N929XJ
Service difficulty reports · 174
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 = 'N929XJ' 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.
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 = 'N929XJ' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR REXA2026072801199Striker · crackedWEAR ON FWD FRAME OVER FS629.00 AND STGR24L / STGR23L AT CENTER BAGGAGE BAY DOOR FOR EXCESSIVE DAMAGE ON FRAME OVER FS629.00 AND STGR24L / STGR23L AT CENTER BAGGAGE BAY DOOR WAS REPLACED PER CRJ-900 SRM 53-31-23-101-001-A02, SRM 51-41-02-001-001-A01 AND SRM 5SDR REXA2026072801198Floorbeam · crackedCRACKED CENTER COCKPIT FLOOR BEAM LBL 12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. FLOOR BEAM LBL 12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-11-2217 REV --SDR REXA2026072801195Stiffener · crackedCRACK ON UPPPER STIFFENER ATTACHED TO POWER-ASSIST MOTOR BTW DATUM 4 AND DATUM 5 (AFT SIDE PANEL) OF PASSENGER DOOR INTERNAL STRUCTURE. STIFFENER ATTACHED TO POWER-ASSIST MOTOR BTW DATUM 4 AND DATUM 5 (AFT SIDE PANEL) OF PASSENGER DOOR INTERNAL STRUCTURE WAS RSDR REXA2026072801194Web · crackedCRACK ON LT FLOOR WEB AT ELECTRICAL BAY (BELOW BRAKE ACCUMULATOR INDICATION SUPPORT DOUBLER) BS 193 LT FLOOR WEB AT ELECTRICAL BAY (BELOW BRAKE ACCUMULATOR INDICATION SUPPORT DOUBLER) FS193.00 WAS REPAIRED PER CRJ900 SRM 53-11-43-201-001-A01SDR REXA2026072801201Seat Track · crackedCORROSION ON SIDE SEAT RAILS IN SECTIONS FS= 437.00 TO FS= 469.00 AND FROM FS 629.00 TO FS 785.00, STGR 15LH. AND FS 613.00 TO FS 797.00 STGR 15RH AT PAX CABIN SIDE SEAT RAILS IN SECTIONS FS= 437.00 TO FS= 469.00 AND FROM FS 629.00 TO FS 785.00, STGR 15LH. ANDSDR REXA2026072801200Seat Track · crackedCORROSION ON FLOOR SEAT RAILS IN SECTIONS FS= 364.00 TO FS= 485.00, LBL 27 AT PAX CABIN. FLOOR SEAT RAILS IN SECTIONS FS= 364.00 TO FS= 485.00, LBL 27 AT PAX CABIN WAS REPLACED PER CRJ900 AMM 53-00-49SDR REXA2026072801192Seat Track · crackedCORROSION ON FLOOR SEAT RAILS IN SECTIONS FS= 379.00 TO FS= 485.00, LBL9 AT PAX CABIN. FLOOR SEAT RAILS IN SECTIONS FS= 379.00 TO FS= 485.00, LBL9 AT PAX CABIN WAS REPLACED PER CRJ900 AMM 53-00-49SDR REXA2026072801196Rib · crackedCRACK ON LEADING EDGE RIB SS57.16 AT RH WING LEADING EDGE RIB SS57.16 AT RT WING WAS REPAIRED PER REO 690-57-41-604 REV - -SDR REXA2026072801197Support Bracket · crackedCRACK ON SUPPORT BRACKET TO TIE BAR AT LEFT PYLON SUPPORT BRACKET TO TIE BAR AT LEFT PYLON WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01SDR REXA2026072801193Support · crackedCRACK AT CORNERS OF SUPPORT AT THE JB 6 MODULE AT FWD EQUIPMENT COMPARTMENT. SUPPORT AT THE JB 6 MODULE AT FWD EQUIPMENT COMPARTMENT WAS REPLACED PER SRM 51-42-06-001-001-A01SDR REXA2026072801191Drag Angle · crackedCRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM WAS REPAIRED PER CRJ900 SRM SDR REXA2026072801190Door Sill · crackedCRACK ON AFT RT