N948QS
Service difficulty reports not matched to an aircraft · 23
They name N948QS, 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 = 'N948QS' 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 = 'N948QS' 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 DXTA2015122906146Coalescer Bag · odorA NASTY FOUL SOUR ODOR IS COMING FROM THE AIR CONDITIONING SYS. REMOVED LT & RT COALESCER SOCKS, THE SOCKS HAD A STRONG OIL ODOR. INSPECTED APU INLET & FOUND OIL IN APU INLET. REMOVED APU. INSTALLED A REPAIRED APU. APU WAS INSTALLED WITH SIX EACH NEW MOUSDR DXTA2015110606117Drive Assy · failedDESCENDING THRU 9000 MSL, 245K, ATTEMPTED TO EXTEND FLAPS TO 5 DEGREES, AT WHICH TIME EICAS INDICATED FLAPS FAIL. SLATS WERE FULLY DEPLOYED & FLAPS WERE EXTENDED LESS THAN 5 DEGREES. PER CHECKLIST, ATTEMPTED TO RESET FLAPS WITH NEGATIVE RESULTS. COMPLETED CSDR DXTA2015100106098Brake Sys · unknownBRAKES ARE SPONGY. TAKES ABOUT 2 INCHES OF BRAKE TRAVEL BEFORE BRAKES CAN BE ENGAGED. INSPECTED BRAKES, PERFORMED BLEEDING PROCEDURE, TAXI ACFT. OPS & LEAK CHECKED SATISFACTORY. SERVICED HYD SYS AS REQUIRED. NO FURTHER DEFECTS NOTED IAW AMM 32-42-00 & 1SDR DXTA2014060505790Acm · odorCOCKPIT A/C PACK INOPERATIVE, HAD AN OILY SMOKE ODOR & COULD NOT CONTROL SOURCE TEMP. R & R AFT ACM IAW MM 21-51-00. OPS & LEAK CHECKED GOOD.SDR DXTA2011060204603Acm · odorTHERE WAS A DISTINCT ODOR OF BURNED WIRES IN THE COCKPIT JUST PRIOR TO LANDING THAT QUICKLY DISSAPATED. NO ABNORMAL ELECTRICAL INDICATIONS WERE NOTED AND NO CIRCUIT BREAKERS WERE TRIPPED. AFTER ACM & WATER SOCK REPLACEMENT, RAN AIR CONDITIONING SYS USING ASDR DXTA2011041804549Carbon Seal · leakingON SHORT FINAL, HAD BRIEF EXHAUST LEAK, SMOKEY ODOR FROM COCKPIT OVERHEAD VENT. RAN APU AND TURNED ON BLEED AIR. THERE IS A NOTICEABLE OILY ODOR IN COCKPIT AND CABIN. STARTED ENGINES AND TURNED OFF APU. ODOR WENT AWAY. BOROSCOPED AREA AND FOUND OIL LEAKINSDR DXTA2010101904266Coupling · wornWHEN TURNING LT, ABOUT 20 DEGREES OF BANK, BELOW 180 KT, FULLY CONFIGURED, THE AIRPLANE LT WING SUDDENLY DROPPED PULLING THE YOKE LT EVEN MORE. THIS HAPPENED MORE THAN 3 TIMES. FOUND LT AILERON POSITION SENSOR FLEXIBLY COUPLING LOOSE ON SHAFT AND RETRACTING SDR 2010FA0001005Frame · crackedTHE PN 6760141-5 FRAME IS PART OF THE AILERON POWER CONTROL UNIT SUPPORT ASSY AND IS APPLICABLE TO ACFT 750-0001 TO 750-0149 THAT HAVE NOT BEEN MODIFIED BY SB750-27-44. DURING SCHEDULED INSP, THE FRAME WAS FOUND TO BE FATIGUE CRACKED. THE PART WAS REPLACED. SDR DXTA2010021603989Control Handle · faultedLANDING GEAR WOULD NOT RETRACT. THE LANDING GEAR HANDLE WOULD NOT MOVE. R & R THE GEAR CONTROL HANDLE WITH REPAIRED UNIT IN REF TO MM 32-30-01. ALL FINAL OPS CHECKS SATISFACTORY.SDR DXTA200803124Static Port · obstructedAT AIRSPEED ALIVE, MACH TRIM & YD KICK OFF AND BOTH AMBER CAS MESSAGES ON EICAS. ABORTED T/O. T/S SYSTEM LT STATIC PORT BLOCKED CLEANED STATIC PORT. PERFORMED LEAK CHECKS. FOUND PILOTS SIDE LEAK RATE HIGH FIXED LOOSE FITTING ON PILOTS STATIC SYSTEM. SYSTEM LSDR DXTA200802997Acm · odorUPON DESCENT BEFORE LANDING MOMENTARILY DETECTED SOMETHING SULFEROUS THAT DISSIPATED IMMEDIATELY - 5 MINUTES AFTER SHUTDOWN THE SAME