SW · Emb EMB120ER · Autopilot SystemSDR SWIA200312251Servo · ratchetingYOKE RATCHETS WHEN MOVED FORWARD AND AFT, REPLACED ELEVATOR SERVO MOTOR WITH SERVICEABLE UNIT IAW EMB MM 27-00-03. SYSTEM OPS CHECKS GOOD.Aug 9, 2003 · N213SW · Emb EMB120ER · Autopilot Main ServoSDR SWIA200312001Bulb · burned outEMERGENCY OVERHEAD LIGHT AT MAIN CABIN DOOR IS INOPERATIVE. REMOVED AND REPLACED LAMP. OPS CHECK GOOD.May 21, 2003 · N213SW · Emb EMB120ER · Emergency LightingSDR SWIA200211567Wire Harness · faultyLANDING GEAR WOULD NOT RETRACT ON DEPARTURE. RETURNED TO LAX. REMOVED AND REPLACED "A" UPLOCK SENSOR AND HARNESS ASSEMBLY. OPS CHECK GOOD PER MM 32-61-01.Dec 10, 2002 · N213SW · Emb EMB120ER · Landing Gear System WiringSDR SWIA200211404Target · out of adjustON TAKEOFF WE PUT THE GEAR HANDLE UP, ALL LIGHTS WENT OUT EXCEPT LEFT RED ''A''. A VERY LOUD NOISE ALSO REMAINED. WE RECYCLED THE GEAR 4 TIMES AND HAD THE SAME RESULTS. RETURNED TO JAC. ADJUSTED LEFT MAIN GEAR TARGET AND RE-RACKED CANNON PLUG FOR LANDING GOct 30, 2002 · N213SW · Emb EMB120ER · Landing Gear Position and WarningSDR SWIA200211324Connector · looseRIGHT MAIN GEAR GREEN A LIGHT DID NOT EXTINGUISH WHEN GEAR RETRACTED. GEAR DID NOT EXTEND WHEN LEVER PUT IN DOWN POSITION. GEAR EXTENDED WITH ELECTRICAL OVERRIDE. CYCLED GEAR 10 TIMES, COULD NOT DUPLICATE. REPLACED LANDING GEAR CONTROL BOX. CYCLED GEAR 10Oct 10, 2002 · N213SW · Emb EMB120ER · Landing Gear Position and WarningSDR SWIA200210702Connector · contaminatedON TAKEOFF ROLL, AT APPROXIMATELY 100 KTS, THE STEERING INOP LIGHT ILLUMINATED ON THE MULTI-ALARM PANEL ALONG WITH A SINGLE CHIME. TAKEOFF WAS ABORTED. CLEANED MOISTURE FROM NOSE STEERING CANNON PLUG ON NOSE GEAR. OPS CHECKS GOOD.Mar 6, 2002 · N213SW · Emb EMB120ER · Landing Gear Steering SystemSDR SWIA200110512Annunciator · malfunctionedOUTBOARD FLAP DISAGREEMENT UPON FLAP RETRACTION IN THE AIR, RESET USING QRH. OPERATES NORMALLY ON THE GROUND. REMOVED AND REPLACED FLAP ANNUNCIATOR UNIT IAW MM 27-50-00. CLEARED FAULTS. OPS CHECK GOOD AT THIS TIME.Dec 31, 2001 · N213SW · Emb EMB120ER · Trailing Flap Position Indicating SystemSDR SWIA200110493Control Box · faultyLANDING GEAR HANGING UP FOR MORE THAN AFTER TAKEOFF. REMOVED AND REPLACED LANDING GEAR CONTROL RELAY BOX PER EMB120 MM 32-31-02. SWUNG GEAR. OPS CHECK GOOD.Dec 29, 2001 · N213SW · Emb EMB120ER · Landing Gear SelectorSDR SWIA200110454Actuator · failedFLAP DISAGREEMENT UPON SELECTION OF FLAPS TO 45 DEGREES. REMOVED AND REPLACED LEFT NACELLE FLAP ACTUATOR IAW EMB MM 