N927XJ
Service difficulty reports · 193
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 = 'N927XJ' 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 = 'N927XJ' 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 REXA2026070301037Intercostal · corrodedCORROSION ON INTERCOSTALS (3 EAS) BTW FS 394 TO FS 409 NEAR STGR 27 ALSO STGR 26L AT MAIN AVIONICS COMPARTMENT INTERCOSTALS (3 EAS) BTW FS 394 TO FS 409 NEAR STGR 27 ALSO STGR 26L AT MAIN AVIONICS COMPARTMENT WERE REPAIRED PER EA NO: CRJ953-20508 REV ASDR REXA2026070301036Frame Splice · crackedCRACK ON FRAME SPLICE AT 31.87% AND STGR 2L TO VERTICAL STABILIZER REAR SPAR DATUM, ON AFT ACCESSORIES COMPARTMENT. FRAME SPLICE AT 31.87% AND STGR 2L TO VERTICAL STABILIZER REAR SPAR DATUM, ON AFT ACCESSORIES COMPARTMENT WAS REPAIRED PER REO 690-53-71-107 REVSDR REXA2026070701031Hinge · crackedCRACK ON FWD SIDE SKIN AT SETTLEMENT AREA OF ACCESS PANEL 832AT AT PASSENGER DOOR. FWD SIDE SKIN AT SETTLEMENT AREA OF ACCESS PANEL 832AT AT PASSENGER DOOR. WAS REPAIRED PER CRJ-900 SRM 52-11-04-201-004-A01SDR REXA2026070301035Channel · crackedCRACK ON AFT RAIL DOUBLER (LOWER END, FS 1047) OF AFT BAGGAGE BAY DOOR. AFT RAIL DOUBLER (LOWER END, FS 1047) OF AFT BAGGAGE BAY DOOR WAS REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01 AND SRM 51-41-02-001-001-A01SDR REXA2025050800572Battery Pack · inoperativeFOUND CLASS DIVIDER EXIT SIGN AFT INOP DURING LINE CHECK. R/R PS36 BATTERY IAW AMM 33-51-17. EXIT SIGN ILLUMINATES. NO FURTHER DEFECTS. A/C OK FOR SVC.SDR REXA2024103101243Door · crackedR/H AFT OVERWING EMERGENCY EXIT DOOR P/N SH670-36600, S/N SB0768 IS CRACKED UNDER UPPER ATTACHMENT LUG. REPAIRED R/H AFT OVERWING EMERGENCY EXIT DOOR P/N SH670-36600, S/N SB0768 IAW MHIRJ REO 690-52-21-146 REV --, DATED 2023-12-29.SDR REXA2024103101312Structure · corrodedWHILE PERFORMING ENDEAVOR AIR EO# R53595 / SB670BA-53--061 FOUND CORRISION AT RH FS801.250 REPAIRED IAW MHIRJ REO# 690-53-41-438 REV - - DATED 2023-12-22.SDR REXA2024103101311Structure · corrodedWHILE PERFORMING ENDEAVOR AIR EO# R53595 / SB670BA-53--061 FOUND CORRISION AT RH FS792.875 REPAIRED IAW MHIRJ REO# 690-53-41-438 REV - - DATED 2023-12-22.SDR REXA2024102801088Support · corrodedWHILE PERFORMING ENDEAVOR AIR EO# R53595 / SB670BA-53--061 FOUND CORRISION AT LH FS792.875 REPAIRED IAW MHIRJ REO 690-53-41-439 REV-- 12/22/2023.SDR REXA2024090300679Stringer · chafedLH FUSELAGE STRINGER HAS CHAFE DAMAGE LOCATED AT F.S. 1162 STRINGER 7L REPAIRED STGR 7 AT FS:1162 IAW SRM 53-00-03SDR REXA2022063000429Unknown · chafedLH FUSELAGE STRINGER HAS CHAFE DAMAGE LOCATED AT F.S. 1162 STRINGER 7L. REPAIRED STGR 7 AT FS: IAW