N834QS
Service difficulty reports not matched to an aircraft · 16
They name N834QS, 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 = 'N834QS' 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 = 'N834QS' 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 2018F00028Skin Panel · corrodedUPPER WING SKIN CORRODED.SDR DXTA2017062306416Unknown · odorIMMEDIATELY AFTER TAKEOFF, CREW DETECTED A STRONG ELECTRICAL BURNING ODOR AND RETURNED TO DEPARTURE. NO SMOKE PRESENT. TURNED OFF AIR CONDITIONING, FORWARD, AFT AND OVERHEAD FANS. LANDING UNEVENTFUL. UNABLE TO DETERMINE SOURCE OF ODOR. INSPECTED THE AFT JSDR DXTR2017012901Service Door · delaminatedTHE OUTBOARD EDGE OF THE HYDRAULIC ACCESS DOOR HAS DELAMINATION, THE DAMAGE MEASURES APPROXIMATELY 3.0 INCHES LONG. ACCOMPLISHED MINOR REPAIR OF HYDRAULIC ACCESS DOOR IAW AQRD ERO-880588.SDR 2017F00124Skin · gougedTHE LT SIDE OF THE FUSELAGE HAS SEVERAL GOUGES. DAMAGE IS LOCATED AT BS 253.4 ABOVE STRINGER WL 104.8. ACCOMPLISHED MAJOR REPAIR IAW AQRD ERO 880379.SDR DXTR2017012801Skin · gougedTHE LT SIDE OF THE FUSELAGE HAS SEVERAL GOUGES. DAMAGE IS LOCATED AT FS 253.4 JUST ABOVE STRINGER WL 104.8. ACCOMPLISHED MAJOR REPAIR IAW AQRD ERO-880379.SDR DXTA201404105726Switch · inoperativeAFTER EXTENDING GEAR, LOW BRAKE PRESSURE & ANTISKID LIGHT REMAINED ILLUMINATED. RAN CHECKLIST WHICH REQUIRED CHECKING CIRCUIT BREAKERS. BOTH THE SKID CONTROL & POWER BRAKES WERE CHECKED IN. WE HAD TO PULL THE EMERGENCY BRAKE HANDLE TO STOP. ON POST FLIGHT SDR DXTA2011052604592Pressure Switch · failedLEVELING AT 45,000, RECEIVED RED "CABIN ALT" & "MASTER WARNING" LIGHTS. MASTER WARNING LIGHT CANCELLED, CABIN ALT LIGHT STAYED ON. PAX MASKS DID NOT DROP. CABIN DIFFERENTIAL PRESSURE DID NOT EXCEED 8.9 PSI AND CABIN ALT DID NOT EXCEED 7800 FT. ALL INDICATIONSDR 2010FA0001114Roller · wornTHE PN LISTED IN LINE 5 IS A 5000 LANDING REPLACEMENT ITEM AS REQUIRED IN CHAPTER 4 OF THE MM. THESE DEFECTIVE ROLLERS WERE FOUND WHILE PERFORMING OTHER WORK THAT REQUIRED REMOVAL OF 2 FLAPS. UPON REMOVAL OF THE FLAPS FOUND, 3 OF THE 8 ROLLERS TO BE DEFECTIVSDR DXTA2009080703754Blower · smokeDURING FLIGHT CREW OBSERVED WHAT SOUNDS LIKE A FAN HUMMING SOUNDS COMPARABLE TO WHAT IT SOUNDS LIKE WHEN ENGINES ARE OUT OF SYNCH. UPON LANDING PAX INFORMED US THAT SHE NOTICED SMOKE IN THE CABIN FOR 10 MIN PRIOR TO LANDING. TROUBLESHOT SYS, FOUND DEFOG BLOWESDR DXTA20082950Pitot System · contaminatedON TAKEOFF ROLL F/O AIRSPEED MISCOMPAIRED WITH CAPT A/S, TAKEOFF WAS ABORTED. DRAINED OUT EXCESS WATER FROM THE PITOT PROBES AND STATIC PROBES, AND PERFORMED AN AIR DATA SYSTEMS - INSPECTION/ CHECK. SYSTEMS CHECKED NORMAL IAW MM REV. 23, 34-11-10 & 34-11-26.SDR DXTA200802784Indicator · inoperativeON TAKEOFF CAPT'S AIRSPEED GAVE NO INDICATION, RED AIRSPEED ENUNCIATION SHOWED ON AIRSPEED INDICATOR. SIMULATED AIRSPEED WITH PITOT/STATIC TEST SET AND COULD NOT DUPLICATE DISCREPANCY. CHECKED NR 1 PITOT HOSE FOR MOISTURE, NO MOISTURE FOUND. BLEW OUT NR 1 PISDR DXTA200702616Pin · out of adjustMAIN CABIN DOOR IS VERY DIFFICULT TO OPEN FROM INSIDE AFTER FLIGHT. FOUND LOWER AFT DOOR PIN OUT OF ADJUSTMENT, ADJUSTED AFT LOWER DOOR PIN IAW CE560 M/M CH 52-10-00. OPS CK GOOD. CHECKED WARM AIR DUCT FOR PROPER INSTALLATION AND DOOR SEAL VALVE. NO DEFECTS SDR DXTA200601596Pressure Switch · failedDURING TAKEOFF UPON APPLICATION OF TAKEOFF POWER THE LEFT FUEL FILTER BYPASS LIGHT ILLUMINATED. TAKEOFF WAS ABORTED. CHANGED FUEL FILTER AND DIFFERENTIAL FUEL SWITCH. RAN LT ENG FOR APPROX 10 MIN WITH 5 MIN AT POWER AND SEVERAL QUICK ACCELERATIONS. TOOK FUSDR DXTA200601527Warning Light · illuminatedON TAKEOFF. ADVANCED THROTTLES TO 88.7 PERCENT. UPON REACHING 88.7 PERCENT THE RT ENGINE FUEL FILTER BYPASS ANNUNCIATOR ILLUMINATED. ITEM IS UNDER INVESTIGATION.SDR DXTA200601225Switch · looseTAIL CONE DOOR ANNUNCIATOR ILLUMINATED ON THE TAKEOFF ROLL. TAKEOFF ABORTED. DUPLICATED DISCREPANCY: FOUND DOOR LOCK SW WAS LOOSE AND OUT OF ADJUSTMENT. SECURED TAIL CONE DOOR WARN SW AND PROPERLY ADJUSTED TAIL CONE DOOR WARN SW. PERFORMED OPS CHECK OF TASDR DXTA200501171Line · failedAFTER LANDING POWER BRAKE AND ANTISKID MASTER CAUTION ILLUMINATED AFTER 1 SECONDS. AFTER 10 SECONDS OF ILLUMINATION TOTAL BRAKE FAILURE OCCURRED. EMERGENCY BRAKES WERE USED. PRECHARGE IS OUTSIDE OF SHADED AREA AFTER EVENT, NO OTHER ABNORMAL CONDITIONS WERE PR
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