N925XJ
Service difficulty reports · 192
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 = 'N925XJ' 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 = 'N925XJ' 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 REXA2019101471444Access Panel · brokenBROKEN ACCESS PANEL 433BT AT LH PYLON. SKIN ON ACCESS PANEL 433BT AT LH PYLON WAS REPLACED FOR A NEW ONE (P/N: CN624-4230-205) PER CRJ-900 SRM 51-42-06.SDR REXA2019101471442Frame · corrodedCORROSION ON FRAME IN STA. FS= 310 BETWEEN STRG 26 LH TO 24RH AT MAIN AVIONIC COMPARTMENT. THE FRAME WAS REPAIRED PER EA NO: CRJ953-09705 REV IR,SDR REXA2019101471441Frame · corrodedCORROSION ON FRAME IN STA. FS= 295 BETWEEN STRG 25 LH TO 26RH AT MAIN AVIONIC COMPARTMENT. THE FRAME WAS REPAIRED PER EA CRJ953-09706 REV. IR.SDR REXA2019101471431Access Panel · wornWEAR ON ACCSSES NBR 422CT AND 422DB AT RH ENGINE. THE ACCESS PANELS WERE REPLACED IAW SRM 51-42-06-001-001-A01.SDR REXA2019101461438Stringer · corrodedCORROSION ON STRINGER 27 IN STA. FS= 280 TO FS= 295 AT MAIN AVIONICS COMPARTMENT. STRINGER WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-20-001-001-A01.SDR REXA2019100501472Canister · leakingINITIAL INSPECTION : CRACK IN CANISTER, WELDED NO.3 IN STA WS148 AT LH MAIN FUEL TANK. (AI). CANISTER WELDED NO.3 IN STA WS148 AT LH MAIN FUEL TANK, WAS REPAIRED PER, REO 670-57-42-577 REV --. FUEL LEAK CHECK LH MAIN FUEL TANK WAS PERFORMED PER CRJ-900 AMM 28-SDR REXA2019101451471Canister · crackedCRACK IN CANISTER, WELDED NR 3 IN WS 148 AT THE RT MAIN FUEL TANK. THE CANISTER WAS REPAIRED PER, REO 670-57-42-577 REV --. FUEL LEAK CHECKED THE RH MAIN FUEL TANK WAS PERFORMED PER AMM 28-11-00-790-801-A01 AND NO LEAK WAS FOUND.SDR REXA2019101451467Support Plate · corrodedCORROSION ON PROTECTION PLATE SUPPORTS IN FS= 322 AND 332 AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. PROTECTION PLATE SUPPORTS (2EA) WERE REPLACED PER CRJ-900 SRM 51-42-06 AND SRM 51-42-21SDR REXA2019101451466Striker · corrodedCORROSION AND WEAR ON LOWER STRIKER BS 319 TO 349 AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. SEAL STRIKER WAS REPLACED PER CRJ 900 SRM 51-42-06SDR REXA2019101451421Intercostal · corrodedCORROSION ON INTERCOSTALS (4EAS) BTW FS 349-364, STGR 26L-26R. INTERCOSTALS (4EAS) BTW FS 349-364, STGR 26L-26R WERE REPLACED PER CRJ900 SRM 51-42-06. AND SRM 51-42-20.SDR REXA201910141469Support Plate · corrodedCORROSION ON PROTECTION PLATE SUPPORTS FS= 336 AND 346 AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. PROTECTION PLATE SUPPORTS (2EA) WERE REPLACED PER CRJ-900 SRM 51-42-06 AND SRM 51-42-21SDR REXA2019101401436Support Angle · corrodedCORROSION ON TIRE BURST SUPPORT STRUCTURE P/N AT LH MLG AFT FACE REAR SPAR. TIRE BURST SUPPORT STRUCTURE AT LH MLG AFT FACE REAR SPAR WAS REPLACED FOR NEW ONE (P/N: CC670-10338-1) PER CRJ-900 SRM 51-42-20. FUEL LEAK CHECK LH MAIN