# Service difficulty reports: N558GJ A list on [N558GJ](https://openairdocs.org/aircraft/N558GJ.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 · 64 reports - [SDR SWIA2026032675574](https://openairdocs.org/sdr/SWIA2026032675574.md): Warning Message · illuminated · Mar 26, 2026 · N558GJ · Cndair CL6002C11 · Landing Gear Retraction/Extension System > GEAR DISAGREE WARNING UPON GEAR UP RETRACTION ASSOCIATED WITH A PROX SYSTEM FAULT 1 STATUS MESSAGE. QRH RESOLVED THE ISSUE AND MESSAGES CLEARED AND GEAR INDICATED DOWN 3 GREEN (FLIGHT 5610) REFERENCE CP 31990225 (R/R PX08 NLG CENTERING PROXIMITY SENSOR TARGET - [SDR SWIA2026032475567](https://openairdocs.org/sdr/SWIA2026032475567.md): Sensor · faulted · Mar 24, 2026 · N558GJ · Cndair CL6002C11 · Landing Gear Position and Warning > GEAR DISAGREE ON TAKEOFF. GEAR DID NOT COME UP. FLIGHT 5428, WIRING CHKD LANDING GEAR CONTROL HANDLE, LANDING GEAR SELECTOR VALVE & PSEU, ADJUSTED OF PX37 BRACKET HARDWARE. RIGGED SENSORS PX24, PX11, & PX37, INSPECTED NLG AFT DOOR DRIVE BRACKET. REPLACED - [SDR SWIA2026032175565](https://openairdocs.org/sdr/SWIA2026032175565.md): Proximity Sensor · faulted · Mar 21, 2026 · N558GJ · Cndair CL6002C11 · Landing Gear Position and Warning > GEAR DISAGREE UPON GEAR UP LEVER BEING PLACED IN THE UP POSITION. (FLIGHT 5565) TROUBLESHOT GREAR DISAGREE REFERENCING APPLICABLE STEPS OF FIM 32-21-00. FOUND NLG PROXIMITY SENSOR PX37 SHOWING FAR (UNREADABLE). ATTEMPTED TO ADJUST SENSOR PX37 REFERENCING A - [SDR SWIA2026013175106](https://openairdocs.org/sdr/SWIA2026013175106.md): Skin · mechanic error · Jan 31, 2026 · N558GJ · Cndair CL6002C11 · Fuselage Main, Plate/Skin > DURING STARLINK INSTALLATION A STRINGER RIVET WAS MISDRILLED AT FWD RIGHT SKIN, STRINGER 2R, BS 437. THIS HAS BEEN DETERMINED TO BE A MAJOR REPAIR, COMPLIED WITH MAJOR REPAIR OF FWD RIGHT SKIN, STRINGER 2R, BS 437 IAW STARLINK EO SPX-00011260. COMPLIED WITH T - [SDR SWIA20251209009](https://openairdocs.org/sdr/SWIA20251209009.md): Stringer · corroded · Sep 9, 2025 · N558GJ · Cndair CL6002C11 · Fuselage Main, Longeron/Stringer > WHILE REMOVING STRINGER 21R FOUND CORROSION ON THE STRINGER CIRCUMFERENTIAL JOINT SPLICE AT BS 477. REPLACED STRINGER 21R JOINT SPLICE IAW SRM 51-40-11-001-001-A01, & 51-42-06-001-001-A01, REV 38. - [SDR SWI2025F01820](https://openairdocs.org/sdr/SWI2025F01820.md): Stringer · corroded · Aug 16, 2025 · N558GJ · Cndair CL6002C11 · Fuselage Main, Longeron/Stringer > STRINGER 20R FOUND TO BE CORRODED BETWEEN BS 319.70 - 333, BEHIND ELECTRICAL CONNECTOR BRACKET. REMOVED THE STRINGER IAW SRM 51-42-06-001-001-A01, REV OA, AND 51-42-21-001-001-A01, REV OA. FABRICATED LOCATED AND DRILLED A NEW STRINGER IAW DRAWING SH670-32428 - [SDR SWIA2025120900816](https://openairdocs.org/sdr/SWIA2025120900816.md): Frame · no discrepancy · Aug 16, 2025 · N558GJ · Cndair CL6002C11 · Standard