N918XJ
Service difficulty reports · 210
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 = 'N918XJ' 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 = 'N918XJ' 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 REXA2026032700248Hinge · corrodedCORROSION WAS FOUND ON FITTINGS LH AND RH SIDE AT AFT NOSE LANDING GEAR DOOR AND ALSO ON FUSELAGE STRUCTURE (4EAS). DUE TO EXCESSIVE CORROSION PER CRJ 900 SRM 51-10-06-001-001-A01 ON FITTINGS (4EAS) LH AND RH SIDE AT AFT NOSE LANDING GEAR DOOR AND ALSO ON FUSESDR REXA2026032700247Fitting · corrodedCORROSION WAS FOUND ON FITTINGS LH AND RH SIDE AT AFT NOSE LANDING GEAR DOOR AND ALSO ON FUSELAGE STRUCTURE (4EAS). DUE TO EXCESSIVE CORROSION PER CRJ 900 SRM 51-10-06-001-001-A01 ON FITTINGS (4EAS) LH AND RH SIDE AT AFT NOSE LANDING GEAR DOOR AND ALSO ON FUSESDR REXA2026032700246Fitting · corrodedCORROSION WAS FOUND ON FITTINGS LH AND RH SIDE AT AFT NOSE LANDING GEAR DOOR AND ALSO ON FUSELAGE STRUCTURE (4EAS). DUE TO EXCESSIVE CORROSION PER CRJ 900 SRM 51-10-06-001-001-A01 ON FITTINGS (4EAS) LH AND RH SIDE AT AFT NOSE LANDING GEAR DOOR AND ALSO ON FUSESDR REXA2026032700273Hinge Bracket · corrodedCORROSION ON FWD HINGE AT FLAP STEP PLATE WAS FOUND. CORROSION ON FWD HINGE AT FLAP STEP PLATE WAS FOUND WAS EVALUATED OUT OFF LIMITS PER CRJ 900 SRM 51-10-06-001-001-A01 AND FWD HINGE AT FLAP STEP WAS REPAIRED PER EA NO:CRJ953-21661 REV.IRSDR REXA2026032700264Web · crackedCRACK ON BIN SUPPORT MEMBRANE ON RBL34 AT FWD FACE OF MLG WHEEL WELL. BIN SUPPORT MEMBRANE ON RBL34 AT FWD FACE OF MLG WHEEL WELL WAS REPLACED PER CRJ900 SRM 51-41-02-001-001-A01SDR REXA2026032700259Floor Support · crackedCRACKED ANGLES AT FLOOR SUPPORT STRUCTURE BTW FS 260.00 TO 280.00 AND RBL 12.00 AND LBL12.00. ANGLES AT FLOOR SUPPORT STRUCTURE BTW FS 260.00 TO 280.00 AND RBL 12.00 AND LBL12.00 WERE REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01 ,SRM 51-42-10-001-001-A01 ANDSDR REXA2026032700258Floor Support · crackedCRACKED ANGLES AT FLOOR SUPPORT STRUCTURE BTW FS 260.00 TO 280.00 AND RBL 12.00 AND LBL12.00. ANGLES AT FLOOR SUPPORT STRUCTURE BTW FS 260.00 TO 280.00 AND RBL 12.00 AND LBL12.00 WERE REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01 ,SRM 51-42-10-001-001-A01 ANDSDR REXA2026032700257Striker · corrodedCORROSION ON STRIKER SILL AND ANGLE MOUNTING AT GALLEY SERVICE DOOR SURROUND STRUCTURE CORROSION ON STRIKER SILL AND ANGLE MOUNTING AT GALLEY SERVICE DOOR SURROUND STRUCTURE WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01, ANGLE MOUNTING WAS EVALUATED WHITIN SDR REXA2026032700255Support · corrodedCORROSION ON SETTLEMENT AREA OF BODY FAIRING ACCESS PANELS 195AB, 195BB, 196AR AND 195AL AT AFT BODY FAIRING SUPPORT STRUCTURE. CORROSION ON SETTLEMENT AREA OF BODY FAIRING ACCESS PANELS 195AB, 195BB, AND 195AL WAS REMOVED AND EVALUATED WITHIN LIMITS CRJ900 SSDR REXA2026032700271Angle · crackedCRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUMSDR REXA2026032700270Angle · crackedCRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD AND AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). CRACKS ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD AND AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5%SDR REXA2026032700256Angle · corrodedCORROSION ON FWD, AFT AND MID CAP ANGLE AT PASSENGER DOOR SURROUND STRUCTURE. CORROSION ON FWD, AFT WAS REMOVED AND EVALUATED WITHIN LIMITS CRJ 900 SRM 51-21-06-001-001-A01 AND CRJ-900 SRM 53-00-00-101-001-A01, AND MID CAP ANGLE AT PASSENGER DOOR SURROUND STRSDR REXA2026032700254Cover · crackedCRACKED HANDLE COVER AT PASSENGER DOOR. HANDLE COVER AT PASSENGER DOOR WAS REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01SDR REXA2026032700269Web · crackedCRACKED FLOOR WEB RIGHT SIDE AT_ ELECTRICAL BAY (BELOW ADG SUPPORT DOUBLER) FS193.00 CRACKED DOUBLER AT FLOOR WEB RIGHT SIDE AT_ ELECTRICAL BAY (BELOW ADG SUPPORT DOUBLER) FS193.00 WAS REPLACED PER CRJ-900 SRM 53-11-43-201-001-A01, SRM 51-42-06-001-001-A01 SDR REXA2026032700268Web · crackedCRACKED FLOOR WEB LEFT SIDE AT_ ELECTRICAL BAY (BELOW BRAKE ACCUMULATOR INDICATION SUPPORT DOUBLER) FS193.00. FLOOR WEB LEFT SIDE AT_ ELECTRICAL BAY (BELOW BRAKE ACCUMULATOR INDICATION SUPPORT DOUBLER) FS193.00 WAS REPAIRED PER CRJ 900 SRM 53-11-43-201-001-A0SDR REXA2026032700267Skin · crackedTORN UPPER AND LOWER AFT SEAL AT RT UPPER AND LOWER THRUST REVERSE ALSO CRACK AFT SEAL PLATE AT RT LOWER THRUST REVERSE. CRACK AFT SEAL PLATE AT RT LOWER THRUST REVERSE WAS REPAIRED PER EA CRJ954-21516 REV IR AND UPPER AND LOWER AFT SEAL AT RT UPPER AND LOWERSDR REXA2026032700263Support · 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 CRJ900 SRM 51-42-06-001-001-A01SDR REXA2026032700261Fitting · corrodedCORROSION ON FITTING (10 EACH) BTW FS280/FS379 AND LBL42/RBL42 AT FLOOR STRUCTURE. CORROSION ON FITTING (10 EAÏ¿½S) BTW FS280/FS379 AND LBL42/RBL42 AT FLOOR STRUCTURE WAS CLEANED, REMOVED, EVALUATED WHITIN LIMITS, EVALUATED DUE TO EXCESSIVE DAMAGE AND REPLACSDR REXA2026032700253Fairing · crackedCRACKED THRUST-REVERSER AFT UPPER HINGE LINE FAIRING 443BT ALSO BEND AND WEAR AFT LOWER HINGE LINE FAIRING 443BB AT RH ENGINE. THRUST-REVERSER AFT UPPER HINGE LINE FAIRING 443BT WAS REPLACED PER CRJ900 AMM 54-12-01 AND AFT LOWER HINGE LINE FAIRING 443BB AT RHSDR REXA2026032700262Fitting · corrodedCORROSION ON PROXIMITY SENSOR PX36 AT GALLEY SERVICE DOOR CORROSION ON FITTING ASSY, SLIDE AT GALLEY SERVICE DOOR WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND DUE TO EXCESSIVE DAMAGE WILL BE REPLACE PER CRJ 900 SRM 53-21-43-101-001-A03 AND WAS REPLACEDSDR REXA2026032700251Hinge · corrodedCORROSION ON HINGE(2EAS), HINGE ARMS(2EAS) AND HARDWARE ATTACHED TO ACCESS DOOR 196DR HINGE ASSY LWR P/N CC670-39189-1 WAS CLEANED PER CRJ900 SRM 51-26-00-001-001-A01 AND CORROSION WAS NOT FOUND AND DUE TO EXCESSIVE CORROSION ON