N978QS
Service difficulty reports not matched to an aircraft · 42
They name N978QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N978QS' AND registry_match IS NULL 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 = 'N978QS' AND registry_match IS NULL 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 DXTA2018120301752Apu · odorCABIN ODOR OIL SMELL - SMELL OF FUMES IN CABIN AND COCKPIT WHEN APU TURNED ON. SMELL OF BURNT OIL.
DETERMINED SOURCE OF ODOR WAS RESIDUAL ODOR LEFT IN THE DUCTING FROM A
PREVIOUS A.P.U THAT WAS REMOVED DUE TO BURNING OIL.SDR DXTA2018062200083Spar Cap · corrodedREPAIR OF LT HORIZONTAL AFT UPPER SPAR CAP CORROSION. AIRCRAFT REPAIR DEFINITION REPORT NR S-750-0187/13RD DATED JUNE 20, 2018 WITH FAA FORM 8100-9 DATED 6/21/2018.SDR 2018FA0000188Skin · dentedRT WING SKIN DENTED. REPAIRED.SDR 2018FA0000187Link · corrodedRIGHT MLG TRAILING LINK WAS CORRODED. REPAIRED.SDR 2018F00009Trunnion · damagedMLG TRUNNION IS LONG FORE AND AFT WITH FORWARD AND AFT PINS INSTALLED ON AIRCRAFT.SDR DXTA2017070606422Latch · out of adjustDURING FLIGHT, THE NOSE DOOR OPEN L EICAS MESSAGE ILLUMINATED. ON LANDING, IT WAS DISCOVERED THAT THE REAR LATCH ON THE LEFT NOSE COMPARTMENT DOOR WAS UNLATCHED. THE LATCH APPEARS WORN AND OPENS UNUSUALLY EASY. ADJUSTED THE LT NOSE DOOR LATCHES IAW MM 52-00SDR DXTA2017021306371Valve · defectiveUPON INITIATING DECENT, WHEN THE THROTTLES WERE REDUCED AND THE PAC HP VALVE OPEN L-R CAS MESSAGE APPEARS, THERE IS A STRONG ODOR OF BURNING RUBBER. REMOVED AND REPLACED A DEFECTIVE HP VALVE ON NR 1 ENGINE. LEAK AND OPS CHECKED GOOD IAW AMM 36-10-00.SDR DXTA020306365Unknown · odorTOP OF DESCENT WHEN THROTTLES ARE RETARDED COCKPIT FILLS WITH A VERY STRONG NOXIOUS BURNT RUBBER TYPE SMELL . IT SEEMS MORE PROMINENT ON LEFT SIDE OF COCKPIT.SUB:RAN APU OPERATED AT VARIOUS TEMP'S FOUND NO ABNORMAL ODORS. RAN LH/RH ENGINES FOR APPROX 45 MIN ASDR CWQR20160226008Bulkhead · crackedDURING THE DISASSEMBLY OF THE ENG INLET ASSEMBLY WE FOUND THIS BULKHEAD CRACKED IN NUMEROUS PLACES AT THE INLET LIP TO THROAT ATTACH FASTENERS. SUBMITTED DEFECT TO MFG UNDER SCR REPORT 746597.SDR CWQR20160226009Channel · crackedDURING THE DISASSEMBLY OF THE ENG INLET ASSEMBLY, WE FOUND THIS CHANNEL CRACKED IN NUMEROUS PLACES AT THE INLET LIP TO BULKHEAD ATTACH FASTENERS. SUBMITTED DEFECT TO MFG UNDER SCR REPORT 746605.SDR DXTA2014072905836Unknown · odorDURING FLIGHT, SMELLED ELECTRICAL SMOKE IN COCKPIT. APPLIED POWER TO THE ACFT, NO ELECTRICAL ODOR NOTED. POWERED UP ACFT WITH APU & BLEED AIR ON FOR 30 MINUTES, NO ODOR NOTED. POWERED UP ACFT WITH BOTH ENGINES FOR 30 MINUTES, NO ODOR NOTED. REMOVED ALL ACFSDR DXTA2014060505794Skin · corrodedLT & RT LOWER WING SKIN CORROSION. REPAIRED IAW REPAIR