N908XJ
Service difficulty reports · 178
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 = 'N908XJ' 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 = 'N908XJ' 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 REXA2026051200573Angle · corrodedAFTER KICKPLATE ANGLE REMOVAL, CORROSION ON AFT CAP AND MID CAP ANGLE WAS FOUND MID CAP ANGLE WAS REPLACED PER CRJ-900 SRM 51-41-02-001-001-A01, CRJ-900 SRM 51-41-04-001-001-A01 AND AFT CAP WAS INSTALLED UNDER NRC 178 IN REFERENCE TO WIP 14.SDR REXA2026072701113Hinge Fitting · corrodedAFTER RT AILERON BUSHINGS REMOVAL: WEAR AND CORROSION ON ALL HINGE FITTINGS OF RT WING TRAILING EDGE WAS FOUND HINGE FITTINGS OF RT WING TRAILING EDGE WERE CLEANED PER SRM 51-26-00-001-001-A01 PAR 5 B CLEANING AND REPAIRED PER REO 690-57-51-491 REV. --SDR REXA2026072701094Hinge · corrodedAFTER LH AILERON BUSHINGS REMOVAL: WEAR AND CORROSION IN ALL BORE LUGS (L1,L2,L3,L4,L5,L6) AT CENTER HINGE FITTING AND HINGE 4 LUG LOWER OF AILERON WAS FOUND BORE LUGS L1 & L6 WERE CLEANED PER CRJ 900 SRM 51-26-00-001-001-A01 CLEANING, BORE LUGS L2, L3, L4 & SDR REXA2026072701135Support · corrodedCORROSION ON SETTLEMENT AREA OF BODY FAIRING SUPPORTS BTW FS881.00 AND FS 847.00. CORROSION ON SEATTLEMENT AREA OF BODY FAIRING SUPPORTS BTW FS881.00 TO FS 847.00 +16.00 WAS REMOVED PER CRJ/900 SRM 51-21-06-001-001-A01 AND WERE EVALUATED WITHIN LIMITS PER CRJ-SDR REXA2026051200570Web · crackedCRACK ON LT ELECTRICAL BAY WEB FLOOR FS 193.00 (BELOW ACCUMULATOR GAUGE INDICATOR) AT FWD EQUIPMENT COMPARTMENT LH ELECTRICAL BAY WEB FLOOR FS 193.00 (BELOW ACCUMULATOR GAUGE INDICATOR) AT FWD EQUIPMENT COMPARTMENT WAS REPAIRED PER EA NO: CRJ953-20697 REV. B ASDR REXA2026051200568Channel · corrodedCORROSION ON SUPPORTS OF SETTLEMENT AREA RT AND LT SIDE OF BINS WHEEL CORROSION ON SUPPORTS OF SEATTLEMENT AREA RT AND LT SIDE OF BINS WHEEL WAS REMOVED IAW SRM 51-21-06-001-001-A01 AND EVALUATED WITHIN OF LIMITS IAW SRM 53-00-00-101-001-A01.SDR REXA2026051200558Angle · crackedCRACK ON WING TO FUSELAGE AFT FAIRING SUPPORT STRUCTURE AT FS849, LBL17'' WING TO FUSELAGE AFT FAIRING SUPPORT STRUCTURE AT FS849, LBL17' WAS REPAIRED PER EA CRJ953-20683 REV. IRSDR REXA2026051200557Doubler · crackedINITIAL INSPECTION: CRACK ON RH ELECTRICAL BAY FLOOR WEB FS 193.00 (BELOW ADG SUPPORT DOUBLER) AT FWD ACCESORY COMPARTMENT RH ELECTRICAL BAY FLOOR WEB FS 193.00 (BELOW ADG SUPPORT DOUBLER) AT FWD ACCESORY COMPARTMENT WAS FABRICATED PER CRJ-900 SRM-53-11-43-20SDR REXA2026051200556Web · corrodedOUT OF SCOPE': CORROSION AT SERVICE DOOR LOWER SILL, FLOOR PROTECTOR WEBS (4 EAS), LOWER SILL ANGLE, PROTECTOR PLATES & STRIKER