HINGES OUTBD (NP: CC670-39095-1SDR REXA2026032700250Hinge · corrodedCORROSION ON HINGE(2EAS), HINGE ARMS(2EAS) AND HARDWARE ATTACHED TO ACCESS DOOR 196DR HINGE ASSY LWR P/N CC670-39189-1 WAS CLEANED PER CRJ900 SRM 51-26-00-001-001-A01 AND CORROSION WAS NOT FOUND AND DUE TO EXCESSIVE CORROSION ON HINGES OUTBD (NP: CC670-39095-1SDR REXA2026032700249Hinge · corrodedCORROSION ON HINGE(2EAS), HINGE ARMS(2EAS) AND HARDWARE ATTACHED TO ACCESS DOOR 196DR HINGE ASSY LWR P/N CC670-39189-1 WAS CLEANED PER CRJ900 SRM 51-26-00-001-001-A01 AND CORROSION WAS NOT FOUND AND DUE TO EXCESSIVE CORROSION ON HINGES OUTBD (NP: CC670-39095-1SDR REXA2026080301384Landing · cracked"CRACK ON AFT RH DOOR LANDING AT FS 188.00 (LATCH CUT OUT OF ACCESS DOOR 212AR) RH DOOR LANDING AT FS 188.00 (LATCH CUT OUT OF ACCESS DOOR 212AR) WAS MANUFACTURED PER EA NO: CRJ953-21561 REV IR, DWG CC670-33151-6 REV ""D"", AND REPLACED PER CRJ 900 SRM 51-42-0SDR REXA2026032700274Landing · crackedCRACK ON AFT RH DOOR LANDING AT FS 188.00 (LATCH CUT OUT OF ACCESS DOOR 212AR) RH DOOR LANDING AT FS 188.00 (LATCH CUT OUT OF ACCESS DOOR 212AR) WAS MANUFACTURED PER EA NO: CRJ953-21561 REV IR, DWG CC670-33151-6 REV ""D"", AND REPLACED PER CRJ 900 SRM 51-42-06SDR REXA2026032700260Support · crackedCRACKED INTERNAL ANGLE OF EXTERNAL POWER RECEPTACLE SUPPORT STRUCTURE INTERNAL ANGLE OF EXTERNAL POWER RECEPTACLE SUPPORT STRUCTURE WAS REPLACED PER CRJ900 SRM 51-41-10-001-001-A01 AND SRM 51-42-06-001-001-A01SDR REXA2022072500532Post · crackedUPON REMOVAL LBL 27 POST WAS FOUND TO BE CRACKED. INSTALLED SERVICABLE LBL 27 POST IAW SERVICE BULLETIN FIGURE 105, SHEET 4 OF 8.SDR REXA2022080801754Fitting · crackedRH FWD EMERGENCY EXIT DOOR HAS CRACK IN AFT PROX SENSOR FITTING. REPAIRED CRACKED STRUCTURE IN RH FWD EMERGENCY EXIT DOOR PER EA CRJ952-14082 REV IR, DATED 7/7/2022SDR REXA2022080301731Channel · chafedRH LOWER TRANSCOWL LATCH DOOR COAMING CHANNEL CHAFED. REPLACED CHANNEL.SDR REXA2022080301730Skin Panel · corrodedPASSENGER DOOR INNER SKIN CORRODED. REPLACED PASSENGER DOOR INNER SKIN.SDR REXA2022072601698Bracket · crackedLH UPPER TRANSCOWL OUTBOARD-FWD STANDOFF ("A" BRACKET) CRACKED/BROKEN. REPLACED LH UPPER TRANSCOWL OUTBOARD-FWD STANDOFF.SDR REXA2022072601697Bracket · crackedLH UPPER TRANSCOWL INBOARD-FWD STANDOFF ("A" BRACKET) CRACKED/BROKEN. REPLACED LH UPPER TRANSCOWL INBOARD-FWD STANDOFF..SDR REXA2022072601694Panel · corrodedPASSENGER DOOR TOP PANEL AT UPPER STAIR WEB CORRODED. REPLACE PAX DOOR TOP PANEL AT UPPER STAIR WEB.SDR REXA2022072201657Transcowl · crackedAFTER REMOVAL OF Z-ANGLE ON UPPER RH TRANSCOWL (FOR REPAIR OF DAMAGED FASTENERS) FOUND 1.159" CRACK IN INNER PERFORATED SKIN. REPAIRED RH UPPER TRANSCOWL SKIN PER EA CRJ954-13905 REV B.SDR REXA2022072601696Sill Drain · corrodedFLOOR SILL CORRODED AT FS 565.00 LH SIDE INSTALLED NEW LH LOWER FLOOR SILL FROM FS517 TO FS565 REF CRJ900 SRM 51-42-06-001-001-A01SDR