N930XJ

Service difficulty reports · 160

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 = 'N930XJ' 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 REXA2026092101839Bulb · inoperativeAFT RIGHT OVERWING EMERGENCY LIGHT BULB INOPERATIVE. R & R RIGHT OVERWING EMERGENCY LIGHT BULB PER AMM 33-51-15.Sep 17, 2026 · N930XJ · Cndair CL6002D24 · Emergency LightingSDR REXA2026091101806Rib · crackedCRACK ON MACHINED RIB OF LEADING EDGE SS58.41 AT LH WING. DUE TO EXCESSIVE DAMAGE ON MACHINED RIB OF LEADING EDGE SS58.41 AT LH WING WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01,SRM 51-42-13-001-001-A01 AND SRM 51-10-06-001-001-ASep 3, 2026 · N930XJ · Cndair CL6002D24 · Wing, Rib/BulkheadSDR REXA2026091101805Angle · crackedCRACKS ON UPPER ANGLES (FIRE PROTECTION KIT 2EAS) FWD CORNERS AT FWD/CENTER BOTH BAGGAGE BAY DOORS. UPPER ANGLES (FIRE PROTECTION KIT 2EAS) FWD CORNERS AT FWD/CENTER BOTH BAGGAGE BAY DOORS WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01 AND 51-42-13-001-001-Aug 9, 2026 · N930XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026091101804Angle · crackedCRACKS ON UPPER ANGLES (FIRE PROTECTION KIT 2EAS) FWD CORNERS AT FWD/CENTER BOTH BAGGAGE BAY DOORS. UPPER ANGLES (FIRE PROTECTION KIT 2EAS) FWD CORNERS AT FWD/CENTER BOTH BAGGAGE BAY DOORS WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01 AND 51-42-13-001-001-Aug 9, 2026 · N930XJ · Cndair CL6002D24 · Cargo/Baggage DoorsSDR REXA2026091101822Fitting · corrodedCORROSION FLOOR FITTING IN AFT AND FWD ACCESS 306 (1EA) ON GALLEY 3. NEW FLOOR FITTING IN AFT AND FWD ACCESS 306 (1EA) ON GALLEY 3 WAS REPLACED IAW CMM 25-33-18 REV 5.Aug 5, 2026 · N930XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026091101821Fitting · corrodedCORROSION FLOOR FITTING IN AFT ACCESS 109 (1EA) ON GALLEY 1. NEW FLOOR FITTING P/N: CDSP2019-7C-620 IN AFT ACCESS 109 (1EA) ON GALLEY 1 WAS REPLACED PER SAFRAN CMM 25-33-67 REV NO10 DATED 20/22Aug 5, 2026 · N930XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026091101815Fitting · corrodedCORROSION FLOOR FITTING IN FWD ACCESS 305 (1EA) ON GALLEY 3. SUMMARY OF NRC 00402: NEW FLOOR FITTING P/N: CDSP2019-7C-700 IN FWD ACCESS 305 (1EA) ON GALLEY 3 WAS REPLACED PER ZODIAC AEROSPACE CMM 25-33-18 REV NO 5 DATED 15/15Aug 5, 2026 · N930XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026091101814Fitting · corrodedCORROSION FLOOR FITTING IN FWD ACCESS 107 (1EA) ON GALLEY 1. SUMMARY OF NRC 00399: NEW FLOOR FITTING P/N: CDSP2019-7C-620 IN FWD ACCESS 107 (1EA) ON GALLEY 1 WAS REPLACED PER SAFRAN CMM 25-33-67 REV NO 10 DATED JUN 20/22Aug 5, 2026 · N930XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026091601817Skin · crackedCRACK ON SETTLEMENT AREA OF PASSENGER DOOR ACCESS PANEL 832DL. SETTLEMENT AREA OF PASSENGER DOOR ACCESS PANEL 832DL WAS REPAIRED PER EA CRJ952-22930 REV BAug 3, 2026 · N930XJ · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2026091601816Skin · crackedCRACK ON SETTLEMENT AREA OF PASSENGER DOOR ACCESS PANEL 832AL SETTLEMENT AREA OF PASSENGER DOOR ACCESS PANEL 832AL WAS REPAIRED PER EA CRJ952-22930 REV BAug 3, 2026 · N930XJ · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2026091101812Access Panel · corrodedCORROSION ON NUTS STRIP OF BODY FAIRING ACCESS PANEL 194AB. 08/02/2026 STRIP OF BODY FAIRING ACCESS PANEL 194AB WAS REPLACED PER CRJ-900 SRM 51-42-13-001-001-A01.Aug 2, 2026 · N930XJ · Cndair CL6002D24 · Aerodynamic FairingsSDR REXA2026091101811Hinge · corrodedCRACK ON HINGE OF FLAP STEP OF AFT BAGAGGE BAY. HINGE OF FLAP STEP OF AFT BAGAGGE BAY WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01.Aug 2, 2026 · N930XJ · Cndair CL6002D24 · Fuselage, Door HingeSDR REXA2026091101810Fitting · crackedCRACK ON LOWER SIDE POST FITTINGS (2 EAS) LH/RH ON INTERNAL STRUCTURE BTW WINDSHIELD AND SIDE WINDOWS. LOWER SIDE POST FITTINGS (2 EAS) LH/RH ON INTERNAL STRUCTURE BTW WINDSHIELD AND SIDE WINDOWS WERE REPLACED PER CRJ-900 SRM 51-42-20-001-001-A01Aug 2, 2026 · N930XJ · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2026091101809Seat Track · corrodedCORROSION & WEAR ON LH SIDE RAILS (4 EAS) BTW FS 379.00/FS 669.40 AND STGR 15L AT PAX CABIN. LH SIDE RAILS (3 EAS) BTW FS 379.00/FS 669.40 AND STGR 15L AT PAX CABIN WAS CLEANED AND NOT DAMAGE WAS FOUND PER CRJ-900 SRM 51-26-00-001-001-A01, AND ON SECTION OF LHAug 1, 2026 · N930XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2026091101808Stringer · corrodedCORROSION ON STGR22R FROM FS280 TO FS310 AT MAIN AVIONICS COMPARTMENT. SUMMARY: CORROSION ON STGR22R FROM FS280 TO FS310 AT MAIN AVIONICS COMPARTMENT WAS EVALUATED OUT OF LIMITS THEREFORE WAS REPLACED PER CRJ-900 SRM 51-10-06-001-001-A01, CRJ-900 SRM 51-42-06-Jul 31, 2026 · N930XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2026091101807Seat Track · corrodedCORROSION & WEAR ON RH SIDE RAILS (5 EAS) BTW FS 669.40/FS 977.00 AND STGR 15R AT PAX CABIN. CORROSION ON SIDE RAILS (5 EAS) BTW FS 669.40/FS 977.00 AND STGR 15R AT PAX CABIN WERE EVALUATED OUT OF LIMITS THEREFORE WERE REPLACED PER CRJ-900 SRM 53-31-49-101-001Jul 31, 2026 · N930XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2026091101819Frame · corrodedCORROSION ON FRAME AT FS 333, BTW STGR 25 AND 26R ON MAIN AVIONICS COMPARTMENT CORROSION ON FRAME AT FS 333, BTW STGR 25 AND 26R ON MAIN AVIONICS COMPARTMENT WAS EVALUATED OUT OF LIMITS THEREFORE WAS REPAIRED PER CRJ-900 SRM 53-00-06-201-006-A01 AND CRJ 900 SRJul 30, 2026 · N930XJ · Cndair CL6002D24 · Fuselage Main, FrameSDR REXA2026091101820Striker · corrodedCORROSION ON SEAL STRIKER OF SERVICE DOOR LOWER CUTOUT BTW FS319.70 TO FS349.00 AND STGR-17R. CORROSION ON SEAL STRIKER OF SERVICE DOOR LOWER CUTOUT BTW FS319.70 TO FS349.00 AND STGR-17R. WAS EVALUATED OUT OF LIMITS PER SRM 51-10-06-001-001-A01 AND WAS REPLACJul 28, 2026 · N930XJ · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2026091101818Retainer · corrodedCORROSION ON INNER CHANNEL OF AFTER CARGO DOOR. INNER CHANNEL OF AFTER CARGO DOOR WAS REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01Jul 28, 2026 · N930XJ · Cndair CL6002D24 · Cargo/Baggage DoorsSDR REXA2026091101803Support · crackedCRACKS ON FWD CORNERS AT JB6 PLATE. JB6 PLATE WAS REPLACED PER SRM 51-42-06-001-001-A01 PAR. 6.C.Jul 27, 2026 · N930XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2025060500631Battery Pack · inoperativeEMEGENCY LIGHTS STATUS MESSAGE & EMERGENCY LIGHT COME ON WHEN EMER LTS SWITCH IS IN THE ARMED POSITION. R/R AND PERFORMED OPS TEST OF THE PS43 EMER BATTERY IAW AMM 33-51-17 TEST PASSED A/C OK FOR SVC.Jun 5, 2025 · N930XJ · Cndair CL6002D24 · Emergency LightingSDR REXA2025040800402Battery Pack · no testDURING LINE CHECK FOUND SEVERAL FWD EMERG ENTRANCE LIGHTS INOP. TROUBLESHOT AND FOUND BATTERY PACK PS35 INOP. REMOVED & REPLACED BATTERY IAW AMM 33-51-17 PERFOMRED OPS TEST IAW AMM 33-51-17. OPS TEST GOOD.Apr 5, 2025 · N930XJ · Cndair CL6002D24 · Emergency LightingSDR REXA2024122301605Lamp · inoperativeDURING COMPLETION OF LINE-900, FOUND PAX DOOR EMERGENCY LIGHT BULB OUT R/R BULB IAW CRJ AMM 33-51-15. PERFORMED OPS TEST OF EXT. EMER. LIGHTS IAW CRJ AMM 33-51-15; OPS TEST GOOD. P/N OFF/ON: 8GH002473-08 NO S/NDec 21, 2024 · N930XJ · Cndair CL6002D24 · Emergency LightingSDR REXA2024050900387Lamp · inoperativeEXTERIOR AFT EMERGENCY LIGHT INOP RELAMPED EMERGENCY LEFT AFT OVERWING LIGHT IAW CRJ 900 AMM 33-51-15. OPC GOOD. P/N OFF/ON: 8GH002473-08May 7, 2024 · N930XJ · Cndair CL6002D24 · Emergency LightingSDR REXA2024032800313Lamp · inoperativeRH OVERWING EMERGENCY LIGHT NOT WORKING R/R OVER THE WING EMERGENCY LAMP IAW CRJ 900 AMM 33-51-15 P/N OFF/ON: 8GH005123-06Mar 27, 2024 · N930XJ · Cndair CL6002D24 · Emergency LightingSDR REXA2024041800356Stiffener · chafedPANEL 172CR BOTTOM AFT STIFFENER CHAFFED. REMOVED AND REPLACED IAW CRJ 900 SRM 51-42-06-001-001-A01.Mar 1, 2024 · N930XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022052300329Floor Support · corrodedPAX DOOR SILL FLOORBOARD SUPPORT MID CAP ANGLE IS CORRODED. REPLACED PAX DOOR SILL FLOORBOARD SUPPORT MID CAP ANGLE IAW CRJ-900 SRM 51-41-02-001-001AO1May 21, 2023 · N930XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022123002731Motor · inoperativePAX DOOR WILL NOT OPEN. REMOVED AND REPLACED PAX DOOR ASSIST MOTOR IAW 52-11-08 . AND REPLACED RELAY K138 IAW AMM 20-42-00.Dec 25, 2022 · N930XJ · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2020012380048Bulb · inoperativeEMERGENCY FLOOR LEVEL FLOOD LIGHTS HAVE 1 BULB INOP AT PAX DOOR AND 3 BULBS INOP AT GALLEY SERVICE DOOR REMOVED AND REPLACED EMERGENCY LIGHT BULBS 4 EA PER CRJ-900 AMM 33-51-11. OPS CHECK GOODJan 18, 2020 · N930XJ · Cndair CL6002D24 · Emergency LightingSDR REXA2019123021840Door Frame · nickedFOUND IMPACT DAMAGE ON THE FRAME FOR THE FWD E/E BAY DOOR, RT SIDE. THE