DOOR LANDING AT FS 188.00 (AFT LATCH CUT OUT OF ACCESS DOOR 212AR) AFT RT DOOR LANDING AT FS 188.00 (AFT LATCH CUT OUT OF ACCESS DOOR 212AR) WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 & SRM 51-42-13-001-001-A01SDR REXA2024042900365Latch · inoperativePAX O2 DEPLOYMENT SYSTEM FAILS OPS CHECK. THE MASKS AT THE FOLLOWING SEAT LOCATIONS FAILED TO DROP: 10DC, 14DC, 17BA, AND 20BA. TROUBLESHOT AND FOUND LATCHES TO BE BAD. REMOVED AND REPLACED PAX O2 MASK BOX LATCHES FOR SEATS 10DC, 14DC, 17BA, AND 20BA IAW CRJ-9SDR REXA2024042400362Door Frame · crackedRH AFT EMERGENCY EXIT FWD LUG IS CRACKED. REPAIRED IAW ENDEAVOR EA CRJ952-16335 REV IR DATED 4-9-2024.SDR REXA2024042400361Door Frame · crackedRH FWD EMERGENCY EXIT AFT LUG IS CRACKED. REPAIRED IAW ENDEAVOR EA CRJ952-16334 REV IR DATED 4-9-2024.SDR REXA2019120621718Battery · dischargedON WAKE UP FOUND MASTER BATTERY SWITCH ON. EMER. LIGHTS WERE NOT COMING ON DUE TO LOW BATTERY CHARGE
R/R MAIN BATTERY IAW CRJ900 JC 24-210-901. OPS TEST GOOD AT THIS TIMESDR REXA2019102481504Intercostal · corrodedINITIAL INSPECTION: CORROSION ON INTERCOSTAL 27(RH SIDE) AND 26R BTW. FS349 AND FS364 (FWD TO E/E DOOR) [IN REFERENCE TASK 900-53-140-300 APPENDIX A].(E/E)(TCI 100-09)
SUMMARY:INTERCOSTAL 27RH AND 26RH BTW. FS349 AND SDR REXA2019102411479Hinge · damagedINITIAL INSPECTION: SPRING DAMAGED AT GROUND POWER ACCESS DOOR(122DR). (SM)(FUS).
SUMMARY: HINGE AT GROUND POWER ACCESS DOOR WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01.SDR REXA2019102471520Hinge Fitting · corrodedAWR HIDDEN DISCREPANCY: AFTER BUSHINGS REMOVAL CORROSION WAS FOUND ON LH/RH HINGE FITTING IN REF JC 900-32-710-902 STEP 5. (FYT)
SUMMARY: ON NRC 00369 LH/RH FITTINGS OF NLG AFT DOOR WERE REPLACED FOR NEW ONES PER CRJ-900 SRM 51-42-21-001-001 A01.SDR REXA2019102471515Frame · corrodedINITIAL INSPECTION: CORROSION ON FRAME FS=265 BTW STGR 26R / 26L AT INTERNAL STRUCTURE OF FWD FUSELAGE (SM) (TCI 100-06)
SUMMARY: CORROSION ON FRAME FS=265 BTW STGR 26R / 26L AT INTERNAL STRUCTURE OF FWD FUSELAGE WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-ASDR REXA2019102471514Support · corrodedINITIAL INSPECTION: CORROSION ON JACK FITTING SUPPORT (2EAS) BTW FS=280 / FS=265 AND STGR 26R / 26L AT INTERNAL STRUCTURE OF FWD FUSELAGE (SM) (TCI 53-10-305).
SUMMARY OF NRC: 00267 CORROSION ON JACK FITTING SUPPORT (2EAS) BTW FS=280 / FS=265 AND STGR 26R /SDR REXA2019102471503Intercostal · corrodedINITIAL INSPECTION: CORROSION ON [INTERCOSTAL] 26L AND 27(LH SIDE) BTW. FS349 AND FS364 (FWD TO E/E DOOR) AT MAIN AVIONICS COMPARTMENT [IN REFERENCE TASK 900-53-140-300 APPENDIX A]. (E/E)(TCI 100-09)
SUMMARY: CORROSION LEVEL 2.INTERCOSTAL 27(LH SIDE) AND 2SDR REXA2019101701497Stringer · corrodedINITIAL INSPECTION: CORROSION ON STRINGER 25R BTW. FS319.70 AND FS349 AT MAIN AVIONICS COMPARTMENT [IN REFERENCE TASK 900-53-140-300 APPENDIX A].(E/E)(TCI 100-09).
