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 REXA2019020200129Floorbeam · corrodedCORROSION ON FLOORBEAM IN STA FS= 280 BETWEEN 11 RBL TO 12RBL AT PAX CABIN FWD WET AREA. FLOORBEAM IN STA FS= 280 BETWEEN 11RBL TO 12RBL AT PAX CABIN FWD WET AREA. WAS REPLACED PER SRM 51-42-06-001-00 1-A01 PAR 6 C; SRM 51-42-20-001-001-A01 PAR 6 C AND SRM 51-SDR REXA2019020200125Floorbeam · crackedCRACK ON FLOORBEAM UPPER/AFT FLANGE IN STA FS= 280 AND 14LBL AT PAX CABIN FWD WET AREA. FLOORBEAM WAS REPLACED PER SRM 51-42-06-001-001-A01 PAR 6 C; SRM 51-42-20-001-001-A01 PAR 6 C. AND SRM 5 1-42-13-001-001-A01 PAR 6 CSDR REXA2019020200124Angle · corrodedCORROSION ON SUPPORT MOUNTING ANGLE IN STA FS= 319 TO FS= 349 AND 41RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. LEVEL CORROSION 2. SUPPORT MOUNTING ANGLE IN STA FS= 319 TO FS= 349 AND 41RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET A
REA. WAS REPLACESDR REXA2019020200123Striker · corrodedCORROSION ON LOWER STRIKER IN STA FS= 319 TO FS= 349 AND 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. LEVEL CORROSION 2. LOWER STRIKER IN STA FS= 319 TO FS= 349 AND 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. WAS REPLACED PER SRM 51-42-06SDR REXA2019020200122Angle · crackedCRACK IN AFT SIDE PANEL LOWER ANGLE AT PASSENGER DOOR. AFT SIDE PANEL LOWER ANGLE AT PASSENGER DOOR WAS REPAIRED PER SRM 52-11-04-201-A01.SDR REXA2019020100128Frame · corrodedCORROSION ON FRAME IN STA FS= 349 BTW STR 26R TO 27 AT MAIN AVIONIC S COMPARTMENT. LEVEL CORROSION 2. FRAME IN STA FS= 349 BTW STR 26R TO 27 AT MAIN AVIONICS COMPARTMENT WAS REPAIRED PER REO 670-53-21-1
281.SDR REXA2019013100127Seat Track · corrodedCORROSION ON FLOOR SEAT RAIL IN SECTIONS FS= 375 TO FS= 485, 9LBL AT PAX CABIN FWD WET AREA. FLOOR SEAT RAILS IN SECTIONS FS= 375 TO FS= 485, 9LBL AT PAX CABIN FWD, WAS REPLACED PER SRM 53-21-49-101-001 -A01 AND AMM 53-00-49-400-801-A7.SDR REXA2019012900132Door Sill · corrodedCORROSION ON MID/AFT PRESSURE SILL AND SILL-SPLICE, WINGBOX, LT SIDE, IN STA FS= 792 TO FS= 802 BETWEEN 36LBL TO 42LB L AT PAX CABIN. LEVEL CORROSION 1. CORROSION WAS REMOVED PER SRM 51-21-06-001-001-A01 AND FLAP PEEN WAS PERFORMED ON REPAIRED AREA PER SRM 51-SDR REXA2019012900131Door Sill · corrodedCORROSION ON MID/AFT PRESSURE SILL AND SILL-SPLICE, WINGBOX, RT SIDE, IN STA FS= 792 TO FS= 802 BETWEEN 36RBL TO 42RB L AT PAX CABIN. LEVEL CORROSION 1. CORROSION WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND FLAPPEEN WAS PERFORMED ON REPAIRED AREA PER SSDR REXA2019012900130Door Sill · corrodedCORROSION ON FWD PRESSURE SILL, WINGBOX, LT SIDE, IN STA FS= 748 TO FS= 750 BETWEEN 36LBL TO 42LBL AT PAX CABIN. LEVEL CORROSION 1. CORROSION WAS REMOVED PER SRM 51-21-06-001-001-A01 AND FLAPPEEN WAS PERFORMED ON REPAIRED AREA