N913QS
Service difficulty reports not matched to an aircraft · 27
They name N913QS, 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 = 'N913QS' 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 = 'N913QS' 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 DXTA201503316000Acm · seizedON START UP WHEN WE POWERED UP, WE GOT SMOKE IN THE COCKPIT & CABIN. VERIFIED THAT THE CABIN ACM IS STARTING TO SEIZE AT THE PROPELLER SHAFT, COCKPIT ACM FOUND TO BE IN NORMAL OPERATION. INSPECTED FWD ACM (COCKPIT PAC) FOUND TURBINE FAN FAILURE EVIDENT, RESDR DXTA2014092205891Skin · corrodedLEFT & RIGHT MUTABLE WING FUEL BAY PANELS LAND HAVE CORROSION ON LAND & ON UPPER SURFACE OF LOWER SKIN. REPAIRED IAW S-750-0113 23RD.SDR DXTA2014090205870Apu · malfunctionedSMOKY & OILY SMELL COMING FROM ENVIRONMENTAL SYS. SMELL OCCURS WITH BOTH COCKPIT & OR CABIN PACS. NO VISIBLE SMOKE IS OBSERVED. REMOVED & REPLACED APU WITH CUSTOMER SUPPLIED UNIT. DONE IN REF WITH CE-750 MM CH 49-10-00. OPS & LEAK CHECKS GOOD. ALL ACCESS CLSDR DXTA2014082405867Skin · corrodedCORROSION WAS FOUND AT SEVERAL LOCATIONS ON THE LT & RT WING LOWER SKINS LOCATED AT 522AB, 621HB & 622EB. VERIFIED CORROSION REMOVAL IAW 750 NONDESTRUCTIVE TESTING MANUAL PART 6 CHAPTER 57-20-01. ACCOMPLISHED REPAIR TO LT & RT LOWER WING SKINS AT 522AB, 621HBSDR DXTA2013070505431Brake Sys · malfunctionedON LANDING, TAKING EXCESSIVE BRAKE PRESSURE TO STOP. NO PULLING LT OR RT, FLUID QUANTITY GOOD, BRAKE WEAR PINS GOOD. HAD DIFFICULTY SETTING PARKING BRAKE. HAD TO PUMP BRAKES 6-8 TIMES FOR LOW PRESSURE LIGHT TO GOING OUT. INSPECTED BRAKES FOR WEAR AND CONDITSDR DXTA2012052904981Unknown · odorON DESCENT DETECTED A BURNING ODOR. F/O WENT BACK AND DETECTED THE BURNING ODOR MORE INTENSELY. NO SMOKE OBSERVED. LANDED UNEVENTFULLY. CLEANED BOTH SOCKS & WATER SEPARATORS, OZONE CONVERTORS AND AU DUCTING ASSOCIATED. ALSO CLEANED DUCTING FROM ACM'S TO SDR DXTA2011012404426Uplock Switch · malfunctionedGEAR UNSAFE LIGHT REMAINED ON AFTER HANDLE WAS RAISED. R & R LT MAIN GEAR UPLOCK SWITCH IAW MM 32-30-05.SDR DXTA2010061404122Gcu · failedWHILE IN CLIMB, WE HAD THE LT GENERATOR AMBER CAS MESSAGE. RAN CHECKLIST. A FEW MINUTES LATER WE HAD MULTIPLE AMBER CAS MESSAGE, NR 1, 2 AND 3 TUBES WENT BLACK AND NR 4 AND 5 TUBES STARTED FLASHING. LANDED WITH NO FLAPS, NO TRS, SUSPECTING BUSS CONTROLLER FAISDR DXTA2009061503687Acm · seizedSWEET SMOKE ODOR IN COCKPIT IN CRUISE AT