N416XJ, cancelled Nov 18, 2015
Service difficulty reports · 68
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 = 'N416XJ' AND deregistration_id = 'N416XJ-2015-11-18' 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 = 'N416XJ' AND deregistration_id = 'N416XJ-2015-11-18' 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 MALA090095Battery Pack · dischargedEMERGENCY LIGHT BATTERY PACK 23LN LOW. REMOVED AND REPLACED 23LN IAW AMM 33-50-10-04-01. OPS CHECK GOOD, IAW JC NR 335003.SDR MALA090094Battery Pack · dischargedEMERGENCY LIGHT BATTERY PACK 21LN LOW. REMOVED AND REPLACED 21LN IAW AMM 33-50-10-04-01. OPS CHECK GOOD, IAW JC NR 335003, PN ON/OFF 3301-51 SN OFF 1405, SN ON 1455.SDR MALA090080Warning System · false activationON TAKEOFF RT TAILPIPE HOT LIGHT CAME ON. RAN QRH ALL ENGINE PARAMETERS WERE NORMAL. PERFORMED VISUAL INSPECTION OF RT TAIL PIPE HOT DETECTION CONNECTORS, HARNESS AND DETECTORS. NO DEFECTS NOTED. RAN AIRCRAFT AND PERFORMED OPERATIONAL TEST OF ENG NACELLE FSDR MAL2008F00018Motor · malfunctionedF/A REPORTS STRONG ODOR IN CABIN AGAIN. SMELLS LIKE AN ELECTRICAL SMELL. NOTED STRONG ELECTRICAL SMELL COMING FROM BURNT UP SUPP AIR MOTOR. SYSTEM ON MEL (INOP). RAN ACFT SYSTEMS. NO FURTHER ELECTRICAL SMELL. (S)SDR MALA070182Skin · dentedSEVERAL DENTS WERE FOUND IN THE RT FUSELAGE SKIN, IN THE ICE GUARD AREA LOCATED FROM STA 313 AND STA 321, BETWEEN STRINGERS SL1615 AND SL 1622. DOUBLER/TRIPLER INSTALLED IAW EO NR S53494.SDR MALA070016Power Supply · inoperativeDURING LC2 NOTED EMERGENCY LIGHTS FROM BATTERY PACK 24LN INOP. REMOVED AND REPLACED POWER SUPPLY 24LN PN 3301-51, SN ON 2205, SN OFF 2129.SDR MALA060632Battery Pack · no testFAILED CAP CHECK PER BF GOODRICH C.M.M.W.O. 417138. REPLACED BATTERY PACK.SDR MALA060503Wire · chafedEMERGENCY CALL LIGHT ON PILOTS OVERHEAD PANEL WAS INOP WHEN EMERGENCY CALL BUTTON WAS PUSHED. LAMP TEST OK. FOUND WIRE RY63-24 CHAFED ALMOST THROUGH. REPLACED WIRE RY63-24 FROM CONNECTOR 91VPP9 TO RESISTOR 10RY.SDR MALA060479Engine · making metalRT CHIP DETECT LIGHT ILLUMINATED INTERMITTENT. AIR RETURNED. CHANGED ENGINE.SDR MALA060332Skin · damagedHAIL CONTACT DAMAGE ON LT AILERON 33 1/4" OB ON LEADING EDGE 2" AFT OF LEADING EDGE AND ALSO AT STA 390.82, 2" FROM AILERON TRAILING EDGE. DAMAGE REPAIRED IAW EOS#51031.SDR MALA060313Skin · dentedHAIL CONTACT DAMAGE ON LEFT HORIZONTAL STABILIZER CAUSED DENT IN UPPER ALUMINUM SKIN AT HS113, .025 INCH DEEP AND .703 INCH DIAMETER. LOCATED 6.5 INCHES AFT OF FWD EDGE OF SKIN PANEL. DAMAGE REPAIRED WITH BONDED DOUBLER IAW SAAB SRM SECTION 55-10-10 AND MESASDR MALA060288Skin · dentedHAIL CONTACT DAMAGE ON RIGHT HORIZONTAL STABILIZER CAUSED DENT IN UPPER ALUMINUM SKIN AT HS 38.58, .022 INCH DEEP AND 1.0 INCH DIAMETER. LOCATED 6.5 INCHES FORWARD OF ELEVATOR LEADING EDGE. DAMAGE REPAIRED WITH BONDED DOUBLER IAW SAAB SRM SECTION