ODOR RETURNED OUT OF CABIN RT SIDE WEMACS. REMOVED THE ACM DUCTING TO GAIN ACCESS TO THE COCKPIT ACM. REMOVED ACM. INSTALLED SDR DXTA200702445A/C Pack · odorCOCKPIT PAC TEMPERATURE IS UNCONTROLLABLE AND PRODUCES A BURNING / SULFUR TYPE ODOR. TROUBLESHOT SYSTEM. FOUND ACM AND TEMPERATURE CONTROL VALVES INOP. TEMP. CONTROL VALVE REMOVED PN 27241287-10, SN 10AT77. INSTALLED O/H PN 27241287, SN 4AR32. ACM REMOVSDR DXTA200701974Pcu · inoperativeON LANDING A "FLIGHT CONTROL FAULT" MESSAGE APPEARED AND THE 'AILERON FLIGHT CONTROL SHUTOFF LIGHT BLINKED. REPLACED "B" PCU (AILERON) , ADJUSTMENT & OPS. IAW. CE 750. M/M CE750. 27-11-05.SDR DXTA20061689Actuator · failedDURING DESCENT THROUGH FL300, THE AMBER CAS MESSAGE "PITCH FEEL FAIL" CAME ON FOR ABOUT 5 MIN THEN WENT OUT AND BACK ON FOR ANOTHER 3 MIN. REMOVED FAILED RT ELEVATOR CONTROL ACTUATOR AND INSTALLED OVERHAULED UNIT IN ACCORDANCE WITH CE 750 MM CH 27-33-00. OPESDR DXTA200601227Electrical Sys · unknownALL INTERIOR ELECTRICS INOPERATIVE. STRONG ELECTRIC SMELL IN AFT CLOSET.SDR DXTA200601215Strut · underservicedAFTER TAKEOFF GEAR WOULD NOT RETRACT. PLACED ACFT ON JACKS AND NOTED NOSE STRUT WOULD NOT FULLY EXTEND ALLOWING THE NOSE WOW SWITCH TO MAKE CONTACT. COMPLIED WITH NOSE STRUT SERVICING IAW 750 AMM 12-10-38. LOWERED ACFT ON GROUND THEN PLACED BACK ON JACKS ANSDR DXTA200501160Landing Gear · malfunctionedGEAR WOULD NOT RETRACT AFTER TAKEOFF. JACKED AIRCRAFT, OPS CHECK OF LANDING GEAR, LANDING GEAR CYCLED NORMALLY. DISCONNECTED ALL CONNECTORS TO UPLOCKS AND SQUAT SWITCHES. CLEANED ALL CONNECTORS. VERIFIED SQUAT SWITCHES WERE PROPERLY RIGGED. CONNECTED ALL CSDR DXTA200501092Line · rupturedHYD VOLUME LOW A CAS MESSAGE IN FLIGHT. LOST A SYSTEM FLUID. LANDED WITH EMERGENCY BRAKES. STEERING GEAR EXTENDED BEFORE PROBLEM, SO WAS NOT BLOW DOWN. JACKED AIRCRAFT, APPLIED PRESSURE, FOUND NOSE GEAR ACTUATOR EXTEND HOSE RUPTURED. REF SQ 9 THIS WORK ORSDR DXTA200500959Handle · dirtyFLAPS FAILED AT 15 DEGREES. FLAPS FAILED AT 15 DEGREES HAD BITES NR 2 AND NR 6 ON CONTROLER REMOVED FLAP HANDLE, REMOVED COVER AND CLEANED LINT FROM INSIDE HANDLE IAW: CE750 M/M 27-50-00. FLAPS OPERATIONALY CHECK GOOD.SDR DXTA200500922Flap System · malfunctionedWHEN FLAPS SELECTED TO FIVE, FLAP FAIL CAS MESSAGE APPEARED. FOLLOWED CHECKLIST, ATTEMPTED RESET, FLAPS FALLEN AGAIN IN THE FLAP FIVE POSITION.SDR DXTA200601194Unknown · unknownTEN MILES FROM DESTINATION AIRPORT, BUSS NR 1 WENT TO EMERGENCY POWER. DECLARED EMERGENGY AND LANDED SAFELY. ITEM IS UNDER INVESTIGATION.SDR DXTA200400279Control Valve · leakingUPON GEAR EXTENSION HYDRAULIC FLUID LEVEL DROPPED BELOW 16 PERCENT, DIVERTED AIRCRAFT TO APA AND LANDED SAFELY. FOUND SLAT SPOOL VALVE LEAKING, REMOVED AND REPLACED VALVE, BLED A/B SYSTEM RESERVOIRS WITH (2) GALLONS OF SKYDROL EACH. LEAK CHECKED GOOD IAW THESDR CWQ2002F00000Transorb · burnedDISPLAY UNITS 4 AND 5, FMS 2 SCREEN AND RADIO CONTROL UNIT SCREEN BLANK. AVIONICS FAN INSPECTION AND CAS MESSAGES DISPLAYED. CAUSE OF DISCREPENCY APPEARS TO BE TRANSORB (PN S3106-5) WIRED INTO QUICK DISCONNECT FITTING CONNECTED TO THE RIGHT SIDE AVIONICS REL
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