N457XJ, cancelled Aug 3, 2018
Service difficulty reports · 49
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 = 'N457XJ' AND deregistration_id = 'N457XJ-2018-08-03' 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 = 'N457XJ' AND deregistration_id = 'N457XJ-2018-08-03' 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 MALA110247Wire · chafedON START OF T/O ROLL, SMELLED & SAW SMOKE EMIT FROM THE THROTTLE QUADRANT AREA OF THE CENTER CONSOLE & CIRCUIT BREAKER G-12 & N-11 POPPED AGAIN. REPLACED QUADRANT PN 53170-6 DUE TO CHAFED WIRE. SN OFF 0192, SN ON 176. REF 409 393116 FOR DETAILS. FUNCTIONAL TESDR MALA110070Battery Pack · faulted24LN BATTERY PACK FAULTS DURING OPS TEST OF EMERGENCY LIGHTING SYS. R & R POWER SUPPLY AT 24LN IAW SF340 AMM 33-50-10. PN ON/OFF 3301-51. SN ON 1288, SN OFF 2163. OPS CHECK GOOD.SDR MALA100147Switch · inoperativeWHILE PERFORMING MX, FOUND EMERGENCY LIGHT SWITCH BAD. REPLACED EMERGENCY LIGHT SWITCH IN COCKPIT. REF AMM 39-40-15-02. P/N ON&OFF MS27406-1. OPS CHECK GOOD REF AMM 33-50-00.SDR MALA100049Power Supply · faultedWHILE PERFORMING TASK CARD 335003 FOR OPS TEST OF EMERGENCY LIGHT SYSTEM, NOTED BATTERY PACK 23LN TRIGGERED FAULT LIGHTS. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY AT POSITION 23LN IAW AMM 33-50-10-04-01. ALL CHECKS GOOD. P/N 3301-51, S/N ON 2035, SSDR MALA100005Switch · misinstalledEMERGENCY TRACK LIGHTS CAME ON DURING TAXI. FOUND SWITCH TO BE INSTALLED INCORRECTLY. REINSTALLED SWITCH ON F/A PANEL. PERFORMED OPS CK AND ALL CHECKS GOOD IAW AMM 33-50.SDR MALA090161Skin · dentedDURING THE 2Y & 6Y CHECKS IN CWA, 1 DENT WITH A SHARP CONTOUR WAS FOUND IN THE LT UPPER TAILCONE SKIN AT STA 826 WITHIN 0.5" OF CHEM-MILL EDGE, 4.75" ABOVE THE ELEVATOR FAIRING, MEASURING 1" X 2.25" X 0.048" DEEP. HFEC WAS ACCOMPLISHED. NO CRACKS NOTED. DENSDR MALA090042Power Supply · inoperativeEMERGENCY LIGHT POWER SUPPLY 20LN FAILED OPS TEST. INSTALLED SERVICEABLE POWER SUPPLY P/N ON/OFF 3301-51, S/N ON 2076, S/N OFF 2038 IAW SAAB AMM 33-50-10.SDR MALA090024Engine · fluctuatesIN CRUISE FLIGHT AT 17,000 FT LEFT PROP BECAME VERY ERRATIC, LEFT TORQUE BEGAN FLUCTUATING, AND L ENGINE ITT WENT UP TO 930, BACK DOWN TO 780, AND ALSO BEGAN FLUCTUATING. RAN EMERGENCY NON-NORMAL CHECKLIST FOR ERRATIC/UNCOMMANDED ENGINE. WHICH LED TO THE POMSDR MALA080057Seat Track · corrodedGALLEY SEAT TRACK CORRODED AT STA 231 TO STA 258. NEW GALLEY SEAT TRACK INSTALLED IAW SRM 51-40-22.SDR MALA080051Seat Track · corrodedSEAT TRACK REPAIR ANGLES CORRODED STA 294 - BL 0 AND BL18.3 AND SUPPORT FRAME. SEAT TRACK REPAIR ANGLES REPLACED AT STA 294 - BL 0 AND BL 18.3 AND SUPPORT FRAME IAW EO NR S53342 AND SRM 51-40-21.SDR MALA080049Track · corrodedAIRSTAIRS TRACK CORRODED. AIRSTAIR TRACK REMOVED AND NEW TRACK INSTALLED IAW SRM 51-40-21 AND 51-40-27, P/N 7253710-871.SDR MALA070093Indicator · inoperativeAFTER DEPARTING MEM, LOST ALL INDICATIONS FROM NAV 1 AND NAV2 ON BOTH EHSI'S AS WELL AS FMS DATA. REPLACED NR 2 DCP PN ON