REXA2022072001612Frame · corrodedFRAME INTERNAL TO PAX DOOR AT FS313.56 BETWEEN DD4-DD5 HAS INTERGRANULAR CORROSION AROUND RIVET HOLES. REMOVED AND REPLACED CORRODED FRAME WITH NEW REPLACEMENT FRAME (P/N 601R318086-1) AND CLEAT (P/N 600-31902-269) USING ALL NEW HARDWARE. REF BOMBARDIER DWG 60SDR REXA2022072001613Latch · chafedRH UPPER TRANSCOWL LATCH DOOR CHAFED IN MULTIPLE AREAS REPLACED RH UPPER TRANSCOWL LATCH DOORSDR REXA2022072001611Floor Panel · corrodedBACKUP SILL, STRINGER 21L, FS310-333 CORRODED BER. REPLACED BACKUP SILL, STRINGER 21L, FS310-333.SDR REXA2022080301729Panel · corrodedPASSENGER DOOR, TOP PANEL ON STAIR WEB, AROUND SCREW HOLES HAS EVIDENCE OF CORROSION. REPLACED PASSENGER DOOR TOP PANEL ON STAIR WEBSDR REXA2022072001614Channel · chafedRH LOWER TRANSCOWL CHANNEL C, FORWARD, IS CHAFED REPLACED CHANNEL C, FORWARDSDR REXA2022071801600Latch · chafedLATCH DOOR COAMING CHAFED ON RH LOWER TRANSCOWL. "
REPLACED LATCH DOOR COAMING ON RH LOWER TRANSCOWL."SDR REXA2022071801598Track · corrodedSEAT TRACK AT RBL9, FS349-379 IS CORRODED IN SEVERAL AREAS, ON SEVERAL ELEMENTS. REPLACED SEAT TRACK PN SH670-32159-1 WITH NEW PART.SDR REXA2022072001610Intercostal · corrodedPASSENGER DOOR INTERNAL STRUCTURE AT MID INTERCOSTAL DD6 HAS EVIDENCE OF CORROSION. REPLACED MID INTERCOSTAL DD6 PER CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-01-001-001-A01, DWG 601R31702 REV N.SDR REXA2022080301728Frame · corrodedFS1031.00 FRAME HAS CORROSION ON ITS ATTACHED FLANGE BETWEEN STGR23L AND 24LSDR REXA2022071801599Panel · chafedLH INBOARD FLAP LEADING EDGE SKIN PANEL 584GB IS CHAFED FROM CONTACT WITH MOVABLE FLAP VANE. REPLACED PANEL 584GB WITH NEW SKIN PANEL PN CC670-14178-1.SDR REXA2020020520149Floor Panel · delaminatedAWR: DELAMINATED FLOOR PANELS NBR , NRB 281DLF AND 282JRF AT AFT CARGO COMPARTMENT (COMPOSITE).
SUMMARY: FLOOR PANELS NBR , NRB 281DLF AND 282JRF AT AFT CARGO COMPARTMENT WERE REPLACED PER CRJ-900 AMM 53-00-47-400SDR REXA2019111421591Unknown · noneWHILE INCORPORATING SB607BA-57-020, CLEARANCE ISSUES WITH 1 FASTENER EACH SIDE UNDER FITTING.
COMPLIED WITH BOMBARDIER REO 690-57-21-322 REV. DATED 2019-11-08. WVAC EMP STAMP 771.SDR REXA2019090501288Light · inoperativeESCAPE PATH LIGHTS IN GALLEY (R & L) BULBS INOP PN OL3071BPEGPL. REPLACED INOP BULBS IAW AMM 33-51-11. OP CK GOOD PN OL3071BPEGPL.SDR REXA2019020300121Stringer Splice · corrodedOUT OF LIMITS CORROSION ON STRINGER SPLICE 25R IN STA FS= 329 TO FS= 339 AT MAIN AVIONICS COMPARTMENT. STRINGER SPLICE 25R BTW FS329/339 WAS REPLACED PER SRM 51-42-06-001-001-A01 PAR 6D AND SRM 51-42-20-001-001-A0 1 PAR 6E.SDR REXA2019020300120Stringer · corrodedCORROSION ON STRINGER 25R IN STA FS= 280 TO FS= 329 AT MAIN AVIONICS COMPARTMENT. CORROSION LEVEL 2; STRINGER 25R IN STA FS= 280 TO FS= 329 AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER SRM 51-42-06-001-001-A01.
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