PER SRM 51-24-11-001-001-A01 IN RSDR REXA2019012800133Seat Track · corrodedINITIAL INSPECTION: CORROSION ON SIDE SEAT RAILS IN SECTIONS [ FS= 485 TO FS= 572, STGR 15LH/RH ] [ FS= 572 TO FS= 661+16, STGR 15LH/RH ] [ FS= 661+16 TO FS= 677, STGR 15LH ] [FS= 661+16 TO FS= 661+90, STGR 15 RH ] [FS= 661+90 TO FS= 677, STGR 15RH ] AT PAX CASDR REXA2019012800134Floorbeam · corrodedCORROSION ON FLOORBEAM LBL27 STA FS=1032 AT AFT CARGO COMPARTMENT. FLOORBEAM LBL27 STA FS=1032 AT AFT CARGO COMPARTMENT WAS REPAIRED PER SRM 51-42-21-001-001-A01 AND 51-00-41-201-001-A03 AND CRJ-953-08282.SDR REXA2019012300136Seat Track · corrodedINITIAL INSPECTION: CORROSION ON FLOOR SEAT RAILS IN SECTIONS [FS= 693 TO FS= 830, 9LBL/9RBL ] [FS= 830 TO FS=849, 9LBL/9RBL ] [FS= 849 TO 977, 9LBL/9RBL ] AT PAX CABIN. (CPAX) (TCI: 100-20). COMPLETE: SUMMARY. FLOOR SEAT RAILS IN SECTIONS [ FS= 693 TO FS= 830SDR REXA2019012300138Canister · crackedINITIAL INSPECTION: CRACK IN CANISTER, WELDED NR 3 IN STA WS148 AT LT MAIN FUEL TANK. CANISTER WELDED NR 3 IN STA WS148 AT LT MAIN FUEL TANK. WAS REPAIRED PER REO 670-57-42-577 REV.SDR REXA2019012300137Canister · crackedINITIAL INSPECTION: CRACK IN CANISTER, WELDED NR 3 IN STA WS148 AT RT MAIN FUEL TANK. CANISTER WELDED NR 3 IN STA WS148 AT RT MAIN FUEL TANK. WAS REPAIRED PER REO 670-57-42-577 REV.SDR REXA2019012300135Seat Track · corrodedINITIAL INSPECTION: CORROSION ON SIDE SEAT RAILS IN SECTIONS [ FS= 677 TO FS= 720, STGR 15LH/RH ] [FS= 744 TO FS= 761, STGR 15LH/RH ] [ FS= 785 TO 847+16, STGR 15LH/RH ] [ FS= 847+16 TO FS= 906, STGR 15LH ][FS= 847+16 TO FS= 865, STGR 15RH ] AT PAX CABIN. (CPASDR REXA2019100700119Flap · puncturedPUNCTURE AT RIGHT-WING INBOARD FLAP ON FLS33. AREA WAS REPAIRED PER PER SRM 57-52-01-201-001-A01 PAR 4 D (ET)(HFEC) WAS ACCOMPLISHED, PER SRM 57-52-01-201-001-A01 PAR 4 & NDT PART 01, 51-20-006-250. NO CRACKS WERE FOUND AFTER TRIM OUT.SDR REXA2018100700118Intercostal · corrodedCORROSION ON INTERCOSTAL BTW STA FS310 TO FS319 AT STR 20R BELOW FLOOR STRUCTURE. LEVEL CORROSION 2. INTERCOSTAL BTW STA FS310
TO FS319 AT STR 20R BELOW FLOOR STRUCTURE WAS REPLACED PER SRM 51-42-21-001-001-A01.SDR REXA2018041100282Light · inoperativeRIGHT FWD OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-51-15, OPS CHECKED GOOD.SDR REXA2018033000236Light · missingFA REPORTED A PORTION OF THE EMERGENCY LIGHT STRIP IS MISSING SEAT 13A/B. LOCATED AND REINSTALLED THE EMERGENCY LIGHT STRIP IWA AMM 33-51-19SDR REXA2017101701104Unknown · odorFA REPORTED FUMES IN CABIN. EMERGENCY PROCEDURES COMPLETE. EMERGENCY DECLARED. COMPLIED WITH TS 002737. RAN BOTH ENGINES ALONG WITH APU IAW AMM 71-00-00. OPERATED PACKS FULL COLD AND FULL HOT AND NO NOTICEABLE ODOR. ALSO SWITCHED BLEED SOURCES TO ISOLATESDR REXA2017072700817Seal · brokenFORWARD PBE IN WARDROBE HAS BOTH SEALS BROKEN. REPLACED THE SEALS IAW AMM 35-31-06.SDR REXA2017071900797Battery · dischargedFORWARD EMER FLASHLIGHT AT FLT ATTENDANT STA IS NOT SECURED OR CHARGED. REMOVED AND REPLACED FLASHLIGHT BATTERY AND RESECURED IAW
