# Service difficulty reports: N213SW, cancelled Nov 14, 2007

A list on [N213SW, cancelled Nov 14, 2007](https://openairdocs.org/deregistered/N213SW-2007-11-14.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 2 · 63 reports

- [SDR SWIA200718727](https://openairdocs.org/sdr/SWIA200718727.md): Window Post · cracked · Aug 2, 2007 · N213SW · Emb EMB120ER · Fuselage Main, Structure
  > FOUND 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.
- [SDR SWIA200718725](https://openairdocs.org/sdr/SWIA200718725.md): Stringer · corroded · Aug 2, 2007 · N213SW · Emb EMB120ER · Fuselage Main, Longeron/Stringer
  > FOUND 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.
- [SDR SWIA200718724](https://openairdocs.org/sdr/SWIA200718724.md): Floorbeam · corroded · Aug 2, 2007 · N213SW · Emb EMB120ER · Fuselage Main, Floor Beam
  > FOUND AT C-CHECK, CORROSION AT PAX DOOR AREA ON FLOORBEAM. REMOVED AND REPLACED OMEGA BEAM AND BUTTSTRAP IAW SRM 51-10-02.
- [SDR SWIA200718714](https://openairdocs.org/sdr/SWIA200718714.md): Seat Track · corroded · Aug 2, 2007 · N213SW · Emb EMB120ER · Fuselage, Seat/Cargo Attach Fittings
  > FOUND 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.
- [SDR SWIA200718713](https://openairdocs.org/sdr/SWIA200718713.md): Control Cable · corroded · Aug 2, 2007 · N213SW · Emb EMB120ER · Elevator Control System
  > FOUND AT C-CHECK, LEFT ELEVATOR INBOARD MIDDLE CABLE IS CORRODED. REPLACED THE LEFT INBOARD CABLE IAW MM 27-00-01.
- [SDR SWIA200717867](https://openairdocs.org/sdr/SWIA200717867.md): Relay · noisy · Mar 1, 2007 · N213SW · Emb EMB120ER · AC Power Distribution System
  > FOUND 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.
- [SDR SWIA200717826](https://openairdocs.org/sdr/SWIA200717826.md): Control Module · malfunctioned · Feb 17, 2007 · N213SW · Emb EMB120ER · Landing Gear Retraction/Extension System
  > AT 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) - 1
- [SDR SWIA200717792](https://openairdocs.org/sdr/SWIA200717792.md): Battery Pack · discharged · Feb 4, 2007 · N213SW · Emb EMB120ER · Emergency Lighting
  > FOUND EXIT ROW LIGHTS INOP. REPLACED CENTER BATTERY PACK IAW EMB MM 33-50-02. OPERATIONAL CHECKS GOOD.
- [SDR SWIA200616294](https://openairdocs.org/sdr/SWIA200616294.md): Fan · smoke · Feb 16, 2006 · N213SW · Emb EMB120ER · Air Distribution Fan
  > ON 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.
- [SDR SWIA200616134](https://openairdocs.org/sdr/SWIA200616134.md): Floor Support · corroded · Jan 12, 2006 · N213SW · Emb EMB120ER · Fuselage Miscellaneous Structure
  > THE 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.
- [SDR SWIA200616133](https://openairdocs.org/sdr/SWIA200616133.md): Floor Support · corroded · Jan 12, 2006 · N213SW · Emb EMB120ER · Fuselage Miscellaneous Structure
  > THE 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.
- [SDR SWIA200515757](https://openairdocs.org/sdr/SWIA200515757.md): Smoke Detector · activated · Oct 28, 2005 · N213SW · Emb EMB120ER · Smoke Detection
  > LAV SMOKE DETECTOR GOES OFF. REPLACED LAV SMOKE DETECTOR. OPERATIONAL CHECK GOOD.