FRAME AT BS 310 STRINGERS 24R - 25R WAS REPAIRED IAW EA CRJ953-10116, REV IR.Dec 21, 2019 · N930XJ · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2019123021811Longeron · corrodedCORROSION FOUND ON LONGERON 25R AT BS 336 - 349 IN THE MAIN AVIONICS COMPARTMENT. THE LONGERON WAS REPLACED IAW SRM 51-42-06-001-001-A01, AND SRM 51-42-21-001-001-A01.Dec 20, 2019 · N930XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2019123071832Support Angle · corrodedCORROSION WAS FOUND ON THE LT, CENTER, AND RH SUPPORT ANGLE AT THE AFT WING-TO-FUSELAGE FAIRING, BS 847. THE SUPPORT ANGLE WAS REPLACED IAW SRM 51-42-13-001-001-A01.Dec 17, 2019 · N930XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019123071800Support · corrodedCORROSION ON FWD JACK FITTING RT SUPPORT IN THE FWD AVIONICS COMPARTMENT. THE JACK FITTING SUPPORT WAS REPLACED IAW SRM 51-42-06, AND SRM 51-42-20.Dec 17, 2019 · N930XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019123071789Hinge Fitting · corrodedCORROSION ON HINGE FITTING AT LAVATORY WASTE SERVICE DOOR NR 196ER AT AFT FAIRING AFT PANEL. THE HINGE FITTING WAS REPLACED IAW SRM 51-41-02-001-001-A01.Dec 17, 2019 · N930XJ · Cndair CL6002D24 · Fuselage, Door HingeSDR REXA2019123071788Stringer · corrodedCORROSION ON STGR27 AND ANGLE BTW FS250-263 AT FWD AVIONICS COMPARTMENT. (FUS). STGR27 WAS REPAIRED AND ANGLE WAS REPLACED PER CRJ900 SRM 53-00-03-201-001-A02 AND SRM 51-42-20-001-001-A01.Dec 17, 2019 · N930XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2019123061841Floor Support · corrodedCORROSION WAS ON FOUND ON THE RT FLOOR SUPPORT BETWEEN BS 985 - 1088 IN THE AFT CARGOBAY. THE CORROSION WAS REMOVED IAW SRM 51-21-06 AND FOUND WITHIN LIMITS IAW SRM 53-00-00, BETWEEN BS BS 1031 AND 1051 WAS REPLACED IAW SRM 51-42-06.Dec 16, 2019 · N930XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019123061833Skin · damagedSUNKEN FASTENERS WERE FOUND ON THE FUSELAGE SKIN BETWEEN BS 250 - 265, STRINGER 26L. THESKIN WAS REPAIRED IAW EA CRJ953-09950, REV IR.Dec 16, 2019 · N930XJ · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR REXA2019123061794Floor Support · corrodedCORROSION THE FLOOR SUPPORT BETWEEN BS 977 - 1088, LBL 27 IN THE AFT CARGO COMPARTMENT. THE FLOOR SUPPORT WAS REPAIRED IAW EA CRJ953-09992 REV: IRDec 16, 2019 · N930XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019123061787Skin · damagedCREASE ON FUSELAGE SKIN BETWEEN BS 310 AND 319, STRINGER 23R. THE FUSELAGE SKIN WAS REPAIRED IAW EA CRJ953-09994 REV. IR.Dec 16, 2019 · N930XJ · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR REXA2019123051839Door · damagedWORN AND BENT CUTOUT OF THE COWLING LATCH DOOR FOR THE RT NACELLE. THE COAMING LATCH DOOR WAS REPLACED IAW SRM 51-42-13-001-001-A01, AND SRM 51-42-21-001-001-A01.Dec 15, 2019 · N930XJ · Cndair CL6002D24 · Nacelle/Pylon, Main FrameSDR REXA2019123051838Latch · wornWEAR FOUND ON THE COAMING LATCH DOOR AT THE TRANSCOWL FOR THE