N930XJ

Service difficulty reports · 160

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 = 'N930XJ' 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.

SDR REXA201912301804Floor Support · corrodedINITIAL INSPECTION: CORROSION ON INTERCOSTAL 2 RBL BTW FS 364-349. AT E/E COMPARTMENT.(TCI:53-20-313). NTERCOSTAL INTERCOSTAL 2 RBL BTW FS 364-349 WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-Dec 13, 2019 · N930XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA201912301803Floor Support · corrodedCORROSION ON INTERCOSTAL 6 LBL BTW FS 364-349. AT E/E COMPARTMENT. INTERCOSTAL 6 LBL BTW FS 364-349 WAS INSTALLED PER CRJ-900 SRM 51-42-06-001-001-A01 PAR 6 C AND SRM 51-42-21-001-001-A01 PAR 6 C.Dec 13, 2019 · N930XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA201912301801Access Panel · corrodedCORROSION ON SETTLEMENT AREA ON ACCESS PANEL 193AB. THE ACCESS PANEL WAS REPLACED IAW SRM 51-42-10-001-001-A01.Dec 13, 2019 · N930XJ · Cndair CL6002D24 · Fuselage Structure (General)SDR REXA201912301797Bracket · corrodedCORROSION ON BRACKETS BETWEEN BS 565 AND 629 IN THE FWD CARGO BAY. THE BRACKETS WERE REPLACED IAW SRM 51-42-13-001-001-A01, AND SRM 51-42-20-001-001-A01.Dec 13, 2019 · N930XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA201912301796Doubler · corrodedCORROSION ON DOUBLER OF ANCHOR NUTS BS 661+32 BETWEEN STRINGERS 26R-26L IN THE FWD CARGO BAY. THE DOUBLER BAY WAS REPAIRED IAW EA CRJ953-09966, REV IR.Dec 13, 2019 · N930XJ · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR REXA201912301795Door Sill · corrodedCORROSION ON AFT BAGGAGE BAY DOOR SILL, BTW FS1000-1047. THE CORROSION WAS REMOVED IAW SRM 51-21-06-001-001-A01 PAR 5,E AND REWORKED AREAS WERE MEASURED, ORIGINAL THICKNESS: 0.063"", REMAINING THICKNESS MEASURED 0.059"", MAXIMUM ALLOWED REMAINING THICKNESS:Dec 13, 2019 · N930XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019123021793Stringer · corrodedCORROSION ON STRINGER 23R BETWEEN BS 280 - 333 IN THE MAIN AVIONIC COMPARTMENT. THE STRINGER WAS REPLACED IAW SRM 51-42-06-001-001-A01, AND SRM 51-42-20-001-001-A01.Dec 12, 2019 · N930XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2019123021791Stringer · corrodedCORROSION ON STRINGER 23R, BS 333 - 379 IN THE MAIN AVIONIC COMPARTMENT. THE STRINGER WAS REPLACED IAW SRM 51-42-06-001-001-A01, AND SRM 51-42-20-001-001-A01.Dec 12, 2019 · N930XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2019123011792Stringer Splice · corrodedCORROSION ON STRINGER SPLICE 23R, BS 333 IN THE MAIN AVIONIC COMPARTMENT. THE STRINGER SPLICE WAS REPLACED IAW SRM 51-42-06-001-001-A01, AND SRM 51-42-20-001-001-A01.Dec 11, 2019 · N930XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2019123011813Stringer · corrodedCORROSION WAS FOUND ON STRINGER 26L, BS 336 - 349 IN THE MAIN AVIONICS COMPARTMENT. THE STRINGER WAS REPLACED IAW SRM 51-42-06-001-001-A01, PAR 6C, AND SRM 51-42-21-001-001-A01, PAR 6C.Dec 10, 2019 · N930XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2019123091843Stringer · corrodedCORROSION WAS FOUND ON STRINGER 25L, BS 280 - 327 IN THE MAIN AVIONICS COMPARTMENT. THE STRINGER WAS REPLACED IAW SRM 51-42-06-001-001-A01.Dec 9, 2019 · N930XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2019123081828Stringer · corrodedCORROSION WAS FOUND ON STRINGER 25R, BS 280 - 327 IN THE MAIN AVIONICS COMPARTMENT. THE STRINGER WAS REPLACED IAW SRM 51-42-06-001-001-A01, AND SRM 51-42-20-001-001-A01.Dec 8, 2019 · N930XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2019123081810Intercostal · corrodedCORROSION WAS FOUND ON THE INTERCOSTAL BETWEEN BS 310 - 333, STRINGER 21L , IN THE MAIN AVIONICS COMPARTMENT. THE INTERCOSTAL WAS REPLACED IAW SRM 51-42-21-001-001-A01, PAR 6 C, AND SRM 51-42-06-001-001-A01.Dec 8, 2019 · N930XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019123081809Floorbeam · corrodedCORROSION FOUND ON THE FLOORBEAM ANGLE AT BS 280, BETWEEN STRINGERS 26L - 26R IN THE MAIN AVIONICS COMPARTMENT. THE FLOORBEAM ANGLE WAS REPLACED IAW SRM 51-42-06-001-001-A01.Dec 8, 2019 · N930XJ · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR REXA2019123081806Stringer Splice · corrodedINITIAL INSPECTION. CORROSION ON STRINGER SPLICE 25L, BS 329 - 339 IN THE MAIN AVIONICS COMPARTMENT. THE STRINGER SPLICE WAS REPLACED IAW SRM 51-42-06-001-001-A01 PAR. 6C, AND SRM 51-42-20-001-001-A01 PAR. 6C.Dec 8, 2019 · N930XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2019123081805Stringer Splice · corrodedINITIAL INSPECTION. CORROSION ON STRINGER SPLICE 26L, BS 329 - 339 AT MAIN AVIONICS COMPARTMENT. THE STRINGER SPLICE WAS REPLACED IAW SRM 51-42-06-001-001-A01, AND SRM 51-42-21-001-001-A01.Dec 8, 2019 · N930XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2019123081786Angle · corrodedAFTER MID CAP ANGLE REMOVAL, CORROSION WAS FOUND ON SILL ANGLE BETWEEN BS 318 - 346, LBL 40 AT PAX CABIN FWD WET AREA. THE SILL ANGLE WAS REPLACED IAW SRM 51-42-06-001-001-A01.Dec 8, 2019 · N930XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019123061834Support · crackedCRACKS WERE FOUND ON THE BRACKET FITTING OF GROUND POWER RECEPTACLE. THE BRACKET FITTING WAS REPLACED IAW SRM 51-42-06-001-001-A01, AND SRM 51-42-21-001-001-A01.Dec 6, 2019 · N930XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019123061827Stringer · corrodedCORROSION WAS FOUND ON STRINGER 19R, BS 295 - 310 IN THE AVIONICS COMPARTMENT. THE STRINGER WAS REPAIRED IAW REO 690-53-21-1174 REV --.Dec 6, 2019 · N930XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2019123061826Seat Track · corrodedCORROSION WAS FOUND ON THE SEAT TRACK BETWEEN BS 349 - 409, RBL 9. THE SEAT TRACK WAS REPLACED IAW AMM 53-00-49-400-801-A07.Dec 6, 2019 · N930XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2019123061825Seat Track · corrodedCORROSION FOUND ON THE SEAT TRACK BETWEEN BS 375 - 409, LBL 9. THE SEAT TRACK WAS REPLACED IAW AMM 53-00-49-400-801-A07.Dec 6, 2019 · N930XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2019123061824Seat Track · corrodedCORROSION WAS FOUND ON THE SEAT TRACK BETWEEN BS 350 - 485, LBL 27. THE SEAT TRACK WAS REPLACED IAW AMM 53-00-49-400-801-A07.Dec 6, 2019 · N930XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2019123061822Seat Track · corrodedCORROSION ON THE SIDE SEAT TRACK, STRINGER 15R, BS 379 - 672. THE SEAT TRACK WAS REPLACED IAW AMM 53-00-49-400-801-A07.Dec 6, 2019 · N930XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2019123061820Seat Track · corrodedCORROSION WAS FOUND ON THE SEAT TRACK BS 670 - 