N707QS
Service difficulty reports not matched to an aircraft · 16
They name N707QS, 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 = 'N707QS' 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 = 'N707QS' 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 DXTA2014042505742Control Column · chafedLEFT PILOT CONTROL COLUMN HAS CHAFING MARKS FROM THE AILERON CABLE INSIDE COLUMN. REMOVED PILOT'S CONTROL COLUMN. MACHINED AND BLENDED DAMAGED AREA. ALODINED AND PRIMED AS REQUIRED. RE-INSTALLED PILOT'S CONTROL COLUMN. PERFORMED ALL FLIGHT CONTROL TRAVEL TSDR DXTA2014040705720Brake Sys · weakDURING LANDING, THE BRAKES WERE SPONGY WITH THE PEDALS TO THE FLOOR. PERFORMED BLEEDING OF THE BRAKE SYSTEM IAW MM 32-40-20. BRAKE SYSTEM OPS & LEAK CHECKED GOOD.SDR DXTA2014040405715Unknown · vibrationVIBRATION BEGINS AT FL260 AT 290KTS, INCREASED INTENSITY TO 350KTS. FELT IN CONTROL COLUMN & NOT IN RUDDER PEDALS. VIBRATION FELT IN COCKPIT SEATS & IN CABIN SEATS. CHECKED ALL ELEVATOR BELLCRANKS, PUSHRODS, CONTROL COLUMS AND HINGE POINTS FOR CONDITION ANDSDR DXTA2012030504905Unknown · odorAFTER STARTING APU, A STRONG ELECTICAL BURNING ODOR DETECTED. APU TURNED TO RAM AIR, COULD NOT DETECT BURNING ODOR. SHUTDOWN ACFT. INSPECTED ACFT, NO DEFECTS NOTED.SDR DXTA2011021004461Control Valve · inoperativeHEARD A MODERATELY LOUD "THUMP" SOMEWHERE BENEATH OUR FEET ON CLIMBOUT AROUND 12,000 FEET, FELT IT AS WELL. THE SOUND WAS SIMILAR TO WHEN YOU CONNECT THE NOSE WHEEL STEERING ON THE GROUND ONLY A BIT LOUDER. REMOVED NOSE STEERING CONTROL VALVE. INSTALLED A MOSDR DXTA2010092004244Display · intermittentCOPILOT'S PFD TURNS ON AND OFF INTERMITTENTLY. REMOVED CO-PILOT MFD. CHECKED THE FILTER SCREEN ON BACK OF MFD. FOUND DEBRIS ON SCREEN. REMOVED AND CLEAN ALL DEBRIS FROM THE FILTER SCREEN. RE-INSTALLED THE CO-PILOT MFD INTO ITS ORIGINAL POSITION. OPS CHECKSDR DXTA2010052604103Brake · wornBRAKES WEAK. ON LANDING IT TAKES AN ABNORMAL AMOUNT OF TOE PRESSURE TO INSURE STOPPING. DURING TAXI IN AT BRISK WALK SPEED APPLIED BRAKE PRESSURE SIMULATING EMERGENCY STOP NECESSITY. MOMENTARY FELT BRAKES ENGAGE, BUT THE ACFT CONTINUED COASTING. IT APPEARS ASDR DXTA2009052603663Slat System · out of rigON CLIMBOUT DURING SLAT RETRACTION RECEIVED A WHITE/ADVISORY FLAP/SLATS FAILED TO RETRACT FULLY. FLAPS AND KRUGER WORKED NORMALLY. ACFT WEIGHT AND TAKEOFF WAS APPROX 33000 LBS. CHECKED SLAT RIGGING NO DEFECTS NOTED. RE RIGGED SLATS IAW MM 27-30-00. OPS CHECKESDR DXTA2009030903535Holder · looseUPON COMPLETION OF RT ENGINE START APU FIRE MASTER WARNING EICAS AND FIRE BELL CAME ON. QRH CHECKLIST RUN;BOTTLE FIRED. FOUND FUSE HOLDER FOR RELAY 205W LOOSE. RESECURED FUSE HOLDER AND PERFORMED G200 261010 APU FIRE DETECTION SYSTEM OPS TEST WITH NO DEFECTS NSDR DXTA200802970Slat · malfunctionedON DEPARTURE, GOT FLAP/SLAT MAINT MESSAGE. SLATS DID NOT COME ALL THE WAY UP. PERFORMED FUNCTIONAL TEST OF THE FLAP/SLAT CONTROL AND DRIVE SYS WITH NO DEFECTS NOTED AT THIS TIME. ALL WORK COMPLETED IAW CMP 275101.SDR DXTA20082970Slat System · malfunctionedON DEPARTURE, GOT FLAP / SLAT MAINT MESSAGE. SLATS DID NOT COME ALL THE WAY UP. PERFORMED FUNCTIONAL TEST OF THE FLAP/SLAT CONTROL AND DRIVE SYSTEM WITH NO DEFECTS NOTED AT THIS TIME. ALL WORK COMPLETED IAW CMP 275101.SDR DXTA200802844Air Duct · contaminatedWITH THE APU ON THE COCKPIT FILLED WITH JET FUEL FUMES STRONG ENOUGH TO BURN YOUR EYES. FOUND AIR COND. DUCTS UNDER CABIN FLOOR TO BE FUEL SOAKED. REMOVED FUEL SOAKED DUCTS AND INSTALLED INSPECTED DUCTS, LEAK AND OPS CHECKED OK. IAW G200 MM 25-00-00. NO ODOR SDR DXTA200701874Trim System · failedAUTOPILOT PITCH TRIM FAILED AFTER TAKEOFF WE WERE UNABLE TO CONTROL TRIM W/YOKE THUMB SELECTOR AUTOPILOT WAS FUNCTIONAL AFTER WE TRIMMED AIRCRAFT IN SECONDARY DISCONNECT POSITION TRIM BECAME SEMI FUNCTIONAL UPON ARRIVAL. TROUBLESHOT SYSTEM AND DETERMINED THATSDR DXTA200500933Transducer · inoperative" ANTI-SKID OFF " LIGHT ILLUMINATED DURING TAXI OUT, PRESSED TO RESET AND APPROX 1 MIN LATER IT ILLUMINATED, CYCLED ANTI-SKID CB'S AND IT AGAIN ILLUMINATED AND CONTINUED TO CYCLE ON /OFF APPROX EVERY MIN. REMOVED TRANSDUCER ON NR 4 WHEEL P/N: 606568 S/N: OLT0SDR DXTA200500644Position Switch · shortedT/O UNSAFE EICAS ILLUMINATED DURING TAKEOFF ROLL. ABORTED AT 120 KNOTS. ATTEMPTED TO DUPLICATE INDICATION IN HANGER WITH EXTERNAL POWER SUPPLIED, COULD NOT DUPLICATE. INSPECTED ALL 8 AIRBRAKE SWITCHES VISUALLY FOR OBVIOUS DEFECTS, NONE NOTED. RANG OUT AIRBSDR 2004F00155Brushes · wornCREW REPORTED APU INOPERATIVE TROUBLESHOT SYSTEM AND FOUND VOLTAGE AVAILABLE AT STARTER GEN. REMOVED STARTER GEN AND BRUSH COVER. FOUND 2 OUT OF 4 BUSHES WELDED IN BRUSH HOLDERS AND BUSH WIRES BROKEN OFF. INSULATION STRIP ON INSIDE OF BRUSH COVER WORN BURNE
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