Practices/Structures > FRAME BS 319 BETWEEN STGR 18L - STGR 21L REQUIRES REMOVAL TO FOM. REMOVED AND REINSTALLED FS319 STUB FRAME 18L-21L IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01AND 51-25-16-001-001-A01 REV 38. - [SDR SWIA2025120900811](https://openairdocs.org/sdr/SWIA2025120900811.md): Stringer Splice · corroded · Aug 11, 2025 · N558GJ · Cndair CL6002C11 · Fuselage Main, Longeron/Stringer > FOUND CORROSION ON STRINGER SPLICE 23R, BS 333. REPLACED THE STRINGER SLICE IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 53-00-00-101-001-A01, 51-25-16-001-001-A01, AND 51-23-00-001-001-A01 REV 38. - [SDR SWIA202512090810](https://openairdocs.org/sdr/SWIA202512090810.md): Stringer · corroded · Aug 10, 2025 · N558GJ · Cndair CL6002C11 · Fuselage Main, Longeron/Stringer > STRINGER 24R FOUND CORRODED BETWEEN BS 349 TO 364. REPAIRED THE STRINGER IAW SRM 51-23-00-001-001-A01, 51-24-36-001-001-A01, 51-25-06-001-001-A01, 51-25-16-001-001-A01, 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-20-001-001-A01, 51-42-21-001-001-A01, 5 - [SDR SWIA2025120900805](https://openairdocs.org/sdr/SWIA2025120900805.md): Support Plate · corroded · Aug 5, 2025 · N558GJ · Cndair CL6002C11 · Fuselage Miscellaneous Structure > CORROSION FOUND ON SUPPORT PLATE AT BS 333, S20R. REPLACED SUPPORT PLATE IAW SRM 51-40-11-001-001-A01, 51-24-36-001-001-A01, AND 51-42-21-001-001-A01, REV 38. - [SDR SWI2025F01810](https://openairdocs.org/sdr/SWI2025F01810.md): Skin · dented · Jul 30, 2025 · N558GJ · Cndair CL6002C11 · Fuselage Main, Plate/Skin > FUSELAGE SKIN HAS PROTRUDING DENTS AT FS 299 BETWEEN STRS 20R AND 21R. REPAIRED FUSELAGE SKIN FS299 STGR 20R-21R IAW REO# 670-53-21-2667 REV - AND SRM 51-23-00-001-001-A01 REV 38 - [SDR SWIA202512090730](https://openairdocs.org/sdr/SWIA202512090730.md): Intercostal · corroded · Jul 30, 2025 · N558GJ · Cndair CL6002C11 · Passenger/Crew Doors > PAX DOOR AFT DD5 INTERCOSTAL FOUND TO BE CORRODED, REQUIRES REPLACEMENT. REPLACED THE PAX DOOR AFT DD5 INTERCOSTAL IAW SRM 51-42-06-001-001-A01, AND 51-40-11-01-001-001-A01, REV 38. - [SDR SWI2025F01819](https://openairdocs.org/sdr/SWI2025F01819.md): Frame · no discrepancy · Jul 29, 2025 · N558GJ · Cndair CL6002C11 · Standard Practices/Structures > STRUCTURES ACCESS FOR STRINGER 23R BETWEEN BS 333 TO 379. REMOVED AND REINSTALLED FRAME AT BS 333 STRINGER 25R IAW SRM 53-00-06-201-006-A01, 51-42-21-001-001-A01, AND 51-42-06-001-001-A01, REV 38 - [SDR SWIA2025120900729](https://openairdocs.org/sdr/SWIA2025120900729.md): Former · corroded · Jul 29, 2025 · N558GJ · Cndair CL6002C11 · Passenger/Crew Doors > PAX DOOR FORMER,FS329.41, BETWEEN DD5 AND DD6 FOUND BE CORRODED REQUIRE REPLACEMENT (C-CHECK RO 12/09/2025)INSTALLED PAX DOOR NEW SERVICEABLE FORMER PN 601R318078-3 AT FS 329.41 IAW CRJ 550 SRM 51-42-06-001-001-A01 AND 51-40-11-001-001-A01 REV 38 JUL 25/202 - [SDR