- [SDR SWIA200514548](https://openairdocs.org/sdr/SWIA200514548.md): Transducer · inoperative · Feb 15, 2005 · N213SW · Emb EMB120ER · Stall Warning System
  > WHEN 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.
- [SDR SWIA200414269](https://openairdocs.org/sdr/SWIA200414269.md): Strut · separated · Dec 8, 2004 · N213SW · Emb EMB120ER · Passenger/Crew Doors
  > MAIN CABIN DOOR WOULD NOT OPEN. REATTACHED F/A JUMP SEAT STRUT. DOOR OPERATES NORMAL. OPERATIONAL CHECK GOOD.
- [SDR SWIA200414152](https://openairdocs.org/sdr/SWIA200414152.md): Seat · out of position · Nov 24, 2004 · N213SW · Emb EMB120ER · Flight Compartment Equipment
  > FORWARD DOOR WILL NOT OPEN. FOUND FORWARD DOOR HANDLE HITTING F/A JUMPSEAT, REPOSITIONED F/A SEAT. OPERATIONAL CHECK GOOD.
- [SDR SWIA200413713](https://openairdocs.org/sdr/SWIA200413713.md): Bolt · out of adjust · Aug 14, 2004 · N213SW · Emb EMB120ER · Passenger/Crew Doors
  > FORWARD ENTRY DOOR WILL NOT OPEN. ADJUSTED FORWARD DOOR FORWARD ECCENTRIC BOLT IAW MM 52-11-00 PAGE 504. OPERATIONAL CHECK GOOD.
- [SDR SWIA200413538](https://openairdocs.org/sdr/SWIA200413538.md): Switch · malfunctioned · Jun 30, 2004 · N213SW · Emb EMB120ER · Elevator Tab Control System
  > WHEN 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.
- [SDR SWIA200413476](https://openairdocs.org/sdr/SWIA200413476.md): Computer · malfunctioned · Jun 16, 2004 · N213SW · Emb EMB120ER · Autopilot System
  > AUTOPILOT 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 2
- [SDR SWIA200413256](https://openairdocs.org/sdr/SWIA200413256.md): Servo · malfunctioned · Apr 24, 2004 · N213SW · Emb EMB120ER · Autopilot Main Servo
  > FEEL A BINDING WHEN MOVING AILERONS. REMOVED AND REPLACED AILERON SERVO WITH SERVICEABLE UNIT IAW EMB 120 MM CHAPTER 22-10-05. OPS CHECK GOOD.
- [SDR SWIA200413070](https://openairdocs.org/sdr/SWIA200413070.md): Window Post · cracked · Mar 24, 2004 · N213SW · Emb EMB120ER · Fuselage Main, Structure
  > ANGLE 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.
- [SDR SWIA200413116](https://openairdocs.org/sdr/SWIA200413116.md): Shear Tie · cracked · Mar 2, 2004 · N213SW · Emb EMB120ER · Fuselage Main, Structure
  > CRACK 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.
- [SDR SWIA200413115](https://openairdocs.org/sdr/SWIA200413115.md): Support Bracket · cracked · Mar 2, 2004 · N213SW · Emb EMB120ER · Fuselage Miscellaneous Structure
  > SUPPORT BRACKET UNDER PILOT WINDOW CRACKED (MARKED). DISCOVERED DURING C-CHECK INSPECTION. REPAIRED SUPPORT BRACKET UNDER PILOT WINDOW IAW SRM 53-00-04.
- [SDR SWIA200413114](https://openairdocs.org/sdr/SWIA200413114.md): Bracket · cracked · Mar 2, 2004 · N213SW · Emb EMB120ER · Fuselage Miscellaneous Structure
  > LEFT 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.
- [SDR SWIA200312438](https://openairdocs.org/sdr/SWIA200312438.md): Mount · malfunctioned · Sep 17, 2003 · N213SW · Emb EMB120ER · Aileron Control System
  > AILERON 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.