SRM SECTIONSDR MALA060287Skin · dentedHAIL CONTACT DAMAGE ON RIGHT HORIZONTAL STABILIZER CAUSED DENT IN UPPER ALUMINUM SKIN AT HS99.92, .025 INCH DEEP AND 0.640 INCH DIAMETER. LOCATED 11.5 INCHES FROM LEADING EDGE AND 36 INCHES FROM OB ELEVATOR HINGE POINT. DAMAGED REPAIRED WITH BONDED DOUBLER IASDR MALA060080Skin · lightning strikeON CLIMBOUT FROM DTW A/C STRUCK BY LIGHTNING. THE STRIKE APPEARED TO HIT NEAR CAPTAIN'S SIDE AROUND PITOT TUBE AREA. ALL INSTRUMENTS FINE. AIR RETURNED TO DTW. COMPLETED LIGHTNING STRIKE INSPECTION PER JC 055-303. ALL CHECKS GOOD.SDR MALA050483Warning Light · illuminatedCREW RETURNED TO MSP FOLLOWING INDICATION OF DUCT OVER TEMPERATURE INDICATION. NO EMERGENCY DECLARED AND FLIGHT RETURNED TO GATE WITHOUT FURTHER INCIDENT. NO FURTHER INFORMATION AT THIS TIME.SDR MALA050384Floor Support · corrodedAIRSTAIR FLOOR RAIL, P/N 7253710-871 IS CORRODED AND WILL BE REPLACED IAW SRM 51-40-21/22.SDR MALA050388Skin · dentedFUSELAGE SKIN IS DENTED BETWEEN FS 339 AND FS 363 AND BETWEEN STRINGER'S SL1504 AND SL1506. THE DENTS ARE OUT OF LIMITS AND HAVE BEEN REPAIRED IAW MESABA EO S53009.SDR MALA050386Structure · corrodedLEFT WRAP AROUND P/N 7253711-245 IS CORRODED AND HAS BEEN REPLACED IAW SRM 51-40-21.SDR MALA050385Structure · corrodedRIGHT WRAP AROUND P/N 7253710243 IS CORRODED AND HAS BEEN REPAIRED IAW SRM 51-40-21.SDR MALA050387Seat Track · corrodedGALLEY SEAT TRACK HAD PROFILE P/N'S 7253721-459 AND 7253721-495 ARE CORRODED AND HAVE BEEN REPLACED IAW SRM 51-40-21 AND 51-40-22.SDR MALA050311Engine · malfunctionedLT ENGINE OIL PRESSURE LIGHT ILLUMINATED AND GAUGE WAS READING LOW (ABOUT 25-30 PSI) ON TAKEOFF. CREW FOLLOWED QRH BUT DID NOT SHUT DOWN ENGINE. AIR RETURNED. REMOVED AND REPLACED LT ENGINE.SDR MALA050107Warning Light · illuminatedLT MAIN AND ESS BUSS BREAKER POPPED INFLIGHT. AIR RETURN TO DTW. MAINTENANCE RAN BOTH ENGINES, APPLIED HEAVY LOAD ON PDU. NO FAULTS NOTED. REFER TO LOG PG NR 1276924-4 FOR ADDITIONAL INFORMATION.SDR MALA040571Control Unit · malfunctionedLOST PRESSURIZATION AT 25,000 FT DESCENDED TO 10,000 FT NOTE CABIN ALTITUDE FOLLOWED TO -1. FOUND C/B G7 POPPED. RESET, SWITCHED TO MANUAL MODE, FOUND IT CONTROLLED PRESSURIZATION SYSTEM. MAINTENANCE REPLACED PRESSURIZATION CONTROL UNIT.SDR MALA040568Charger · inoperativeCABIN EMERGENCY FLASHLIGHT INOP. MAINTENANCE REPLACED HOLDER.SDR MALA040385Generator · failedDURING TAXI OUT, LT AC GEN FAILED TO COME ON LINE. PAX REPORTED SMOKE AND FLAMES EXIT A/C OF EXHAUST HOLE. A/C RETURNED TO GATE. MAINTENANCE REPLACED LT AC GEN. ALL CHECKS GOOD DONE IAW SF340MM CHAP 24.SDR MALA040343Engine · overtempLEFT ENGINE OVER TEMPED INFLIGHT. CLIMBING THROUGH 8000 FT LEFT ENG FAILED APPEARED TO HAVE COMPRESSOR STALL. TORQUE WAS LESS THAN 10 PERCENT ITT WAS 1200-1300C (QRH COMPLETE WITH SHUTDOWN ENG) AIR RETURN TO MSP. REMOVED AND REPLACED ENG IAW