# Service difficulty reports: N592SW, cancelled Feb 3, 2012

A list on [N592SW, cancelled Feb 3, 2012](https://openairdocs.org/deregistered/N592SW-2012-02-03.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 · 58 reports

- [SDR COMA0760631](https://openairdocs.org/sdr/COMA0760631.md): Flap System · malfunctioned · Nov 8, 2007 · N592SW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5308 - EN ROUTE CVG-LGA RECEIVED FLAP FAIL MESSAGE. DIVERTED TO JFK, DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C) FLAP SYSTEM WAS RESET
- [SDR COMA0760432](https://openairdocs.org/sdr/COMA0760432.md): Control Handle · faulty · Jun 11, 2007 · N592SW · Cndair CL6002B19 · Landing Gear Selector
  > AT 4000FT AND 210KTS RECEIVED GEAR HORN, TERRAIN WARNING AND GEAR DOWN AMBER. CLEARED AFTER 45 SECONDS. GEAR IND TURNED WHITE AFTER 10 SECONDS. 2ND INCIDENT, FIRST HAD NO TERRAIN WARNING. PERFORMED OPERATIONAL TEST. REPLACED LANDING GEAR CONTROL ASSEMBLY.
- [SDR COMA0760389](https://openairdocs.org/sdr/COMA0760389.md): Flap System · failed · May 20, 2007 · N592SW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5067 - FLAP FAIL AT GATE. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER MESSAGES.
- [SDR COMA0760313](https://openairdocs.org/sdr/COMA0760313.md): Flap · malfunctioned · Apr 11, 2007 · N592SW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > AFTER LANDING DURING FLAP RETRACTION RECEIVED A FLAP FAIL MESSAGE AT 27 DEGREES. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES.
- [SDR COMA0760229](https://openairdocs.org/sdr/COMA0760229.md): Window · cracked · Mar 6, 2007 · N592SW · Cndair CL6002B19 · Flight Compartment Windows
  > FLIGHT 9438 - F/O'S SIDE WINDOW CRACKED PASSING THROUGH 26,000 FT. REPLACED WINDOW.
- [SDR COMA0660408](https://openairdocs.org/sdr/COMA0660408.md): Sensor · faulty · Jun 27, 2006 · N592SW · Cndair CL6002B19 · Cabin Cooling System
  > FLIGHT 5480 - AFTER TAKEOFF RECEIVED A RIGHT PACK OVERPRESSURE WARNING, FLIGHT RETURNED TO THE FIELD. REPLACED THE DUCT TEMPERATURE SENSOR.
- [SDR COMA0660400](https://openairdocs.org/sdr/COMA0660400.md): Connector · dirty · Jun 22, 2006 · N592SW · Cndair CL6002B19 · APU Indicating System
  > FLIGHT 5506 - RECEIVED APU TEMP MASTER CAUTION IN FLIGHT/ DIVERTED TO ORF AND LANDED WITHOUT INCIDENT. FOUND APU OIL SERVICED PROPERLY. CLEANED CONNECTOR ON OIL TEMP BULB AND RESECURED. PERFORMED APU RUN, NO FURTHER DEFECTS.
- [SDR SWIA200516048](https://openairdocs.org/sdr/SWIA200516048.md): Pin · loose · Dec 27, 2005 · N592SW · Cndair CL6002B19 · Flight Control System Wiring
  > STAB TRIM CH 1 STATUS MESSAGE OCCURRED TWICE, ONCE ON CLIMB-OUT, ONCE ON TAXI IN. REPLACED HSTA AND MCU IAW AMM 27-40-00, 27-42-05 AND RECONNECTED LOOSE PINS AT P268. OPERATIONAL CHECK GOOD, PN: 7062-3, SN OFF: 934, PN: 8396-3 SN OFF: 794.
- [SDR SWIA200516002](https://openairdocs.org/sdr/SWIA200516002.md): Trim Switch · malfunctioned · Dec 16, 2005 · N592SW · Cndair CL6002B19 · Stabilizer Position Indicating
  > CA STAB TRIM INTERMITTENT, BOTH DIRECTIONS. REPLACED CAPTIANS TRIM SWITCH. IAW 27-41-05. OPERATIONAL CHECK GOOD IAW 27-41-01.
