N935XJ

Service difficulty reports · 165

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 = 'N935XJ' 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 REXA2018011300061Seat Track · corrodedIN MAIN CABIN RIGHT SIDEWALL SEAT RAIL NR 3 IS CORRODED AND GOUGED TCI 53-20-217. REMOVED DAMAGE FROM SEAT TRACK RT SIDEWALL FS 533-635. MAT LOSS OF .041 REMAINING MAT .329 FOUND TO BE OUT OF LIMITS IAW SRM 53-31-49. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-Jan 13, 2018 · N935XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2018011300060Seat Track · corrodedFAB NEW RIGHT SIDE WALL SEAT TRACK NR 3 TCI 53-20-217. FABRICATED NEW SEAT TRACK FS 535-635 IAW SRM TR 53-0055(53-00-49) AND SRM 51-40-11.Jan 13, 2018 · N935XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2018011200059Seat Track · corrodedIN MAIN CABIN LEFT SIDEWALL SEAT RAIL NR 8 IS CORRODED AND GOUGED TCI 53-20-233. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-00-49-400-801.Jan 12, 2018 · N935XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2018011200057Hinge · wornRT WING OB FLAP IB BUTE DOOR HINGE HAS PLAY. REMOVED AND REPLACED RT WING OB FLAP INBOARD BUTE DOOR HINGE IAW SRM 51-42-06.Jan 12, 2018 · N935XJ · Cndair CL6002D24 · Trailing Edge FlapsSDR REXA2018011200056Drag Angle · crackedPAX DOOR AFT DRAG ANGLE CRACKED. REPAIRED PAX DOOR AFT DRAG ANGLE IAW SRM 52-11-04.Jan 12, 2018 · N935XJ · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2018011100055Stowage Box · brokenTHIRD CREW MEMBER/OBSERVER O2 MASK STOWAGE BOX HAS BROKEN COVER. REMOVED THIRD CREW MEMBER/OBSERVER O2 MASK STOWAGE BOX IAW AMM 35-11-15. REINSTALLED NEW OBSERVER O2 MASK STOWAGE BOX IAW AMM TA 001820. TORQUED FITTING/ADAPTER (4, PAGE 408 OF AMM 35-11-15) TO 5Jan 11, 2018 · N935XJ · Cndair CL6002D24 · Crew Oxygen SystemSDR REXA2018010800058Seat Track · corrodedIN MAIN CABIN FLOOR SUPPORT NR 1 AT LBL27 IS CORRODED AND GOUGED TCI 53-20-243. REMOVED AND REPLACED CABIN FLOOR SEAT TRACK NR 1 LBL27 IAW AMM 53-00-49-400-801.Jan 8, 2018 · N935XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2017091501004Charger · inoperativeAFT INTERIOR AND EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BOTH BATTERY PACKS AND BATTERY CHARGER NR 5 IAW AMM 33-51-17.Sep 15, 2017 · N935XJ · Cndair CL6002D24 · Emergency LightingSDR REXA2017072500807Flashlight · inoperativeFA REPORTED THAT THE FWD EMER FLASHLIGHT IS INOP. R&R FWD EMER FLASHLIGHT IAW AMM 25-61-02. OPS CHECK GOOD. A/C OK FOR SERVICE.Jul 25, 2017 · N935XJ · Cndair CL6002D24 · Emergency EquipmentSDR REXA2017030100309Cover · missingOVERHEAD EMERGENCY EXIT SIGN AMBER BULB COVER MISSING. REPLACED THE COVER IAW AMM 33-51-07Mar 1, 2017 · N935XJ · Cndair CL6002D24 · Emergency LightingSDR REXA2017021100201Sign · missingMID CABIN EXIT SIGN COMPLETELY MISSING. ONCE PAX DEPLANED, SEARCHED THE WHOLE CABIN AND FOUND THE EXIT SIGN AT OVERHEAD BIN. RESECURED OVERHEAD EXIT SIGN IAW AMM 33-51-07Feb 11, 2017 · N935XJ · Cndair CL6002D24 · Emergency LightingSDR REXA2016110102130Battery · inoperativeFORWARD F/A FLASHLIGHT. REMOVED AND REPLACED FLASHLIGHT BATTERY PACK IAW AMM 25-61-00. OPS CHECKED GOOD.Nov 1, 2016 · N935XJ · Cndair CL6002D24 · Emergency EquipmentSDR REXA2016102802017Battery · inoperativeAED BATTERY DEAD. REPLACED THE AED IAW MM.Oct 28, 2016 · N935XJ · Cndair CL6002D24 · Emergency EquipmentSDR REXA2016100401873Frame · corrodedFRAME END AT BS 661 ALONG STRINGER 18L IS CORRODED ABOVE CENTER CARGO DOOR CUTOUT. REPAIRED THE FRAME EA CRJ953-04821 AND CRJ953-04855.Oct 4, 2016 · N935XJ · Cndair CL6002D24 · Fuselage Main, FrameSDR REXA2016100401871Angle · corrodedPAX DOOR SILL ANGLE WAS CORRODED AND OUT OF LIMITS. REMOVED AND REPLACED DOOR SILL ANGLE IAW SRM 51-42-21-001-001-A01.Oct 4, 2016 · N935XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2016100401863Retainer · corrodedGALLEY SERVICE DOOR SEAL RETAINER ON THE BOTTOM CORRODED. REMOVED AND REPLACED DOOR SEAL RETAINER IAW SRM 51-42-06-001-010-A01.Oct 4, 2016 · N935XJ · Cndair CL6002D24 · Service DoorsSDR REXA2016100401862Angle · corrodedANGLE ON FS 319 AT STRINGER 21R IS CORRODED. REMOVED & REPLACED