SRM 53-00-03 THIS IS CONSIDERED A MAJOR REPAIRSDR REXA2022022300238Skin · chafed"PANEL 684EB IS CHAFFED. RECEIVED NEW PANEL P/N CC670-14177-2. LOCATED AND DRILLED IAW CRJ900 SRM 51-40-11-001-001-A01 "SDR REXA2022022300237Angle · crackedR/H VERTICAL STAB. AFT DRAG ANGLE APPEARS TO BE CRACKED AT FORWARD END. FURTHER INVESTIGATION REQUIRED. REPLACED R/H AFT DRAG ANGLE IAW CRJ 900 SRM 51-42-13-001-001-A01, 51-42-21-001-001-A01, AND 51-42-22-001-001-A01SDR REXA2022022400244Web · deformedWHILE REPAIRING LH TRU BAY FLOOR WEB AT FS193.00 PER CRJ 900 SRM 53-11-43-201-001-A01 (REF: NON-ROUTINE TASK CARD 81518831$M212) FOUND 1 EA. FASTENER HOLE COMMON TO REPAIR ELONGATED. REPAIRED IAW MHIRJ REO 690-53-11-1529 REV - DATED 2023-02-18.SDR REXA2022022400242None · crackedR/H AFT TRU LATCH CUTOUT ANGLE IS CRACKED. INSTALLED NEW AVIONIC BAY DOOR LANDING ON RH SIDE BETWEEN FS 193 TO 168 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01SDR REXA2022022400241None · crackedR/H FWD EQUIPMENT BAY FLOOR IS CRACKED AT F.S. 193.00. INSTALLED NEW ELECTRIC BAY WEB DOUBLER IAW CRJ-900 SRM 51-42-06-001-001-A01. REF. CRJ-900 SRM 53-11-43-201-001-A01SDR REXA2022010300001Lamp · inoperativeAFT LH EMERGENCY LIGHT BULB INOP "REMOVED AND REPLACED AFT LH EXT EMERGENCY LIGHT BULB IAW CRJ 900 AMM
33-51-15. OPS CHECK GOOD. "SDR REXA2021072600526Battery Pack · inoperativeEMER LIGHTS ON CEILING FLICKERING ALSO BULK HEAD AFT EMER LIGHT FLICKERS. DEFERRED CABIN EMERGENCY LIGHT PER MEL 33-51-1A PLACARD INSTALLED MMO2 UPDATED MOC NOTIFIED 101954//////R&R #2 EPSU BATTERY PACK PS36 IAW AMM 33-51-17 OPS CHECK GOOD. MMO2 UPDATED PLACARSDR REXA2021030900083Wire · brokenL/H AFT OVER THE WING EMERGENCY LIGHT HAS BROKEN WIRE. REPAIRED BROKEN WIRE AT THE L/H AFT OVERWING EMERGENCY LIGHT (DS102) IAW CRJ 900 ESPM 20-16-05. PERFORMED OPERATIONAL TEST OF THE EXTERIOR EMERGENCY LIGHT IAW CRJ 900 MM 33-51-710-801-A01. NO DEFECTS NOTEDSDR REXA2020070600592Battery Pack · dischargedMULTIPLE CABIN EMERGENCY LIGHTS INOP. R&R EMER BATT PACK NR 2 IAW AMM 33-51-17. OPS CK GOOD.SDR REXA2020011760049Wire · brokenDURING ROUTINE INSPECTION FOUND EMERGENCY EXIT LIGHT INOP ON RH AFT OVERWING EXIT. RELAMPED AFT RH EMERGENCY EXIT LIGHT IAW AMM 33-51-15 (P/N 8GH005123-06). ALSO FOUND WIRE FOR ELECTRICAL LEAD BROKE, REPAIRED BROKEN WIRE BY
CRIMPING AN NEW PIN (P/N B0808002-3SDR REXA2019090701378Hinge · crackedPART RACKS: CRACKED HINGES ON FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT. (CCT) (SM). SUMMARY: FWD HINGE, MID AND AFT HINGE WERE REPLACED PER SRM 51-42-06-001-001-A01.SDR REXA2019090701342Cleat · corrodedIN REF NRC 00242 DUE TO CORROSION LEVEL : CORROSION ON CLEAT INTERNAL STRUCTURE 20 FROM LOWER EDGE AT PASSENGER DOOR ( L1 )