FL430. NO VISIBLE SMOKE. NO PAX SMOKING. EMERGENCY DESCENT TO LANDING PERFORMED. PAX DIDN'T DETECT ANYTHING. FOUND COCKPIT PAC TO HAVE NO COOLING OUTPUT. VISUALLY INSPECTED INLET IMPELLER, VERIFIED NO ROTATION WITH PACSDR DXTA200803226Wheel · vibrationSTRONG NOSE WHEEL SHIMMY ON TAKEOFF. ABORTED TAKEOFF. (S)SDR DXTA200808153226Wheel · out of balanceSTRONG NOSE WHEEL SHIMMY ON TAKEOFF. PREVIOUS HISTORY SHOWED NOSE WHEEL UNDER TORQUED AND REPLACED, UPPER AND LOWER WERE REPLACED. BOTH NOSE TIRES HAD NO FLATS SPOTS. RECORDED ALL TIRE PRESSURES, TREAD DEPTH. RT NOSE WHEEL NOT TORQUED TO 200"LBS AND LT TORQUESDR DXTA200803165Scissor Link · damagedDURING TAKE OFF AT 40 KTS A SEVERE SHIMMY VIBRATION AT THE NOSE WHEEL THRU 55 KTS. IT WAS SO SEVERE THAT IT KICKED THE YD LOWER. TAKEOFF GROSS WEIGHT 30,773. FUEL 8400. REMOVED AND REPLACED NOSE LANDING GEAR UPPER AND LOWER SISSOR TORQURED LINKS ASSYING OPERSDR DXTA200803121A/C Pack · odorAT FL390 DETECTED SMOKE AND PERFORMED AND EMERGENCY DECENT AND DIVERTED TO OMA. NO VISIBLE SMOKE UNTIL PACKS OFF. A HAZE DEVELOPED. REPLACED AFT ACM TURBINE REMOVED & REPLACED BOTH LT & RT COALESCER SOCKS & O-RINGS. F/T'D ACMM BY OPERATING APU , AT THIS TIMSDR DXTA200803109Switch · out of adjustNOSE DOOR OPEN L MESSAGE DISPLAYED AFTER TAKEOFF AT GEAR RETRACTION. ADJUSTED DOOR WARNING SWITCHES IAW MM 52-70-00 OPS CHECK GOOD.SDR DXTA200803092Wheel · vibrationTAKE OFF ABORTED DUE TO SEVERE NOSE WHEEL SHIMMY AND VIBRATION. R&R BOTH NOSE TIRE & WHEEL ASSY'S IAW MM 32-41-00 TAXI CHECK GOOD.SDR DXTA200802819Computer · inoperativeAT FL410 GOT AMBER PRI STAB TRIM FAIL. TROUBLESHOT TO NR1 (LT) IAC, REMOVED REPLACED AND OPS CHECK GOOD, NR1(LT) IAC IAW MM 34-25-01 NO OTHER DEFECTS NOTED.SDR DXTA200702500Lamp · burned outLT PANEL LIGHTING C/B POPPED WITH BURNING INSULATION ODOR UPON ACTIVATION OF DAY/ NIGHT DIM SWITCH PRIOR TO ENGINE START. KPHL CHECKED AND LT PANEL LTS AND CB OPERATED NORMALLY. PERFORMED PIN OUT FOR POWER, GND AND CONTINUITY. AH PANEL CB JC028 AND LIGHTING SDR DXTA200702312Acm · leakingEXTREME SULPHUR FUMES IN COCKPIT AND CABIN AT FL390, BOTH PACS IN NORM, BOTH TEMP SELECT IN AUTO, ENROUTE TIME 60 MINUTES. FUMES DISIPATED DURING DESCENT. DECLARED AN EMERGENCY. NORMAL APPROACH AND LANDING. REMOVED AND REPLACED AFT ACM IAW MM 21-51-00. OPSSDR DXTA200702254Ptu · inoperativeHYD A PRESSURE DROPPED TO 2000 PSI, FOLLOWED BY AMBER CAS (HYD LOW QTY B) AND (HYD O TEMP