THE ANGLE IAW SRM 51-40-11-001-001-A01 & 51-42-21-001-001-A01.Oct 4, 2016 · N935XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2016100401890Intercostal · corrodedINTERCOSTAL ON STRINGER 20L IS CORRODED BETWEEN BS 319 & 333. REMOVED LIGHT SURFACE CORROSION IAW SRM 53-21-23-101-001-A03,Oct 4, 2016 · N935XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2016100301860Stringer · corrodedSTRINGER 25R IS CORRODED AT MULTIPLE LOCATIONS BETWEEN BS 295 TO 349. REMOVED & REPLACED THE STRINGER IAW SRM 51-42-06-001-001-A01, & 51-42-21-001-001-A01.Oct 3, 2016 · N935XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2016100301859Stringer · corrodedSTRINGER 25R IS CORRODED AT MULTIPLE LOCATIONS BETWEEN BS 295 TO 349. REMOVED & REPLACED THE STRINGER IAW SRM 51-42-06-001-001-A01, & 51-42-21-001-001-A01.Oct 3, 2016 · N935XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2016100301858Stringer · corrodedSTRINGER 25R IS CORRODED AT MULTIPLE LOCATIONS BETWEEN BS 295 TO 349. REMOVED & REPLACED THE STRINGER IAW SRM 51-42-06-001-001-A01, & 51-42-21-001-001-A01.Oct 3, 2016 · N935XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2016100301852Stringer · corrodedSTRINGER 24R HAS CORROSION BETWEEN FS 295 TO FS 349. REMOVED & REPLACED THE STRINGER IAW SRM 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.Oct 3, 2016 · N935XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2016100201874Frame · corrodedFRAME END AT BS 645, STRINGER 18L IS CORRODED DIRECTLY ABOVE CENTER BAGGAGE BAY DOOR CUTOUT. REPAIRED THE FRAME SEGMENT IAW EA CRJ953-04822.Oct 2, 2016 · N935XJ · Cndair CL6002D24 · Fuselage Main, FrameSDR REXA2016100201861Stringer Splice · corrodedSTRINGER SPLICE 21R AT BS 333 IS CORRODED. REMOVED AND REPLACED THE STRINGER SPLICE IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, & 51-42-21-001-001-A01.Oct 2, 2016 · N935XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2016100101886Door · corrodedCENTER CARGO DOOR LINTLE AT BS 645 CORRODED. REPAIRED THE CARGO DOOR LINTLE IAW EA CRJ953-04851.Oct 1, 2016 · N935XJ · Cndair CL6002D24 · Cargo/Baggage DoorsSDR REXA2016093001882Retainer · corrodedTHREE TRIM RETAINERS ON RT SIDEWALL SEAT TRACKS CORRODED. REPAIRED IAW SRM 53-41-51-101-001-001-A02.Sep 30, 2016 · N935XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2016093001870Door Sill · corrodedSERVICE DOOR LOWER SILL ANGLE IS CORRODED. REPLACED THE DOOR SILL IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.Sep 30, 2016 · N935XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2016092801857Stringer · corrodedSTRINGER SPLICE 26R IS CORRODED BS 333. REMOVED AND REPLACED STRINGER SPLICE IAW SRM 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.Sep 28, 2016 · N935XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2016092801856Stringer Splice · corrodedSTRINGER SPLICE 26L IS CORRODED AT BS 333. REMOVED AND REPLACED STRINGER SPLICE IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.Sep 28, 2016 · N935XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2016092701872Door Frame · corrodedCORROSION ON AFT CARGO DOOR AFT LOWER SURROUND STRUCTURE LOWER FRAME AT BS 1047. REPAIRED IAW SRM 51-42-06-001-001-A01.Sep 27, 2016 · N935XJ · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2016092601885Stringer · corrodedSTRINGER 23R IS CORRODED BETWEEN BS 364 - 379. REPAIRED THE STRINGER IAW EA CRJ953-04839.Sep 26, 2016 · N935XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2016092601867Bulkhead Web · corrodedLEFT 280 AFT BULKHEAD WEB HAS CORROSION ABOVE CROSSBEAM. REMOVED & REPLACED THE WEB IAW REO 670-53-11-594 REV A STEPS 3-12.Sep 26, 2016 · N935XJ · Cndair CL6002D24 · Fuselage Main, BulkheadSDR REXA2016092501869Angle · corrodedFWD J-ANGLE AT FS 280 IS CORRODED. REMOVED & REPLACED THE ANGLE IAW SRM 51-42-21-001-001-A01, 51-42-06-001-001-A01, & 51-42-22-001-001-A01.Sep 25, 2016 · N935XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2016092501866Floorbeam · corrodedRIGHT BS 280 FLOORBEAM IS CORRODED. REMOVED & REPLACED THE FLOORBEAM IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-42-22-001-001-A01, & 51-40-11-001-001-A01.Sep 