FUEL TANK WAS PERFORMED AND SDR REXA2019101401435Angle · corrodedCORROSION ON TIRE BURST SUPPORT STRUCTURE AT RH MLG AFT FACE REAR SPAR. TIRE BURST SUPPORT STRUCTURE AT RH MLG AFT FACE REAR SPAR WAS REPLACED FOR NEW ONE (P/N: CC670-10338-2) PER CRJ-900 SRM 51-42-20. FUEL LEAK CHECK WAS PERFORMED AND NO LEAK WAS FOUND.SDR REXA2019101401434Crossbeam · crackedAWR IN REF EO R53581 STEP 22 DURING REMOVAL OF RH DRIP TRAY, CRACK WAS FOUND ON CROSS BEAM FS 280 RBL 13. CROSS BEAM FS 280 RH SIDE WAS REPLACED PER CRJ-900 SRM 51-42-06. AND SRM 51-42-21.SDR REXA2019101421468Stringer · corrodedCORROSION ON STRINGER 23RH IN STA. FS= 337 TO FS=364 AT MAIN AVIONICS COMPARTMENT. STRINGER 23RH IN STA. FS= 337 TO FS= 364 AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01 AND SRM 51-42-06-001-001-A01.SDR REXA2019101421463Stringer · corrodedINITIAL INSPECTION: CORROSION ON STRINGER 23RH IN STA. FS= 280 TO FS=327 AT MAIN AVIONICS COMPARTMENT. STRINGER 23RH IN STA. FS= 280 TO FS= 333 WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.SDR REXA2019101421462Stringer · corrodedINITIAL INSPECTION: CORROSION ON STRINGER 22RH IN STA. FS= 280 TO FS=327 AT MAIN AVIONICS COMPARTMENT. STRINGER 22RH IN STA. FS= 280 TO FS= 333 WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.SDR REXA2019101421459Floor Support · corrodedINITIAL INSPECTION:CORROSION ON FLOOR BEAM LBL 27 BTW STA FS:1015 AND 1030 AT AFT CARGO COMPARTMENT FLOOR BEAM LBL 27 BTW FS1015/1030 AT AFT CARGO COMPARTMENT WAS REPAIRED PER CRJ-900 SRM 53-00-41-201-001-A03, SRM 51-42-20-001-001-A01 AND SRM 51-42-06-001-001SDR REXA2019101421443Frame · corrodedCORROSION ON FRAME BS 349 BETWEEN STRINGERS 25L TO 24R IN THE MAIN AVIONIC COMPARTMENT. THE FRAME SECTION WAS REPLACED IAW SRM 51-42-20-001-001-A01, AND SRM 51-42-06-001-001-A01.SDR REXA2019101421439Intercostal · corrodedCORROSION ON STRINGER 25RH IN STA. FS= 280 TO FS= 310 AT MAIN AVIONICS COMPARTMENT. THE STRINGER WAS REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01SDR REXA2019101421422Intercostal · corrodedCORROSION ON INTERCOSTALS (2EAS) BTW FS 394-409, LBL3-RBL3. INTERCOSTALS (2EAS) BTW FS 394-409, LBL3-RBL3. WERE REPLACED PER CJ900 SRM 51-42-06. AND SRM 51-42-20.SDR REXA2019101421419Structure · crackedINITIAL INSPECTION: CRACK ON BOX [INTERNAL STRUCTURE] AT AC-EXTERNAL GROUND POWER SERVICE PANEL. BOX AT AC-EXTERNAL GROUND POWER SERVICE PANEL(122DR) WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-20-001-001-A01.SDR REXA2019101401452Seat Track · corrodedINITIAL INSPECTION. CORROSION ON FLOOR SEAT RAIL LBL9, FS 581-661+32, 661+32 -691. (TCI 53-20-245). SEAT RAILS LBL9, FS 581-661+32, 661+32 -691.WERE REPLACED PER CRJ-900 AMM 53-00-49-400-801 (CONFIG A07) .SDR REXA2019101401437Intercostal · corrodedCORROSION ON INTERCOSTALS BTW FS 310 TO FS 319 STRG 20R AT MAIN AVIONICS COMPARTMENT. (E/E)(SM)(TSI 53-20-304).