986. THE SEAT TRACK WAS REPLACED IAW AMM 53-00-49-400-801-A07.Dec 6, 2019 · N930XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2019123061814Stringer · corrodedCORROSION FOUND ON STRINGER 22L, BS 349 - 364 IN THE MAIN AVIONICS COMPARTMENT. THE STRINGER WAS REPAIRED IAW SRM 53-00-03-201-001-A02.Dec 6, 2019 · N930XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2019123061798Lug · corrodedAFTER BUSHING REMOVAL, CORROSION WAS FOUND ON INBD LUGS OF THE PCU LINK CONNECTION AT THE LT AILERON FRONT SPAR. THE INBD LUG WAS REPAIRED IAW REO 670-57-61-237 REV. --Dec 6, 2019 · N930XJ · Cndair CL6002D24 · AileronsSDR REXA2019123041807Stringer Splice · corrodedINITIAL INSPECTION. CORROSION ON STRINGER SPLICE 22LH IN STA. FS= 329 TO FS= 339 AT MAIN AVIONICS COMPARTMENT. (E/E)(TCI:53-20-304). SUMMARY CORROSION LEVEL 2: STRINGER SPLICE 22LH IN STA. FS= 329 TO FS=339 WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001Dec 4, 2019 · N930XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2019123011821Seat Track · corrodedCORROSION WAS FOUND ON THE SEAT TRACK, BS 670 - 986. THE SEAT WAS REPLACED IAW AMM 53-00-49-400-801-A07, PAR 1 TO 4.Dec 1, 2019 · N930XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2019123011819Seat Track · corrodedCORROSION ON THE FLOOR SEAT TRACK LBL 9, BS 581 - 661+32, 661+32 - 691. THE SEAT WAS REPLACED IAW AMM 53-00-49.Dec 1, 2019 · N930XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2019123011818Seat Track · corrodedCORROSION WAS FOUND ON THE SEAT TRACK RBL9, BS 485 - 691. THE SEAT TRACK WAS REPLACED IAW AMM 53-00-49.Dec 1, 2019 · N930XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019123011817Seat Track · corrodedCORROSION WAS FOUND ON THE SEAT TRACK, LBL 27, BS 483 - 581. THE SEAT TRACK WAS REPLACED IAW AMM 53-00-49-400-801-A07.Dec 1, 2019 · N930XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2019123011816Seat Track · corrodedCORROSION WAS ON THE SEAT TRACK LBL9, BS 847+51 - 977. THE SEAT TRACK WAS REPLACED IAW AMM 53-00-49-400-801-A07.Dec 1, 2019 · N930XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019123011815Seat Track · corrodedCORROSION FOUND ON THE SEAT TRACK RBL9, BS 691-847. THE SEAT TRACK WAS REPLACED IAW AMM 53-00-49.Dec 1, 2019 · N930XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2019123081830Floorbeam · corrodedCORROSION FOUND THE ON THE FLOORBEAM ANGLE, BS 280 BETWEEN LBL 12 TO RBL 12. THE FLOORBEAM ANGLE WAS REPLACED IAW SRM 51-42-06-001-001-A01.Nov 28, 2019 · N930XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019123081799Floorbeam · crackedCRACKED FLOORBEAM ANGLE LBL 9 - RBL 9, BS 280. THE ANGLE WAS REPLACED IAW SRM 51-42-21-001-001-A01.Nov 28, 2019 · N930XJ · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR REXA2019123061831Floorbeam · crackedCRACK FOUND ON THE FLOORBEAM AT BS 280, LBL 14. THE FLOORBEAM WAS REPLACED IAW SRM 51-42-21-001-001-A01, AND SRM 51-42-06-001-001-A01.Nov 26, 2019 · N930XJ · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR REXA2018061500518Light · missingFA`S REPORT, LUMINESANT STRIP IN FRONT OF GALLEY CARTS MISSING. REPLACED ILLUM STRIP IN GALLEY PER AMM 33-51-01, CHECKS SECURE PN PL88-930-LH07, PL88-900-LH00 STRIP.Jun 15, 2018 · N930XJ · Cndair CL6002D24 · Emergency LightingSDR