S-750-0187-09.SDR DXTA2013010405229Inverter · failedAFTER SHUTDOWN DETECTED A VERY STRONG ELECTRICAL BURNING ODOR FROM THE AFT CLOSET INSIDE THE ELECTRICAL BOX. NO FIRE. TROUBLESHOT ELECTRICAL BURNING ODOR TO THE 110V AC INVERTER IN AFT CLOSET. R & R INVERTER WITH AN OVERHAULED UNIT IAW MM 25-40-03. OPS CHECKSDR DXTA2012121005203Computer · inoperativeTAKEOFF REJECTED AT 50 KTS DUE TO FAILURE OF DU 1, 2 AND 3, AS WELL AS FMS 1 AND RMU 1. ALL AVIONICS REPOWERED WITHIN 15 SECONDS. THE FOLLOWING AMBER CAS MSG. REMAINED: FADEC REV ADC R, YD OFF LOWER, FADEC FAULT R A, FADEC FAULT L A. TROUBLESHOT TO DEFECTISDR DXTA2011111504789Limiter · failedAT 300' AGL ON DEPARTURE , RUDDER LIMIT FAIL B CAS MESSAGE ILLUMINATED. RUDDER LIMITED TO 79 PERCENT. R & R LOWER RUDDER LIMITER "B" IAW MM 27-23-00. PERFORMED OPS CHECKS IAW MM CH 27-20-00. RUDDER LIMITERS, OPS CHECKED GOOD.SDR DXTA2011050204570Line · failedWHEN SELECTING GEAR HANDLE TO UP, HYD A SYSTEM QUANTITY WENT TO ZERO. GEAR DID NOT RETRACT. MANUAL GEAR EXTENTION WAS PERFORMED. VERIFIED "A" RESERVIOR DEPLETED. FOUND RT MLG RETRACT LINE BURST CAUSING LOSS OF ALL FLUID. REMOVED PRESSURE LINE FROM HYD PUMSDR DXTA2010122304377Strut · dischargedON TAKEOFF GEAR HANDLE WOULD NOT COME UP. JACKED ACFT, FOUND NOSE STRUT SERVICE TO BE FLAT AND RESERVICED UPPER BARREL, SERVICED LOWER BARREL, VERIFIED BRAKE HANDLE OPERATION, ALLOWED STRUT TO SIT. COMPLETED LEAK CHECK. LEAK CHECKS GOOD. ALL WORK DONE IAW MSDR DXTA2010071304151Ptu · leakingB HYD FLUID LOSS IN FLIGHT AT CRUISE 36,000 FT AMBER CAS HYD VOL LOW B; RAN CHECKLIST. UNLOADED B HYD PUMP WHEN VOLUME WAS DOWN TO 8 PERCENT. AFTER UNLOAD, VOLUME RECOVERED TO 13 PERCENT AND HYD TEMP ROSE TO 74. ON POST FLIGHT INSPECTION FOUND BRAKES SMOKING FSDR DXTA2009022203522Module · inoperativePERFORMED PITCH FEEL SYS FUNCTIONAL TEST USING DMU AND ARING CABLE- A SOFTWARE AND COULD NOT DUPLICATE FAULT. SUSPECT INTERMITTENT PITCH FEEL PCB FAIL REMOVED AND REPLACED PITCH FEEL PCB NK122 AND OPS CHECKED GOOD IAW CHAP 27-30-00.SDR DXTA2009022303522Warning Light · illuminatedPITCH FEEL FAIL LIGHT ILLUMINATED.SDR 2008FA0000674Frame · crackedDURING ROUTINE INSP FOUND FWD FRAME PN 6712617-13 CRACKED. THE CRACKED FRAME WAS LOCATED IN THE UPPER LT SIDE UNDER THE RUDDER TO STINGER FAIRING. (K)SDR DXTA200807213192Computer · intermittentON DEPARTURE AT 1500 FT AGL & 200 KNOTS EICAS SCREEN WENT BLANK THEN REPLACED BY A RED X EICAS (AMBER) DISPLAYED ON PILOT & COPILOT PFD. ALL FLT DIRECTOR BUTTONS FAILED WITH ALTITUDE HOLD BUTTON ENGAGED. COULDN'T DISENGAGE ALT HOLD OR ENGAGE OTHER FUNCTIONS.SDR DXTA200803192Display · inoperativeON DEPARTURE AT 1500 FT AGL AND 200 KNOTS EICAS SCREEN WENT BLANK THEN WAS REPLACED BY A RED X EICAS (AMBER) DISPLAYED ON PILOT