# Service difficulty reports: N492SW, cancelled Feb 16, 2023

A list on [N492SW, cancelled Feb 16, 2023](https://openairdocs.org/deregistered/N492SW-2023-02-16.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 4 · 157 reports

- [SDR SWIA2021070259276](https://openairdocs.org/sdr/SWIA2021070259276.md): Landing Gear · malfunctioned · Jul 1, 2021 · N492SW · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE MESSAGE APPEARED ON APPROACH. RAN QRH PROCEDURE AND WAS ABLE TO SUCCESSFULLY EXTEND THE GEAR. MEL 32-30-1 / CAT A DUE 7/2/21 / CAT II DOWNGRADE / GEAR DISAGREE MESSAGE APPEARED ON APPROACH. RAN QRH PROCEDURE AND WAS ABLE TO SUCCESSFULLY EXTEND
- [SDR SWIA202158610](https://openairdocs.org/sdr/SWIA202158610.md): Fuel Tank · out of balance · Jun 2, 2021 · N492SW · Cndair CL6002B19 · Aircraft Fuel Distribution System
  > DURING CLIMB, 400 FT BEFORE LEVELING OUT, AT 32000 FT. RECEIVED FUEL IMBALANCE CAUTION MSG. LEFT WING TANK SHOWED 4400 CENTER SHOWED APPROX 1500 AND 3300 IN RIGHT WING TANK. COMPLIED WITH QRH AND FUEL IMBALANCE CORRECTED ITSELF WITHIN 10 MINS. PER QRH SUSPECTE
- [SDR SWIA202053860](https://openairdocs.org/sdr/SWIA202053860.md): Windshield · failed · Nov 9, 2020 · N492SW · Cndair CL6002B19 · Flight Compartment Windows
  > SHATTERED RT WINDSHIELD WHILE AT CRUISE ALTITUDE. FLIGHT 4642-FILED CLOSED. REMOVED AND REPLACED RT WINDSHIELD IN REFERENCE WITH AMM. COMPLIED WITH TASK CARD, OPERATIONS CHECKS GOOD WITH NO LEAKS NOTED.
- [SDR SWIA2020030248870](https://openairdocs.org/sdr/SWIA2020030248870.md): Controller · failed · Mar 2, 2020 · N492SW · Cndair CL6002B19 · Cabin Pressure Controller
  > CABIN ALT CAUTION MESSAGE IN FLIGHT. DISAPPEARED ONCE CABIN PRESSURE REGAINED IN FLIGHT FLIGHT 5308 - FILED CLOSED PERFORMED GVI OF OUTFLOW VALVES. NO DEFECTS NOTED. ACFT WOULD NOT PRESSURIZE ABOVE.6 P UNTIL CABIN PRESSURE CONTROLLER 1 CB WAS PULLED. REMO
- [SDR SWIA2019112246781](https://openairdocs.org/sdr/SWIA2019112246781.md): Actuator · failed · Nov 22, 2019 · N492SW · Cndair CL6002B19 · Landing Gear Door Actuator
  > LEFT MAIN GEAR DISAGREE WARNING MESSAGE IN FLIGHT. LEFT MAIN NEVER SHOWED DOWN AND LOCKED FLIGHT 5644 CLOSED INTERROGATED PSEU AND FOUND LT MLG DOWNLOCK PROX SENSORS S19, S34 INDICATING FAR WITH GEAR DOWN/LOCKED. REPLACED LT MLG SIDE STAY ACTUATOR IAW AM
- [SDR SWIA2019073046101](https://openairdocs.org/sdr/SWIA2019073046101.md): Actuator · failed · Jul 30, 2019 · N492SW · Cndair CL6002B19 · Landing Gear Door Actuator
  > GEAR DISAGREE WARNING MESSAGE. FLT 5226. REMOVED AND REPLACED THE NLG EXTENSION/RETRACTION ACTUATOR IAW AMM. OPS CHECK GOOD AT THIS TIME.