AMM 25-61-00.SDR REXA2017061800716Connector · defectiveTHRU 17,000 FT ON CLIMB OUT BOTH PACKS FAILED, AIRCRAFT DEPRESSURIZED. WE LEVELED THEN DESCENDED TO 10,000. WE COMPLETED THE QRH AND RETURNED TO CVG. DUE TO ANTI-ICE LEAK DETECTION CONTROLLER (AILC) DETECTING A BLEED LEAK IN BOTH A AND B SYSTEMS. THE BLEED AISDR REXA2017030400326Oxygen Mask · unwanted deployPAX OXYGEN MASKS DEPLOYED OVER 18 C+D. REINSTALLED PAX OXYGEN MASK OVER 18 C+D PER AMM 35-21-09.
"SDR REXA2017013000147Light · missingEMERGENCY LIGHT MISSING IN ROW 13 A/B. REINSTALLED REPLACED THE LIGHT IAW AMM 33-51-01.SDR REXA2017011600043Flashlight · inoperativeFO'S EMERGENCY FLASH LIGHT INOP. REMOVED AND REPLACED FO'S EMERGENCY FLASHLIGHT AND BRACKET IAW AMM 25-61-02. NO FURTHER DEFECTS NOTED.SDR REXA2016122902540Pin · not seatedLT FWD OVERWING EMERG EXIT LOWER EMERG LIGHT EXIT SIGN INOP. FOUND PIN BUSHED/NOT LOCKED AT CONNECTOR J5422. SEATED/LOCKED PIN IAW ESPM 20-26-00. EMER LIGHT OPS TEST GOOD IAW AMM 33-51-00-710-802-A16.SDR REXA2016122802538Hinge · gougedAFT LUG LANDING FOR PAX DOOR PIANO HINGE ON FUSELAGE SIDE IS GOUGED FROM ROLL PIN. REPAIRED PAX DOOR AFT LUG LANDING FOR PAX DOOR PIANO HINGE ON FUSELAGE SIDE IAW REO:670-53-21-582 REPAIR TYPE 4.SDR REXA2016122802536Fitting · chafedLT AFT BOTTOM INBD LUG ON WING ATTACHMENT FITTING IS CHAFED. REPAIRED IAW REO 690-57-11-069 REV--DATED 12/28/16.SDR REXA2016122802535Fitting · chafedRT WING AFT BOTTOM INBD LUG ON WING ATTACHMENT FITTING IS CHAFED. REPAIRED IAW REO 690-57-11-069 REV-- DATED 12/28/16.SDR REXA2016122802523Support · corrodedCORROSION ON FWD JACKING FITTING AND LT JACK FITTING SUPPORT. REMOVED AND REPLACED THE SUPPORT IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND EA CRJ953-05156.SDR REXA2016122602524Floor Support · corrodedRIGHT FLOOR SUPPORT IS CORRODED FROM BS 280.00 - 319.70. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-13-001-001-A01, AND 51-42-21-001-001-A01.SDR REXA2016122302537Plate · chafedAFT FRAME CHAFED ON THE LT & RT SIDES. REMOVED AND REPLACED LT & RT PLATES ON VERT STAB AFT FRAME BULLET FAIRING IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 & 51-25-16-001-001-A01. P/N PLATE : AV670-21413-007 ; P/N PLATE : AV670-21413-008SDR REXA2016122302532Skin · chafedRUDDER RT LOWER L/E SKIN IS CHAFED APPROX 36"L X .3"W X .005"D. REMOVED AND REPLACED L/E SKIN IAW SRM'S 51-40-11-001-001-A01, 51-42-06-001-001-A01 &