- [SDR SWIA200515884](https://openairdocs.org/sdr/SWIA200515884.md): Lamp · burned out · Nov 22, 2005 · N592SW · Cndair CL6002B19 · Emergency Lighting
  > NR 2 CEILING EMERGENCY FLOODLIGHT INOP. RELAMPED NR 2 CEILING EMERGENCY FLOODLIGHT. OPERATIONAL CHECK GOOD.
- [SDR SWIA200515668](https://openairdocs.org/sdr/SWIA200515668.md): Bolt · loose · Oct 11, 2005 · N592SW · Cndair CL6002B19 · Drag Control System
  > ABORTED T/O DUE TO "CONFIG SPOILERS" WARNING MSG. REPLACED BOLT AND BUSHINGS AT ROD END ATTACH POINT RIGHT FLIGHT SPOILER OB PCU AND ADJUSTED PCU IAW MM 27-62-01. OPERATIONAL CHECK GOOD.
- [SDR SWIA200515470](https://openairdocs.org/sdr/SWIA200515470.md): Pcu · malfunctioned · Aug 26, 2005 · N592SW · Cndair CL6002B19 · Drag Control System
  > FLIGHT SPOILERS FAULT STATUS MSG ON ED2. REPLACED RIGHT NR 2 OUTBOARD FLIGHT SPOILER PCU IAW MM 29-62-01. OPERATIONAL CHECK GOOD.
- [SDR SWIA200515100](https://openairdocs.org/sdr/SWIA200515100.md): Connector · loose · Jun 4, 2005 · N592SW · Cndair CL6002B19 · Light System Wiring
  > OVERHEAD EMERGENCY EXIT SIGN AT OVERWING EXITS INOP. RESECURED LOOSE CONNECTOR. OPERATIONAL CHECK GOOD IAW AMM SUBTASK 33-51-00-720-801.
- [SDR SWIA200515553](https://openairdocs.org/sdr/SWIA200515553.md): Angle · cracked · May 16, 2005 · N592SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 625 LT ANGLE STR 14L CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06.
- [SDR SWIA200515112](https://openairdocs.org/sdr/SWIA200515112.md): Floorbeam · cracked · May 15, 2005 · N592SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 280 BELOW FLOOR RBL 9.0 OUTBOARD ANGLE CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-13, 51-42-21, 51-23-00, 51-25-00.
- [SDR SWIA200515111](https://openairdocs.org/sdr/SWIA200515111.md): Floor Support · corroded · May 15, 2005 · N592SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR ANGLE CORRODED IN NUMEROUS LOCATIONS FROM FS 409 +128 TO FS 559 AND LBL 36 TO 47, ITEM FOUND AT C-CHECK INSPECTION. BLENDED OUT DAMAGE IAW CRJ SRM 53-41-45 PAGE 101-108. FOUND TO BE WITHIN LIMITS IAW SRM 53-41-45.
- [SDR SWIA200515110](https://openairdocs.org/sdr/SWIA200515110.md): Floor Support · corroded · May 15, 2005 · N592SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR ANGLE CORRODED IN NUMEROUS LOCATIONS FROM FS 409 +128 TO FS 559 AND RBL 36 TO 47, ITEM FOUND AT C-CHECK INSPECTION. BLENDED OUT DAMAGE IAW CRJ SRM 53-41-45 PAGE 101-108, FOUND TO BE WITHIN LIMITS IAW SRM 53-41-45.
- [SDR SWIA200515109](https://openairdocs.org/sdr/SWIA200515109.md): Step · corroded · May 15, 2005 · N592SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR TOP STEP HAS CORROSION ON HINGE, ITEM FOUND AT C-CHECK INSPECTION. HINGE REPLACED IAW CRJ SRM 51-41-02.
- [SDR SWIA200515108](https://openairdocs.org/sdr/SWIA200515108.md): Floor Panel · cracked · May 15, 2005 · N592SW · Cndair CL6002B19 · Fuselage Floor Panel
  > FS 193 - LEFT SIDE ELECTRICAL BAY FLOOR CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED CRACK IAW CRJ REO 601R-53-11-001 REV NC.
- [SDR SWIA200514664](https://openairdocs.org/sdr/SWIA200514664.md): Light · burned out · Mar 2, 2005 · N592SW · Cndair CL6002B19 · Emergency Lighting
  > ONE CEILING LEVEL EMERGENCY FLOODLIGHT INOPERATIVE. RELAMPED, OPERATIONAL CHECKS GOOD.