- [SDR SWIA200312437](https://openairdocs.org/sdr/SWIA200312437.md): Computer · malfunctioned · Sep 12, 2003 · N213SW · Emb EMB120ER · Autopilot System
  > FO'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.
- [SDR SWIA200312251](https://openairdocs.org/sdr/SWIA200312251.md): Servo · ratcheting · Aug 9, 2003 · N213SW · Emb EMB120ER · Autopilot Main Servo
  > YOKE RATCHETS WHEN MOVED FORWARD AND AFT, REPLACED ELEVATOR SERVO MOTOR WITH SERVICEABLE UNIT IAW EMB MM 27-00-03. SYSTEM OPS CHECKS GOOD.
- [SDR SWIA200312001](https://openairdocs.org/sdr/SWIA200312001.md): Bulb · burned out · May 21, 2003 · N213SW · Emb EMB120ER · Emergency Lighting
  > EMERGENCY OVERHEAD LIGHT AT MAIN CABIN DOOR IS INOPERATIVE. REMOVED AND REPLACED LAMP. OPS CHECK GOOD.
- [SDR SWIA200211567](https://openairdocs.org/sdr/SWIA200211567.md): Wire Harness · faulty · Dec 10, 2002 · N213SW · Emb EMB120ER · Landing Gear System Wiring
  > LANDING 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.
- [SDR SWIA200211404](https://openairdocs.org/sdr/SWIA200211404.md): Target · out of adjust · Oct 30, 2002 · N213SW · Emb EMB120ER · Landing Gear Position and Warning
  > ON 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 G
- [SDR SWIA200211324](https://openairdocs.org/sdr/SWIA200211324.md): Connector · loose · Oct 10, 2002 · N213SW · Emb EMB120ER · Landing Gear Position and Warning
  > RIGHT 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 10
- [SDR SWIA200210702](https://openairdocs.org/sdr/SWIA200210702.md): Connector · contaminated · Mar 6, 2002 · N213SW · Emb EMB120ER · Landing Gear Steering System
  > ON 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.
- [SDR SWIA200110512](https://openairdocs.org/sdr/SWIA200110512.md): Annunciator · malfunctioned · Dec 31, 2001 · N213SW · Emb EMB120ER · Trailing Flap Position Indicating System
  > OUTBOARD 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.
- [SDR SWIA200110493](https://openairdocs.org/sdr/SWIA200110493.md): Control Box · faulty · Dec 29, 2001 · N213SW · Emb EMB120ER · Landing Gear Selector
  > LANDING 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.
- [SDR SWIA200110454](https://openairdocs.org/sdr/SWIA200110454.md): Actuator · failed · Dec 13, 2001 · N213SW · Emb EMB120ER · Trailing Edge Flap Actuator
  > FLAP 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.
- [SDR SWIA200110439](https://openairdocs.org/sdr/SWIA200110439.md): Solenoid Valve · failed · Dec 13, 2001 · N213SW · Emb EMB120ER · Landing Gear Door Retract Section
  > ON 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
- [SDR SWIA200110437](https://openairdocs.org/sdr/SWIA200110437.md): Controller · malfunctioned · Dec 8, 2001 · N213SW · Emb EMB120ER · Cabin Pressure Controller
  > CLIMBING 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 T
- [SDR SWIA200110353](https://openairdocs.org/sdr/SWIA200110353.md): Control Box · malfunctioned · Nov 11, 2001 · N213SW · Emb EMB120ER · Landing Gear Retraction/Extension System
  > LANDING 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.
- [SDR SWIA200110352](https://openairdocs.org/sdr/SWIA200110352.md): Controller · malfunctioned · Nov 11, 2001 · N213SW · Emb EMB120ER · Cabin Pressure Controller
  > WHILE 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 CH
- [SDR SWIA200110252](https://openairdocs.org/sdr/SWIA200110252.md): Control Panel · faulty · Oct 12, 2001 · N213SW · Emb EMB120ER · Trailing Flap Position Indicating System
  > NACELLE 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.