RT ENGINE. THE COAMING LATCH DOOR WAS REPLACED IAW SRM 51-42-13-001-001-A01.Dec 15, 2019 · N930XJ · Cndair CL6002D24 · Nacelle/Pylon, Main FrameSDR REXA2019123051836Retainer · wornWEAR WAS FOUND ON THE LOWER SEAL RETAINER AFT/FWD CORNER AT CTR/FWD CARGO DOORS. THE DAMAGED SEAL RETAINERS WERE REPLACED IAW SRM 52-35-07-201-001-A01, PAR. 6B, AND AMM 52-35-07-400-802.Dec 15, 2019 · N930XJ · Cndair CL6002D24 · Cargo/Baggage DoorsSDR REXA2019123051802Floor Support · corrodedINITIAL INSPECTION: CORROSION ON INTERCOSTAL 2 LBL BTW FS 364-349. AT E/E COMPARTMENT. INTERCOSTAL 2 LBL BTW FS364/349 AT E/E COMPARTMENT WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. (LEVEL CORROSION 2)Dec 15, 2019 · N930XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019123041837Pad · wornWEAR WAS FOUND ON THE BEARING PAD LATCH DOOR FOR THE RT ENGINE TRANSCOWL. THE PAD LATCH DOOR FOR THE RT ENGINE TRANSCOWL WAS REPLACED IAW SRM 51-42-06-001-001-A01.Dec 14, 2019 · N930XJ · Cndair CL6002D24 · Nacelle/Pylon, Main FrameSDR REXA2019123041790Skin · crackedDAMAGE SEALS AND CRACK ON PYLON ACCESS PANELS SKIN 422CT AND 412CT. DAMAGE SEALS AND CRACKED SKIN ON PYLON ACCESS PANELS 422CT AND 412CT WERE REPLACED IAW SRM 51-42-06-001-001-A01 PAR. 6C, AND SRM 51-42-10-001-001-A01 PAR. 8C.Dec 14, 2019 · N930XJ · Cndair CL6002D24 · Nacelle/Pylon, Plate/SkinSDR REXA201912301842Stringer · corrodedCORROSION WAS FOUND ON STRINGER 26L, BETWEEN BS 319 - 327 IN THE MAIN AVIONICS COMPARTMENT. THE STRINGER WAS REPLACED IAW SRM 51-42-06-001-001-A01, AND SRM 51-42-21-001-001-A01.Dec 13, 2019 · N930XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA201912301835Retainer · dentedA DENT WAS FOUND ON THE LOWER SEAL RETAINER AT THE FWD CORNER OF THE CENTER CARGO DOOR, AND AFT CORNER OF THE FWD CARGO DOOR. THE LOWER SEAL RETAINERS WERE REPLACED IAW SRM 52-35-07-201-001-A01, AND AMM 52-35-07-400-802.Dec 13, 2019 · N930XJ · Cndair CL6002D24 · Cargo/Baggage DoorsSDR REXA2019123011829Frame · corrodedCORROSION WAS FOUND ON THE FRAME AT BS 349, BETWEEN STRINGERS 26 - 27R IN THE MAIN AVIONIC COMPARTMENT. THE CORROSION WAS REMOVED IAW SRM 51-21-06-001-001-A01, AND THE REWORKED AREAS WERE MEASURED AT ORIGINAL THICKNESS 0.050", MAXIMUM DEPTH REMOVED WAS 0.0Dec 13, 2019 · N930XJ · Cndair CL6002D24 · Fuselage Main, FrameSDR REXA2019123011812Stringer · corrodedCORROSION WAS FOUND ON STRINGER 26R, BS 336 - 364 IN THE MAIN AVIONICS COMPARTMENT. THE STRINGER WAS REPLACED IAW SRM 51-42-06-001-001-A01, AND SRM 51-42-21-001-001-A01.Dec 13, 2019 · N930XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2019123011808Doubler · corrodedCORROSION WAS FOUND ON THE INTERNAL DOUBLER AT BS 295 TO 310, BETWEEN STRINGERS 26L TO 26R IN THE MAIN AVIONICS COMPARTMENT. INTERNAL DOUBLER WAS REPLACED IAW SRM 51-42-06-001-001-A01.Dec 13, 2019 · N930XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
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