- [SDR SWIA200514653](https://openairdocs.org/sdr/SWIA200514653.md): Pcu · malfunctioned · Feb 28, 2005 · N592SW · Cndair CL6002B19 · Drag Control System
  > SPOILERON FAULT STATUS MESSAGE UPON LANDING. REPLACED RIGHT OUTBOARD PCU IAW 22-61-05, OPERATIONAL CHECK GOOD.
- [SDR SWIA200414062](https://openairdocs.org/sdr/SWIA200414062.md): Converter · inoperative · Nov 4, 2004 · N592SW · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY TRACK LIGHTING AT SEAT 12AB IS NOT ILLUMINATING. REMOVED AND REPLACED CONVERTER IAW 33-00-00. OPERATIONAL CHECK GOOD.
- [SDR SWIA200413847](https://openairdocs.org/sdr/SWIA200413847.md): Actuator · malfunctioned · Sep 25, 2004 · N592SW · Cndair CL6002B19 · Stabilizer Control System
  > COULD NOT GET STAB CHANNEL NR 2 TO ENGAGE. REMOVED AND REPLACED THE HORIZONTAL STAB TRIM ACTUATOR AND THE MOTOR CONTROL UNIT. OPERATIONAL CHECK GOOD. P/N 7062-3, S/N OFF 1095.
- [SDR SWIA200413821](https://openairdocs.org/sdr/SWIA200413821.md): Control Unit · malfunctioned · Sep 20, 2004 · N592SW · Cndair CL6002B19 · Stabilizer Position Indicating
  > STAB CHANNEL 2 WILL NOT ENGAGE. REMOVED AND REPLACED HSTCU IAW AMM 27-41-01. OPERATIONAL CHECK GOOD.
- [SDR SWIA200413794](https://openairdocs.org/sdr/SWIA200413794.md): Trim Switch · malfunctioned · Sep 10, 2004 · N592SW · Cndair CL6002B19 · Stabilizer Position Indicating
  > STAB TRIM CHANNEL 2 WILL NOT ENGAGE. REMOVED AND REPLACED BOTH TRIM SWITCHES IAW MM 27-41-30. OPERATIONAL CHECK GOOD.
- [SDR SWIA200413689](https://openairdocs.org/sdr/SWIA200413689.md): Control Unit · malfunctioned · Aug 12, 2004 · N592SW · Cndair CL6002B19 · Stabilizer Position Indicating
  > STAB TRIM CHANEL 1 INOPERATIVE. REMOVED AND REPLACED STAB TRIM ACTUATOR AND MOTOR CONTROL UNIT IAW MM 27-42-01 AND 27-42-05. OPERATIONAL CHECK GOOD. P/N: 8396-3 S/N OFF: 682
- [SDR SWIA200413679](https://openairdocs.org/sdr/SWIA200413679.md): Switch · malfunctioned · Aug 2, 2004 · N592SW · Cndair CL6002B19 · Stabilizer Position Indicating
  > STAB CH 1 INOP MESSAGE. REMOVED AND REPLACED CAPTIANS STAB TRIM DISCONNECT SWITCH IAW MM 27-41-30. OPERATIONAL CHECK GOOD.
- [SDR SWIA200413394](https://openairdocs.org/sdr/SWIA200413394.md): Pcu · malfunctioned · Jun 4, 2004 · N592SW · Cndair CL6002B19 · Drag Control System
  > SPOILERON FAULT MESSAGE ON TAXI OUT WITH BOTH ENGINES RUNNING. REMOVED AND REPLACED LT NR 1 SPOILERON PCU IAW MM 27-62-01. OPERATIONAL CHECK GOOD.
- [SDR SWIA200413373](https://openairdocs.org/sdr/SWIA200413373.md): Pcu · malfunctioned · May 31, 2004 · N592SW · Cndair CL6002B19 · Drag Control System
  > SPOILERON FAULT STATUS MESSAGE WOULD NOT CLEAR. REMOVED AND REPLACED LEFT WING INBOARD FLIGHT SPOILER INBOARD PCU IAW MM 27-61-00. LEAK AND OPS CHECK GOOD.
- [SDR SWIA200413007](https://openairdocs.org/sdr/SWIA200413007.md): Control Unit · failed · Mar 8, 2004 · N592SW · Cndair CL6002B19 · Drag Control System
  > LEFT SPOILERON FAULT MESSAGE ON EICAS. REMOVED AND REPLACED NR 1 SECU IAW MM 27-61-05. OPS CHECK GOOD. P/N 49-164-06, S/N OFF 0929.