B) MESSAGES ILLUMINATED. REMOVED & REPLACED PTU, LH ENGINE DRIVEN HYD. PUMP & "A" HYD FILTER ASSEMBLY, IAW THE 750 MAINT. MANUAL 29-10-02, 29-10-09 & 29-20-04. OPERATISDR 2006FA0001233Connector · shortedBATTERY OVERTEMP INDICATED R-RED CAS MESSAGE IN FLIGHT. FOUND SPLICE AT THE BATTERY TEMP SENSOR CONNECTOR PY044 BROKEN. ALSO CONNECTOR WAS FOUND BADLY CORRODED INSIDE OF CONNECTOR. REPLACED CONNECTOR PY044 AND REPLACED WIRES IAW CE750 WIRING MANUAL 20-10-06SDR DXTA200601801Connector · corrodedBATT O'TEMP RIGHT RED CAS MESSAGE ILLUMINATED IN FLIGHT. REMOVED AND REPLACED CONNECTOR PY044 & REPLACED WIRES IAW CE750 W/M CH 20-10-06. OPS CHECKED GOOD.SDR DXTA200601531Acm · seizedCABIN PAC OVERHEAT WHILE USING AIR CONDITIONING FROM THE APU ON THE GROUND. SMOKE FILLED THE CABIN, APU AND PAC WAS SHUT DOWN DURING FLIGHT FROM IAD TO ADS. INSPECTION OF ACM REVEALED BLACK OIL IN SIGHT GAUGE. REMOVED FORWARD ACM AND INSTALLED CUSTOMER SUPPSDR DXTA200501144Anti-Ice System · failedANTI-ICE ON BEFORE TAKEOFF RECEIVED NO COLD MESSAGES POWER TO TAKEOFF DETENT GOT 'SLAT COLD' MSG AND 'HOT STAB' MSG. ABORTED, SHUT DOWN ANTI-ICING AND ALLOWED TO COOL. RESET ANTI-ICING POWER UP. SAME MESSAGES REPEATED +GOT 'WING ANTI-ICE HOT R' MSG. PERFORSDR DXTA200501020Warning Light · illuminatedAFTER TAKEOFF, GREEN NOSE WHEEL DOWN INDICATOR LIGHT REMAINING ON. NO RED UNLOCK INDICATOR, AND NO AUDIBLE GEAR OR GEAR DOOR NOISE. GEAR EXTENDED NORMALLY, NORMAL LANDING. ITEM IS UNDER INVESTIGATION.SDR DXTA200500913Autopilot Sys · malfunctionedARRIVING 180 KNOTS, AUTO-PILOT REPEATEDLY CAME OFF-LINE. ELEV FELT HEAVY ON CONTROLS. AT 140 KNOTS, PRIMARY TRIM WOULD NOT WORK. NO CAS MESSAGES RECEIVED EXCEPT WHEN SECONDARY TRIM ARMED. SECONDARY TRIM NOT ATTEMPTED. DOWNLOADED FAULT HISTORY FROM IAC NR 1&SDR DXTA200500728Control Cable · out of adjustAIRCRAFT ROLLS RIGHT DURING CRUISE. AILERON TRIM IS ROLLED OVER HALFWAY TO HOLD LEVEL FLIGHT. RUDDER TRIM IS ALSO TO LEFT OF CENTER. CONTROL RIGGING NEEDS TO BE CHECKED. - TROUBLESHOT BOTH AILERON AND RUDDER SYS. FOUND AILERONS TO BE RIGGED CORRECTLY. RUDDERS SDR DXTA200400332Odor · detectedALL WEMAC EMITTED A STRONG SULFUR SMELL INTERMITTENTLY IN DIFFERENT VALVE AND PAC POSITIONS, AS A RESULT CANNOT DETERMINE SOURCE. RAN ENGINES AND APU, USED BLEED AIR WITH NO ODOR FROM WEMACS. INSPECTED COALESCER SOCKS WITH NO DISCREPANCY OR ODORS NOTED. SYS
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