SWI2025F01818](https://openairdocs.org/sdr/SWI2025F01818.md): Frame · no discrepancy · Jul 25, 2025 · N558GJ · Cndair CL6002C11 · Standard Practices/Structures > FRAME 469 REQUIRES REMOVAL FOR STRINGER REPAIRS. (C-CHECK RO 12/09/2025)REMOVED AND REINSTALLED/SPLICED FRAME AT FS469 MHIRJ REO# 670-53-21-2665 REV. -- DATED 2025-09-15 AND CRJ 550 SRM 51-42-20-001-001-A01 AND 51-42-06-001-001-A01 REV 38 JUL 25/2020. REFERE - [SDR SWIA2025120900725](https://openairdocs.org/sdr/SWIA2025120900725.md): Frame · no discrepancy · Jul 25, 2025 · N558GJ · Cndair CL6002C11 · Standard Practices/Structures > FRAME BS 295 REQUIRES REMOVAL FOR AVI BAY STRINGER REPLACEMENT. INSTALLED FRAME AND SPLICE IAW SRM 53-00-06-201-A03, SRM 51-42-21-001-001-A01, 51-42-06-001-001-A01, 51-25-16-001-001-A01, 51-25-06-001-001-A01, 51-23-00-001-001-A01, REV 38. AND REO 670-53-21-26 - [SDR SWIA2025120900722](https://openairdocs.org/sdr/SWIA2025120900722.md): Stringer Splice · corroded · Jul 22, 2025 · N558GJ · Cndair CL6002C11 · Fuselage Main, Longeron/Stringer > FOUND EVIDENCE OF CORROSION ON STRINGER SPLICE 21L, BS 333. REMOVED THE STRINGER SPLICE, BS 333 IAW SRM 51-42-06-001-001-A01, REV OA. INSTALLED THE STRINGER SPLICE IAW SRM 51-42-06-001-001-A01, REV OA. - [SDR SWI2025F01809](https://openairdocs.org/sdr/SWI2025F01809.md): Intercostal · corroded · Jul 21, 2025 · N558GJ · Cndair CL6002C11 · Passenger/Crew Doors > PAX DOOR INTERCOSTAL DD6 CORRODED BETWEEN BS 320 AND 338. REPLACED PAX DOOR INTERCOSTAL IAW SRM 51-40-11-001-001-A01, AND 51-42-06-001-001-A01, REV 38. - [SDR SWI2025F01808](https://openairdocs.org/sdr/SWI2025F01808.md): Intercostal · corroded · Jul 21, 2025 · N558GJ · Cndair CL6002C11 · Passenger/Crew Doors > PAX DOOR INTERCOSTAL DD5 CORRODED BETWEEN BS 311.75 AND 320. INSTALLED NEW SERVICEABLE FWD DD5 IAW SRM 51-42-06-001-001-A01, REV 38 AND REO 670-52-11-1492, REV -. - [SDR SWI2025F01807](https://openairdocs.org/sdr/SWI2025F01807.md): Former · corroded · Jul 21, 2025 · N558GJ · Cndair CL6002C11 · Passenger/Crew Doors > PAX DOOR AFT FORMER AT FS347.27 CORRODED BETWEEN DD4 AND DD7. REPLACED PAX DOOR AFT FORMER AT BS 347.27 IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND 51-42-13-001-001-A01 REV 38. - [SDR SWI2025F01806](https://openairdocs.org/sdr/SWI2025F01806.md): Former · corroded · Jul 21, 2025 · N558GJ · Cndair CL6002C11 · Passenger/Crew Doors > PAX DOOR FWD FORMER BS 311.75 BETWEEN DD4 AND DD7 CORRODED. REMOVED AND REPLACED PAX DOOR FWD FORMER IAW SRM 51-42-06-001-001-A01, AND 51-42-21-001-001-A01, REV 38. - [SDR SWIA202512090721](https://openairdocs.org/sdr/SWIA202512090721.md): Stringer · corroded · Jul 21, 2025 · N558GJ · Cndair CL6002C11 · Fuselage Main, Longeron/Stringer > EVIDENCE OF CORROSION FOUND ON STRINGER 20R BETWEEN BS 280 AND 295. INSTALLED STRINGER 20R FROM BS 280 TO 319 IAW SRM 51-42-06-001-001-A01, & SRM 51-42-21-001-001-A01, REV 