N627QS
Service difficulty reports not matched to an aircraft · 17
They name N627QS, 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 = 'N627QS' 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 = 'N627QS' 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 EBVR20190304001Pivot · crackedFOUND DURING INSPECTION: HORIZONTAL STAB AFT PIVOT FITTING CRACKED. P/N 6631102-31.SDR CWQR20150129005Fitting · crackedDURING A SCHEDULED INSPECTION, FOUND THE HORIZONTAL STABILIZER ATTACH FITTING CLIP CRACKED IN TWO PLACES. THE CRACKS WERE IN THE CUT OUT RADIUS ABOUT .12 INCH LONG. CLIP WAS SENT TO FOR EVALUATION. A REPORT WAS FILED UNDER SCR 708902.SDR DXTA2014101705912Unknown · smokeSMOKE WAS OBSERVED IN THE COCKPIT & CABIN. ODOR WAS ALSO OBSERVED.SDR 2012FA0000710Control Cable · frayedWHILE TROUBLESHOOTING, AN AUTO PILOT PORPOISE DISCREPANCY, THE TECH PULLED ON A PRIMARY RUDDER CABLE IN THE TAIL CONE AND IT SNAPPED. THE CABLE HAS BEEN BROKEN EXCEPT FOR A FEW STRANDS. IT APPEARS THE CABLE WAS NOT RIDING IN A PULLEY AND WAS CHAFING ON THE USDR DXTA2012052504979Unknown · odorAPPROX 1 HR INTO A FLIGHT, AT 41,000 AND IN NORMAL CRUISE MODE. CO-PILOT AND PILOT COULD DETECT AN ODOR OF FUEL. WENT TO BACK OF PLANE WHERE FOUR OTHER CREW MEMBERS COULD DETECT IT AS WELL. DURING DESCENT IT WASN'T AS NOTICABLE AT LOW POWER SETTINGS. INCRESDR DXTA2011042004551Water Separator · odorDISTINCT EXHAUST ODOR IN COCKPIT AT TAKE OFF WITH APU ON AND APU BLEED AIR ON. WITH BLEED AIR OFF THE ODOR IS REDUCED. IN FLIGHT THERE IS AN EXHAUST ODOR (NOT AS DISTINCT). IT IS REDUCED WHEN EITHER PRESS SOURCE IS SELECTED. FOUND APU OIL OVERSERVICED. REMSDR DXTA2011022104471Gyro · inoperativeAT FL 430, WITH PFD 2 SELECTED (RT SEAT FLYING) LT PFD COMMAND BAR TURNED BLUE ALONG WITH ALL TREND BARS AND COURSE INDICATORS. THE RED AIRSPEED TAPE DISSAPEARED AND THE ATTITUDE GYRO TURNED TO GRAY, VICA, BLUE AND BROWN. REPOSITIONED THE NR 1 PFD TO THE MFSDR 2010F00010Indicator · malfunctionedAFTER TAKE OFF (L) FUEL GUAGE ANNUNCIATOR ILLUMINATED. FUEL LOAD INITIALLY SHOWED 1000 LBS HIGH, THEN STABILIZED SHOWING 1000 LBS LOW AND REMAINED THERE.SDR DXTA2010010803933Flow Valve · inoperativeMOVING THE FUEL TRANSFER SWITCH FROM LT TO OFF CAUSES THE L/R LOW PRESS ANNUN. TO ILLUMINATE MOMENTARY & TURN THE L/R FUEL BOOST PUMP ANNUN. ON. TROUBLESHOT TO RT MOTIVE FLOW VALVE. R & R VALVE IAW MM CH 28-21-06. OPS & LEAK CHECK GOOD.SDR DXTA2009090303770Actuator · inoperativeLEFT GREEN DOWN AND LOCKED ANNUNCIATOR ILLUMINATED INTERMITTENTLY IN FLIGHT. HYDRAULIC PRESS LIGHT DID NOT ILLUMINATE. ALL OTHER INDICATIONS NORMAL. INSTALLED REPAIRED ACTUATOR IAW THE MM 32-30-04. OPS CKED GOODSDR DXTA2009033003571Indicator · unknownAT BEGINNING OF TAKEOFF ROLL THE RT FUEL QUANTITY INDICATOR DROPPED TO ZERO AND THE RT FUEL GAUGE ANNUNCIATOR AND MASTER CAUTION ILLUMINATED. STARTED APU AND WAITED 15 MIN. CHECKED SIGNAL CONDITIONER LED'S NO FAULTS DISPLAYED. STARTED ENGINES & TAXIED ACFT.SDR 2008FA0000676Control Cable · brokenDURING ROUTINE INSP, FOUND CABLE STRANDS BROKEN AND FRAMED. THE DAMAGED AREA OF THE CABLE IS WHERE IT GOES OVER A SERIES OF "S" PULLEYS MOUNTED IN THE HORIZ STAB. SHOULD MAKE THIS A TIME CHANGE ITEM. (K)SDR DXTA200803081Warning System · activatedBOTH L/R FUEL GAUGE ANNUNCIATORS ILLUMINATED ON TAKEOFF. TAKEOFF WAS ABORTED. FUEL QTY GAUGES BOTH READ ZERO. GAINED ACCESS TO LT/RT WING ROOT ELECTRICAL CONNECTORS FOR MOISTURE NONE FOUND. INSPECTED FUEL SIGNAL CONDITIONER FOR FAULT BITES NONE FOUND.SDR DXTA20082874Probe · reads lowON TAKEOFF ROLL, MASTER CAUTION CAME ON, REJECTED TAKEOFF, LT FUEL GAUGE ANNUNCIATOR LIGHT ON. CONNECTED TEST SET, FOUND PROBE NR 6 READING LOW. REMOVED NR6 PROBE, CLEANED AND REINSTALLED, PROBE NOW READING IN SAME RANGE AS OTHER PROBES, C/W WET CAL IAW MM CHSDR DXTA200702737Actuator · leakingON TAKEOFF, GOT A STAB MISCOMPARE LIGHT AND THE HYDRAULIC PRESS LIGHT. REPLACED ACTUATOR DUE TO EXCESS LEAKAGE IN ACTUATOR IAW 560XL M/M 23-40-00. OPS AND LEAK CHECK GOOD.SDR DXTA200702304Brake · stuckLT BRAKE IS STICKING CAUSING CONTROL ISSUES WHILE TAXIING. INSTALLED AN OVERHAULED BRAKE IN LT POSITION IAW MM CH 32-42. INSTALLED AN OVERHAULED METERING VALVE IN LT POSITION IAW THE MM CH 32-42.SDR DXTA200300108Pushrod · chafedDURING ROUTINE INSPECTION FOUND MAIN ENTRY DOOR PUSHROD (OPENING/CLOSING) RUBBING AGAINST THE CUTOUT IN THE DOOR STRUCTURE. ADJUSTED PUSHROD TO PREVENT CHAFING, PERFORMED BLEND OUT REPAIR TO CABIN DOOR FORMER IAW MFG REPAIR DEFINITION REPORT NR S-560XL-5227/01
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