SUMMARY OF NRC; 00170: CORROSION LEVEL #2 ON STRINGER 25R BTW. FS319.70 AND FS349 AT MAIN AVIONSDR REXA2019102471495Stringer · corrodedINITIAL INSPECTION: CORROSION ON STRINGER 25R BTW. FS280 AND FS333 ALSO HYDRAULIC LINES STANDOFF (2E/A) AT MAIN AVIONICS COMPARTMENT [IN REFERENCE TASK 900-53-140-300 APPENDIX A]
SUMMARY: ON NRC. 00167 CORROSION LEVEL 2, STRINGER 25R BTW. FS280 AND FS333 AND SDR REXA2019102471480Coaming · crackedINITIAL INSPECTION : CRACKED COAMING LATCH DOOR AND AFT CHANNEL ON LOWER HALF TRANSCOWL RH ENGINE ( MOT 2 ). SUMMARY: ON NRC. 00041, COAMING LATCH DOOR AND AFT CHANNEL ON LOWER HALF TRANSCOWL RH ENGINE WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRSDR REXA2019102451516Floor Support · corrodedINITIAL INSPECTION: CORROSION ON FLOOR BEAM 27LBL FROM FS1000 TO FS1047 AT AFT BAGGAGE BAY. (CCT) (TCI: 53-30-306).
SUMMARY : DUE CORROSION LEVEL 2 ON FLOOR BEAM LBL27 STA FS 1000 TO FS 1047 AT AFT CARGO COMPARTMENT WAS REPAIRED PER CRJ/900 SRM 53-00-41-201SDR REXA2019102451509Doubler · corrodedHIDDEN DAMAGE IN REF. JOBCARD 900-34-900-702. CORROSION ON DOUBLE IN SETTLEMENT AREA OF TRANSMIT ANTENNA 2 E19. (SM) (FUS).
SUMMARY: DOUBLES (SPACER) WAS FABRICATED PER E/A CRJ 953-09832 REV IR. AND WAS INSTALLED PER CRJ 900 SRM 51-42-06-001-001-A01.SDR REXA2019102451501Stringer · corrodedINITIAL INSPECTION: CORROSION ON STRINGER 26L BTW FS333 AND FS349 AT MAIN AVIONICS COMPARTMENT [ IN REFERENCE TASK 900-53-140-300 APPENDIX A].(E/E)(TCI).
SUMMARY: STRINGER 26LH FROM FS 333-364 AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ-900 SRM 51-42-0SDR REXA2019102451494Frame · corrodedINITIAL INSPECTION: CORROSION ON FRAME FS295 BTW. STGR.26L AND 26R AT MAIN AVIONICS COMPARTMENT [IN REFERENCE TASK 900-53-140-300 APPENDIX A].(E/E)(TCI 100-09).
SUMMARY:ON NRC. 00163 CORROSION LEVEL 1 ON FRAME FS295 BTW. STGR.26L AND 26R AT MAIN AVIONICS COSDR REXA2019102451493Stringer · corrodedINITIAL INSPECTION: CORROSION ON STRINGER 26R BTW FS280 AND FS364 AT MAIN AVIONICS COMPARTMENT [IN REFERENCE TASK 900-53-140-300 APPENDIX A].(E/E)(TCI 100-09).
SUMMARY: STRINGER 26R BTW FS280 AND FS364 AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ-900 SRMSDR REXA2019102451492Stringer · corrodedINITIAL INSPECTION: CORROSION ON STRINGER 27 BTW.FS280 AND FS310 AT MAIN AVIONICS COMPARTMENT [IN REFERENCE TASK 900-53-140-300 APPENDIX A].(E/E) (TCI 100-09).
SUMMARY: ON NRC. 00160 CORROSION LEVEL 2, STRINGER 27 BTW.FS280 AND FS310 AT MAIN AVIONICS COMPARTMSDR REXA2019102451483Striker · wornINITIAL INSPECTION: WEAR FWD STRIKER SEAL AT CENTER BAGGAGE BAY DOOR SURROUND STRUCTURE (C1) (SM).