DUE TO CORROSION LEVEL 2 ON INTERCOSTAL BTW FS310/319 AND STRG 20R AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ-900 SRM 51-42-13-001-001-A01.SDR REXA2019101401430Floor Support · corrodedCORROSION ON THE FLOOR SUPPORT BS 349 TO 366 BETWEEN RBL 41 TO RBL 46. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-42-06. AND CRJ-900 SRM 51-42-13.SDR REXA2019101491464Doubler · corrodedCORROSION ON INTERNAL DOUBLER IN STA. FS= 295 TO FS= 310 BETWEEN STRG 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT. A NEW INTERNAL DOUBLER IN STA. FS= 295 TO FS= 310 BETWEEN STRG 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT WAS INSTALLED PER CRJ 900 SRM 51-42-06-00SDR REXA2019101493457Stringer · corrodedINITIAL INSPECTION: CORROSION ON STRG 26R BTW FS 501 TO 565 AT FWD BAGGAGE BAY. CORROSION ON STRG 26R BTW FS 501/565 AT FWD BAGGAGE BAY WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 PAR. 5, BLENDED AREAS WERE MEASURED AND FOUND WITHIN LIMITS PER CRJ-900 SRSDR REXA2019101490440Stringer · corrodedINITIAL INSPECTION: CORROSION ON STRINGER 26RH IN STA. FS= 333 TO FS=349 AT MAIN AVIONICS COMPARTMENT. THE STRINGER WAS REPLACED FOR A NEW ONE PER CRJ 900 SRM 51-42-06-001-001-A01.SDR REXA2019101491460Floor Support · corrodedCORROSION ON LH FLOOR SUPPORT SILL IN STA. FS= 1047 TO FS= 1088 AT BAGGAGE BAY. CORROSION ON LH FLOOR SUPPORT SILL BTW FS 1047-1088 AT BAGGAGE BAY WAS REMOVED PER CRJ-900 SRM 53-00-45-201-001-A01 PAR. 6B. AREA WAS MEASURED AND FOUND WITHIN LIMITS PER CRJ-900 SDR REXA2019101491445Intercostal · corrodedCORROSION ON INTERCOSTALS BTW FS 349 TO FS 364 STRG 20R AT MAIN AVIONICS COMPARTMENT. INTERCOSTAL BTW FS 349 TO FS 364 ON STRINGER 20RH WAS REPLACED PER CRJ-900 SRM 51-42-06. AND CRJ-900 SRM 51-42-21.SDR REXA2019101491448Angle · crackedAWR IN REF EO R53581 STEP 33, DURING ANGLE RBL9 REMOVAL ON CROSS BEAM FS280 IT WAS FOUND CRACKED. ANGLE RBL 9 FS 280 WAS REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01.SDR REXA2019101401433Crossbeam · crackedAWR IN REF EO R53581 STEP 21 DURING REMOVAL OF LH DRIP TRAY CRACK WAS FOUND ON CROSS BEAM FS 280 LBL13. CROSS BEAM FS 280 LH SIDE WAS REPLACED PER CRJ-900 SRM 51-42-06. AND CRJ-900 SRM 51-42-21.SDR REXA2019101421428Seat Track · corrodedCORROSION ON FLOOR SEAT RAIL BS 349 TO 409, RBL 9. THE SEAT TRACK WAS REPLACED PER AMM 53-00-49-400-801-A01-A07.SDR REXA2019101471450Seat Track · corrodedINITIAL INSPECTION. CORROSION ON SIDE SEAT RAILS STGR 15RH FS 670-722, 743-763, 785-847+14, 847+14-907, 907-986. (TCI 53-20-318) SIDE SEAT RAILS STGR 15RH FS 670-722, 743-763, 785-847+14, 847+14-907, 907-986. WERE REPLACED PER CRJ-900 AMM 53-00-49-400-801 (COSDR REXA2019101471449Seat Track · corrodedINITIAL INSPECTION. CORROSION ON SIDE SEAT RAILS STGR 15LH, FS 670-722, 743-763, 785-847+14, 847+14-907, 907-986. SIDE SEAT RAILS STGR 15LH, FS 670-722, 743-763, 785-847+14, 847+14-907, 907-986 WERE REPLACED PER CRJ-900 AMM 53-00-49-400-801 (CONF. A07).SDR REXA2019101491470Angle · crackedDURING REMOVAL OF LH CROSS BEAM FS 280, CRACK ON LH ANGLE CAP WAS FOUND. CAP ANGLE LH FS 280 WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01AND SRM 51-42-13-001-001-A01SDR REXA2019101491456Seat Track · corrodedINITIAL INSPECTION. CORROSION ON FLOOR SEAT RAILS LBL9/RBL9, FS 691-836, 836-847+51. SIDE SEAT RAILS STRGLBL9/RBL9, FS 691-836, 836-847+51. WERE REPLACED PER