- [SDR SWIA200412970](https://openairdocs.org/sdr/SWIA200412970.md): Bpsu · malfunctioned · Mar 2, 2004 · N592SW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > RECEIVED A FLAPS FAIL WHEN SELECTING FLAPS 20 DURING APPROACH. REMOVED AND REPLACED LEFT BPSU IAW CRJ MM 27-51-10. OPS CHECK GOOD. P/N: 855D100-9, S/N ON: 316B, S/N OFF: 0811B.
- [SDR SWIA200412945](https://openairdocs.org/sdr/SWIA200412945.md): Sensor · malfunctioned · Feb 27, 2004 · N592SW · Cndair CL6002B19 · Stall Warning System
  > STALL FAIL AFTER ROTATION. REMOVED AND REPLACED LEFT AOA SENSOR IAW CL600 MM 27-35-05. OPS CHECKS GOOD.
- [SDR SWIA200412757](https://openairdocs.org/sdr/SWIA200412757.md): Pdu · malfunctioned · Jan 4, 2004 · N592SW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAP FAIL MESSAGE WHEN SELECTING FLAPS AT 45 DEGREES. REMOVED AND REPLACED FLAP PDU IAW MM 27-52-01. OPS CHECKS GOOD.
- [SDR SWIA200312668](https://openairdocs.org/sdr/SWIA200312668.md): Support · cracked · Dec 5, 2003 · N592SW · Cndair CL6002B19 · Engine Mount Section
  > ENGINE SUPPORT BEAM UPPER WEB RBL 6 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. UPPER WEB REPAIRED IAW CRJ REO 601R-53-61-345 REV ''C'' AND RII 53-401.
- [SDR SWIA200312667](https://openairdocs.org/sdr/SWIA200312667.md): Sill · cracked · Dec 5, 2003 · N592SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO PIT CARGO DOOR FLOOR LANDING SILL IS CRACKED UNDER STEP PLATE ASSY PIN STOP FITTING; FS 576.00; LBL 42.0. DISCOVERED DURING C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-40-11 & RII 53-401.
- [SDR SWIA200312666](https://openairdocs.org/sdr/SWIA200312666.md): Beam · cracked · Dec 5, 2003 · N592SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > TRANSVERSE BEAM REMOTE ANGLE FOR DOOR STOP FITTING IS CRACKED; FS 589.00; LBL 42.0. DISCOVERED DURING C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-40-11 & RII 53-401.
- [SDR SWIA200312665](https://openairdocs.org/sdr/SWIA200312665.md): Beam · cracked · Dec 5, 2003 · N592SW · Cndair CL6002B19 · Engine Mount Section
  > ENGINE SUPPORT BEAM LOWER WEB RIGHT SIDE RBL 34 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. WEB REPAIRED IAW CRJ REO 601R-53-61-366 REV ''D'', RII 53-401.
- [SDR SWIA200312664](https://openairdocs.org/sdr/SWIA200312664.md): Beam · cracked · Dec 5, 2003 · N592SW · Cndair CL6002B19 · Engine Mount Section
  > ENGINE SUPPORT BEAM LOWER WEB LT SIDE LBL 34 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. WEB REPAIRED IAW CRJ REO 601R-53-61-366 REV ''D'' AND RII 53-401.
- [SDR SWIA200312663](https://openairdocs.org/sdr/SWIA200312663.md): Intercostal · cracked · Dec 5, 2003 · N592SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 625 RIGHT INTERCOSTAL STRINGER 14R CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED INTERCOSTAL IAW CRJ SRM 51-40-11, 51-42-06.
- [SDR SWIA200312662](https://openairdocs.org/sdr/SWIA200312662.md): Floorbeam · cracked · Dec 5, 2003 · N592SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 460 RIGHT FLOORBEAM RBL 9.0 O/B FITTING CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED FITTING IAW CRJ SRM 51-40-11, 51-23-00, 51-42-06, 51-42-21 & RII 53-401.
- [SDR SWIA200312661](https://openairdocs.org/sdr/SWIA200312661.md): Beam · cracked · Dec 5, 2003 · N592SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 280 TRANSVERSE BEAM RBL 11 LOWER FLANGE CRACKED. DISCOVERED DURING C-CHECK INSPECTION. CUT-OUT AND REPAIRED DAMAGED SECTION OF TRANSVERSE BEAM IAW CRJ REO 601R-53-11-171 REV ''NC''.