SUMMARY: FWD STRIKER SEAL AT CENTER BAGGAGE BAY DOOR SURROUND STRUCTURE NO DAMAGE ALLOWED PER CRJ-900 SRM 53-31-23-101-001-A02. DAMAGED FWD STRIKER SEAL AT CENTSDR REXA201910241508Floor Support · corrodedAWR: CORROSION ON FLOOR SUPPORTS BTW FS310 TO FS349 AT PAX CABIN FLOOR STRUCTURE, PASSENGER DOOR LOWER SILL. (CPAX).
SUMMARY OF NRC 00233: FLOOR SUPPORTS BTW FS310 TO FS349 AT PAX CABIN FLOOR STRUCTURE, PASSENGER DOOR LOWER SILL WERE REPLACED PER CRJ-900 SRM SDR REXA2019102401500Stringer Splice · corrodedINITIAL INSPECTION: CORROSION ON SPLICE STA FS333 OF STRINGERS (3 E/A) STGR. 26L, 26R, AND 25R AT MAIN AVIONICS COMPARTMENT[IN REFERENCE TASK 900-53-140-300 APPENDIX A].(E/E)(TCI 100-09).
SUMMARY: SPLICE STA FS333 OF STRINGERS (3 E/A) STGR. 26L, 26R, AND 25R SDR REXA2019102431499Frame · corrodedINITIAL INSPECTION: CORROSION ON FRAME FS319.70 BTW STGR 26L AND 26R AT MAIN AVIONICS COMPARTMENT [IN REFERENCE TASK 900-53-140-300 APPENDIX A].(E/E)(TCI 100-09).
SUMMARY OF NRC 00172: CORROSION LEVEL-1 ON FRAME FS319.70 BTW STGR 26L AND 26R AT MAIN AVIONISDR REXA2019101301498Frame · corrodedINITIAL INSPECTION: CORROSION ON FRAME FS333 BTW. STGR 26L AND 25R AT MAIN AVIONICS COMPARTMENT [IN REFERENCE TASK 900-53-140-300 APPENDIXA]. (E/E)(TCI 100-09).
SUMMARY: CORROSION LEVEL 1 ON FRAME FS333 BTW. STGR 26L AND 25R AT MAIN AVIONICS COMPARTMENT WAS RSDR REXA2019102431496Frame · corrodedINITIAL INSPECTION: CORROSION ON FRAME FS310 BTW. STGR.26L AND 25R AT MAIN AVIONICS COMPARTMENT [IN REFERENCE TASK 900-53-140-300 APPENDIXA].(E/E)(TCI 100-09).
CORROSION LEVEL 1 ON FRAME FS310 BTW. STGR.26L AND 25R AT MAIN AVIONICS COMPARTMENT WAS REMOVED PERSDR REXA2019102431488Support Angle · corrodedINITIAL INSPECTION: CORROSION ON FLOOR SETTLEMENT (141ALF) AT MAIN AVIONICS COMPARTMENT FS280 BTW. STGR 25L AND 25R.(E/E)(100-09).
SUMMARY: DAMAGED ANGLE SUPPORT, CRAWLWAY FLOOR ON FS=280.00 BTW STGR 25L AND 25R AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMSDR REXA2019102411506Door Frame · corrodedINITIAL INSPECTION: CORROSION ON MOUNTING ANGLE OF SERVICE DOOR SURROUND STRUCTURE LOWER SILL.(PTAS)(TCI 53-20-219).
SUMMARY: ON NRC: 00218 CORROSION LEVEL 2, MOUNTING ANGLE OF SERVICE DOOR SURROUND STRUCTURE LOWER SILL WAS REPLACED PER CRJ-900 SRM 51-42-06-0SDR REXA2019102411505Scuff Plate · corrodedINITIAL INSPECTION: CORROSION ON SCUFF PLATE SUPPORTS AND ANGLES AT GALLEY SERVICE DOOR LOWER SURROUND STRUCTURE. (PTAS)(TCI:53-20-219).
SUMMARY: ON NRC. 00215 CORROSION LEVEL 2 SCUFF PLATE SUPPORTS AND ANGLES AT GALLEY SERVICE DOOR LOWER SURROUND STRUCTURE WSDR REXA2019102411502Frame · corrodedINITIAL INSPECTION: CORROSION ON FRAME FS349 BTW. STGR. 26L AND 25R AT MAIN AVIONICS COMPARTMENT [IN REFERENCE TASK 900-53-140-300 APPENDIX A].(E/E)(TCI 100-09).