27-50-00. OPS CHECK, LEAK CHECK GOOD.Dec 13, 2001 · N213SW · Emb EMB120ER · Trailing Edge Flap ActuatorSDR SWIA200110439Solenoid Valve · failedON MISSED APPROACH CLIMBOUT IN JAC, SELECTED GEAR UP. THE GEAR DID NOT RETRACT. RAN QRH PROCEDURE AND CYCLED GEAR HANDLE. GEAR DID NOT RETRACT, STILL INDICATED SIX RED DISAGREEMENT AND SIX GREEN DOWNLOCKED INDICATION LIGHTS. PLACED HANDLE IN DOWN POSITION Dec 13, 2001 · N213SW · Emb EMB120ER · Landing Gear Door Retract SectionSDR SWIA200110437Controller · malfunctionedCLIMBING THROUGH 9,000, CABIN RATE CLIMBED TO 2,000 FPM, THEN A DESCENT TO 1500 FPM. AT 11,000, PRESSURE DIFFERENTIAL WENT TO ZERO. THE CABIN ALT LIGHT ON THE MAP ILLUMINATED. PERFORMED THE QRH PROCEDURE. THE MANUAL MODE DID NOT WORK EITHER. UPON RETURN TDec 8, 2001 · N213SW · Emb EMB120ER · Cabin Pressure ControllerSDR SWIA200110353Control Box · malfunctionedLANDING GEAR LEVER WAS SELECTED TO DOWN POSITION AND THE GEAR DID NOT COME DOWN. USED ELECTRIC OVERRIDE TO LOWER THE LANDING GEAR. REPLACED RELAY CONTROL BOX ASSEMBLY. C/W OPS CHECK AND GEAR SWING. OPS CHECK GOOD.Nov 11, 2001 · N213SW · Emb EMB120ER · Landing Gear Retraction/Extension SystemSDR SWIA200110352Controller · malfunctionedWHILE ADVANCING POWER LEVERS FOR TAKEOFF, PRESSURIZATION SYSTEM WENT TO FULL SCALE (>2000 FPM) DOWN. ABORTED TAKEOFF AND SYSTEM WENT FULL SCALE UP. CHECKED ALL SWITCHES AND CONFIRMED SYSTEM WAS IN AUTO MODE. INSTALLED ELECTRONIC ALTITUDE CONTROLLER. OPS CHNov 11, 2001 · N213SW · Emb EMB120ER · Cabin Pressure ControllerSDR SWIA200110252Control Panel · faultyNACELLE FLAPS GO TO 2 DOTS AND STICK. FIRST CONTROL FAULT, THEN DISAGREEMENT. REMOVED AND REPLACED FLAP ANNUNCIATOR CONTROL PANEL IAW MM 75-50-05. OPS CHECK GOOD IAW 27-50-00.Oct 12, 2001 · N213SW · Emb EMB120ER · Trailing Flap Position Indicating SystemSDR SWIA200110244Propeller · out of balanceBAD VIBRATION INFLIGHT, POSSIBLY DUE TO PROP ICING. RETURNED TO SLC. FOUND PROPS OUT OF BALANCE. PERFORMED PROP BALANCE ON BOTH. OPS CHECK GOOD.Oct 11, 2001 · N213SW · Emb EMB120ER · Propeller AssemblySDR SWIA200110240Fcu · failedFLAP DISAGREEMENT REQUIRED ZERO FLAP LANDING. REMOVED AND REPLACED FLAP CONTROL UNIT IAW 27-50-00. RAN FLAPS THROUGH 20 CYCLES. NO DEFECTS NOTED.Oct 9, 2001 · N213SW · Emb EMB120ER · Trailing Flap Position Indicating SystemSDR SWIA200110143Connector · dirtyAFTER TAKEOFF ON RETRACTION FLAP DISAGREEMENT WITH ASSOCIATED AIRCRAFT ROLL TO THE RIGHT. INSPECTED FLAP SYSTEM WITH BREAKOUT BOX AND THE MAINTENANCE MODE. FOUND NO