# Service difficulty reports: N429SW, cancelled Jul 30, 2023

A list on [N429SW, cancelled Jul 30, 2023](https://openairdocs.org/deregistered/N429SW-2023-07-30.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 3 · 113 reports

- [SDR SWIA202053466](https://openairdocs.org/sdr/SWIA202053466.md): Target · unsecure · Oct 20, 2020 · N429SW · Cndair CL6002B19 · Landing Gear Position and Warning
  > GEAR DISAGREE WARNING MESSAGE ON DEPARTURE. RAN QRH MESSAGE CLEARED. RETURNED TO FIELD FLIGHT 4266. FILED CLOSED. FOUND RT MLG UPLOCK TARGET TO BE UNSECURE AND OUT OF RANGE. ADJUSTED AND RESECURED RT MLG UPLOCK TARGET TO WITHIN LIMITS, REF AMM. PERFORMED
- [SDR SWIA2019120946834](https://openairdocs.org/sdr/SWIA2019120946834.md): Line · damaged · Dec 9, 2019 · N429SW · Cndair CL6002B19 · Hydraulic System, Main
  > HYD 1 FAIL AFTER TAKEOFF. COMPLIED WITH QRH PROCEDURE. ON HYD SYNOPTIC PAGE, SYSTEM 1 SHOWED NO QUANTITY, NO TEMP, OR FLOW. PLEASE REFERENCE AML 328199 PLEASE REFERENCE AML 328200THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 20033850 WITH THE FOLLOWING CORR
- [SDR SWIA2019061145967](https://openairdocs.org/sdr/SWIA2019061145967.md): Engine · failed · Jun 7, 2019 · N429SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > DURING CLIMB OUT, LOUD BANG FOLLOWED BY SPIKE IN ITT AND CONSTANT N2 VIB MESSAGE. (FLT#4330) REMOVED AND REPLACED RIGHT ENGINE ASSEMBLY IAW AMM. OPS AND LEAK CHECK GOOD.
- [SDR SWIA2019050145814](https://openairdocs.org/sdr/SWIA2019050145814.md): Structure · dented · Apr 15, 2019 · N429SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > APPROXIMATELY 8EA DENTS OR PREVIOUS BLENDS AT APPROXIMATE FS589-FS605 APPROXIMATE STR 26R TO STR 23R (C-CHECK) RO: 04/28/2019 COMPLIED WITH DENTS REPAIR IAW REO.
- [SDR SWIA2019050145813](https://openairdocs.org/sdr/SWIA2019050145813.md): Panel · corroded · Apr 11, 2019 · N429SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT FLOOR SILL PANEL, FS409.00+128 THRU FS559.00. BETWEEN APPROX RBL36.00 TO APPROX RBL 45.00, AREAS OF CORROSION. (C-CHECK) RO: 04/28/2019 REMOVED CORROSION ON THE RT FLOOR SILL PANEL AT LOCATIONS AT FS441 RBL45 IAW REO. PRESSURE LEAK CHECK GOOD.
- [SDR SWIA2019050145812](https://openairdocs.org/sdr/SWIA2019050145812.md): Door Sill · corroded · Apr 8, 2019 · N429SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ALONG TOP PARTION OF PASSENGER DOOR SILL ANGLE FROM FS 312.00 THRU FS 346.00. (C-CHECK) RO: 04/28/2019 REMOVED AND REPLACED PAX DOOR SILL ANGLE ASSY WITH NEW PAX DOOR SILL ASSEMBLY IAW SRM.
- [SDR SWIA2019050145811](https://openairdocs.org/sdr/SWIA2019050145811.md): Door Sill · corroded · Apr 1, 2019 · N429SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR LOWER FWD AND AFT SILL HAVE SPOTS OF CORROSION. (C-CHECK) RO: 04/28/2019 BLENDED CORROSION ON PAX DOOR STRAP AT LOWER LONGERON IAW SRM AND REO.
