N951QS
Service difficulty reports not matched to an aircraft · 25
They name N951QS, 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 = 'N951QS' 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 = 'N951QS' 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 DXTA2016060506250Float Valve · defectiveWING TANK O'FULL R CAS MSG CLIMBING THROUGH 37000' 270 KIAS WITH 30LBS FUEL IN CENTER TANK & APPROX 3100 LBS IN EACH WING TANK. VISUALLY OBSERVED FUEL VENTING. LOST 200 LBS IN 2 MINUTES. DE-FUELED ACFT, DOWN TO BE ABLE TO REMOVE OTBD WING ACCESS PANEL. REMSDR DXTA2012112605194Module · malfunctionedAT TOUCH DOWN A STRONG ODOR DETECTED IN COCKPIT AND GOT STRONGER WHEN APU BLEED AIR WAS PLACED IN HIGH. AT THE SAME TIME AURAL WARNING TONES 1 AND 2 CONTINUOUSLY SOUNDED AND DID NOT GO OUT UNTIL AVIONICS WAS TURNED OFF. TROUBLESHOT AND FOUND NR 1 AURAL ANNSDR DXTA2012070605038Access Panel · damagedLT AND RT WINGS HAVE A COMBINED 33 WING PANEL LANDS THAT ARE CORRODED BEYOND PUBLISHED LIMITS. REPAIRED IAW RD S750-0151/13RD2.SDR DXTA2010063004135Acm · failedON POWER REDUCTION, DESCENDING THROUGH 41000 FT, WHEN THE PAC HP VALVE OPEN ICAS COMES ON THERE IS A STRONG HOT SMELL FROM THE VENTS. ISOLATED THE PROBLEM TO THE COCKPIT PAC. R & R THE COCKPIT ACM PAC.SDR DXTA2010030804021Uplock Switch · out of adjustLANDING GEAR DID NOT RETRACT NORMALLY. RED UNLOCK LIGHT ILLUMINATED ALONG WITH REPETITIVE LOUD BANGING FROM THE NOSEWELL AREA. GEAR EXTENDED NORMALLY. ADJUSTED THE NOSE GEAR UPLOCK SWITCH IAW MM CH 32-30-05. REPACKED THE NOSE STRUT IAW CMM CH 32-20-02. THE SDR DXTA2009121803899Compressor · inoperativeDURING DESCENT BELOW FL300 WITH THROTTLES PULLED BACK & PA HP VALVE OPEN L-R CAS MESSAGE ILLUMINATED, A LOUD BANG HEARD BY BOTH PAX & CREW. COMING FROM AFT OF PILOT SEATS BUT FWD OF PAX SEATS & ACRID BURNING ODOR FILLED ACFT FOR SEVERAL MINTUES THEN ODOR DISSDR DXTA2009072903744Uplock Switch · out of rigDESCENDING THRU 20,000 FT AND 340KTS INDICATED THE NOSE GEAR STARTED TO EXTEND FOLLOWED BY GEAR UNLOCK LIGHT THEN RETRACTED BACK UP. FOUND ALL 3 UPLOCK SWITCHES OUT OF RIG. COMPLIED WITH ADJUSTMENTS OF ALL 3 UPLOCK SWITCHES TO SPEC'S OPS CHECKS GOOD IAW MM 32SDR DXTA2009070603717Brake Assy · weakPILOT SIDE BRAKES FEEL SOFT AND SEEM TO REQUIRE EXTRA PRESSURE TO GET ADEQUATE BRAKING, ESPECIALLY AT HIGH SPEEDS AND HIGH WEIGHTS, ALSO WHEN SETTING PARKING BRAKE. FOUND LEFT INBOARD & OUTBOARD BRAKE ASSEMBLIES WORN. REPLACED BOTH BRAKES WITH OVERHAULED ASSESDR DXTA2009070603719Brake Assy · weakPILOT SIDE BRAKES FEEL SOFT AND SEEM TO REQUIRE EXTRA PRESSURE TO GET ADEQUATE BRAKING ON LANDING AND WHEN SETTING THE PARKING BRAKE. VERIFIED SQUAWK. PERFORMED BLEED OF POWER BRAKE AND ANTISKID SYSTEM IAW MM 32-402. OP CHECK IS GOOD. PILOT AND COPILOT BRAKESDR DXTA20082947Actuator · inoperativeRUD LIMIT FAIL A CAS MSG CAME ON IN FLIGHT. RUDDER LIMIT 20 PERCENT. REMOVED ACTUATOR P/N 9914558-12 S/N 072 AND INSTALLED OVERHAULED ACTUATOR P/N 9914558-12 S/N 086. OPS CHECK IS GOOD. WORK PERFORMED IAW 27-23-00 AND 27-20-00.SDR DXTA200702146Unknown · warning lightTAKEOFF ABORTED DUE TO MACH TRIM OFF AND YD DAMP OFF CAS MESSAGE PRIOR TO 80 KTS. [SUP 05-02-07] CONFIRMED SPLIT IN AIRSPEED INDICATION AS WELL AS CONFIRIMED DISCREPANCY CAS MESSAGES. TROUBLESHOT TO A LARGE AMOUNT OF WATER IN PITOT PLUMBING. PURGED PLUMBING. SDR DXTA200702087Handle · stuckLANDING GEAR HANDLE WOULD NOT MOVE TO THE GEAR RETRACTED/ GEAR UP POSITION AFTER TAKEOFF. GEAR REMAINED EXTENDED. RIGGED NOSE LANDING GEAR SQUAT SWITCH IAW 750 MM CHP 32-60-00 LANDING GEAR SYSTEM. OPS