25, 2016 · N935XJ · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR REXA2016092501865Floorbeam · corrodedLEFT 280 FLOORBEAM IS CORRODED. REMOVED & REPLACED THE FLOORBEAM IAW SRM 51-42-06-001-001-A01, 51-42-22-001-001-A01, & 51-40-11-001-001-A01.Sep 25, 2016 · N935XJ · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR REXA2016092401884Seat Track · corrodedCORROSION ON LEFT SEAT TRACK, BS 708. REPLACED SEAT TRACK IAW REO 670-53-00-343, SRM 51-40-11-001-001-A02, AND AMM 53-00-49-000/-400-801-A07.Sep 24, 2016 · N935XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2016092401883Seat Track · corrodedCORROSION ON SEAT TRACK BETWEEN BS 786.15 AND 830.40. REPLACED THE SEAT TRACK IAW REO 670-53-00-343, SRM 51-40-11-001-001-A01, AND AMM 53-00-49-000/-400-801-A07.Sep 24, 2016 · N935XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2016092401877Seat Track · corrodedLBL 9 SEAT TRACK CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-11-001-001-A01, AMM 53-00-49-400-801-A07, AND REO 670-53-00-342 REV M.Sep 24, 2016 · N935XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2016092401876Seat Track · corrodedLBL 9 SEAT TRACK CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-11-001-001-A01, AMM 53-00-49-400-801-A07, AND REO 670-53-00-342 REV M.Sep 24, 2016 · N935XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2016092401875Seat Track · corrodedLBL 9 SEAT TRACK CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-11-001-001-A01, AMM 53-00-49-400-801-A07, AND REO 670-53-00-342 REV M.Sep 24, 2016 · N935XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2016092301881Seat Track · corrodedRBL 9 SEAT TRACK CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000/-400-801-A07, REO 670-53-00-343, AND SRM 51-40-11-001-001-A01.Sep 23, 2016 · N935XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2016092301880Seat Track · corrodedRBL 9 SEAT TRACK CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-400-801-A07, REO 670-53-00-343, AND 51-40-11-001-001-A01.Sep 23, 2016 · N935XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2016092301879Seat Track · corrodedRBL 9 SEAT TRACK CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-400-801-A07, REO 670-53-00-343, AND SRM 51-40-11-001-001-A01.Sep 23, 2016 · N935XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2016092301878Seat Track · corrodedRBL 9 SEAT TRACK CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-400-801-A07, REO 670-53-00-343, AND SRM 51-40-11-001-001-A01.Sep 23, 2016 · N935XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2016092301855Intercostal · corrodedINTERCOSTAL ON STRINGER 27L IS CORRODED BETWEEN BS 349 - 364. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.Sep 23, 2016 · N935XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2016092301854Intercostal · corrodedINTERCOSTAL AT STRINGER 27R IS CORRODED BETWEEN BS 349 - 364. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.Sep 23, 2016 · N935XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2016092301853Attach Angle · corrodedANGLE AT STRINGER 26R IS CORRODED BETWEEN BS 349 TO 364. REMOVED AND REPLACED THE ATTACH ANGLE IAW SRM 51-40-11-001-001-A01 AND 51-42-21-001-001-A01.Sep 23, 2016 · N935XJ · Cndair CL6002D24 · Fuselage Main, Attach FittingsSDR REXA2016092201851Access Panel · chafedACCESS PANEL 699AB IS CHAFED ACROSS THE CENTER. REPLACED THE ACCESS PANEL IAW SRM 51-40-11-001-001-A01.Sep 22, 2016 · N935XJ · Cndair CL6002D24 · AileronsSDR REXA2016092101850Access Panel · chafedPANEL 699BB IS CHAFED ACROSS THE CENTER. DAMAGE FOUND TO BE OUT LIMITS IAW EA CRJ957-04804 STEP 3, LOCATED HOLES IN THE NEW PANEL IAW SRM 51-40-11-001-001-A01.Sep 21, 2016 · N935XJ · Cndair CL6002D24 · AileronsSDR REXA2016073001427Metering Valve · malfunctionedDURING LANDING, MODERATE BRAKE APPLICATION HAD MUSHY BRAKE POWER WHEN PUSHING THE BRAKES FURTHER , IT SUDDENLY GRABS HARD. R & R THE OTBD AND INBD BRAKE METERING VALVE IAW AMM 32-43-06. NR 3 HYD RESERVOIR ALSO REPLACED IAW AMM 29-12-30Jul 30, 2016 · N935XJ · Cndair CL6002D24 · Landing Gear Brake System
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