- [SDR SWIA200110244](https://openairdocs.org/sdr/SWIA200110244.md): Propeller · out of balance · Oct 11, 2001 · N213SW · Emb EMB120ER · Propeller Assembly
  > BAD VIBRATION INFLIGHT, POSSIBLY DUE TO PROP ICING. RETURNED TO SLC. FOUND PROPS OUT OF BALANCE. PERFORMED PROP BALANCE ON BOTH. OPS CHECK GOOD.
- [SDR SWIA200110240](https://openairdocs.org/sdr/SWIA200110240.md): Fcu · failed · Oct 9, 2001 · N213SW · Emb EMB120ER · Trailing Flap Position Indicating System
  > FLAP DISAGREEMENT REQUIRED ZERO FLAP LANDING. REMOVED AND REPLACED FLAP CONTROL UNIT IAW 27-50-00. RAN FLAPS THROUGH 20 CYCLES. NO DEFECTS NOTED.
- [SDR SWIA200110143](https://openairdocs.org/sdr/SWIA200110143.md): Connector · dirty · Sep 3, 2001 · N213SW · Emb EMB120ER · Trailing Edge Flap Control System
  > AFTER 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.
- [SDR SWIA200110126](https://openairdocs.org/sdr/SWIA200110126.md): Control Unit · malfunctioned · Aug 20, 2001 · N213SW · Emb EMB120ER · Trailing Edge Flap Control System
  > FLAP 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: 0221
- [SDR SWIA200110030](https://openairdocs.org/sdr/SWIA200110030.md): Computer · faulty · Jul 12, 2001 · N213SW · Emb EMB120ER · Integrated Flight System
  > COPILOT'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.
- [SDR SWIA972631](https://openairdocs.org/sdr/SWIA972631.md): Harness · failed · Jun 14, 2001 · N213SW · Emb EMB120ER · Landing Gear Position and Warning
  > AFTER 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.
- [SDR SWIA972164](https://openairdocs.org/sdr/SWIA972164.md): Receiver · failed · Dec 6, 2000 · N213SW · Emb EMB120ER · ATC Transponder System
  > NUMBER 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-4
- [SDR SWIA972163](https://openairdocs.org/sdr/SWIA972163.md): Wire · broken · Dec 6, 2000 · N213SW · Emb EMB120ER · Instrument System Wiring
  > TAKEOFF AURAL WARNING ''TRIM'' ON TAKEOFF. TRIM WAS PROPERLY SET IN THE GREEN RANGE. REPAIRED BROKEN WIRE IN TAIL CONE. TRIM WARNING OPS CHECK GOOD.
- [SDR SWIA971637](https://openairdocs.org/sdr/SWIA971637.md): Filter · replaced · Dec 26, 1999 · N213SW · Emb EMB120ER · Hydraulic Filter, Main
  > LEFT HYDRAULIC FILTER LIGHT CAME ON AFTER TAKEOFF, RETURNED TO LAX. REMOVED AND REPLACED LEFT HYDRAULIC RETURN FILTERS, OPS CHECKS GOOD.
- [SDR SWIA971614](https://openairdocs.org/sdr/SWIA971614.md): Actuator · malfunctioned · Nov 28, 1999 · N213SW · Emb EMB120ER · Rudder Actuator
  > UNABLE 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.
- [SDR SWIA971523](https://openairdocs.org/sdr/SWIA971523.md): Indicator · inop · Jul 5, 1999 · N213SW · Emb EMB120ER · Propeller Indication System
  > RIGHT NP ANALOG GAUGE INOP. RETURNED TO FIELD. REMOVED AND REPLACED NUMBER TWO NP INDICATOR WITH SERVICEABLE UNIT. GROUND RAN ENGINE AND OPS CHECKS GOOD.

Next page: https://openairdocs.org/deregistered/N213SW-2007-11-14/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/deregistered/N213SW-2007-11-14/reports

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