CORROSION LEVEL 2: MEASSURE WAS ACCOMPLISHED ON CLEAT INTERNAL STRUCTURE 20" FROM LOWER EDGE AT PASSENGER DOOR. ORIGINAL THICKNESS=0.05SDR REXA2019090401343Frame · corrodedMTC REQUEST: IN REFERENCE NRC 140 THIS NRC WAS ISSUED DUE CORROSION LEVEL 2 ON FRAME FS319.7 BTW STR 27 AND STR 26L AT MAIN AVIONICS COMPARMENT. (SM) TCI: 100-09. SUMMARY: CORROSION LEVEL 2. FRAME FS319.7 BTW STR 27 AND STR 26L AT MAIN AVIONICS COMPARMENT WAS SDR REXA2019090201375Intercostal · corrodedINITIAL INSPECTION: CORROSION ON INTERCOSTAL STR 20R BTW FS310 TO FS349 AT E&E BAY. (SM) SUMMARY: CORROSION ON INTERCOSTAL FS=310 TO FS=349 STRINGER 20R WAS REMOVED, MEASURED AND WAS FOUND OUT LIMITS THEREFORE WAS REPLACED PER SRM 51-42-21-001-001-A01 PAR 6C ASDR REXA2019090101347Bracket · wornINITIAL INSPECTION. WEAR ON FWD/AFT LOWER DOOR TRACKS AND BRACKETS. SUMMARY: WEAR ON FWD/AFT LOWER DOOR TRACKS AND BRACKETS, LOWER DOOR TRACKS WERE REPAIRED PER EA CRJ953-09634 REV IR AND EA CRJ953-09636 REV IR AND BRACKETS NO DAMAGE ALLOWED THEREFORE BRACKETSSDR REXA2019083101376Skin · crackedINITIAL INSPECTION: CRACK ON AFT SKIN LOWER AND UPPER EDGE OF MID STEP ASSEMBLY AT PASSENGER DOOR STRUCTURE. (L1). SUMMARY: AFT SKIN LOWER AND UPPER EDGE OF MID STEP ASSEMBLY AT PASSENGER DOOR STRUCTURE WAS REPAIRED PER SRM 52-11-04-201-004-A01 PAR 5.SDR REXA2019082801367Seat Track · corrodedINITIAL INSPECTION: CORROSION AND WEAR ON SIDE SIDE RAIL FS379.00 TO FS699.40 STR 15L (SM)TCI: 53-20-217 SUMMARY: OF NRC 00167:SIDE RAIL ON FS379.00 TO FS669.40, STR 15L WERE REPLACED PER AMM 53-00-49-400-801 (CONFIG A07).LEVEL CORROSION II.SDR REXA2019082801366Retainer · corrodedAWR: CORROSION ON RETAINER TRIM BTW FS=744-752, 785-797, AND 810-816 AT LEFT SIDE SEAT RAIL (CPAX) (SM). SUMMARY OF NRC:00464 CORROSION ON RETAINER TRIM BTW FS=744-752, 785-797, AND 810-816 AT LEFT SIDE SEAT RAIL WAS REMOVED PER SRM 51-21-06-001-001-A01, STA: SDR REXA2019082801365Retainer · corrodedAWR: CORROSION ON RETAINER TRIM BTW FS=693-720, 785-797, 810-816 AND 847-847+16 AT RIGHT SIDE SEAT RAIL (CPAX) (SM). SUMMARY OF NRC:00465 CORROSION ON RETAINER TRIM BTW FS=693-720, 785-797, 810-816 AND 847-847+16 AT RIGHT SIDE SEAT RAIL WAS REMOVED PER SRM 51-SDR REXA2019082801346Splice · corrodedINITIAL INSPECTION: CORROSION ON SPLICE FS280 BTW STR 24R AND STR 24L AT MAIN AVIONICS COMPARMENT. (SM)TCI: 100-09 SUMMARY OF NRC 00145: CORROSION LEVEL 1 ON SPLICE FS280 BTW STR 24R AND STR 24L AT MAIN AVIONICS COMPARTMENT WAS REPAIRED PER EA NR CRJ953-09611 SDR REXA2019082601362Bulkhead · corrodedAWR HIDDEN DAMAGE: DURING REMOVAL OF FLOORBEAM STA FS=280 WAS FOUND CORROSION ON BULKHEAD WEB BTW LBL 12 IN REF NRC 373