SEAL. PROTECTOR PLATES, FLOOR PROTECTOR WEB (2EAS) AND LOWER SILL ANGLE WERE CLEANED AND NOT DAMAGE WAS FOUND PER CRJ900 SRM 51-26-0SDR REXA2026051200555Angle · corrodedOUT OF SCOPE: CORROSION AT SERVICE DOOR LOWER SILL, FLOOR PROTECTOR WEBS (4 EAS), LOWER SILL ANGLE, PROTECTOR PLATES & STRIKER SEAL. PROTECTOR PLATES, FLOOR PROTECTOR WEB (2EAS) AND LOWER SILL ANGLE WERE CLEANED AND NOT DAMAGE WAS FOUND PER CRJ900 SRM 51-26-00SDR REXA2026051200553Seat Track · corrodedCORROSION AT PASSENGER SEAT TRACK, LBL 9, RBL 9 & LBL 27, BTW 349 TO FS 469.00. (INCLUDED SEAT TRACK FITTING). CORROSION AT PASSENGER SEAT TRACK, LBL 9, RBL 9 & LBL 27, BTW 349 TO FS 469.00. WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-21-49-101-001-A01 THESDR REXA2026051200551Bracket · corrodedCORROSION ON RT & LT MLG HYDRAULIC LINES SUPPORT PLATE (IN BK, LG EXT, LG RET) ON WHEEL WELL AREA, RBL 45/LBL 45. CORROSION ON LH MLG HYDRAULIC LINES SUPPORT PLATE WAS REMOVED AND EVALUATED WITHIN OF LIMITS PER CRJ-900 SRM 51-21-06-001-001-A01, CRJ-900 SRM 53-SDR REXA2026072701133Skin · crackedCRACK ON AFT UPPER BRACKET AT LH FWD AND AFT OVER WING EMERGENCY-EXIT STRUCTURE. AFT UPPER BRACKET AT LH FWD AND AFT OVERWING EMERGENCY-EXIT STRUCTURE WERE REPAIRED REO 670-52-21-103 REV: --SDR REXA2026072701132Bracket · crackedCRACK ON AFT UPPER BRACKET AT LH FWD AND AFT OVER WING EMERGENCY-EXIT STRUCTURE. AFT UPPER BRACKET AT LH FWD AND AFT OVERWING EMERGENCY-EXIT STRUCTURE WERE REPAIRED REO 670-52-21-103 REV: --SDR REXA202601134Bracket · crackedCRACK ON AFT UPPER BRACKET AT RH AFT OVERWING EMERGENCY-EXIT STRUCTURE AFT UPPER BRACKET AT RH AFT OVERWING EMERGENCY-EXIT STRUCTURE WERE REPAIRED PER REO 670-52-21-103 REV: REV: --SDR REXA2026051200567Angle · crackedCORROSION ON SILL AND ANGLE KICKPLATE AT PASSENGER DOOR SURROUND. ANGLE KICKPLATE AT PASSENGER DOOR SURROUND WAS REPLACED PER SRM 51-21-06-001-001-A01, SRM 53-21-23-101-001-A02 AND SILL WAS CLEANED PER SRM 51-26-00-001-001-A01 AND NOT DAMAGE WAS FOUND.SDR REXA2026051200541Beam · corrodedSECONDARY NRC FROM NRC 00244 - AFTER PAINT REMOVAL, CORROSION AT TRANSVERSAL BEAM, FS 333.00, BTW BL 0.0 & RBL 27 TRANSVERSAL BEAM, FS 333.00, BTW BL 0.0 & RBL 27 WAS REPAIRED PER EA NO: CRJ953-20738 REV. ASDR REXA2026051200540Skin · wornWEAR ON EXTERNAL FUSELAGE SKIN FS913.00 TP FS 927.00 BTW STGR 26LH TO STGR 26RH DISTRIBUTION DUCT FS913.00 TP FS 927.00 WAS REMOVED AND INSTALLED PER CRJ-900 AMM 21-23-38, LEAK TEST WAS PERFORMED PER CRJ-900 AMM 21-23-00. WEAR ON EXTERNAL FUSELAGE SKIN FS913.0SDR REXA2026051200564Fitting · crackedINITIAL INSPECTION: CRACK ON AFT CAM FITTING AT FS. 349.00 FRAME ON