AND OFF 6226320002, SN ON 382 SN OFF 1184 TESTS ARE GOOD REF AMM 34-24-25-02.SDR MALA070041Heater · separatedON FINAL INTO TVF ABOUT 8-10 MINUTES OUT, COCKPIT FILLED WITH A STRONG SMOKE ODOR. FA LATER REPORTED FAINT ODOR IN CABIN AND NO VISIBLE SMOKE. NOTED SHORT FINAL SHUT OFF BOTH BLEED VALVES. FOUND APPROX 2 1/2'' BY 2 1/2'' PIECE OF INTAKE HEATING MAT TO HAVE SDR MALA070002Intake Duct · failedNOTICED SLIGHT ODOR. FO THEN NOTICED RIGHT ENGINE INTAKE SPARKING, TURNED OFF RIGHT INTAKE, SMOKE ODOR WENT AWAY. THE RIGHT INTAKE LIGHT DID NOT COME ON. REMOVED AND REPLACED RIGHT INTAKE DUCT P/N NH24668-081-08 IAW SF340 AMM 71-60-05. SECURITY CHECK GOOD,SDR MALA060620Smoke Warning · illuminatedAVIONICS SMOKE LIGHT ILLUMINATED ON TAXI IN. DEFERRED.SDR MALA060450Skin · ground damageTHE AIRCRAFT WAS STRUCK BY A BAGGAGE CART CAUSING DAMAGE TO THE LEFT VENTRAL FIN AND THE REAR FUSELAGE SKIN AT FRAME STATION 773.55 AND STRINGER 1520. THE SKIN WAS DAMAGED OVER AN AREA APPROXIMATELY 3 INCHES BY 5 INCHES. THE FRAME AT STATION 773.55 WAS DEFORSDR MALA060233Deice System · malfunctionedINFLIGHT R PROP CAUTION LIGHT ILLUMINATED W/SWITCH IN NORM IN ICING CONDITIONS. FOLLOWED QRH. STILL NOT WORKING. LIGHT COMES ON WITHIN 35 SECONDS. REPLACED RT PROP DEICER LEADS ON NR 1 AND NR 3 PROP BLADES PER TASK 3060-301, P/N 660714263.SDR MALA060194Battery Pack · no testFAILED CAP CHECK PER WO 406707. REPLACED BATTERY PACK.SDR MALA050638Indication Sys · fluctuatesCREW RETURNED TO MSP DUE TO ENGINE TEMPERATURE (ITT) FLUCTUATIONS. NO FURTHER INFORMATION AT THIS TIME.SDR MALA050314Hose · leakingRT BLEED AIR LEAK LIGHT ILLUMINATED INFLIGHT ALONG WITH BLEED CLOSED. THE LIGHT DID NOT EXTINGUISH WITH BLEEDS CLOSED. REMOVED AND REPLACED RT BLEED AIR HOSE.SDR MALA050285Indicator · malfunctionedSHORTLY AFTER TAKEOFF FROM MSP THE GYRO FOR THE STANDBY HORIZON TUMBLED. REPLACED STANDBY HORIZON P/N ON/OFF H341ADM2. S/N ON 5329. S/N OFF 5117.SDR MALA050141Bearing · failedCREW REPORTED LOUD BANG, FOLLOWED BY CHIP LIGHT, OIL PRESSURE LOSS, AND OVERTEMP. IN FLIGHT SHUTDOWN. NR 2 BEARING FAILURE. NO FURTHER INFO AT THIS TIMESDR MALA040443Seal · leakingIN CRUISE FLIGHT LT ENGINE OIL PRESSURE FLUCTUATES AND CWP LIGHT ILLUMINATED. PRESSURE GAUGE FLUCTUATES +/- 10 PSI ALL OTHER PARAMETERS NORMAL. AIR RETURN TO DTW. MAINTENANCE REPLACED LT ENGINE BB AXIS SEAL.SDR MALA040425Seat Track · corrodedDURING 4Y/2Y INSPECTION IN LCQ, FS 300 RT I/B SEAT TRACK CORRODED. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK AT FS 300 I/B IAW MESABA EO S53060. A/C RELEASE DATE 6/4/05.SDR MALA040424Seat Track · corrodedDURING 4Y/2Y INSPECTION IN LCQ, FS 300 LEFT I/B SEAT TRACK CORRODED. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK AT FS 300 I/B IAW MESABA EO S53060. A/C RELEASE DATE 6/4/05.SDR MALA040426Cargo Track · corrodedDURING 4Y/2Y INSPECTION IN LCQ, FS 630.112 CARGO COMPARTMENT CENTER SEAT TRACK CORRODED. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK AT FS 300 I/B IAW MESABA EO S53060. A/C RELEASE DATE 6/4/05.SDR MALA040430Battery · dischargedDURING CAPACITY CHECK IN MSP, EMERGENCY POWER SUPPLY P/N 501-1712-02, S/N 1510 FAILED CAPACITY CHECK. MAINTENANCE REPLACED (2EA) BATTERY ASSEMBLY P/N 549-1324-06 & UNIT PASSED CMM CHECKS. RETURNED TO SERVICE 5/21/04.SDR MALA040348Smoke Detector · failedCARGO SMOKE ILLUMINATED ON CWP DURING PREFLIGHT. MAINTENANCE REMOVED & REPLACED CARGO AFT SMOKE DETECTOR P/N CGAB1201-01, S/N ON 1128, S/N OFF 750, OPS CHECK GOOD.SDR MALA030447Engine · malfunctionedDURING FLIGHT, LT ENGINE SHUTDOWN DUE TO CHIP LIGHT ON AND OIL PRESSURE LOSS. LT ENGINE CHIP LIGHT LITE UP AT 16000 FT. FOLLOWED QRH & REDUCED POWER. ENGINE PARAMETERS NORMAL FOR 10 MINS THEN A SUDDEN POP AND A/C SHOOK TO THE LT. ITT SUDDENLY RISED FOLLOWED SDR MALA030236Connector · disconnectedDURING APPROACH ON FLIGHT NR 3098, LT MAIN LANDING GEAR LIGHT DID NOT ILLUMINATE. MAINTENANCE INSPECTED LEFT MAIN LANDING GEAR FOUND CONNECTOR 5GA-P1 DISCONNECTED. MAINTENANCE RECONNECTED AND CLEANED CANNON PLUG, ALL CHECKS GOOD. PERFORMED LANDING GEAR SWISDR MALA030167Computer · malfunctionedDURING FLIGHT NR 2996, CAPT AND F/O'S HEADING OFF 10 DEGREES. YELLOW HEADING ON EHSI ON ABOUT EVERY 2 MINUTES. HDG SLAVE RESETS TO ABOUT 5 DEGREE DIFFERENCE. F/O'S HDG MATCHES MAG COMPASS, CAPTS HDG DRIFTS TO ABOUT +9 DEGREES. AIR RETURN TO DTW. MAINTENANSDR MALA020510Control Valve · defectiveDURING FLIGHT #3309 LANDING GEAR WOULD NOT EXTEND INFLIGHT. RESET F7 C/B WAS RESET PER QRH AND GEAR EXTENDED SUCCESSFULLY. MAINTENANCE REMOVED AND REPLACED LANDING GEAR CONTROL VALVE, PERFORMED GEAR SWINGS, AND LEAK CHECK GOOD. IAW AMM 32-31-15-4 PN HP84843SDR MALA020353Engine · malfunctionedDURING APPROACH OF FLIGHT 3326, RH ENGINE POWER SURGE. UNCOMMANDED TORQUE POWER SURGES OF 15 PERCENT ON RT ENGINE DURING CRUISE FLIGHT AT 60 PERCENT TORQUE. THIS WAS AN ACTUAL POWER SURGE WITH AN ASSOCIATED YAW. AC LANDED WITHOUT INCIDENT. MAINTENANCE REMOVSDR MALA020348Seat Track · corrodedDURING 4Y/2Y-CHECK IN CWA, CARGO CENTER AISLE SEAT TRACK BLO HAS CORROSION ON SIDE AT APPROXIMATELY STA 637. MAINTENANCE BLENDED OUT CORROSION IAW 51-70-40. REF: 409 #140132 FOR DETAILS. A/C RELEASE DATE IS 06/13/2002.SDR MALA020347Frame · corrodedDURING 4Y/2Y-CHECK IN CWA, WEB ON TOP OF FRAMES 288 & 294 HAVE CORROSION. MAINTENANCE BLENDED OUT CORROSION IAW SRM 51-70-40. REF: 409 # 140139 FOR DETAILS. A/C RELEASED DATE 6/13/02.SDR MALA020346Frame · corrodedDURING 4Y/2Y-CHECK IN CWA, FRAME TOP STA 272 AT APPROXIMATELY RBL 22 HAS CORROSION. MAINTENANCE BLENDED OUT CORROSION AT SA 272 APPROX RBL 22 IAW SRM 51-70-40. REF: 409 # 140140. A/C RELEASE DATE 6/13/2002.SDR MALA020345Seat Track · corrodedDURING 4Y/2Y-CHECK IN CWA, RHIB GALLEY SEAT TRACK TOP HAS CORROSION. MAINTENANCE BLENDED OUT SURFACE CORROSION IAW SRM 51-70-40. REF; 409 # 140141 FOR DETAILS. A/C RELEASE DATE 6/12/02SDR MALA020344Angle · corrodedDURING 4Y/2Y-CHECK IN CWA, TOP FRAME ANGLE AT STA 258 HAS CORROSION. MAINTENANCE