- [SDR SWIA2019050145810](https://openairdocs.org/sdr/SWIA2019050145810.md): Doubler · dented · Mar 30, 2019 · N429SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DENT LOCATED JUST AFT OF FS 589.0 JUST BETWEEN STR 21L & STR 22L. (C-CHECK) RO: 04/28/2019 PERFORMED CUT-OUT TO REPAIR AND WET INSTALLED REPAIR DOUBLER TO REPAIR AREA LOCATION ON FUSELAGE FS 589.0 BETWEEN STR 21L & STR 22L IAW SRM. PRESSURIZATION LEAK CHECK OF
- [SDR SWIA2019050145809](https://openairdocs.org/sdr/SWIA2019050145809.md): Skin · corroded · Mar 30, 2019 · N429SW · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT WING PLANK. FUEL TANK ACCESS 650HB HAS CORROSION AND FRETTING DAMAGE. (C-CHECK) RO: 04/28/2019 BLENDED, ROTOPEENED AND REPAIRED WING TANK ACCESS HOLE 650HB IAW SRM AND REO. ALL CHECKS GOOD.
- [SDR SWIA2019050145808](https://openairdocs.org/sdr/SWIA2019050145808.md): Hinge · worn · Mar 27, 2019 · N429SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR HINGE ON DOOR SIDE, PIANO HINGE PIN HOLES ARE WORN OUT OF ROUND AND SCRATCHED INTERNALLY. (C-CHECK) RO: 04/28/2019 REMOVED AND REPLACED THE PAX DOOR HINGE (DOOR SIDE) IAW SRM. PRESSURE CHECK GOOD.
- [SDR SWIA2019050145807](https://openairdocs.org/sdr/SWIA2019050145807.md): Hinge · worn · Mar 27, 2019 · N429SW · Cndair CL6002B19 · Fuselage, Door Hinge
  > PAX DOOR HINGE ON FUSELAGE SIDE, PIANO HINGE PIN HOLES ARE WORN OUT OF ROUND AND SCRATCHED INTERNALLY. (C-CHECK) RO: 04/28/2019 REMOVED AND REPLACED DAMAGED PAX DOOR HINGE (FUSELAGE SIDE) IAW SRM AND REO.
- [SDR SWIA2019050145806](https://openairdocs.org/sdr/SWIA2019050145806.md): Strap · corroded · Mar 24, 2019 · N429SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT SIDE FUSELAGE STRAP AT 559.0 HAS CORROSION.AT APPROX RBL 36. (C-CHECK) RO: 04/28/2019 REMOVED AND REPLACED THE RT STRAP AT FS559 RBL 27 - RBL 42 IAW SRM. ALL CHECKS GOOD.
- [SDR SWIA2019050145805](https://openairdocs.org/sdr/SWIA2019050145805.md): Door Sill · corroded · Mar 24, 2019 · N429SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT SIDE INTERNAL FUSELAGE FLOOR SILL AT APPROX LBL 42 HAS CORROSION IN VARIOUS AREAS FROM FS 559.0 TO 559.0+ 80. (C-CHECK) RO: 04/28/2019 BLENDED OUT CORROSION AT VARIOUS LOCATIONS ON FLOOR SILL AT LBL 42 BETWEEN FS 559.0 TO FS 559.0 + 80 IAW SRM AND REO.
- [SDR SWIA2019050145804](https://openairdocs.org/sdr/SWIA2019050145804.md): Strap · corroded · Mar 24, 2019 · N429SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AT FS 559.0 INTERNAL FUSELAGE LEFT SIDE UPPER STRAP (FLOOR LEVEL) HAS CORROSION. (C-CHECK) RO: 04/28/2019 REMOVED AND INSTALLED NEW LT FLOOR STRAP AT FS559 LBL 27 - LBL 42 IAW SRM. PRESSURE CHECK GOOD.
- [SDR SWIA2019050145803](https://openairdocs.org/sdr/SWIA2019050145803.md): Intercostal · corroded · Mar 23, 2019 · N429SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AVIONICS BAY, BELOW FLOOR BOARD BETWEEN FS 394.0 TO FS FS 409.0 THERE IS EVIDENCE OF CORROSION AT INTERCOSTAL AT STR 27L. (C-CHECK) RO: 04/28/2019 REMOVED AND REPLACED THE LT INTERCOSTAL BETWEEN FS 394.0 AND 409 AT STR 27L IAW SRM. PRESSURE LEAK CHECK GOOD.