AND COPILOT PFD. ALL FLIGHT DIRECTOR BUTTONS FAILED WITH ALTITUDE HOLD BUTTON ENGAGED. COULDN’T DISENGAGE ALT HOLD OR ENGAGE OTHERSDR DXTA200803125Warning Message · illuminatedAMBER CAS "FADEC FAIL L A" ILLUMINATED PRIOR TO TAKEOFF. ABORTED T/O. REPOSITIONED FADEC FROM THE RT - A TO LT - A POSITION; FADEC FROM THE RT - B TO LT - B POSITION; FADEC FROM THE LT-A TO RT-A POSITION; FADEC FROM THE LT-B TO RT-B POSITION IAW MM 76-12-00 OSDR DXTA20082924Controller · failedUPON SELECTING FLAPS FOR 15 DEGREES FROM35 DEGREES FLAPS FAILED AT APPROX 17 DEGREES. T/S. FOUND FLAPS AT FULL UP UPON ARRIVAL AT AIRCRAFT. FOUND BITE 2 ON FLAP CONTROLLER. RAN FLAPS THROUGH NO DEFECTS. RESET FLAPS AND RAN SOME MORE. NO BITE CODES PRESENT. PESDR DXTA200802781Pdu · failedFLAP FAIL AMBER CAS MESSAGE FAILURE OCCURED BETWEEN 15 AND 35 DEGREES. TROUBLESHOT TO BAD PDU CLUTCH. REMOVED REPLACED AND OPS CHECK GOOD OF FLAP PDU IAW MM 27-51-00.SDR DXTA200802782Acm · malfunctionedCABIN PACK MAKING SMOKE AND BURNED RUBBER ODOR. REMOVED FAULTY ACM. INSTALLED ACM REPAIRED BY HAMILTON SUNDSTRAND. OPERATIONAL & LEAK CHECKS GOOD. WORK DONE IAW 750 MM 21-51-00SDR DXTA200702681Connector · looseAT FL430 BAGGAGE DOOR SEAL EICAS MSG FOLLOWED BY RAPID CABIN ALTITUDE INCREASE. AFTER A FEW MINUTES ISOLATED BAGGAGE AND BELOW FL200 EICAS MSG OFF. FOUND SOFT SPLICE CONNECTION FOR DOOR SEAL VALVE, HEAT BLANKET NOT PROPERLY CONNECTED. RECONNECTED SPLICE. PUSDR DXTA200702543Computer · faultedON FINAL APPROACH, FGC B FAIL CASS MESSAGE APPEARED AND SYSTEM SWITCHED TO FGC A. CHECKED SYSTEM IN PROPER OPERATION -COULD NOT DUPLICATE- REPOSITIONED NR 1&2 IC-800'S- OPS CHECKED GOOD IAW 750 M/M CH 34-25-01.SDR DXTA200702388Acm · failedDURING DESCENT WITH POWER REDUCED TO APPROX 75-80 PERCENT N1 A PUFF OF SMOKE COME FROM BOTH OF THE COCKPIT WEMACS BELOW THE GLARESHIELD FOLLOWED BY VERY STRONG SULFUR ODOR. TROUBLESHOT DISCREPANCY TO A FAILED COCKPIT ACM. REMOVED AND REPLACED ACM IAW 750 MM SDR DXTA200702421Hose · rupturedIMMEDIATELY AFTER RAISING, THE LANDING GEAR HANDLE AFTER TAKEOFF, ALL (A) SYSTEM HYDRAULIC PRESSURE WAS LOST AND THE EICAS INDICATED 4 PERCENT HYDRAULIC FLIUD REMAINING. THE MAIN LANDING GEAR RETRACTED AND THE NOSE GEAR REMAINED DOWN. FOUND "NWS" CETERING HYSDR DXTA200702255Switch · inoperativeAFTER TAKEOFF, STAB TRIM WOULD ONLY TRIM NOSE UP ON THE LT SIDE. COULD NOT TRIM NOSE DOWN ON LT SIDE. REMOVED OLD PILOTS SIDE STAB TRIM SWITCH AND REPLACED WITH NEW SWITCH OPERATIONAL TEST GOOD. ALL WORK PERFORMED I.A.W. CH 27-13-00 OF THE CE750 M.M.SDR DXTA200701968Motor · inoperativeAIRCRAFT CONTINUOUSLY DUTCH ROLLS, ALL ALTITUDES AND SPEEDS- ONE TO TWO DEGREES LEFT & RIGHT. SWAPPED YAW DAMPERS ON UPPER RUDDER- STILL NO IMPROVEMENT. REMOVED AND REPLACED