N558GJ

Service difficulty reports · 64

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

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR SWIA2026032675574Warning Message · illuminatedGEAR 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 TARGETMar 26, 2026 · N558GJ · Cndair CL6002C11 · Landing Gear Retraction/Extension SystemSDR SWIA2026032475567Sensor · faultedGEAR 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 Mar 24, 2026 · N558GJ · Cndair CL6002C11 · Landing Gear Position and WarningSDR SWIA2026032175565Proximity Sensor · faultedGEAR 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 AMar 21, 2026 · N558GJ · Cndair CL6002C11 · Landing Gear Position and WarningSDR SWIA2026013175106Skin · mechanic errorDURING 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 TJan 31, 2026 · N558GJ · Cndair CL6002C11 · Fuselage Main, Plate/SkinSDR SWIA20251209009Stringer · corrodedWHILE 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.Sep 9, 2025 · N558GJ · Cndair CL6002C11 · Fuselage Main, Longeron/StringerSDR SWI2025F01820Stringer · corrodedSTRINGER 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 SH670-32428Aug 16, 2025 · N558GJ · Cndair CL6002C11 · Fuselage Main, Longeron/StringerSDR SWIA2025120900816Frame · no discrepancyFRAME 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.Aug 16, 2025 · N558GJ · Cndair CL6002C11 · Standard Practices/StructuresSDR SWIA2025120900811Stringer Splice · corrodedFOUND 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.Aug 11, 2025 · N558GJ · Cndair CL6002C11 · Fuselage Main, Longeron/StringerSDR SWIA202512090810Stringer · corrodedSTRINGER 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, 5Aug 10, 2025 · N558GJ · Cndair CL6002C11 · Fuselage Main, Longeron/StringerSDR SWIA2025120900805Support Plate · corrodedCORROSION 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.Aug 5, 2025 · N558GJ · Cndair CL6002C11 · Fuselage Miscellaneous StructureSDR SWI2025F01810Skin · dentedFUSELAGE 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 38Jul 30, 2025 · N558GJ · Cndair CL6002C11 · Fuselage Main, Plate/SkinSDR SWIA202512090730Intercostal · corrodedPAX 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.Jul 30, 2025 · N558GJ · Cndair CL6002C11 · Passenger/Crew DoorsSDR SWI2025F01819Frame · no discrepancySTRUCTURES 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 38Jul 29, 2025 · N558GJ · Cndair CL6002C11 · Standard Practices/StructuresSDR SWIA2025120900729Former · corrodedPAX 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 25/202Jul 29, 2025 · N558GJ · Cndair CL6002C11 · Passenger/Crew DoorsSDR SWI2025F01818Frame · no discrepancyFRAME 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. REFEREJul 25, 2025 · N558GJ · Cndair CL6002C11 · Standard Practices/StructuresSDR SWIA2025120900725Frame · no discrepancyFRAME 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 670-53-21-26Jul 25, 2025 · N558GJ · Cndair CL6002C11 · Standard Practices/StructuresSDR SWIA2025120900722Stringer Splice · corrodedFOUND 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.Jul 22, 2025 · N558GJ · Cndair CL6002C11 · Fuselage Main, Longeron/StringerSDR SWI2025F01809Intercostal · corrodedPAX 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.Jul 21, 2025 · N558GJ · Cndair CL6002C11 · Passenger/Crew DoorsSDR SWI2025F01808Intercostal · corrodedPAX 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 -.Jul 21, 2025 · N558GJ · Cndair CL6002C11 · Passenger/Crew DoorsSDR SWI2025F01807Former · corrodedPAX 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.Jul 21, 2025 · N558GJ · Cndair CL6002C11 · Passenger/Crew DoorsSDR SWI2025F01806Former · corrodedPAX 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.Jul 21, 2025 · N558GJ · Cndair CL6002C11 · Passenger/Crew DoorsSDR SWIA202512090721Stringer · corrodedEVIDENCE 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.Jul 21, 2025 · N558GJ · Cndair CL6002C11 · Fuselage Main, Longeron/StringerSDR SWIA2025120900720Floor Support · corrodedLBL 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.Jul 20, 2025 · N558GJ · Cndair CL6002C11 · Fuselage Miscellaneous StructureSDR SWI2025F01790Floorbeam · corrodedRBL 9 FLOORBEAM IS CORRODED AT BS 661, ON THE UPPER INBD FLANGE. COMPLIED WITH REO 670-53-31-1067, REV -.Jul 19, 2025 · N558GJ · Cndair CL6002C11 · Fuselage Main, Floor BeamSDR SWI2025F01789Floor Support · corrodedRBL 9 FLOOR SUPPORT IS CORRODED BETWEEN BS 469 & 485 ON THE UPPER INBD FLANGE. COMPLIED WITH REO 670-53-31-1066 REV-.Jul 19, 2025 · N558GJ · Cndair CL6002C11 · Fuselage Miscellaneous StructureSDR SWIA20250719Floor Support · corrodedLBL 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.Jul 19, 2025 · N558GJ · Cndair CL6002C11 · Fuselage Miscellaneous StructureSDR SWIA2025120900717Intercostal · corrodedFOUND 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 LOSSJul 17, 2025 · N558GJ · Cndair CL6002C11 · Fuselage Miscellaneous StructureSDR SWIA202512090716Antenna · corrodedADF 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.Jul 16, 2025 · N558GJ · Cndair CL6002C11 · Navigation SystemSDR SWI2025F01800Stringer · corrodedSTRINGER 20R IS CORRODED BETWEEN BS 437 TO 453. REPAIRED THE STGR IAW REO 670-53-21-2662, REV -.Jul 14, 2025 · N558GJ · Cndair CL6002C11 · Fuselage Main, Longeron/StringerSDR SWI2025F01799Stringer · corrodedSTRINGER 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.Jul 14, 2025 · N558GJ · Cndair CL6002C11 · Fuselage Main, Longeron/StringerSDR SWI2025F01798Splice · corrodedH 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.Jul 14, 2025 · N558GJ · Cndair CL6002C11 · Fuselage Main, FrameSDR SWI2025F01797Intercostal · corrodedPAX DOOR INTERCOSTAL IS CORRODED BETWEEN BS 333 TO 349, STRINGER 20L. INSTALLED THE INTERCOSTAL BETWEEN IAW SRM 51-42-06-001-001-A01.Jul 14, 2025 · N558GJ · Cndair CL6002C11 · Passenger/Crew DoorsSDR SWI2025F01796Stringer · corrodedSTRINGER 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 SJul 14, 2025 · N558GJ · Cndair CL6002C11 · Fuselage Main, Longeron/StringerSDR SWI2025F01795Stringer · corrodedSTRINGER 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 .Jul 14, 2025 · N558GJ · Cndair CL6002C11 · Fuselage