- [SDR SWIA2019050145802](https://openairdocs.org/sdr/SWIA2019050145802.md): Intercostal · corroded · Mar 23, 2019 · N429SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AVIONIC BAY BELOW FLOOR BOARD IN BETWEEN FS 349 AND FS 364 INTERCOSTAL HAS EVIDENCE OF CORROSION.AT STR 27R (C-CHECK) RO: 04/28/2019 BLENDED OUT CORROSION FROM INTERCOSTAL AT AVIONIC BAY BELOW FLOOR BOARD IN BETWEEN FS 349 AND FS 364, STR 27R IAW SRM. PRESSURE
- [SDR SWIA2019050145801](https://openairdocs.org/sdr/SWIA2019050145801.md): Intercostal · corroded · Mar 23, 2019 · N429SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AVIONICS BAY BELOW FLOOR BOARD INTERCOSTAL BETWEEN FS 349 AND FS 364 HAS EVIDENCE OF CORROSION AT STR27L. (C-CHECK) RO: 04/28/2019 REMOVED AND REPLACED INTERCOSTAL BETWEEN FS 349.0 AND FS364.0 AT STR27L IAW SRM. ALL CHECKS GOOD
- [SDR SWIA2019050145800](https://openairdocs.org/sdr/SWIA2019050145800.md): Frame · corroded · Mar 23, 2019 · N429SW · Cndair CL6002B19 · Fuselage Main, Frame
  > AT FS 349.0 IN BETWEEN STR 25L AND STR 25R APPROX, THERE IS EVIDENCE OF CORROSION. (C-CHECK) RO: 04/28/2019 REMOVED AND REPLACED FRAME AT FS 349.00 LOWER SECTOR IAW SRM. ALL CHECKS GOOD.
- [SDR SWIA2019050145799](https://openairdocs.org/sdr/SWIA2019050145799.md): Frame · corroded · Mar 23, 2019 · N429SW · Cndair CL6002B19 · Fuselage Main, Frame
  > AT FS 333.0 APPROX IN BETWEEN STR 25L AND STR 25R FRME HAS EVIDENCE OF CORROSION. (C-CHECK) RO: 04/28/2019 REMOVED AND REPLACED LOWER FRAME SECTOR AT FS 333.00 BETWEEN STR 23L AND STR 23R IAW SRM. PRESSURE LEAK CHECK GOOD.
- [SDR SWIA2019050145798](https://openairdocs.org/sdr/SWIA2019050145798.md): Frame · corroded · Mar 23, 2019 · N429SW · Cndair CL6002B19 · Fuselage Main, Frame
  > AT FS 310 AVIONICS BAY BELOW FLOOR BOARD IN APPROX INBETWEEN STR 25L AND STR25R FRAME FLANGE HAS EVIDENCE OF CORROSION. (C-CHECK) RO: 04/28/2019 REMOVED AND REPLACED LOWER FRAME BETWEEN STR 23L AND STR 23R IAW SRM. PRESSURE LEAK CHECK GOOD.
- [SDR SWIA2019050145797](https://openairdocs.org/sdr/SWIA2019050145797.md): Support · cracked · Mar 22, 2019 · N429SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR SUPPORT STRUCTURE FWD TRACK SUPPORT AT FS 578.0 HAS CRACKED ANGLE. (C-CHECK) RO: 04/28/2019 NEW AFT CARGO DOOR FWD TRACK SUPPORT ANGLE INSTALLED IAW SRM.
- [SDR SWIA2019050145796](https://openairdocs.org/sdr/SWIA2019050145796.md): Track · damaged · Mar 22, 2019 · N429SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR FWD SUPPORT TRACK STRUCTURE. U CHANNEL IS DAMAGED. APPROX FS 574.0. (C-CHECK) RO: 04/28/2019 REPAIRED AFT CARGO DOOR FWD SUPPORT TRACK STRUCTURE U CHANNEL IAW REO.