SUMMARY OF NRC 00447: CORROSION LEVEL 2; BULKHEAD WEB LOWER ON LBL 12 FS=280 WAS REPLACED PER SRM 53-11-10-201-003-A01 PAR 4D FIG 53-11-10-SDR REXA2019082601361Bulkhead · corrodedAWR HIDDEN DAMAGE: DURING REMOVAL OF FLOORBEAM STA FS=280 WAS FOUND CORROSION ON BULKHEAD WEB BTW RBL 12 IN REF. NRC 373
SUMMARY OF NRC 00446: CORROSION LEVEL 2; BULKHEAD WEB BTW RBL 12 OF FLOORBEAM STA FS=280 WAS REPLACED PER SRM 53-11-10-201-003-A01 PAR 4D SDR REXA2019082601360Support · corrodedINITIAL INSPECTION: CORROSION ON FLOOR PANEL SUPPORT OF FS 280 AND LBL12 TO RBL12 (CPIL). SUMMARY: ON NRC 00207 CORROSION LEVEL 2 ON FLOOR PANEL SUPPORT OF FS 280 AND LBL12 TO RBL12 WAS REPLACED PER SRM 51-42-06-001-001-A01.SDR REXA2019082601359Angle · crackedAWR HIDDEN DAMAGE: DURING REMOVAL LT BULKHEAD WEB, ANGLE WAS FOUND CRACKED AT STA FS280 LBL26 PAX CABIN ( CPAX ) ( IN REF. NRC 00447 ) SUMMARY: SUMMARY: OF NRC 00448: BULKHEAD WEB ANGLE AT STA FS 280 LBL 26 PAX CABIN WAS REPLACED PER SRM 51-42-10-001-001-A01 SDR REXA2019082601358Floorbeam · crackedAWR HIDDEN DISCREPANCY:DURING REPAIR ON FLOOR SILL, CRACK WAS FOUND ON FLOORBEAM STA FS=280 AND RBL 42. (W1) IN REF. NRC S/N 00303
SUMMARY OF NRC 00373: FLOORBEAM BTW BL 0 TO RBL 42 AT FS=280 WAS REPLACED PER SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01 ANDSDR REXA2019082601357Crossbeam · crackedINITIAL INSPECTION: CRACK ON FS 280.00 CROSSBEAM LBL 14 (TCI:53-10-219). SUMMARY: ON NRC. 00353 CROSSBEAM BTW BL0 TO LBL 42 AT FS 280.00 WAS REPLACED PER SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01 AND 51-42-20-001-001-A01.SDR REXA2019082501354Drag Angle · crackedINITIAL INSPECTION: CRACK ON AFT ANGLE BTW INNER SKIN AND SIDE STEPS PANEL. (L1). SUMMARY: AFT DRAG ANGLE BTW INNER SKIN AND SIDE STEPS PANEL WAS REPAIRED PER SRM 52-11-04-201-002-A01.SDR REXA2019082501344Stringer · wornAWR : HIDDEN DAMAGE : AFTER REMOVAL OF BRACKET, WEAR ON STR 7R BTW STA FS1144 TO FS1162 WAS FOUND AT AFT ACCESORY COMPARTMENT ( CAT ) ( IN REF NRC 00116 ) SUMMARY: ON NRC. 00508 AREA WAS REPAIRED PER SRM 53-00-03-201-004-A01 REPAIR C.SDR REXA2019082201353Panel · bentPART RACKS: BENT FILTER GUARD PANEL. PANEL (PN:P16778) OF WIFI RACK. SUMMARY: PANEL WAS REPAIRED PER EA CRJ946-09568 REV IR.SDR REXA2019082001371Stringer · corrodedAWR EDV: CORROSION ON STR 19R BTW FRAME FS280 TO FS319 AT MAIN AVIONICS COMPARMENT. (SM) TCI: 100-09 SUMMARY: ON NRC. 00453 CORROSION LEVEL 2 ON STR 19R BTW FRAME FS280 TO FS319 AT MAIN AVIONICS COMPARMENT WAS REPLACED PER SRM 51-42-06-001-001-A01.SDR REXA2019081601377Canister · crackedINITIAL