Main, Longeron/StringerSDR SWI2025F01794Stringer · corrodedSTRINGER 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.Jul 14, 2025 · N558GJ · Cndair CL6002C11 · Fuselage Main, Longeron/StringerSDR SWIA2025120900714Stringer · corrodedSTRINGER 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.Jul 14, 2025 · N558GJ · Cndair CL6002C11 · Fuselage Main, Longeron/StringerSDR SWI2025F01805Slider · chafedRIGHT TRANSCOWL LOWER OTBD SLIDER IS CHAFED. RECEIVED AND COMPLIED WITH ALL STEPS OF REO 670-54-21-1751 REV -.Jul 12, 2025 · N558GJ · Cndair CL6002C11 · Engine Thrust ReverserSDR SWI2025F01804Slider · chafedRIGHT TRANSCOWL UPPER INBD SLIDER IS CHAFED. RECEIVED AND COMPLIED WITH ALL STEPS OF REO 670-54-21-1750 REV -.Jul 12, 2025 · N558GJ · Cndair CL6002C11 · Engine Thrust ReverserSDR SWI2025F01803Slider · chafedRIGHT TRANSCOWL LOWER INBD SLIDER IS CHAFED. RECEIVED AND COMPLIED WITH ALL STEPS OF REO 670-54-21-1751 REV -.Jul 12, 2025 · N558GJ · Cndair CL6002C11 · Engine Thrust ReverserSDR SWI2025F01802Slider · chafedRIGHT TRANSCOWL UPPER OB SLIDER IS CHAFED. RECEIVED AND COMPLIED WITH ALL STEPS OF REO 670-54-21-1750 REV -.Jul 12, 2025 · N558GJ · Cndair CL6002C11 · Engine Thrust ReverserSDR SWI2025F01801Slider · chafedLEFT TRANSCOWL LOWER OTBD SLIDER IS CHAFED. RECEIVED AND COMPLIED WITH ALL STEPS OF REO 670-54-21-1749 REV -.Jul 12, 2025 · N558GJ · Cndair CL6002C11 · Engine Thrust ReverserSDR SWIA202512090712Slider · chafedLEFT TRANSCOWL LOWER IB SLIDER IS CHAFED. RECEIVED AND COMPLIED WITH ALL STEPS OF REO 670-54-21-1749 REV -.Jul 12, 2025 · N558GJ · Cndair CL6002C11 · Engine Thrust ReverserSDR SWI2025F01817Slat Track · chafedRIGHT SLAT TRACK 2-3 IS CHAFED. REPAIRED RT SLAT TRACK 2-3 IAW REO 670-57-42-2151, REV -.Jul 8, 2025 · N558GJ · Cndair CL6002C11 · Leading Edge DevicesSDR SWI2025F01816Slat Track · chafedRIGHT SLAT TRACK 1-3 IS CHAFED. REPAIRED THE RT SLAT TRACK 1-3 IAW REO 670-57-42-2149, REV -.Jul 8, 2025 · N558GJ · Cndair CL6002C11 · Leading Edge DevicesSDR SWI2025F01815Slat Track · chafedRIGHT SLAT TRACK 1-1 IS CHAFED. REPAIRED RT SLAT TRACK 1-1 IAW REO 670-57-42-2148, REV -.Jul 8, 2025 · N558GJ · Cndair CL6002C11 · Leading Edge DevicesSDR SWI2025F01814Slat Track · chafedLEFT SLAT TRACK 1-3 IS CHAFED. COMPLIED WITH REO 670-57-42-2145, REV -.Jul 8, 2025 · N558GJ · Cndair CL6002C11 · Leading Edge DevicesSDR SWI2025F01813Slat Track · chafedLEFT SLAT TRACK 1-1 IS CHAFED. COMPLIED WITH REO 670-57-42-2144, REV -.Jul 8, 2025 · N558GJ · Cndair CL6002C11 · Leading Edge DevicesSDR SWI2025F01812Slat Track · chafedRIGHT SLAT TRACK 2-1 IS CHAFED. REPAIRED THE RT SLAT TRACK 2-1 IAW REO 670-57-42-2150 REV -.Jul 8, 2025 · N558GJ · Cndair CL6002C11 · Leading Edge DevicesSDR SWI2025F01811Slat Track · chafedLEFT SLAT TRACK 2-3 IS CHAFED. COMPLIED WITH REO 670-57-42-2147 REV -.Jul 8, 2025 · N558GJ · Cndair CL6002C11 · Leading Edge DevicesSDR SWIA202512090708Slat Track · chafedLEFT SLAT TRACK 2-1 IS CHAFED. COMPLIED WITH REO 670-57-42-2146 REV-.Jul 8, 2025 · N558GJ · Cndair CL6002C11 · Leading Edge Devices
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