- [SDR SWIA2019050145795](https://openairdocs.org/sdr/SWIA2019050145795.md): Longeron · corroded · Mar 21, 2019 · N429SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > RT SIDE FUSELAGE BELOW FLOOR LEVEL, LONGERON ASSEMBLY JUST BELOW WL 73.50 RBL 42 AT FS 513.00 VERTICAL CHANNEL HAS CORROSION. (C-CHECK) RO: 04/28/2019 REMOVED CORROSION FROM RT SIDE FUSELAGE BELOW FLOOR LEVEL, LONGERON ASSEMBLY JUST BELOW WL 73.50 RBL 42 AT F
- [SDR SWIA2019050145794](https://openairdocs.org/sdr/SWIA2019050145794.md): Skin · corroded · Mar 19, 2019 · N429SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > EXTERIOR BOTTOM SKIN AT APPROX. FS 559+112 EITHER SIDE OF BL 0 HAS SEVERAL AREAS OF CORROSION AROUND FASTENER HOLES FOR FAIRING 195BB AS WELL AS A DETERIORATED SEALING PAD. (C-CHECK) RO: 04/28/2019 REMOVED CORROSION FROM EXTERIOR BOTTOM SKIN AT APPROX. FS 559+
- [SDR SWIA2019050145793](https://openairdocs.org/sdr/SWIA2019050145793.md): Skin · corroded · Mar 19, 2019 · N429SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > EXTERIOR BOTTOM SKIN FROM APPROX. FS559.0 TO FS559.0+112 AND SEVERAL INCHES EITHER SIDE OF BL 0 HAS MULTIPLE AREAS OF CORROSION AROUND FASTENERS AS WELL AS AROUND BELLY DRAINS. (C-CHECK) RO: 04/28/2019 REMOVED CORROSION UNDER FASTENERS HEAD APPROXIMATELY FROM
- [SDR SWIA2019050145792](https://openairdocs.org/sdr/SWIA2019050145792.md): Window · delaminated · Mar 18, 2019 · N429SW · Cndair CL6002B19 · Flight Compartment Windows
  > CO-PILOTS SIDE WINDOW HAS INDICATIONS OF DELAMINATION ALONG ITS BOTTOM EDGE. (C-CHECK) RO: 04/28/2019REMOVED AND REPLACED COPILOT'S SIDE WINDOW IAW AMM. OPS CHECK GOOD AT THIS TIME.
- [SDR SWIA2019050145791](https://openairdocs.org/sdr/SWIA2019050145791.md): Plate · corroded · Mar 17, 2019 · N429SW · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR PROTECTOR PLATE HAS CORROSION BEHIND SCREW HOLES. (C-CHECK) RO: 04/28/2019 RECEIVED AND INSTALLED NEW PROTECTOR PLATE IAW SRM.
- [SDR SWIA2019050145790](https://openairdocs.org/sdr/SWIA2019050145790.md): Fitting · corroded · Mar 17, 2019 · N429SW · Cndair CL6002B19 · Ailerons
  > RIGHT AILERON. OUTBOARD PCU, FORK ATTACHMENT CORRODED. (C-CHECK) RO: 04/28/2019 REMOVED AND INSTALLED NEW SERVICEABLE RT AILERON O/B PCU IAW AMM. RIGGING AND OPERATIONAL TESTS GOOD.
- [SDR SWIA201743082](https://openairdocs.org/sdr/SWIA201743082.md): Skin · damaged · Feb 10, 2017 · N429SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > MULTIPLE CREASES ON AFT FUSELAGE SKIN PANEL FROM FS 640 - 700, BETWEEN STRINGERS 20 - 22L. REPAIRED IAW REO.
- [SDR SWIA201743081](https://openairdocs.org/sdr/SWIA201743081.md): Intercostal · corroded · Feb 5, 2017 · N429SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT INTERCOSTAL AT DD4 HAS CORROSION. REPLACED PAX DOOR INTERCOSTAL IAW REO. PRESSURIZATION LEAK CHECK GOOD.
- [SDR SWIA201743080](https://openairdocs.org/sdr/SWIA201743080.md): Intercostal · corroded · Feb 5, 2017 · N429SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL HAS CORROSION AT DD3 CENTER. REPLACED PAX DOOR INTERCOSTAL IAW REO. PRESSURIZATION LEAK CHECK GOOD
- [SDR SWIA201743084](https://openairdocs.org/sdr/SWIA201743084.md): Intercostal · corroded · Feb 2, 2017 · N429SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL ABOVE PRESSURE VALVE OPENING HAS CORROSION. INSTALLED PAX DOOR INTERCOSTAL IAW REO. PRESSURE CHECK GOOD.