38. - [SDR SWIA2025120900720](https://openairdocs.org/sdr/SWIA2025120900720.md): Floor Support · corroded · Jul 20, 2025 · N558GJ · Cndair CL6002C11 · Fuselage Miscellaneous Structure > LBL 9 FLOOR SUPPORT IS CORRODED BETWEEN BS 863 AND 879 ON THE UPPER INBD FLANGE. REMOVED CORROSION BY BLENDING IAW REO 670-53-51-353, REV -. COMPLETED TASK CARD 51-900-1002- SKY. - [SDR SWI2025F01790](https://openairdocs.org/sdr/SWI2025F01790.md): Floorbeam · corroded · Jul 19, 2025 · N558GJ · Cndair CL6002C11 · Fuselage Main, Floor Beam > RBL 9 FLOORBEAM IS CORRODED AT BS 661, ON THE UPPER INBD FLANGE. COMPLIED WITH REO 670-53-31-1067, REV -. - [SDR SWI2025F01789](https://openairdocs.org/sdr/SWI2025F01789.md): Floor Support · corroded · Jul 19, 2025 · N558GJ · Cndair CL6002C11 · Fuselage Miscellaneous Structure > RBL 9 FLOOR SUPPORT IS CORRODED BETWEEN BS 469 & 485 ON THE UPPER INBD FLANGE. COMPLIED WITH REO 670-53-31-1066 REV-. - [SDR SWIA20250719](https://openairdocs.org/sdr/SWIA20250719.md): Floor Support · corroded · Jul 19, 2025 · N558GJ · Cndair CL6002C11 · Fuselage Miscellaneous Structure > LBL 9 FLOOR SUPPORT IS CORRODED ON THE UPPER INBD FLANGE BETWEEN BS 645 & 693. REPAIRED THE FLOOR SUPPORT ON THE UPPER FLANGE IAW REO 670-53-31-1068 REV-. COMPLETED TASK CARD 51-900-1003-SKY. - [SDR SWIA2025120900717](https://openairdocs.org/sdr/SWIA2025120900717.md): Intercostal · corroded · Jul 17, 2025 · N558GJ · Cndair CL6002C11 · Fuselage Miscellaneous Structure > FOUND CORROSION ON INTERCOSTAL AT STRINGER 20R BETWEEN BS 349-364. UPON FURTHER INVESTIGATION FOUND INSTERCOSTAL AT STGR 20R BETWEEN FS349-FS364 TO HAVE DAMAGE IN MORE THAN ONE ELEMENT AT A GIVEN CROSSSECTION INSTERCOSTAL IS OUT OF LIMITS 100% MATERIAL LOSS - [SDR SWIA202512090716](https://openairdocs.org/sdr/SWIA202512090716.md): Antenna · corroded · Jul 16, 2025 · N558GJ · Cndair CL6002C11 · Navigation System > ADF ANTENNA HAS CORROSION AROUND FASTENER HOLES. REPAIRED AREA AROUND ADF ANTENNA FASTENER HOLES IAW REO 670-53-31-1065 REV -. INSTALLED 4EA LOCK FASTENERS IAW SRM 51-42-21-001-001-A01, REV 38. - [SDR SWI2025F01800](https://openairdocs.org/sdr/SWI2025F01800.md): Stringer · corroded · Jul 14, 2025 · N558GJ · Cndair CL6002C11 · Fuselage Main, Longeron/Stringer > STRINGER 20R IS CORRODED BETWEEN BS 437 TO 453. REPAIRED THE STGR IAW REO 670-53-21-2662, REV -. - [SDR SWI2025F01799](https://openairdocs.org/sdr/SWI2025F01799.md): Stringer · corroded · Jul 14, 2025 · N558GJ · Cndair CL6002C11 · Fuselage Main, Longeron/Stringer > STRINGER 23R CORRODED BETWEEN BS 364 TO 379. INSTALLED NEW SERVICEABLE STRINGER BETWEEN BS 333 - 379 IAW SRM 51-42-06-001-001-A01, AND 51-40-11-001-001-A01, REV 38. - [SDR SWI2025F01798](https://openairdocs.org/sdr/SWI2025F01798.md): Splice · corroded · Jul 14, 2025 · N558GJ · Cndair CL6002C11 · Fuselage Main, Frame > H SPLICE AT BS 581, STRINGER 26L IS