BLENDED OUT CORROSION IAW SAAB SRM 57-70-40.SDR MALA020343Angle · corrodedDURING 4Y/2Y-CHECK IN CWA, LT BEAM ANGLE BETWEEN STA 236.5 TO 258 HAS CORROSION. MAINTENANCE BLENDED OUT SURFACE CORROSION ON LT BEAM ANGLE IAW SRM 51-70-40.SDR MALA020342Floor Support · corrodedDURING 4Y/2Y-CHECK IN CWA, U-CHANNEL FLOORBOARD INTERCONNECT PIECES IN FWD CABIN AREA HAVE MINOR CORROSION. MAINTENANCE REMOVED CORROSION IAW SRM 51-20-42 AND 51-70-40. APPLIED PRIMER AND TOP COAT IAW SRM 51-20-43.SDR MALA020197Control Unit · malfunctionedWHEN STARTING RT ENGINE, AFTER STARTER CUT OUT, NG AND ITT KEPT ACCELERATING. WHEN NG REACHES 85 PERCENT WHITE SMOKE APPREARS FROM VENTILATION SYSTEM. SMOKE IS FAIRLY DENSE WITH NO ODOR. MAINTENANCE BORESCOPED POWER UNIT, FOUND NO EVIDENCE OF OVERTEMP OR OTSDR MALA020181Control Unit · malfunctionedREPORTED SMOKE FROM RT AIRCRAFT VENTS IN CABIN ON ENGINE START. MAINTENANCE BORESCOPED POWER UNIT, FOUND NO EVIDENCE OF OVERTEMP OR OTHER DEFECTS. REMOVED DECU IAW GE MM 71-00-00. OPS & LEAK CHECK GOOD.SDR MALA000736Skin · dentedFOUND DURING C-CHECK, DENT ON CARGO DOOR. REFER TO MESABA 408 CARD 059539, CELSIUS W/O 19097, CELSIUS TASK CARD 8501, AND SAAB STATEMENT 340 SDS000528. MAINTENANCE INSPECTED, NO CRACKS NOTED IAW FFVNDT006 . FILLED DENT, FABRICATED REPAIR DOUBLER, TREATED ANDSDR MALA000734Seat Track · corrodedFOUND DURING C-CHECK, SEAT TRACK CORROSION AT BLO FROM STA 294 THRU STA 401. REFER TO CELSIUS W/O 19097, TASK CARD 1514 AND SAAB STATEMENT340 SDS000528. MAINTENANCE REMOVED THREE NUT PLATES, REMOVED CORROSION IAW SRM 51-70-40. REMAINING MATERIAL IS OUT OF LISDR MALA000733Floorbeam · corrodedFOUND DURING C-CHECK, CORROSION ON UPPER ANGLE OF UNDER FLOORBEAM AT STA 258. REFER TO CELSIUS W/O 19097, TASK CARD 1521. MAINTENANCE BLENDED OUT CORROSION DAMAGE IAW SRM 51-10-10, CORROSION FOUND TO BE OUT OF LIMITS.SEE IPM 123 FORM FOR REPAIRS.SDR MALA000732Floor Support · corrodedFOUND DURING C-CHECK, CORROSION ON LT FLOOR SUPPORT FLANGE AT FLOOR PANELS 131BZ, AND 141BZ. REFER TO CELSIUS W/O 19097, TASK CARD 1516. MAINTENANCE REMOVED CORROSION IAW SRM 51-70-40. REMAINING MATERIAL IS WITNIN LIMITS REF: SRM 51-10-10. TREATED, PRIMED ANDSDR MALA000731Seat Track · corrodedFOUND DURING C-CHECK, CORROSION ON SEAT TRACK LBL 18.3 AND AT WEB STA 294 THRU 401. REFER TO CELSIUS W/O 19097, TASK CARD 1515, AND SAAB STATEMENT 340 SDS000528. MAINTENANCE REMOVED CORROSION IAW SRM 51-70-40. REMAINING MATERIAL IS OUT OF LIMITS REF: SRM 51SDR MALA976449Bleed Valve · failedLEFT BLEED FAULT LIGHT ILLUMINATED IN FLIGHT. FOLLOWED QRH AND CLOSED LEFT BLEED VALVE, WITH LEFT BLEED VALVE CLOSED, LEFT BLEED FAULT LIGHT ILLUMINATED FOR ABOUT 3 SECONDS, ROUGHLY EVERY 4 MINUTES. MAINTENANCE REPLACED LEFT PRESSURE BLEED SWITCH. ALL CHECKSDR MALA976289Deice Module · failedDURING FLIGHT, RIGHT INTAKE HEAT INOP. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED RIGHT DEICE MODULE IAW 30-20-15, OPS CHECK GOOD.
Back to N457XJ, cancelled Aug 3, 2018