INSPECTION: CRACK IN CANISTER, WELDED NR 3 IN STA. WS148 AT RT MAIN FUEL TANK. (AD) SUMMARY: ON NRC. 00355 CRACK IN CANISTER, WELDED NR 3 RT IN STA WS148 AT RT MAIN FUEL TANK. WAS REPAIRED PER INSTRUCTIONS OF REO 670-57-42-577 REV-.SDR REXA2019081601355Seat Track · corrodedINITIAL INSPECTION: WEAR AND CORROSION ON SEAT RAILS FS280 TO 693.00 ABOVE FLOOR RIGHT SIDE. (SM) SUMMARY: SEAT RAILS FS280 TO 693.00 ABOVE FLOOR RIGHT SIDE WERE REPLACED PER AMM 53-00-49-400-801-CONF A07, AMM 53-00-49-000-801 CONF A07 AND SRM 51-41-02-001-001SDR REXA2019081601352Canister · crackedINITIAL INSPECTION: CRACK IN CANISTER, WELDED NR 3 IN STA. WS148 AT LH MAIN FUEL TANK. (AI) SUMMARY: ON NRC 00356 CRACK IN CANISTER, WELDED NR 3 IN STA. WS148 AT LT MAIN FUEL TANK WAS REPAIRED PER INSTRUCTIONS OF CRJ-900 REO 670-57-42-577 REV-.SDR REXA2019081501363Seat Track · corrodedINITIAL INSPECTION: CORROSION AND WEAR ON SIDE SEAT RAIL ABOVE THE FLOOR LEFT SIDE FS693.00 TO FS977, (SM) SUMMARY OFNRC:00325 CORROSION LEVEL # 2 AND WEAR ON SIDE SEAT RAIL ABOVE THE FLOOR LEFT SIDE FS693 TO FS977. SIDE SEAT RAIL ABOVE THE FLOOR LEFT SIDE FS6SDR REXA2019081401373Intercostal · corrodedINITIAL INSPECTION: CORROSION ON INTERCOSTAL STR 21L BTW FS310 TO FS349 AT E&E BAY. (SM) SUMMARY: ON NRC. 00283 CORROSION LEVEL 2 ON INTERCOSTAL STR 21L BTW FS310 TO FS349 AT E&E BAY WAS REPLACED PER SRM 51-42-06-001-001-A01.SDR REXA2019081401368Skin · corrodedAWR HIDDEN DAMAGE: CORROSION ON SETTLEMENT SKIN OF RADIO ALTIMETER RECEIVE E18, TRANSMIT E19, AND TRANSMIT E8 (SM). SUMMARY: ON NRC. 00253, CORROSION LEVEL 2 ON SETTLEMENT SKIN OF RADIO ALTIMETER RECEIVE E18, TRANSMIT E19, AND TRANSMIT E8 WERE REPAIRED PER EA SDR REXA2019081301351Angle · corrodedINITIAL INSPECTION: CORRODED ON LOWER ANGLE MOUNTING OF GALLEY SERVICE DOOR SURROUND STRUCTURE (SM). SUMMARY: CORRODED ON LOWER ANGLE MOUNTING OF GALLEY SERVICE DOOR SURROUND STRUCTURE, IN THIS ANGLE NOT ALLOWABLE DAMAGE PER SRM 53-21-23-101-002-A02. THEREFORESDR REXA2019081301350Support Angle · corrodedINITIAL INSPECTION: CORRODED PLATE PROTECTOR SUPORTS ANGLES OF GALLEY SERVICE DOOR SURROUND STRUCTURE (SM). SUMMARY: ON NRC. 00210 CORROSION LEVEL 2 ON PLATE PROTECTOR SUPORTS ANGLES OF GALLEY SERVICE DOOR SURROUND STRUCTURE (4EAS) WERE REPLACED PER SRM 51-42-SDR REXA2019081301349Floor Support · corrodedINITIAL INSPECTION: CORROSION ON FLOOR SUPPORT AT FUSELAGE STRUCTURE BTW FS 565 / FS 581 AND STR 22L/23L (C1). SUMMARY OF NRC 00214, CORROSION LEVEL-2: SUPPORT ON FUSELAGE STRUCTURE BTW FS 565 / FS 581 AND STR 22L/23L WAS REPLACED PER SRM 51-42-06-001-001-A01
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