CRJ-900 AMM 53-00-49-400-801(CONFIG A07), (LEVEL CORROSION 2).SDR REXA2019101401455Seat Track · corrodedCORROSION ON FLOOR SEAT RAILS LBL9/RBL9, FS 847+51-977. (TCI 53-20-325) SEAT RAILS LBL9/RBL9, FS 847+51 -977 WERE REPLACED PER CRJ-900 AMM 53-00-49-400-801 (CONFIG A07).SDR REXA2019101461454Seat Track · corrodedCORROSION ON FLOOR SEAT RAIL RBL9, FS 364-485, 485-581, 581-661+32, 661+32 -691. (TCI 53-20-245). FLOOR SEAT RAIL RBL9, FS364/485, 485/581, 581/661+32 AND 661+32/691 WERE REPLACED PER CRJ-900 AMM 53-00-49-400-801 (CONFIG A07),SDR REXA2019101461453Seat Track · corrodedCORROSION ON FLOOR SEAT RAIL LBL27, FS 483-581. (TCI 53-20-245). FLOOR SEAT RAILS LBL27, FS 483-581WERE REPLACED PER CRJ-900 AMM 53-00-49-400-801 (CONFIG A07).SDR REXA2019101421447Seat Track · corrodedCORROSION ON SIDE SEAT RAILS STRG15RH FS 379-483, 483-573, 573-661+14, 661+14-672. SIDE SEAT RAILS STRG15RH FS 379-483, 483-573, 573-661+14, 661+14-672. WERE REPLACED PER CRJ-900 AMM 53-00-49-400-801 (CONFIG A07),SDR REXA2019101461446Seat Track · corrodedCORROSION ON SIDE SEAT RAILS STRG15LH FS 379-483, 483-573, 573-661+14, 661+14-672. SIDE SEAT RAILS STRG15LH FS379/483, 483/573, 573/661+14 AND 661+14/672 WERE REPLACED PER CRJ-900 AMM 53-00-49-400-801 (CONFIG A07),SDR REXA2019101421473Cover · corrodedCORROSION ON PLATE COVER (PROTECTOR PLATE) OF SERVICE DOOR . CORROSION ON PLATE COVER (PROTECTOR PLATE) WAS REMOVED PER SRM 51-21-06-001-001-A01 PAR. 1 TO 5.B. (1) AND REWORKED AND FOUND WITHIN OF LIMITS PER SRM 52-00-01-101-001-A01, PAR 4.SDR REXA2019101451451Seat Track · corrodedINITIAL INSPECTION. CORROSION ON FLOOR SEAT RAIL LBL27, FS 364-483. (TCI 53-20-243). SIDE SEAT RAILS LBL27, FS 364-483. WERE REPLACED PER CRJ-900 AMM 53-00-49-400-801 (CONFIG A07).SDR REXA2019101401432Access Panel · corrodedCORRSION ON ACCESS PANEL 832DL ON THE PASSENGER DOOR. CORROSION ON THE ACCESS PANEL WAS REMOVED IAW SRM 51-21-06-001-001-A01 PAR. 1 TO 5.B. (1) AND REWORKED AREA WAS MEASURED AS FOLLOW 832DL ORIGINAL THICKNESS: .050"" AND REMAINING THICKNESS: .044"" THEREFORSDR REXA2019101401429Seat Track · corrodedCORROSION ON FLOOR SEAT TRACK BS 375 TO 409, LBL 9. THE SEAT TRACK WAS REPLACED IAW AMM 53-00-49-400-801-A07.SDR REXA2019101401425Skin · corrodedINITIAL INSPECTION: CORROSION ON INNER SKIN AT INTERCOSTAL DD2 OF PASSENGER DOOR . CORROSION ON INNER SKIN AT INTERCOSTAL DD2 OF PASSENGER DOOR WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 PAR. 5. B AND REWORKED AREA WAS MEASURED AS FOLLOW O.T.=0 .040" ANSDR REXA2019101401424Skin · corrodedSEVERAL CORROSION ON EXTERNAL AND INTERNAL INNER SKIN OF PASSENGER DOOR, ON SENTTLEMENT AREAS OF ACCESS PANELS. CORROSION ON EXTERNAL AND INTERNAL INNER SKIN OF PASSENGER DOOR, ON SENTTLEMENT AREAS OF ACCESS PANELS WERE REMOVED PER CRJ-900 SRM 51-21-06-001-00SDR REXA2019101421418Spring · corrodedCRACKED FWD/AFT SPRING CLIPS ON HANDRAILS STOWAGE BRACKET AT PASSENGER DOOR. FWD/AFT SPRING CLIPS ON HANDRAILS WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-0A1.SDR REXA2019101421417Panel · corrodedCORROSION ON FWD/AFT STAIRS SIDE PANEL BELOW LOWER HANDRAILS SUPPORT AT PASSENGER DOOR. CORROSION ON FWD/AFT STAIRS SIDE PANEL BELOW LOWER HANDRAILS SUPPORT AT PASSENGER DOOR WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 PAR. 5. B AND REWORKED AREA WAS MEAS
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