SUMMARY: ON NRC. 00175, CORROSION LEVEL 1, FRAME FS349 BTW. STGR. 26L AND 25R AT MAIN AVIONICS COSDR REXA2019102411510Floor Support · corrodedINITIAL INSPECTION: CORROSION ON FLOOR SUPPORT AT FUSELAGE STRUCTURE BTW FS 565 / FS 581 AND STGR 22L/23L (C1).
SUMMARY OF NRC 00257 CORROSION LEVEL 2: FLOOR SUPPORT AT FUSELAGE STRUCTURE BTW FS 565 / FS 581 AND STGR 22L/23L WAS REPLACED PER CRJ 900 SRM 51-4SDR REXA2019102491522Floorbeam · crackedAWR HIDDEN DAMAGE: DURING REMOVAL FLOOR BEAM FS=280, ANGLE WAS FOUND CRACKED AT STA FS280 LBL26 PAX CABIN (CPAX) (IN REF. NRC 00264)
SUMMARY: ON NRC. 00393, ANGLE AT STA FS280 LBL26 PAX CABIN WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-13SDR REXA2019102491521Floorbeam · crackedAWR HIDDEN DAMAGE: DURING REMOVAL FLOOR BEAM 280, ANGLE WAS FOUND CRACKED AT STA FS280 RBL26 PAX CABIN (CPAX) (IN REF. NRC 00263)
SUMMARY: ON NRC. 00392, ANGLE AT STA FS280 RBL26 PAX CABIN WAS REPLACED PER CRJ-900 SRM 51-42-06-001 AND SRM 51-42-13-001-001-A01SDR REXA2019102491513Floorbeam · corrodedAWR HIDDEN DISCREPANCY: AFTER FLOOR PANEL SUPPORT ANGLE REMOVAL CORROSION WAS FOUND ON FLOOR BEAM STA 280 BTW BL0.00 AND LBL 11 AT PAX CABIN (W1) IN REF NRC S/N 00159.
SUMMARY: ON NRC. 00264 CORROSION LEVEL 2, CROSSBEAM AT FS 280.00 BTW BL 0 TO LBL 42 WAS REPSDR REXA2019102491512Floorbeam · corrodedAWR HIDDEN DISCREPANCY: AFTER FLOOR PANEL SUPPORT ANGLE REMOVAL CORROSION WAS FOUND ON FLOOR BEAM STA 280 BTW BL0.00 AND RBL 11 AT PAX CABIN (W1) IN REF NRC S/N 00159.
SUMMARY: ON NRC. 00263, CORROSION LEVEL 2, CROSSBEAM AT FS 280.00 BTW BL 0 TO RBL 42 WAS RESDR REXA2019102491484Intercostal · corrodedINITIAL INSPECTION: CORROSION ON INTERCOSTAL DD6 BTW FORMER FS 338.9 AND FRAME FS 327.7 INSIDE STRUCTURE AT PASSENGER DOOR. (PTAS)(TSI: 52-10-301).
SUMMARY: INTERCOSTAL DD6 WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 PAR. 6. (C) AND SRM 51-42-21-001-001SDR REXA2019102491481Strap · corrodedINITIAL INSPECTION: CORROSION ON SETTLEMENT AREA AT PANEL ACCESS 193AB AND 195AB (SM).
SUMMARY: ON NRC. 00110, ON SETTLEMENT AREA AT PANEL ACCESS 193AB AND 195AB, STRAPS WERE REPLACED PER CRJ-900 SRM 51-42-10-001-001-A01 PAR. 8SDR REXA2019102481519Canister · crackedINITIAL INSPECTION: CRACK IN CANISTER, WELDED NO.3 IN STA. WS148 AT LH MAIN FUEL TANK. (AI)
SUMMARY: ON NRC. 00303 CANISTER, WELDED NO.3 IN STA. WS148 AT LH MAIN FUEL TANK WAS REPAIRED PER CRJ-900 REO 670-57-42-577 REV.SDR REXA2019102481518Stringer Splice · corrodedINITIAL INSPECTION: CORROSION ON STGR SPLICE 22 RH AND FS=333 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT (SM) (TCI 53-20-319).
SUMMARY: ON NRC. 00289 CORROSION LEVEL 2, STGR SPLICE 22 RH AND FS=333 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT
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