- [SDR SWIA2019073046105](https://openairdocs.org/sdr/SWIA2019073046105.md): Actuator · failed · Jul 28, 2019 · N492SW · Cndair CL6002B19 · Aileron Tab Control System
  > AILERON TRIM STUCK LEFT WING DOWN POSITION. FLIGHT 5117. REPLACED AILERON TRIM ACTUATOR IAW AMM.
- [SDR SWIA2019022145562](https://openairdocs.org/sdr/SWIA2019022145562.md): Door Sill · corroded · Feb 1, 2019 · N492SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT FLOOR SILL FS409+73.2 - FS409+128 HAS MULTIPLE AREAS OF CORROSION. (C-CHECK) RO: 02/20/2019 REPAIRED RIGHT FLOOR SILL FS 409+73 TO 409+128 IAW REO.
- [SDR SWIA2019022145561](https://openairdocs.org/sdr/SWIA2019022145561.md): Skin · dented · Jan 23, 2019 · N492SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > EXTERNAL FUSELAGE SKIN IS DENTED AT FS605 - FS621 STR 21L-22L. (C-CHECK) RO: 02/20/2019 REPAIRED DENT IAW REO. ALL STEPS COMPLIED WITH.
- [SDR SWIA2019022145560](https://openairdocs.org/sdr/SWIA2019022145560.md): Floor Support · corroded · Jan 21, 2019 · N492SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT FS 621.00 BETWEEN LBL9 AND LBL27 CORROSION AT FLOOR SUPPORT ANGLE UNDER FLOOR PANEL 281JLF. (C-CHECK) RO: 02/20/2019 REPAIRED FLOOR SUPPORT ANGLE AT FS621 BETWEEN LBL9 AND LBL27 IAW SRM. ALL STEPS IAW REO COMPLIED WITH.
- [SDR SWIA2019022145559](https://openairdocs.org/sdr/SWIA2019022145559.md): Floorbeam · corroded · Jan 21, 2019 · N492SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CENTER FS 617.00 BETWEEN RBL9 AND LBL9 CORROSION AT AFT FLOORBEAM SUPPORT TOP CAP UNDER FLOOR PANEL 281DLF. (C-CHECK) RO: 02/20/2019 REMOVED AND REPLACED VENT ASSY AND PACKER PN: 601R35235-61 WITH NEW VENT ASSY AND PACKER AT CENTER FS 617 BETWEEN RBL9 AND LBL
- [SDR SWIA2019022145558](https://openairdocs.org/sdr/SWIA2019022145558.md): Stiffener · corroded · Jan 18, 2019 · N492SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR HAS CORROSION UNDER UPPER EDGE MEMBER ON STIFFENER. (C-CHECK) RO: 02/20/2019 REMOVED AND REPLACED PAX DOOR UPPER EDGE MEMBER STIFFENER, PN 601R31907-43 IAW SRM.
- [SDR SWIA2019022145551](https://openairdocs.org/sdr/SWIA2019022145551.md): Skin · dented · Jan 18, 2019 · N492SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DENT #5 LOCATED 3.5€? AFT OF FS640 AND 1.5€? ABOVE STR25R HAS OIL CANNING CONDITION. (C-CHECK) RO: 02/20/2019 REPAIRED DENT #5 LOCATED 3.5€? AFT OF FS640 AND 1.5€? ABOVE STR25R IAW REO.
- [SDR SWIA2019022145557](https://openairdocs.org/sdr/SWIA2019022145557.md): Panel · corroded · Jan 17, 2019 · N492SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT PRESSURE FLOOR SILL PANEL HAS MULTIPLE AREAS OF CORROSION. (C-CHECK) RO: 02/20/2019 COMPLIED WITH REPAIR TO THE RT PRESSURE FLOOR SILL PANEL MULTIPLE AREAS OF CORROSION IAW REO.
- [SDR SWIA2019022145556](https://openairdocs.org/sdr/SWIA2019022145556.md): Angle · corroded · Jan 17, 2019 · N492SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT PRESSURE FLOOR SILL ANGLE HAS MULTIPLE AREAS OF CORROSION. (C-CHECK) RO: 02/20/2019 BLENDED CORROSION FROM LT PRESSURE FLOOR SILL ANGLE IAW SRM.