- [SDR SWIA201743079](https://openairdocs.org/sdr/SWIA201743079.md): Threshold · corroded · Feb 2, 2017 · N429SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR THRESHOLD HAS CORROSION. INSTALLED A NEW SERVICE DOOR THRESHOLD PANEL IAW SRM.
- [SDR SWIA201743083](https://openairdocs.org/sdr/SWIA201743083.md): Skin · dented · Feb 1, 2017 · N429SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > MULTIPLE DENTS ON THE LT FUSELAGE 12 TO 14 INCHES AFT OF ICE DETECTOR. PERFORMED REPAIR TO FUSELAGE SKIN BETWEEN BS 235 AND 265, STRINGER 16L IAW REO.
- [SDR SWIA201540892](https://openairdocs.org/sdr/SWIA201540892.md): Skin · corroded · Feb 26, 2015 · N429SW · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT WING PLANK, TANK ACCESS CUT OUT RIM AT 510 AB, HAS PITTING CORROSION ON LOWER SURFACE, INBD AND OTBD AREAS AS MARKED, C-CHECK, RO 3/12/15, COMPLIED WITH CORROSION REMOVAL, ROTO PEEN AND RESTORED FINISH TO TANK CUTOUT, RIM AT 510AB AROUND ENTIRE CIRCUMFERE
- [SDR SWIA201540891](https://openairdocs.org/sdr/SWIA201540891.md): Skin · dented · Feb 26, 2015 · N429SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > AFT FUSELAGE EXTERIOR SKIN DENTED FORWARD OF FS700.0 BETWEEN STR 16L AND 17L. C-CHECK, RO 3/12/15. INSTALLED NEW REPAIR DOUBLER, PN 601R-53-61-770-1, REF CRJ 200, REO. WEIGHT OF MATERIAL REMOVED 1.84 LBS, WEIGHT OF NEW REPAIR DOUBLER 2.26 LBS WEIGHT ADDED.
- [SDR SWIA201540893](https://openairdocs.org/sdr/SWIA201540893.md): Fairing · chafed · Feb 21, 2015 · N429SW · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT STUB FAIRING CHAFED, C-CHECK, RO 3/12/15, RT FLAP STUB FAIRING CHAFE OUT OF LIMITS IAW REO. REPLACED RT FLAP STUB FAIRING IAW DWG AND SRM.
- [SDR SWIA201540895](https://openairdocs.org/sdr/SWIA201540895.md): Web · cracked · Feb 20, 2015 · N429SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SUSPECTED CRACK IN RT TRU BAY AFT AREA, ON FLOOR WEB AT FS 193, APPROXIMATELY RBL 29, C-CHECK RO 3/12/15, REPAIRED CRACK IN RT TRU BAY FLOOR AREA AT FS 193, RBL 29, REF CRJ 200 REO.32LBS, WEIGHT ADDED COMPLETED ST 51-900-1003.
- [SDR SWIA201540894](https://openairdocs.org/sdr/SWIA201540894.md): Floor Panel · cracked · Feb 20, 2015 · N429SW · Cndair CL6002B19 · Fuselage Floor Panel
  > SUSPECTED CRACK IN LEFT TRU BAY AFT AREA, ON FLOOR WEB AT FS 193, APPROXIMATELY LBL 29, C-CHECK RO 3/12/15, NDT VERIFIED CRACK. REPAIRED LT TRU BAY FLOOR WEB AT FS 193, LBL 29, REF STS EA. COMPLIED WITH ATTACHED ST 51-900-1003.
- [SDR SWIA201438378](https://openairdocs.org/sdr/SWIA201438378.md): Smoke Detector · false indication · Jun 23, 2014 · N429SW · Cndair CL6002B19 · Smoke Detection
  > RECEIVED TWO ERRONEOUS MOMENTARY SMOKE CARGO WARNING MESSAGES. ONE DURING CRUISE AND ONE DURING TAXI TO THE GATE. NO SMOKE DETECTED BY F/A OR GROUND CREW. R & R BOTH CARGO SMOKE DETECTORS IAW AMM.