51-25-01-001-001-A01.SDR REXA2016122302527Door Sill · corrodedFOUND CORROSION ON AFT CARGO DOOR SILL AROUND NUTPLATE HOLE JUST AFT OF BS 1000. REMOVED AND REPLACED THE AFT CARGO DOOR SILL IAW SRM 51-42-06-001-001-A01, AND 51-42-13-001-001-A01.SDR REXA2016122102533Stringer · crackedFS 280 AFT OF BULKHEAD, STRINGER 3L IS CRACKED. REPAIRED FS 280 AFT OF BULKHEAD STRINGER 3L IAW EOR53568.SDR REXA2016122102531Panel · chafedRIGHT WING PANEL 699AB HAS CHAFE. LOCATED AND DRILLED A NEW PANEL IAW SRM 51-40-11-001-001-A01.SDR REXA2016121902530Panel · chafedRIGHT FLAP VANE L/E PANEL 684ET HAS TWO MINOR CHAFES. REMOVED & REPLACED THE PANEL IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, & 51-25-01-001-001-A01.SDR REXA2016121802539Hinge · corrodedPAX DOOR TOP STEP LOWER HINGE CRACKED / MISSING LUG. REMOVED & REPLACED LOWER HINGE TO PAX DOOR TOP STEP IAW SRM 51-40-11-001-001-A01 & SRM 51-42-06-001-001-A01.SDR REXA2016121802529Panel · chafedRIGHT FLAP VANE L/E PANEL 684HT HAS A MINOR CHAFE. REMOVED & REPLACED THE PANEL IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, & 51-25-01-001-001-A01.SDR REXA2016121702541Hinge · bentAFT BAGGAGE BAY STEP PLATE AFT HINGE IS BENT AND BINDING. REMOVED TAPE. REMOVED AND REPLACED HINGE AT AFT BAGGAGE BAY STEP PLATE AFT HINGE IAW SRM 51-40-11-001-001-A01 AND SRM 51-42-06-001-001-A01.SDR REXA2016121502534Attach Angle · corrodedPAX DOOR BOTTOM STEP LOWER ATTACHMENT ANGLE HAS ELONGATED FASTENER HOLE. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE ANGLE, BOTTOM "C" P/N:601R-317726-3 IAW SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.SDR REXA2016121502528Fitting · corrodedFWD CLOSING FITTING AT PASSENGER DOOR OPENING IS CORRODED. LOCATED, DRILLED AND INSTALLED A NEW FITTING IAW SRM 51-40-11-001-001-A01, AND
51-42-06-001-001-A01.SDR REXA2016121502526Angle · corrodedPAX DOOR KICK PLATE IS CORRODED. REMOVED AND REPLACED THE KICK PLATE IAW SRM 51-40-11-001-001-A01, AND 51-42-06-001-001-A01.SDR REXA2016121502522Post · corrodedLEFT BS 280 FLIGHT DECK DOOR POST IS CORRODED ON LOWER END. REPAIRED IAW CRJ953-05137 REV A.SDR REXA2016101501933Light · inoperativeLIGHTING STRIPS FORWARD CABIN. R&R FORWARD CABIN EMERGENCY FLOOR TRACK LIGHT IAW AMM 33-51-01.
SDR REXA2016083101673Light · unsecureEMERGENCY FLOOR STRIP AT EXIT ROW FELL OFF. REINSTALLED EMERGENCY FLOOR PATH MARKING STRIP, EXIT ROW 15 A AND B IAW AMM 33-51-01. NO FURTHER DETAILS NOTED.SDR REXA2016083001613Oxygen Mask · damagedCAPTAIN SIDE, O2 MASK BUTTON USED TO PURGE MASK MISSING PLASTIC BUTTON PIECE. R & R CREW O2 MASK IAW AMM 35-11-12. PERFORMED OPS TEST OF CREW O2 SYS. OPS TEST GOOD. CREW O2, 1790 PSI IAW AMM 23-51-00 AND AMM 35-10-00.SDR REXA2016082801612Light · missingLIGHT STRIP NEXT TO FORWARD LAV AND BY EXIT ROWS 12+13 MISSING. REINSTALLED FLOOR STRIPS ON FWD LAV AND ROWS 12+13. NO FURTHER DEFECTS NOTED. REINSTALLED AS REQUIRED.
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