JC 7100-301. PSDR MALA020546Structure · corrodedDURING 4K-INSPECTION IN CWA, LT FWD SEAT TRACK WRAP AROUND HAS HEAVY CORROSION AT STA 294. MAINTENANCE INSTALLED NEW WRAP AROUND.SDR MALA020539AngleDURING 4K-INSPECTION IN CWA, CARGO FLOOR ANGLE BETWEEN AFT CENTER AISLE SEAT TRACK HAS CORROSION. MAINTENANCE REMOVED AND REPLACED NEW ANGLE IAW SRM CHAP 51. RELEASE DATE 9/4/02. REF 409 # 138436 FOR DETAIL.SDR MALA020547Seat Track · corrodedDURING 4K-INSPECTION IN CWA, RH CENTER AISLE SEAT TRACK FWD PORTION AND CLIP HAS CORROSION AT APPROXIMATELY STA 294. MAINTENANCE REMOVED CORROSION IAW SRM 51-70-40. RELEASE DATE 9/4/02. REF 409 # 141859 FOR DETAIL.SDR MALA020545Floorboard · corrodedDURING 4K-INSPECTION IN CWA, RT O/B FLOORBOARD FLANGE HAS CORROSION AFT OF STA 288. MAINTENANCE REMOVED CORROSION IAW SRM 51-70-40.SDR MALA020544Seat Track · corrodedDURING 4K-INSPECTION IN CWA, RT GALLEY I/B SEAT TRACK TOP AND PROFILE HAS CORROSION. MAINTENANCE REMOVED AND REPLACED GALLEY SEAT TRACK IAW SRM 51.SDR MALA020541Angle · corrodedDURING 4K-INSPECTION IN CWA, ANGLE AT FRAME STA 225 HAS CORROSION. MAINTENANCE REMOVED CORROSION IAW SRM 51-70-40.SDR MALA020540Structure · corrodedDURING 4K-INSPECTION IN CWA, RT SEAT TRACK FWD WRAP AROUND AT STA 294 HAS HEAVY CORROSION. MAINTENANCE INSTALLED NEW WRAP AROUND.SDR MALA020538Channel · corrodedDURING 4K-INSPECTION IN CWA, AIRSTAIR SLIDE UNIT CHANNEL HAS CORROSION. MAINTENANCE REMOVED CORROSION IAW SRM 51-70-40.SDR MALA020537Seat Track · corrodedDURING 4K-INSPECTION IN CWA, LT CENTER AISLE SEAT TRACK FWD PORTION STA 297 HAS CORROSION. MAINTENANCE REMOVED CORROSION IAW SRM 51-70-40.SDR MALA020543Frame · corrodedDURING 4K-INSPECTION IN CWA, FRAME AND ANGLE TOPS AT STA 258 HAS CORROSION. MAINTENANCE REMOVED CORROSION IAW SRM 51-70-40.SDR MALA020542Beam · corrodedDURING 4K-INSPECTION IN CWA, LT BEAM AND ANGLE LBL 10.5 BETWEEN FRAME STA 258 & 236.5 HAS CORROSION. MAINTENANCE REMOVED CORROSION IAW SRM 51-70-40.SDR MALA020352Speaker · shortedON FLIGHT 3349, F/A NOTED SMOKE FROM ANC SPEAKER, ROW 3 / 4A. FOLLOWED BY AN ELECTRICAL ODOR, F/A SHUT OFF ANC AND ODOR WENT AWAY. MAINTENANCE PERFORMED OPS CHECK OF ANC SYSTEM IAW SF-340 MM 23, NO DEFECTS NOTED.SDR MALA020141Module · failedDURING FLIGHT 3317, RT INTAKE HEAT FAILED, INTAKE HEAT WAS CYCLING ON AND OFF AT ABOUT 14 SECOND INTERVALS. AC DIVERTED TO CWA, BECAUSE OF WEATHER CONDITIONS IN MSP. MAINTENANCE REMOVED AND REPLACED RT DEICE MODULE P/N 44730-501, SN/ON A00421, SN/OFF L248464SDR MALA010284Selector Valve · defectiveON FLIGHT 2861, WHILE ON APPROACH IN MSP THE GEAR DISCREPANCY LIGHT ILLUMINATED. AFTER GOING MISS APPROACH AND PERFORMING THE ORH, DISCOVERED THE F7 C/B WAS POPPED. LANDING CONTROL AFTER RESETTING IT WORKED FINE. MAINTENANCE REPLACED LANDING GEAR SELECTOR VSDR MALA010153Power Lever · undertorquedLT AND RT ENGINE WILL ONLY