- [SDR SWIA201438298](https://openairdocs.org/sdr/SWIA201438298.md): Connector · broken · Jun 22, 2014 · N429SW · Cndair CL6002B19 · Light System Wiring
  > EMERGENCY EXIT SIGN DOES NOT ILLUMINATE. SIGN IS LOCATED NEAR MAIN CABIN DOOR. FOUND A WIRE CONNECTOR ON THE MAIN CABIN DOOR EMERGENCY EXIT SIGN BROKEN. INSTALLED NEW CONNECTOR IAW ESPM. OPS CHECKS GOOD.
- [SDR SWIA201437989](https://openairdocs.org/sdr/SWIA201437989.md): Light · inoperative · Jun 4, 2014 · N429SW · Cndair CL6002B19 · Emergency Lighting
  > LEFT EXTERNAL AFT EMERGENCY LIGHT INOPERATIVE. SERVICE, R & R EXTERNAL EMERGENCY LIGHT IAW AMM.
- [SDR SWIA201334748](https://openairdocs.org/sdr/SWIA201334748.md): Light · inoperative · Sep 25, 2013 · N429SW · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY POD LIGHT INOPERATIVE. FLT#7392 RELAMPED, PN ON OFF 1317.
- [SDR SWIA201334442](https://openairdocs.org/sdr/SWIA201334442.md): Light · inoperative · Sep 1, 2013 · N429SW · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHT BY SERVICE DOOR BURNED OUT. FLT#4769 RELAMPED. PN ON OFF 1317.
- [SDR SWIA201333346](https://openairdocs.org/sdr/SWIA201333346.md): Bulkhead · cracked · Apr 27, 2013 · N429SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > THE 202 BULKHEAD IS CRACKED AT PARK BRAKE ROD, FWD HYDRAULIC BAY. (C-CHECK) REPAIRED LEFT FS 202 PRESSURE BULKHEAD IAW REO.
- [SDR SWIA201333348](https://openairdocs.org/sdr/SWIA201333348.md): Cargo Track · corroded · Apr 17, 2013 · N429SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO SEAT RAIL AT FS 559+85 TO FS 559+96 RBL 9 HAS CORROSION AROUND FASTENERS. (C-CHECK) REPLACED CORRODED SEAT RAIL WITH NEW FABRICATED RAIL P/N 601R-53-00-485-1 AT RBL 9 FS 559 +85 TO FS 559+96 IAW REO.
- [SDR SWIA201333347](https://openairdocs.org/sdr/SWIA201333347.md): Cargo Track · corroded · Apr 17, 2013 · N429SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO SEAT RAIL AT FS 559+96 TO FS 559+115 RBL 9 HAS CORROSION AROUND FASTENERS. (C-CHECK) REPLACED CORRODED SEAT RAIL WITH NEW FABRICATED RAIL P/N 601R-53-00-485-1 AT RBL 9 FS 559 +96 TO FS 559+115 IAW REO.
- [SDR SWIA201333349](https://openairdocs.org/sdr/SWIA201333349.md): Bulkhead · cracked · Apr 16, 2013 · N429SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621 BULKHEAD HAS A CRACK AT THE TOP OF THE LINTEL FITTING. (C-CHECK) REPAIRED LINTEL CRACK ON THE 621 BULKHEAD IAW REO.
- [SDR SWIA201231723](https://openairdocs.org/sdr/SWIA201231723.md): Light · inoperative · Sep 9, 2012 · N429SW · Cndair CL6002B19 · Emergency Lighting
  > NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4501) RELAMPED EMERGENCY LIGHT.
- [SDR SWIA201231319](https://openairdocs.org/sdr/SWIA201231319.md): Light · inoperative · Jul 19, 2012 · N429SW · Cndair CL6002B19 · Emergency Lighting
  > ROW 13 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4680) RELAMPED EMERGENCY LIGHT.

Next page: https://openairdocs.org/deregistered/N429SW-2023-07-30/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 = 'N429SW' AND deregistration_id = 'N429SW-2023-07-30'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N429SW-2023-07-30/reports

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