- [SDR SWIA2019022145555](https://openairdocs.org/sdr/SWIA2019022145555.md): Panel · corroded · Jan 17, 2019 · N492SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT PRESSURE FLOOR SILL PANEL HAS MULTIPLE AREAS OF CORROSION. (C-CHECK) RO: 02/20/2019 BLENDED CORROSION ON LT PRESSURE FLOOR SILL PANEL IAW SRM AND REO.
- [SDR SWIA2019022145540](https://openairdocs.org/sdr/SWIA2019022145540.md): Floor Support · corroded · Jan 17, 2019 · N492SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > REPLACE RH FLOOR BEAM AT FS.589.00 TO FS.621.00 RBL27 WITH SERVICEABLE DUE TO OUT OF LIMITS CORROSION. (C-CHECK) RO: 02/20/2019 REMOVED AND REPLACED RH FLOOR BEAM AT FS.569.00 TO FS.621.00 RBL27 IAW REO.
- [SDR SWIA2019022145539](https://openairdocs.org/sdr/SWIA2019022145539.md): Floor Support · corroded · Jan 17, 2019 · N492SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > REPLACE THE RH FLOOR SILL FROM FS 559.0+16 TO 559.0+80 WITH SERVICEABLE DUE TO OUT OF LIMITS CORROSION. REMOVED AND INSTALLED NEW RH FLOOR SILL FROM FS 559+16 TO FS 559+84.9 IAW SRM.
- [SDR SWIA2019022145538](https://openairdocs.org/sdr/SWIA2019022145538.md): Floor Support · damaged · Jan 17, 2019 · N492SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > REPLACE R/H FLOOR BEAM UPPER CAP AT RBL 9 FROM FS 559+12 TO FS 559+120 DUE TO DAMAGE. (C-CHECK) RO: 02/20/2019 REPLACED FLOOR BEAM CAP WITH NEW BEAM CAP LOCATED AT RBL9 BETWEEN FS559+12 TO FS559+120 IAW REO AND SRM.
- [SDR SWIA2019022145554](https://openairdocs.org/sdr/SWIA2019022145554.md): Floorbeam · corroded · Jan 15, 2019 · N492SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CENTER FS 589.00 + 00 BETWEEN RBL9 AND LBL9 CORROSION AT AFT FLOORBEAM TOP CAP UNDER FLOOR PANEL 281CLF. (C-CHECK) RO: 02/20/2019 REMOVED AND REPLACED FS589 BETWEEN RBL9 AND LBL9 CAP STRIP IAW SRM.
- [SDR SWIA2019022145553](https://openairdocs.org/sdr/SWIA2019022145553.md): Door Sill · corroded · Jan 15, 2019 · N492SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT FLOOR SILL CORRODED FROM FS 559.0 TO FS 559.0+80. (C-CHECK) RO: 02/20/2019 REPLACED THE LT FLOOR SILL FROM FS559.00 TO FS559+84.9 WITH NEW SILL IAW SRM AND REO.
- [SDR SWIA2019022145552](https://openairdocs.org/sdr/SWIA2019022145552.md): Skin · dented · Jan 12, 2019 · N492SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > EXTERNAL FUSELAGE SKIN DENTS. A/C LT SIDE BETWEEN FS621 AND FS672 BETWEEN STGRS 21L AND 26L. (C-CHECK) RO: 02/20/2019 PERFORMED HAND DRESS DENT NR 1, NR 2, NR 3 AND NR 4 IAW REO.
- [SDR SWIA2019022145550](https://openairdocs.org/sdr/SWIA2019022145550.md): Skin · dented · Jan 12, 2019 · N492SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > EXTERNAL FUSELAGE SKIN DENTS. A/C R/H SIDE, BETWEEN FS672 AND FS690 BETWEEN STGRS 23R AND 26R. (C-CHECK) RO: 02/20/2019 PERFORMED DRESS-BACK DENTS ON EXTERNAL FUSELAGE SKIN R/H SIDE BETWEEN FS672 AND FS690 BETWEEN STGR23R AND STGR26R IAW REO.