AILERON SERVO MOTOR IAW CE750 MM CH 22-10-01. GROUND CHECKED GOOD.SDR DXTA200601701Adc · failedAT SPEEDS ABOVE .82 M, AIRCRAFT YAW LT AND RT UPPER YAW DAMPNER APPEARS NOT TO MOVE. UPPER AND LOWER YD SEVERED SELECTED TO (B) SIDE MACH TRIM WAS ALSO (B) SIDE FGS WAS LT SIDE. (M2B) REPLACED NR1 MADC DUE TO FAILURE IAW MM 31-44-00. OPS CHECK GOOD.SDR DXTA200601652Air Data Module · failedAT SPEEDS ABOVE .82M AIRCRAFT YAW LT AND RT UPPER YAW DAMPNER APPEARS NOT TO MOVE. UPPER AND LOWER YD SEVERED SELECTED TO (B) SIDE MACH TRIM WAS ALSO (B) SIDE FGS WAS LT SIDE. REPLACED NR 1 MADC DUE TO FAILURE IAW MM 31-44-00. OPS CHECK GOOD.SDR DXTA200601698Control Switch · stickingAFTER TAKEOFF AND DURING CLIMB, THE AIRCRAFT FELT VERY SLOPPY IN THE YAW AXIS. THE AIRCRAFT WOULD NOT COORDINATE TURNS. ATTEMPTED (S) TURNS AT FL340 AND WE GOT FULL BALL DEFLECTION. TRIED BOTH FGS NO CHANGE. UPPER RUDDER CHANNEL WOULD NOT CHANGE FROM B TO SDR DXTA200601600Pitot Head · cloggedDURING TAKEOFF ROLL AT 70 KIAS YAW DAMP FAIL AND MACH TRIM OFF YD NOT CENTERING ALL AMBER AND FGC A AND B FAIL CYAN EICAS MESSAGE. ENTERED IMT + PULLED CODES. FOUND CODES FOR AIR DATA MISCOMPARE. INSPECTED AIR DATA SYSTEM FOUND WATER IN THE PITOT LINES PUSDR DXTA200601447Strut · lowGEAR WOULD NOT RETRACT AFTER TAKEOFF. CHECKED OPERATION AT ALL PINS WITH OHMMETER AT NOSE AND MAIN GEAR SQUAT SWITCHES. CHECKED GOOD. JACKED A/C. CHECKED GEAR FOR FULL EXTENSION. FOUND NOSE GEAR NOT FULLY EXTENDING. SERVICED NOSE STRUT WITH HYDRAULIC FLUSDR DXTA200601255Acm · odorAFTER INITIATING DESCENT HEARD A LOUD POP AROUND THE GALLEY AND BRIEFLY SMELLED AN ACRID SMELL. PAX SAW A BRIEF PUFF OF WHITE SMOKE AROUND THE GALLEY FLOOR. NO OTHER ABNORMALTIES IN FLIGHT. AFTER LANDING THERE WAS A SMELL OF BURNING RUBBER IN THE CABIN. RESDR DXTA200501131Position Switch · faultyUPON TAKEOFF RIGHT MAIN GEAR LIGHT WOULD NOT EXTINGUISH (NO UNSAFE LIGHT OR HORN). RECYCLED GEAR SEVERAL TIMES AND LIGHT WOULD STAY ON MIDWAY TO DIVERSIONARY AIRPORT THE LIGHT EXTINGUISHED. REMOVED FAULTY RT DOWNLOCK SWITCH. INSTALLED NEW, OPS CHECK GOOD IASDR DXTA200501108Warning Light · false indicationAFTER GEAR RETRACTION RIGHT MAIN GEAR INDICATOR REMAINED ILLUMINATED. THERE WAS NO RED UNLOCK LIGHT. PUT THE GEAR DOWN AND THEN UP AND THE GREEN LIGHT ILLUMINATED FOR 30 SECONDS AND WENT OUT. PERFORMED LANDING GEAR OPERATIONAL TEST IAW CESSNA 750 MM 32-00-0SDR DXTA200500646Uplock Switch · out of adjustNOSE GEAR REPEATEDLY RAISING INTO WHEEL WELL AT 13,000, 17,000, 23,000 FT CAUSING A LOUD BANGING NOISE. DID NOT NOTICE UNLOCK LIGHT ILLUMINATING. SERVICED NOSE GEAR OLEO IAW CE 750 MM CHPT 12-10-38. ACCOMPLISHED NOSE GEAR UPLOCK SWITCH RIG CHECK, RIG CHECK
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