PASSENGER DOOR SURROUND STRUCTURE. CAM FITTING AT FS. 349.00 FRAME ON PASSENGER DOOR SURROUND STRUCTURE WAS REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01SDR REXA2026051200539Drag Angle · crackedCRACK ON LH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD & AFT DRAG ANGLE BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUM CRACK ON LH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD & AFT DRAG ANGLE BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUMSDR REXA2026051200538Attach Angle · crackedCRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD & AFT DRAG ANGLE BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUM RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUM WAS REPAIRED PER CRJ-900 SRM SDR REXA2026072701114Lug · corrodedWEAR AND CORROSION IN ALL BORE LUGS (R1,R2,R3,R4,R5,R6) AT CENTER HINGE FITTING AND HINGE 4 LUG UPPER OF AILERON WAS FOUND. BORE LUGS R1, R6 & HINGE 4 LUG UPPER WERE CLEANED PER CRJ 900 SRM 51-26-00-001-001-A01 AND NO DAMAGE FOUND. LUGS R3 Y R4 WERE REPAIRED PSDR REXA2026051200559Support · crackedINTERNAL LOWER ANGLE OF EXTERNAL POWER RECEPTACLE SUPPORT STRUCTURE IINTERNAL LOWER ANGLE OF EXTERNAL POWER RECEPTACLE SUPPORT STRUCTURE WAS REPLACED PER SRM 51-42-06-001-001-A01 AND SRM 51-42-10-001-001-A01 TO GAIN ACCESS EXTERNAL AC POWER RECEPTACLE P/N: MS9SDR REXA2026051200549Web · crackedPASSENGER DOOR BELOW TOP STEP WEB IS CRACKED ON AFT SIDE TOP STEP WEB ON AFT SIDE OF PASSENGER DOOR WAS REPAIRED PER SRM 52-11-04-201-006-A01SDR REXA2026051200548Support · crackedCRACK ON MAIN LANDING GEAR BINS SUPPORT STRUCTURE RETAINER ANGLE RH (FS 797.00 AND RBL 34). MAIN LANDING GEAR BINS SUPPORT STRUCTURE RETAINER ANGLE RH (FS 797.00 AND RBL 34) WAS REPLACED PER CRJ-900 SRM 51-41-02-001-001-A01SDR REXA2026051200547Hinge · crackedCRACK AT FWD / MIDDLE & AFT HINGES OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT FWD / MIDDLE & AFT HINGES OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT WERE REMPLACED PER CRJ-900 SRM 51-42-06-001-001-A01.SDR REXA2026051200546Hinge · crackedCRACK AT FWD / MIDDLE & AFT HINGES OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT FWD / MIDDLE & AFT HINGES OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT WERE REMPLACED PER CRJ-900 SRM 51-42-06-001-001-A01SDR REXA2026051200545Hinge · crackedCRACK AT FWD / MIDDLE & AFT HINGES OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT FWD / MIDDLE & AFT HINGES OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT WERE REMPLACED PER CRJ-900 SRM 51-42-06-001-001-A01SDR REXA2026051200544Stop · crackedBROKEN STOPPERS 2 EAS OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT STOPPERS 2 EAS OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT WERE REPAIRED PER EA NO. CRJ953-20779 REV. IR AND EA NO. CRJ953-20769 REV. IRSDR REXA2026051200543Stop · crackedBROKEN STOPPERS 2 EAS OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT STOPPERS 2 EAS OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT WERE REPAIRED PER EA NO. CRJ953-20779 REV. IR AND EA NO. CRJ953-20769 REV. IRSDR REXA2026051200542Attach Angle · crackedCRACK ON ATTACHMENT ANGLE INNER SKIN-TO-AFT SIDE PANEL AT PASSENGER DOOR EXTERNAL STRUCTURE ANGLE INNER SKIN-TO-AFT SIDE PANEL AT PASSENGER DOOR EXTERNAL STRUCTURE WAS REPAIRED PER CRJ-900 SRM 52-11-04-201-002-A01SDR REXA2024123001621Battery Pack · inoperativeMULTIPLE EMERGENCY LIGHTS INOP NEAR FWD LH AND RH EMERGENCY EXITS R/R EPSU #5 PS43 IAW AMM 33-51-17 OPS CHECK GOOD PN ON/OFF 2013-1ASMI SN OFF 19038 SN ON 19242SDR REXA2024041900358Controller · failedLEFT WINDSHIELD CONTROLLER PRODUCED ELECTRICAL SMELL AND SMOKE. INSPECTED LEFT HAND WINDSHIELD, NO DAMAGE TO STRUCTURE REF AMM 56-11-01. DEFERRED LEFT WINDSHIELD HEAT MEL 30-41-01A MX PROCEDURE C/W MOC NOTIFIED 7821 PLACARD INSTALLED**REMOVED AND REPLACED LH SDR REXA2022060901086Power Supply · dischargedFOUND EMER LIGHT AT FWD CABIN INOP. REMOVED AND REPLACED EMER LIGHT BATT PS35 IAW AMM 33-51-17. OPS CHECK GOOD.SDR REXA2022051800968Frame · corrodedFRAME FS 954.00 IS CORRODED BETWEEN STGR 26L AND 25R. REMOVED AND INSTALLED FS954.00. FRAME SECTOR FROM STRINGER 25L TO STRINGER 25R REF. CRJ900 SRM 51-42-06-001-001-A01 AND ENDEAVOR AIR EA CRJ953-13485 DATED 4/30/2022 REV IR.SDR REXA2022051800967Frame · corrodedFRAME AT FS 942.00 BETWEEN STGR 22R AND 26L IS CORRODED. COMPLIED WITH EA CRJ953-13484 DATED 4/30/2022 REV IR REPAIRED/REPLACED FS942 FRAME STR 20R-STR 25LSDR REXA2022051800966Frame · corrodedPAX DOOR FORWARD FORMER HAS CORROSION ON ITS INTERIOR SIDE AT THE LOWER LATCH CAM AREA REPLACED CORRODED PAX DOOR FWD FORMER WITH NEW REPLACEMENT FORMER (PN 601R318031-5S) USING ALL NEW FASTENERS. REF BOMBARDIER DWG#601R31702 REV N AND CRJ900 SRM 51-42-06-001-SDR REXA2022051800948Frame · corrodedFRAME FS501.00 LOWER FLANGE AND WEB ARE CORRODED STGR24L-26L REPLACED WITH NEW FRAME SECTOR AT FS-501 BETWEEN STGR 25L AND STGR 19L REF CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-20-001-001-A01 AND DWG. NO. SH690-33750 REV Y.SDR REXA2022051800947Angle · corrodedLEFT MAIN LANDING GEAR WHEEL WELL FORWARD ATTACH ANGLE FOR 542AZ IS CORRODED. REMOVED UNSERVICEABLE AND INSTALLED NEW RIGHT MAIN LANDING GEAR WHEEL WELL FORWARD. ATTACH ANGLE FOR 542AZ. REF CRJ900 SRM 