- [SDR SWIA2019022145549](https://openairdocs.org/sdr/SWIA2019022145549.md): Skin · dented · Jan 12, 2019 · N492SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > EXTERNAL FUSELAGE SKIN DENTS ON A/.C R/H SIDE BETWEEN FS672 AND FS690 BETWEEN STGRS 23R AND 26R. (C-CHECK) RO: 02/20/2019 DRESSED BACK 4EA DENTS LOCATED ON AFT RH SIDE OF FUSELAGE FROM FS672-690 BETWEEN STGRS 23R AND 26R IAW REO.
- [SDR SWIA2019022145542](https://openairdocs.org/sdr/SWIA2019022145542.md): Door Sill · corroded · Jan 10, 2019 · N492SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR SILL AREA €“ ANGLE ATTACHED TO LOWER SILL HAS CORROSION. (C-CHECK) RO: 02/20/2019 REMOVED AND REPLACED WITH NEW SERVICE DOOR SILL ANGLE IAW SRM.
- [SDR SWIA2019022145548](https://openairdocs.org/sdr/SWIA2019022145548.md): Intercostal · corroded · Jan 9, 2019 · N492SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AVIONICS BAY RH INTERCOSTAL OUTBOARD OF STR 27 BETWEEN FS 349 AND FS 364 HAS CORROSION. (C-CHECK) RO: 02/20/2019 REPLACED AVIONICS BAY RH INTERCOSTAL OUTBOARD OF STR 27 BETWEEN FS 349 AND FS 364. ALL CHECKS GOOD.
- [SDR SWIA2019022145547](https://openairdocs.org/sdr/SWIA2019022145547.md): Door Frame · corroded · Jan 9, 2019 · N492SW · Cndair CL6002B19 · Fuselage Main, Structure
  > AVIONICS BAY DOOR SURROUND FS349 FRAME ATTACHMENT FLANGE AND VERTICAL FLANGE HAS CORROSION BETWEEN S 25L AND S 26R. (C-CHECK) RO: 02/20/2019 REMOVED CORROSION FROM FRAME FS349.00 AT STR 25 LH TO 26 RH IAW SRM.
- [SDR SWIA2019022145546](https://openairdocs.org/sdr/SWIA2019022145546.md): Door Frame · corroded · Jan 9, 2019 · N492SW · Cndair CL6002B19 · Fuselage Main, Structure
  > AVIONICS BAY DOOR SURROUND FS364 FRAME HAS CORROSION ON ATTACHMENT AND VERTICAL FLANGES BETWEEN STR 25R TO APPROXIMATELY 1€? OUTBOARD OF STR 26L. (C-CHECK) RO: 02/20/2019 COMPLIED WITH ALL STEPS OF REO. PERFORMED PRESSURIZATION CHECK IAW AMM. NO DEFECTS NOTED
- [SDR SWIA2019022145545](https://openairdocs.org/sdr/SWIA2019022145545.md): Hinge · damaged · Jan 5, 2019 · N492SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR PIANO HINGE ON FUSELAGE SIDE HAS MIGRATED ROLL PIN. (C-CHECK) RO: 02/20/2019 REMOVED DAMAGE FROM PAX DOOR (FUSELAGE SIDE) AFT LUG LAND IAW REO.
- [SDR SWIA2019022145544](https://openairdocs.org/sdr/SWIA2019022145544.md): Skin · dented · Jan 5, 2019 · N492SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > PASSENGER DOOR CUTOUT €“ DENT IN FUSELAGE SKIN AT FS 349 (LOCATED AT AFT UPPER LATCH PIN FITTING). (C-CHECK) RO: 02/20/2019 REPAIRED PASSENGER DOOR CUTOUT €“ DENT IN FUSELAGE SKIN AT FS 349 IAW REO.