MAKE 72 PERCENT TORQUE WITH POWER LEVERS FIREWALLED. AT FL210 WHILE SETTING POWER FOR TREND TRIED TO SET TORQUE TO 74 PERCENT, PL''S MAXED OUT AT 73 - 74 PERCENT AFTER RAM RISE. MAINTENANCE COMPLETED GPA RUNS WITH BOTH ENGINES, FOUSDR MALA000684Module · failedRH ENGINE INTAKE LIGHT ON IN FLIGHT. QRH RESET THEN LIGHT CAME ON AGAIN. AIR TURN BACK TO DTW. MAINTENANCE REPLACED RH DEICE CONTROL MODULEPN 44730-501, SN/ON A00021. PERFORMED 30 MINUTE GROUND RUN.. ALL COMPONENTS VERIFIED TO BE HEATING. ALL CHECKS GOOD ATSDR MALA000624Duct · crackedFOUND DURING C-CHECK, RT ENGINE INBOARD NACA DUCT CRACKED AT PANEL 463AL. REFER TO CELSIUS TASK CARD 4535, W/O 18843 AND SAAB STATEMENT 340 SDS000144. MAINTENANCE REPAIRED DAMAGE REF SAAB STATEMENT 340SDS000144. PERFORM NDT PER FFVNDT006EC NO CRACKS PAST ROSDR MALA000623Skin · dentedFOUND DURING C-CHECK, RT HORIZONTAL STABILIZER UPPER SURFACE AT HS STA 439.2 HAS SEVERAL DENTS. REFER TO CELSIUS TASK CARD 3510, W/O 18843 AND SAAB STATEMENT 340SDS000144. MAINTENANCE FOUND DENTS OUT OF ALLOWABLE LIMIT REF SAAB SRM 51-10-10 LEXX THAN 4L AND 5SDR MALA000622Skin · dentedFOUND DURING C-CHECK, GROUP OF DENTS IN LT FUSELAGE BENEATH ICE SHIELD STA 331, WL 107. REFER TO CELSIUS TASK CARD 2548, W/O 18843, AND SAAB STATEMENT 340SDS000144. MAINTENANCE FOUND DENTS ARE OUT OF LIMITS, REF 51-10-10. DENTS ARE ACCEPTABLE AS IS IAW SAAB SDR MALA000625Rib · crackedFOUND DURING C-CHECK, 3 RIBS CRACKED ON LEADING EDGE PANEL 611BR. REFER TO CELSIUS TASK CARD 6506, W/O18843. MAINTENANCE REMOVED CRACKED SECTION OF 3 CRACKED RIBS IAW SRM 57-10-30. NDT PERF FVNDT006EC NO CRACKS NOTED. FABRICATED 3 REPAIR ANGLES AND SHIMS ISDR MALA000620Skin · dentedLT FUSELAGE HAS SEVERAL DENTS AT STA 350.0 REFER TO CELSIUS TASK CARD 2531, W/O 18843. MAINTENANCE FOUND DENTS OUT OF ALLOWABLE LIMIT REF SAAB SRM 51-10-10 LEXX THAN 4L. FABRICATED REPAIR DOUBLER/TRIPLER PER PRINCIPLES OF SRM 53-70-10, ALODINED, PRIMED AND TSDR MALA000619Skin · dentedFOUND DURING C-CHECK, LT FUSELAGE HAS SEVERAL DENTS AT STA 350.0 REFER TO CELSIUS TASK CARD 2531, W/O 18843. MAINTENANCE FOUND DENTS OUT OF ALLOWABLE LIMIT REF SAAB SRM 51-10-10 LESS THAN 4L. FABRICATED REPAIR DOUBLER / TRIPLER PER PRINCIPLES OF SRM 53-70-10SDR MALA000618Skin · dentedFOUND DURING C-CHECK, SEVERAL DENTS IN RT FUSELAGE ABOVE AND BELOW PREVIOUS REPAIR AT STA 339.0. REFER TO CELSIUS TASK CARD 2528, W/O 18843. MAINTENANCE FOUND DENTS OUT OF ALLOWABLE LIMIT REF SAAB SRM 51-10-10 LESS THAN 4L. NDT PERF FVNDT006 EDDY CURRENT, NSDR MALA000617Floor Support · corrodedFOUND DURING C-CHECK, CORROSION ON RT FLOORBOARD BL 0 FROM STA 294 TO STA 350. REFER TO CELSIUS TASK CARD 1524, W/O 18843 AND SAAB STATEMENT 340SDS000144. MAINTENANCE REMOVED CORROSION ON RT FLOOR FLANGE FROM STA 294 TO 350 IAW SRM 51-70-40. MATERIAL REMAIN
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