- [SDR SWIA200312660](https://openairdocs.org/sdr/SWIA200312660.md): Beam · cracked · Dec 5, 2003 · N592SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 280 TRANSVERSE BEAM LBL 11 LOWER FLANGE CRACKED. DISCOVERED DURING C-CHECK INSPECTION. CUT-OUT AND REPAIRED DAMAGED SECTION OF TRANSVERSE BEAM IAW CRJ REO 601R-53-11-171 REV ''NC''.
- [SDR SWIA200312659](https://openairdocs.org/sdr/SWIA200312659.md): Floorbeam · cracked · Dec 5, 2003 · N592SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 280 RT FLOORBEAM RBL 90 INBOARD AND OUTBOARD ATTACH ANGLE CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11 & RII 53-401.
- [SDR SWIA200312760](https://openairdocs.org/sdr/SWIA200312760.md): Rib · cracked · Nov 28, 2003 · N592SW · Cndair CL6002B19 · Nacelle/Pylon, Attach Fittings
  > LT PYLON FS 605 RIB CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED RIB IAW CRJ SRM 51-40-11. P/N: 601-37004-85.
- [SDR SWIA200312759](https://openairdocs.org/sdr/SWIA200312759.md): Intercostal · cracked · Nov 28, 2003 · N592SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 484 LT INTERCOSTAL O/B FLANGE LBL 36 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED INTERCOSTAL IAW CRJ REO 601R-53-41-059 REV A AND RII 53-401.
- [SDR SWIA200312758](https://openairdocs.org/sdr/SWIA200312758.md): Frame · cracked · Nov 28, 2003 · N592SW · Cndair CL6002B19 · Fuselage Main, Frame
  > OUTER FLANGE ON FUSELAGE FRAME AT FS 220 AND STR 23L IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED FLANGE IAW CRJ DWG 600-34013 & RII 53-401.
- [SDR SWIA200312270](https://openairdocs.org/sdr/SWIA200312270.md): Heater · malfunctioned · Aug 17, 2003 · N592SW · Cndair CL6002B19 · Heating System
  > THE NR 1 GALLEY HTR CAUSES A SMOKEY SMELL WHEN ON. CREW REPORTS THAT THERE IS A STRONG BURNT ELECTRICAL SMELL IN THE GALLEY OR FLIGHT DECK JUST AFTER PUSHBACK. REMOVED AND REPLACED NR 1 GALLEY HEATER IAW CRJ AMM 21-23-05. P/N: 2831-45 S/N OFF: 584. ALS
- [SDR SWIA200312198](https://openairdocs.org/sdr/SWIA200312198.md): Engine · malfunctioned · Jul 16, 2003 · N592SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > LEFT ENGINE FAILED ON DESCENT. JUST PRIOR TO FAILURE, ''L MAIN EJECTOR'' AND ''L SCAV EJECTOR'' MSG DISPLAYED ON EICAS. REMOVED AND REPLACED LEFT POWER PLANT IAW CRJ MM 72-00-00. OPS AND LEAK CHECKS GOOD.
- [SDR SWIA200211614](https://openairdocs.org/sdr/SWIA200211614.md): Engine · malfunctioned · Dec 24, 2002 · N592SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > ENGINE NR 2 FAILURE INFLIGHT. DURING CRUISE FLIGHT THE RT ITT WAS 50 DEGREES HIGHER THAN ENGINE NR 1 WITH A REDUCTION OF N1 ON ENGINE NR 2 OF 4 PERCENT. REMOVED AND REPLACED RIGHT ENGINE ASSEMBLY IAW CRJ MM 71-00-00 DUE TO COMPRESSOR BLADE DAMAGE.
- [SDR SWIA200211563](https://openairdocs.org/sdr/SWIA200211563.md): Warning System · activated · Dec 8, 2002 · N592SW · Cndair CL6002B19 · Stabilizer Control System
  > STAB TRIM CHANNELS 1 AND 2 FAILED ON TAKEOFF. STAB TRIM AND MACH TRIM CAUTION MESSAGES. RETURNED TO MEM. PERFORMED BITE CHECK OF HSTCU. HSTCU SHOWS NO FAULTS IAW AMM 7-41-00. SYSTEM OPS CHECK GOOD.

Next page: https://openairdocs.org/deregistered/N592SW-2012-02-03/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 = 'N592SW' AND deregistration_id = 'N592SW-2012-02-03'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N592SW-2012-02-03/reports

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