- [SDR SWIA2019022145543](https://openairdocs.org/sdr/SWIA2019022145543.md): Retainer · corroded · Jan 5, 2019 · N492SW · Cndair CL6002B19 · Emergency Exits
  > RH OVERWING EMERGENCY EXIT DOOR HAS CORROSION ON SEAL RETAINER AT LOWER AFT FITTING. (C-CHECK) RO: 02/20/2019 COMPLETED REPAIR OF RH OVERWING EMERGENCY EXIT DOOR IAW REO.
- [SDR SWIA2019022145541](https://openairdocs.org/sdr/SWIA2019022145541.md): Structure · cracked · Jan 5, 2019 · N492SW · Cndair CL6002B19 · Fuselage Main, Structure
  > RH TRU BAY FLOOR CRACKED FS193 LOCATED BY ADG PUMP. PERFORMED PERMANENT REPAIR TO RH TRU BAY FLOOR AT FS 193.00 IAW REO.
- [SDR SWIA201844126](https://openairdocs.org/sdr/SWIA201844126.md): Wire Harness · failed · Jan 3, 2018 · N492SW · Cndair CL6002B19 · Flight Control System Wiring
  > FLAPS FAILED ENROUTE. DECLARED AN EMERGENCY. REMOVED AND REPLACED THE RT BPSU WIRE HARNESS IAW AMM. CYCLED FLAPS NUMEROUS TIMES WITHOUT FAILURE. OPS CHECKED GOOD.
- [SDR SWIA201844116](https://openairdocs.org/sdr/SWIA201844116.md): Flap System · failed · Jan 2, 2018 · N492SW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAILED MID FLIGHT, ONCE RETRACTED FULLY THE FLAPS FAILED AT ZERO. EMERGENCY DECLARED. RETURNED TO FIELD. RESET IAW FIM AND OPERATED FLAPS FOR MULTIPLE CYCLES. OK FOR SERVICE.
- [SDR SWIA2017122944112](https://openairdocs.org/sdr/SWIA2017122944112.md): Flap System · failed · Dec 29, 2017 · N492SW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL DURING CRUISE. DECLARED EMERGENCY AND DIVERTED. LANDED WITHOUT INCIDENT. RESET THE SYSTEM IAW FIM AND OPERATED FLAPS 5 FULL CYCLES AND COMPLETED AD.
- [SDR SWIA201743580](https://openairdocs.org/sdr/SWIA201743580.md): Floorbeam · corroded · Jul 1, 2017 · N492SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CARGO COMPARTMENT FLOORBEAM CORRODED AT SCREW HOLES. REMOVED AND REPLACED FLOORBEAM IAW REO.
- [SDR SWIA201743579](https://openairdocs.org/sdr/SWIA201743579.md): Floorbeam · corroded · Jun 30, 2017 · N492SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM CORRODED AT SCREW HOLES. REMOVED AND REPLACED FLOORBEAM IAW REO.
- [SDR SWIA2017073143581](https://openairdocs.org/sdr/SWIA2017073143581.md): Panel · corroded · Jun 24, 2017 · N492SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR PANEL CORRODED. REPLACED THE DOOR PANEL.
- [SDR SWIA201540794](https://openairdocs.org/sdr/SWIA201540794.md): Tire · failed · Mar 8, 2015 · N492SW · Cndair CL6002B19 · Tire
  > CREW REPORT NOSE WHEEL SHIMMY DURING TAKEOFF-RETURNED TO THE FIELD. MAINTENANCE CHANGED BOTH NOSE TIRES AND THE AFT SPADE DOOR. R & R IAW AMM.
- [SDR SWIA201540494](https://openairdocs.org/sdr/SWIA201540494.md): Trim Switch · failed · Jan 4, 2015 · N492SW · Cndair CL6002B19 · Stabilizer Control System
  > CREW REPORTS STAB TRIM CAUTION MESSAGE DURING DESCENT. R & R F/O'S PITCH TRIM SWITCH. OPS CHECK GOOD IAW AMM.