FAULTS. CLEANED CANNON PLUGS. FOUND MOISTURE AND GREASE. OPS CHECK GOOD.Sep 3, 2001 · N213SW · Emb EMB120ER · Trailing Edge Flap Control SystemSDR SWIA200110126Control Unit · malfunctionedFLAP ASYMMETRY THEN DISAGREEMENT ON THE GROUND AFTER APU START. NO HYDRAULIC PUMPS ON.INSTALLED A SERVICEABLE FCU. OPERATED FLAPS SEVERAL TIMES. OPS CHECK GOOD. NO FAULTS NOTED. S/N ON: 0028 S/N OFF: 0221Aug 20, 2001 · N213SW · Emb EMB120ER · Trailing Edge Flap Control SystemSDR SWIA200110030Computer · faultyCOPILOT'S FLIGHT DIRECTOR WENT INTO A BANK AND HEADING WAS OFF 60 DEGREES IN LEVEL FLIGHT. RETURNED TO SLC.REMOVE AND REPLACE RIGHT AHC85 AHRS. REINITIALIZED SYSTEM. NOTE NEW AHRS RIGHTED COPILOT'S ATTITUDE INDICATION.Jul 12, 2001 · N213SW · Emb EMB120ER · Integrated Flight SystemSDR SWIA972631Harness · failedAFTER DEPARTING, GEAR WOULD NOT RETRACT. GEAR LEVER MOVED FREELY WITH NO GEAR MOVEMENT. LEFT MAIN SYSTEM ''A'' TRANSITION LIGHT (RED) DID NOT ILLUMINATE. FOUND LEFT ''A'' UP LOCK HARNESS BAD. REMOVED AND REPLACED WITH SERVICEABLE HARNESS IAW AMM 32-61-01. Jun 14, 2001 · N213SW · Emb EMB120ER · Landing Gear Position and WarningSDR SWIA972164Receiver · failedNUMBER ONE TRANSPONDER INOP WITH CORRESPONDING ''DIAG'' MESSAGE. NUMBER TWO TRANSPONDER INOP IN ALL POSITIONS WITH NUMBER ONE TRANSPONDER OFF OR ON. NO CORRESPONDING ''DIAG'' MESSAGE ON NUMBER TWO. RETURNED TO LAX. VERIFIED TRANSPONDER RECEIVER BAD USING T-4Dec 6, 2000 · N213SW · Emb EMB120ER · ATC Transponder SystemSDR SWIA972163Wire · brokenTAKEOFF AURAL WARNING ''TRIM'' ON TAKEOFF. TRIM WAS PROPERLY SET IN THE GREEN RANGE. REPAIRED BROKEN WIRE IN TAIL CONE. TRIM WARNING OPS CHECK GOOD.Dec 6, 2000 · N213SW · Emb EMB120ER · Instrument System WiringSDR SWIA971637Filter · replacedLEFT HYDRAULIC FILTER LIGHT CAME ON AFTER TAKEOFF, RETURNED TO LAX. REMOVED AND REPLACED LEFT HYDRAULIC RETURN FILTERS, OPS CHECKS GOOD.Dec 26, 1999 · N213SW · Emb EMB120ER · Hydraulic Filter, MainSDR SWIA971614Actuator · malfunctionedUNABLE TO APPLY NORMAL RIGHT RUDDER AFTER TAKEOFF. LEFT RUDDER WORKED OK AND SYSTEM WORKED NORMALLY ON DESCENT. REPLACED BLUE SYSTEM RUDDER ACTUATOR. NO LEAKS NOTED. GROUND FUNCTIONAL CHECKS GOOD.Nov 28, 1999 · N213SW · Emb EMB120ER · Rudder ActuatorSDR SWIA971523Indicator · inopRIGHT NP ANALOG GAUGE INOP. RETURNED TO FIELD. REMOVED AND REPLACED NUMBER TWO NP INDICATOR WITH SERVICEABLE UNIT. GROUND RAN ENGINE AND OPS CHECKS GOOD.Jul 5, 1999 · N213SW · Emb EMB120ER · Propeller Indication System
Back to N213SW, cancelled Nov 14, 2007