REXA2018010600011Remote Switch · failedDURING OPS CHECK OF ELF, ELT WOULD NOT STOP TRANSMITTING WHEN SWITCH RETURNED TO OFF/ARM. R&R ELT REMOTE SWITCH IAW AMM 25-62-03. OP TEST OK. OK FOR SVC.Jan 6, 2018 · N930XJ · Cndair CL6002D24 · Emergency Locator BeaconSDR REXA2017073000853Stringer · corrodedE & E COMPARTMENT STRINGER 21R CORRODED AT STA 375, REMOVED AND REPLACED THE STRINGER BETWEEN BS 333 - 375 IAW SRM 51-42-06, OPS TEST OF GALLEY HEATER AND EXHAUST FAN GOOD IAW AMM 21-23-64-710-801, AND 21-23-93-710-801.Jul 30, 2017 · N930XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2017072800854Handle · crackedMAIN AVIONICS BAY DOOR HANDLE HOUSING CRACKED. REMOVED AND REPLACED THE HANDLE ASSY IAW SRM 51-42-21 AND AMM 52-42-02. OPS CHECKED GOOD IAW AMM 52-42-00-710-801.Jul 28, 2017 · N930XJ · Cndair CL6002D24 · Electrical/Electronic Compartment DoorsSDR REXA2017072200852Retainer · crackedPYLON PANEL 433BB SEAL RETAINER CRACKED. REMOVED AND REPLACE THE SEAL RETAINER IAW SRM 51-42-06.Jul 22, 2017 · N930XJ · Cndair CL6002D24 · Nacelle/Pylon, Main FrameSDR REXA2017072100851Angle · crackedPANEL 196DR CENTER STRAP AFT ANGLE CRACKED. REMOVED & REPLACED THE ANGLE IAW SRM 51-42-01-001-001-A01.Jul 21, 2017 · N930XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2017060800682Flashlight · inoperativeFWD FA FLASHLIGHT RED LIGHT NOT BLINKING. R & R THE FWD FA FLASHLIGHT IAW AMM 25-61-000-801, & 25-61-02-400-801. PERFORMED OPS TEST, TESTED OK IAW AMM 25-61-00-710-801. OPS CHECKED GOOD. FLASHLIGHT SECURED. ACFT OK FOR SERVICE.Jun 8, 2017 · N930XJ · Cndair CL6002D24 · Emergency EquipmentSDR REXA2016111802249Skin · damagedFAN COWL AFT HINGE SKIN ROLLED UNDER HINGE FAIRING. REPAIRED THE SKIN IAW EA CRJ954-05064. OPS CHECKED GOOD.Nov 18, 2016 · N930XJ · Cndair CL6002D24 · Nacelle/Pylon, Main FrameSDR REXA2016111802248Light · looseEMERGENCY LIGHT LOOSE. REPLACED THE LIGHT IAW 25-25-00.Nov 18, 2016 · N930XJ · Cndair CL6002D24 · Emergency LightingSDR REXA2016111802247Light · missingEMEGENCY LIGHT AT 12C FWD MISSING. REPLACED THE LIGHT IAW 25-25-00Nov 18, 2016 · N930XJ · Cndair CL6002D24 · Emergency LightingSDR REXA2016082301571Light · unsecureEMERGENCY LIGHTING STRIP PULLED UP AT SEAT 12C/D. SECURED LIGHT LIGHT AT SEAT 12C/D IAW AMM 33-51-01.Aug 23, 2016 · N930XJ · Cndair CL6002D24 · Emergency LightingSDR REXA2016072201403Light · missingEMERGENCY LIGHT AT 11C CROSS SECTION FOR EMERGENCY EXIT MISSING. REPLACED THE EMERGENCY LIGHT IAW AMM 33-51-01.Jul 22, 2016 · N930XJ · Cndair CL6002D24 · Emergency LightingSDR REXA2016061701104Retainer · damagedFORWARD BAGGAGE BAY DOOR LOWER SEAL RETAINER IS DAMAGED ON FWD AND AFT CORNERS. R & R THE FWD BAGGAGE BAY DOOR LOWER SEAL RETAINER WITH NEW SERVICEABLE PART & PERFORMED A PRESSURIZATION CHECK IAW AMM 31-00-910-801-A02 & SRM 51-42-06-001-001-A01 & AMM 52-35-07Jun 17, 2016 · N930XJ · Cndair CL6002D24 · Cargo/Baggage DoorsSDR REXA2016061701101Door Sill · corrodedAFT BAGGAGE BAY DOOR SILL IS CORRODED FROM FS 1000.00 TO FS 1047.00. CONTINUATION CARD 81519211 OP 113. R & R AFT BAGGAGE BAY DOOR FLOOR SILL, PN MM670-35655-003 IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-42-13-001-001-A01. Jun 17, 2016 · N930XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
Back to N930XJ