51-42-21-001-001-A01, LEAK CHECK GOOD.SDR REXA2022051800946Angle · corrodedRIGHT MAIN LANDING GEAR WHEEL WELL FORWARD ATTACH ANGLE FOR 642AZ IS CORRODED. REMOVED UNSERVICEABLE AND INSTALLED NEW RIGHT MAIN LANDING GEAR WHEEL WELL FORWARD. ATTACH ANGLE FOR 642AZ. REF CRJ900 SRM 51-42-21-001-001-A01, LEAK CHECK GOOD.SDR REXA2022051800951Stringer · corrodedSTRINGER 25R REPLACMENT FS280-FS333 DUE TO HEAVY CORROSION DAMAGE. COMPLIED WITH REPLACEMENT OF THE STRINGER 25R FROM FS280 TO FS333 REF ENGINEERING AUTHORIZATION CRJ953-13383, DATED 4/16/2022SDR REXA2022051800952Piston · corrodedLH MAIN LANDING GEAR HAS MINOR CORROSION AND MISSING FINISH AT #2 AXLE ROOT RADIUS. ATTACHED GENERIC REO 670-32-11-361 REV-DATED 2014-07-30 ROUTINELY USED TO REPAIR THIS DAMAGE. COMPLIED WITH THE REPAIR ON LH MLG PISTON AXLE #2 REF REO 670-32-11-361 REV A, DASDR REXA2022051800950Intercostal · corrodedINTERCOSTAL 20R HAS CORROSION. AFT OF FS 379.00. REPLACED INTERCOSTAL 20R LOCATED AT FS319 TO FS349 REF CRJ900 SRM 51-42-06-01-001-001-A01, CRJ900 SRM 51-42-21-001-001-A01, DWG #SH670-31950 REV YSDR REXA2022051800949Intercostal · corrodedINTERCOSTAL 20R HAS CORROSION. FORWARD OF FS 379.00. REPLACED INTERCOSTAL 20R LOCATED AT FS310 TO FS319 REF CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-21-001-001-A01 DWG #SH670-31950 REV Y.SDR REXA2019021100140Wire · burnedONCE IN FLIGHT GOT A STRONG SMELL OF FUMES IN FLIGHT DECK. WAS AN ELECTRIC BURNING SMELL. DECIDED IT WAS TO STRONG AND DIVERTED BACK TO JFK. T/S AND FOUND LT WINDOW WIRES P1/P2 BURNED, R&R P1&P2 TERMINALS IAW ESPM 20-16-00. R&R LT WINDOW IAW JC 900-56-900-902,SDR REXA2018080870677Oxygen Mask · brokenCAPTAIN`S SIDE OXYGEN MASK, RED TAB WAS BROKEN. R & R THE OXYGEN MASK IAW AMM 33-25-03, OPS CHECKED GOOD.SDR REXA2018072400641Light · wornEMERGENCY PATH LIGHTING STRIPS IN FRONT OF WARDROBE AND FWD LAV ARE WORN. REMOVED AND REPLACED EPL WARDROBE AND FWD LAV IAW AMM 33-51-01-000-801 A021 AND 33-51-01-400-801-A021.SDR REXA2018072400639Angle · crackedMAIN ENTRY DOOR HAS A CRACKED ANGLE AFT SIDE FWD OF DOOR ASSIST SWIVEL PULLEY. REMOVED AND REPLACED AFT ANGLE ON MAIN ENTRY DOOR ASSIST SWIVEL PULLEY IAW SRM 52-11-04.SDR REXA2018072400640Lens · crackedPANEL ABOVR SERVICE DOOR EMERGENGY LIGHT LENS CRACKED. REMOVED AND REPLACED NEW LIGHT LENS AT PANEL ABOVE SERVICES DOOR AS REQUIRED WITH LIGHT HAND PRESSURE.SDR REXA2018072400638Floorbeam · corrodedWHILE REMOVING FWD FLIGHT DECK FLOOR SUPPORT FOUND RT 280 FLOORBEAM CORRODED. REMOVED DAMAGED FS280 RT FLOOR SUPPORT BEAM & INSTALLED NEW BEAM IAW SRM 51-42-06, 51-42-13, 51-42-21.
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