CKED GOOD IAW 750 MM CHP 32-30-00.SDR DXTA200702071Wire · damagedAPPROXIMATELY 40 KTS ON TAKEOFF ROLL AIRCRAFT SHIMMEYED VIOLANTLY TAKEOFF ABORTED YAW DAMP OFF LOWER NOTED IN NOTED IN EICAS. VISUAL INSPECTION NOTED NOSE GEAR CENTERED 90 DEGREES RT TAXI LIGHT BROKEN. AIRCRAFT TOWED IN TO THE RAMP. INSPECTED NOSE GEAR, FOUNDSDR DXTA200601733Brake Assy · failedANTISKID AMBER CAS MESSAGE ON DURING FLIGHT. ON LANDING EMERGENCY BRAKES USED AND ALL 4 TIRES BLEW OUT. COMPLIED WITH ANTI SKID FUNCTION CHECK IAW MM 30-42-00 OPS CHECK GOOD. ALSO COMPLIED WITH MM TASK NR 32-42-06-210. VISUAL INSP OF TRANSDUCERS AND WIRING NSDR DXTA200601752Servo Control · bindingCONTROL WHEEL RATCHETING. LT CONTROL WHEEL THE RATCHETING IS MORE DEFINED. REMOVED AND REPLACED AFT AILERON SECTOR PCU IAW MM CHPT. 27-10-01.SDR DXTA200601726Control Unit · ratchetingCONTROL WHEEL RATCHETING. THE RATCHETING IS MORE DEFINED IN THE LT CONTROL WHEEL. REMOVED AND REPLACED AFT AILERON SECTOR PCU IAW MM CH 27-10-01.SDR DXTA200601715Mixer Box · wornCONTROL WHEEL FEELS LIKE THERE IS A DETENT AS YOU TURN EACH DIRECTION. PRIOR TO THAT POINT FROM CENTER (NEUTRAL) POSITION, TURN RATE IS SLOW. AFTER THE DETENT THE TURN RATE INCREASES. A/C DIVERTED TO SERVICE CENTER. REMOVED ROLL SPOILER MIXER BACK ASSEMBLYSDR DXTA200601489Yoke · bindingYOKE CONTROL BINDING WHEN DISPLACING LEFT. ADD MORE PRESSURE, YOKE WOULD MOVE. CHECKED CABLE TENSIONS, ALL CHECKED GOOD. REMOVED AND INSPECTED AILERON PUSH RODS AT AILERON FOUND BEARING TO BE TIGHT. CLEANED AND LUBED BEARINGS. REINSTALLED PUSHRODS SYSTEM,SDR DXTA200601482Brake Assy · unknownWITH EQUAL AMOUNT OF PRESSURE APPLIED TO THE BRAKES PEDALS, AIRCRAFT PULLS TO THE LEFT. AIRCRAFT RESPONDS THE SAME WITH LEFT SIDE OR RIGHT SIDE BRAKE APPLICATION. PILOT OR COPILOT BRAKE APPLICATION. PERFORMED POWER BRAKE SYSTEM FUNCTIONAL TEST WITH SATISFACSDR DXTA200601260Landing Gear · malfunctionedGEAR WILL NOT RETRACT, HANDLE WOULD NOT MOVE. COMPLETED GEAR SWING, NO DEFECTS NOTED, CHECKED NOSE WHEEL CENTERING CHECK GOOD. COMPLETED LANDING GEAR TROUBLESHOOTING TREE FOR GEAR HANDLE FAULT, NO FAULTS FOUND IAW CE-750 M/M CHPT 32-30-00. CONNECTED DMC MONSDR DXTA200601251Squat Switch · failedAFTER TAKEOFF, THE LANDING GEAR HANDLE WAS STUCK IN THE DOWN POSITION AFTER CYCLING IT, IT WAS RETRACTED, BUT THE RED GEAR UNSAFE LIGHT WAS ON. AFTER FURTHER CYCLING, THE GEAR WAS FINALLY DEPLOYED WITH NORMAL INDICATIONS (3 GREEN NO RED). REMOVED AND REPLACESDR DXTA200601239Acm · making metalIN CRUISE GOT STRONG BURNING SMELL FOR 2 TO 3 MIN FOLLOWED BY A LOSS OF CONTROL OF THE COCKPIT PAC TEMP. TEMP WENT HOT AND COULD NOT BE REDUCED IN MANUAL MODE OR AUTO, 35 DEGREES CHECK GOOD 43.5K OHMS. CLEANED RT COALESCER IAW CE750 MM CHAPTER 12-10-01-160. SDR DXTA200501022Odor · detectedREMOTE CB TRIPPED CYAN CAS MESSAGE CAME ON DURING DESCENT. BURNING ODOR WAS NOTICED FOR ABOUT 30 -45 SEC. ITEM IS UNDER INVESTIGATION.SDR DXTA200400354Fire Detector · malfunctionedAMBER FIRE DETECTOR FAIL R MESSAGE ILLUMINATED DURING CRUISE, DIVERTED AND LANDED SAFELY. ITEM IS UNDER INVESTIGATION. TROUBLESHOT AND FOUND THE ENGINE FIRE LOOP CHAFFED, REMOVED AND REPLACED THE RT ENGINE FIRE LOOP OPERATIONAL CHECK GOOD IAW MFG M/M CHAPTERSDR DXTA200400290Starter · failedAFTER TAKE-OFF FROM TEB, AT 1500 FT LEFT ENGINE FIRE INDICATION CAME ON, PULLED LEFT THROTTLE BACK AND INDICATION IMMEDIATELY EXTINGUISHED. DECLARED EMERGENCY AND LANDED SAFELY. – INITIAL INSPECTION NOTICED THE LT ENGINE COWLING HAS HEAT DAMAGE WITH A DELAMINA
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