- [SDR SWIA201439698](https://openairdocs.org/sdr/SWIA201439698.md): Battery Pack · inoperative · Oct 28, 2014 · N492SW · Cndair CL6002B19 · Emergency Lighting
  > ALL EMERGENCY LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED NR 1 AND 2 EMERGENCY BATTERY PACKS IAW AMM.
- [SDR SWIA201439472](https://openairdocs.org/sdr/SWIA201439472.md): Lock · obstructed · Sep 6, 2014 · N492SW · Cndair CL6002B19 · Passenger/Crew Doors
  > UNABLE TO OPEN MAIN CABIN DOOR. REMOVED INSULATION FOULING TOP DOOR LOCK PINS AND LUBRICATED DOOR IAW AMM.
- [SDR SWIA201335873](https://openairdocs.org/sdr/SWIA201335873.md): Panel · corroded · Dec 15, 2013 · N492SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SILL PANEL CORRODED AT FS 527.00 TO 529.00 LBL 40. C-CHECK REPAIRED BLEND AREA AT FS 527.00 TO 529.00, LBL 40 IAW REO.
- [SDR SWIA201335881](https://openairdocs.org/sdr/SWIA201335881.md): Floorbeam · corroded · Dec 13, 2013 · N492SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > PRESS FLOOR LOCAL TO FLOOR BEAM AT LBL 36 HAS CORROSION AT FS 532 LBL 42. C-CHECK REPAIRED BLEND AREA AT FS 532.00 LBL 42 IAW REO.
- [SDR SWIA201335880](https://openairdocs.org/sdr/SWIA201335880.md): Sill · damaged · Dec 13, 2013 · N492SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PRESS FLOOR LOCAL TO FLOOR BEAM AT LBL 36 HAS PULLED FREEZE PLUG AT FS 535 LBL42. C-CHECK REPAIRED LT PRESS FLOOR SILL WEB IAW REO.
- [SDR SWIA201335879](https://openairdocs.org/sdr/SWIA201335879.md): Floorbeam · corroded · Dec 13, 2013 · N492SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > PRESS FLOOR LOCAL TO FLOOR BEAM AT LBL 36 HAS CORROSION AT FS 538 LBL 42 OVER NUT PLATE. C-CHECK REPAIRED BLEND AREA AT FS 538.00 LBL 42 IAW REO.
- [SDR SWIA201335878](https://openairdocs.org/sdr/SWIA201335878.md): Floorbeam · corroded · Dec 13, 2013 · N492SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > PRESS FLOOR LOCAL TO FLOOR BEAM AT LBL 36 HAS CORROSION AT FS 540 LBL 36. C-CHECK REPAIRED BLEND AREA AT FS 540.00 LBL 36 IAW REO.
- [SDR SWIA201335877](https://openairdocs.org/sdr/SWIA201335877.md): Floorbeam · corroded · Dec 13, 2013 · N492SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > PRESS FLOOR LOCAL TO FLOOR BEAM AT LBL 36 HAS CORROSION AT FS 544, LBL 36. C-CHECK REPAIRED BLEND AREA AT FS 544.00 LBL 36 IAW REO.
- [SDR SWIA201335876](https://openairdocs.org/sdr/SWIA201335876.md): Floorbeam · corroded · Dec 13, 2013 · N492SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > PRESS FLOOR LOCAL TO FLOOR BEAM AT LBL 36 HAS CORROSION AT FS 558, LBL 36. C-CHECK REPAIRED BLEND AREA AT FS 558.00 LBL 36 IAW REO.
- [SDR SWIA201335875](https://openairdocs.org/sdr/SWIA201335875.md): Strap · corroded · Dec 13, 2013 · N492SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PRESS FLOOR, LOCAL TO FLOOR BEAM AT LBL 3 HAS CORROSION ON STRAP AT FS 559, LBL 36-42. C-CHECK R & R STRAP AT FS 559 LBL 36-42 IAW REO.

Next page: https://openairdocs.org/deregistered/N492SW-2023-02-16/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 = 'N492SW' AND deregistration_id = 'N492SW-2023-02-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N492SW-2023-02-16/reports

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