CORRODED. COMPLIED WITH REO 670-53-31-1064, REV-. INSTALLED SIX JO-BOLTS IAW SRM 51-42-22-001-001-A01. - [SDR SWI2025F01797](https://openairdocs.org/sdr/SWI2025F01797.md): Intercostal · corroded · Jul 14, 2025 · N558GJ · Cndair CL6002C11 · Passenger/Crew Doors > PAX DOOR INTERCOSTAL IS CORRODED BETWEEN BS 333 TO 349, STRINGER 20L. INSTALLED THE INTERCOSTAL BETWEEN IAW SRM 51-42-06-001-001-A01. - [SDR SWI2025F01796](https://openairdocs.org/sdr/SWI2025F01796.md): Stringer · corroded · Jul 14, 2025 · N558GJ · Cndair CL6002C11 · Fuselage Main, Longeron/Stringer > STRINGER 18L IS CORRODED BETWEEN BS 319 TO 333. REMOVED CORROSION FROM STRINGER 19L IAW SRM 51-21-06-001-001-A01, FOUND TO BE OUT OF LIMITS DUE TO DAMAGE BEING IN MORE THAN ONE ELEMENT AT A GIVEN CROSS SECTION IAW SRM 53-21-03-101-001-A01. INSTALLED A NEW S - [SDR SWI2025F01795](https://openairdocs.org/sdr/SWI2025F01795.md): Stringer · corroded · Jul 14, 2025 · N558GJ · Cndair CL6002C11 · Fuselage Main, Longeron/Stringer > STRINGER 21R IS CORRODED BETWEEN BS 409 TO 421. INSTALLED STRINGER 21R FROM BS 394 - 477 IAW SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01, 51-42-21-001-001-A01, 53-21-03-101-002-A01, AND 53-21-03-101-006-A01, REV 38. - [SDR SWI2025F01794](https://openairdocs.org/sdr/SWI2025F01794.md): Stringer · corroded · Jul 14, 2025 · N558GJ · Cndair CL6002C11 · Fuselage Main, Longeron/Stringer > STRINGER 20R CORRODED BETWEEN BS 349 TO 364. REPAIRED THE STRINGER IAW REO 670-53-21-2661 REV-, SRM 51-21-06-001-001-A01, 51-21-16-001-001-A01, 51-42-02-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND 53-21-03-101-006-A01, REV 38. - [SDR SWIA2025120900714](https://openairdocs.org/sdr/SWIA2025120900714.md): Stringer · corroded · Jul 14, 2025 · N558GJ · Cndair CL6002C11 · Fuselage Main, Longeron/Stringer > STRINGER 21R IS CORRODED BETWEEN BS 280 TO 295. REPLACED THE STRINGER 21R, BS 280-333 IAW SRM 51-42-21-001-001-A01, 51-40-11-001-001-A01, 51-42-20-001-001-A01, 51-42-06-001-001-A01, AND 53-21-03-101-001-A01, REV 38. - [SDR SWI2025F01805](https://openairdocs.org/sdr/SWI2025F01805.md): Slider · chafed · Jul 12, 2025 · N558GJ · Cndair CL6002C11 · Engine Thrust Reverser > RIGHT TRANSCOWL LOWER OTBD SLIDER IS CHAFED. RECEIVED AND COMPLIED WITH ALL STEPS OF REO 670-54-21-1751 REV -. - [SDR SWI2025F01804](https://openairdocs.org/sdr/SWI2025F01804.md): Slider · chafed · Jul 12, 2025 · N558GJ · Cndair CL6002C11 · Engine Thrust Reverser > RIGHT TRANSCOWL UPPER INBD SLIDER IS CHAFED. RECEIVED AND COMPLIED WITH ALL STEPS OF REO 670-54-21-1750 REV -. - [SDR SWI2025F01803](https://openairdocs.org/sdr/SWI2025F01803.md): Slider · chafed · Jul 12, 2025 · N558GJ · Cndair CL6002C11 · Engine Thrust Reverser > RIGHT TRANSCOWL LOWER INBD SLIDER IS CHAFED. RECEIVED AND COMPLIED WITH ALL STEPS OF REO 670-54-21-1751 REV -. - [SDR SWI2025F01802](https://openairdocs.org/sdr/SWI2025F01802.md): Slider · chafed · Jul 12, 2025 · N558GJ · Cndair CL6002C11 · Engine Thrust Reverser > RIGHT TRANSCOWL UPPER OB SLIDER IS CHAFED. RECEIVED AND COMPLIED WITH ALL STEPS OF REO 670-54-21-1750 REV -. - [SDR SWI2025F01801](https://openairdocs.org/sdr/SWI2025F01801.md): Slider · chafed · Jul 12, 2025 · N558GJ · Cndair CL6002C11 · Engine Thrust Reverser > LEFT TRANSCOWL LOWER OTBD SLIDER IS CHAFED. RECEIVED AND COMPLIED WITH ALL STEPS OF REO 670-54-21-1749 REV -. - [SDR SWIA202512090712](https://openairdocs.org/sdr/SWIA202512090712.md): Slider · chafed · Jul 12, 2025 · N558GJ · Cndair CL6002C11 · Engine Thrust Reverser > LEFT TRANSCOWL LOWER IB SLIDER IS CHAFED. RECEIVED AND COMPLIED WITH ALL STEPS OF REO 670-54-21-1749 REV -. - [SDR SWI2025F01817](https://openairdocs.org/sdr/SWI2025F01817.md): Slat Track · chafed · Jul 8, 2025 · N558GJ · Cndair CL6002C11 · Leading Edge Devices > RIGHT SLAT TRACK 2-3 IS CHAFED. REPAIRED RT SLAT TRACK 2-3 IAW REO 670-57-42-2151, REV -. - [SDR SWI2025F01816](https://openairdocs.org/sdr/SWI2025F01816.md): Slat Track · chafed · Jul 8, 2025 · N558GJ · Cndair CL6002C11 · Leading Edge Devices > RIGHT SLAT TRACK 1-3 IS CHAFED. REPAIRED THE RT SLAT TRACK 1-3 IAW REO 670-57-42-2149, REV -. - [SDR SWI2025F01815](https://openairdocs.org/sdr/SWI2025F01815.md): Slat Track · chafed · Jul 8, 2025 · N558GJ · Cndair CL6002C11 · Leading Edge Devices > RIGHT SLAT TRACK 1-1 IS CHAFED. REPAIRED RT SLAT TRACK 1-1 IAW REO 670-57-42-2148, REV -. - [SDR SWI2025F01814](https://openairdocs.org/sdr/SWI2025F01814.md): Slat Track · chafed · Jul 8, 2025 · N558GJ · Cndair CL6002C11 · Leading Edge Devices > LEFT SLAT TRACK 1-3 IS CHAFED. COMPLIED WITH REO 670-57-42-2145, REV -. - [SDR SWI2025F01813](https://openairdocs.org/sdr/SWI2025F01813.md): Slat Track · chafed · Jul 8, 2025 · N558GJ · Cndair CL6002C11 · Leading Edge Devices > LEFT SLAT TRACK 1-1 IS CHAFED. COMPLIED WITH REO 670-57-42-2144, REV -. - [SDR SWI2025F01812](https://openairdocs.org/sdr/SWI2025F01812.md): Slat Track · chafed · Jul 8, 2025 · N558GJ · Cndair CL6002C11 · Leading Edge Devices > RIGHT SLAT TRACK 2-1 IS CHAFED. REPAIRED THE RT SLAT TRACK 2-1 IAW REO 670-57-42-2150 REV -. - [SDR SWI2025F01811](https://openairdocs.org/sdr/SWI2025F01811.md): Slat Track · chafed · Jul 8, 2025 · N558GJ · Cndair CL6002C11 · Leading Edge Devices > LEFT SLAT TRACK 2-3 IS CHAFED. COMPLIED WITH REO 670-57-42-2147 REV -. - [SDR SWIA202512090708](https://openairdocs.org/sdr/SWIA202512090708.md): Slat Track · chafed · Jul 8, 2025 · N558GJ · Cndair CL6002C11 · Leading Edge Devices > LEFT SLAT TRACK 2-1 IS CHAFED. COMPLIED WITH REO 670-57-42-2146 REV-. Next page: https://openairdocs.org/aircraft/N558GJ/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 = 'N558GJ' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N558GJ/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.