N812QS
Service difficulty reports not matched to an aircraft · 16
They name N812QS, 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 = 'N812QS' 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 = 'N812QS' 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 DXTA2013090305492Uplock Switch · malfunctionedAFTER TAKEOFF "GEAR UNLOCKED" ANNUNCIATOR WOULD NOT EXTINGUISH. HYD PRESSURE ANNUNCIATOR REMAINED ON. LOWERED GEAR. LANDING WAS NORMAL. FOUND HYD FLUID ON NOSEWHEEL. JACKED AIRCRAFT, PERFORMED GEAR SWING, NOSE GEAR WOULD NOT LOCK. INSPECTED GEAR, CHECKED STRSDR DXTA2013081605475Motor · failedLOW BRAKE PRESSURE AND ANTI SKID INOPERATIVE ILLUMINATED DURING TAXI , EMERGENCY BRAKE HANDLE WAS USED TO STOP ACFT MOVEMENT . AFTER ENGINE SHUTDOWN, NOTICED BRAKE ACCUMULATOR MOTOR WAS NOT RUNNING WITH BATTERY SWITCH ON AND CIRCUIT BREAKER CLOSED. AFTER 30SDR CWQR20120306013Transfer Tube · chafedFOUND FUEL TRANSFER TUBE CHAFED BY THE CLAMP ASSY BEYOND ALLOWABLE LIMITS. HAVE FOUND A NUMBER OF THESE TUBES CHAFED BECAUSE OF MISALINEMENT. A NEW TUBE WAS INSTALLED IAW ACFT MM.SDR CWQR20120306012Transfer Tube · chafedWHILE WORKING SL560-28-09, FOUND FUEL TRANSFER TUBE CHAFED BY CLAMP ASSY BEYOND ALLOWABLE LIMITS. FOUND A NR OF THESE TUBES CHAFED BECAUSE OF MISALIGNMENT. A NEW TUBE WAS INSTALLED IAW ACFT MM.SDR CWQR20120306011Transfer Tube · chafedWHILE WORKING SL560-28-09, FOUND FUEL TRANSFER TUBE CHAFED BY CLAMP ASSY BEYOND ALLOWABLE LIMITS. FOUND A NR OF THESE TUBES CHAFED BECAUSE OF MISALIGNMENT. A NEW TUBE WAS INSTALLED IAW ACFT MM.SDR CWQR20120306010Tube · chafedWHILE COMPLYING WITH SL560-28-09, FOUND FUEL TUBE ASSEMBLY DAMAGED BEYOND LIMITS BY THE CLAMP. THE TUBE WAS REPLACED AND THE TUBE ASSY WAS INSTALLED WITH LESS THA 4 DEGREES OF MISMATCH IAW THE MM. THIS REPORT AND PICTURES HAVE BEEN SENT TO MFG UNDER SCR 610SDR CWQR20120215007Fitting · chafedWHILE PREFORMING THE INSPECTION FOR SL560-28-09, FOUND CHAFE MARKS ON THE FUEL FITTINGS. AFTER REMOVAL OF THE FUEL LINE ASSY, FOUND THAT THE FITTING CLAMP ANTI-ROTATION STRAPS HAD CUT INTO THE FITTING BELL MOUTH BEYOND THE ALLOWABLE LIMITS.SDR CWQR20120210005Line · chafedWHILE PERFORMING THE INSPECTION FOR SL560-28-09, FOUND A DENT IN THE FUEL LINE. AFTER REMOVAL OF THE FUEL LINE ASSY, FOUND THAT THE FITTING CLAMP ANTI-ROTATION STRAPS HAD CUT INTO THE FITTING BELL MOUTH BEYOND THE ALLOWABLE LIMITS.SDR DXTA2009060803680Fuel Control · inoperativeON TAKEOFF, LT ENG SLOW TO ACCELERATE. NORMAL CLIMB OUT, N1 SYNC ON FL 180. LEVELED FL 390 N1 MATCHED 90 % ACCELERATING TO CRUISE. LESS THAN 2 MIN INTO ACCELERATION N1 DROPPED TO 60 % & FUEL FLOW DROPPED TO 220 PPH. DESCENDED TO FL 290. MOVING THROTTLE DID NOTSDR DXTA2009050803640Motor · faultyDURING GROUND GPU POWER OPERATION THE FREON AIR CONDITIONER BEGAN SMOKING INSIDE THE ACFT. THE AC UNIT APPEARS BURNED AND CHARRED. NO FIRE WAS NOTED FOLLOWING REMOVAL OF POWER FROM THE ACFT. INSPECTED THE FREON AIR CONDITIONING UNIT AND FOUND THE MOTOR/BRUSHESDR DXTA2009041309596Outflow Valve · contaminatedC/W M/M STATIC TEST, LIGHT DQUENCE SHOWS THAT CONTROLLER IS OUT OF CALIBRATION. FURTHER TROUBLESHOOTING FOUND SEQUENCE IS CORRECT. SUSPECT MOISTURE IN PLUMBING LEADING TO OUTFLOW VALVE FREEZING. REMOVED MAIN BATT. FOR ACCESS. REMOVED ACCESS PNL'S. AFT. CABIN. SDR DXTA2009041303596Cabin Pressure · malfunctionedCLIMBING THROUGH FL230 THE CABIN PRESSURE BEGAN TO RAPIDLY RISE. AN EMERGENCY DESCENT WAS INITIATED TO 10,000 FT. DURING THE DESCENT THE CAB ALT ANNUNCIATOR ILLUMINATED WHEN CABIN PRESSURE EXCEEDED 10,000 FT.SDR DXTA200702404Filter · dirtyLOW BRAKE PRESS/ANTISKID INOP, ANNUNICATOR ILLUMINATED AT BEGINNING OF OUR TAXI. CHANGED ANTI-SKID PUMP FILTER. BLEED ANTI-SKID BRAKE SYSTEM. RECONNECTED LOW PRESSURE SWITCH. C/W OPS CHECK, LEAK CHECK, & TAXI CHECK. ALL CHECKS GOOD. WORK C/W IAW 560MM 32-42-SDR DXTA200601554Air Filter · odorAFTER TAKEOFF, HAD ODOR IN COCKPIT, VERIFIED BY PASSENGERS IN CABIN. TURNED OFF A/C AND ODOR DISAPPEARED. NOTE: WHEN FREON SYSTEM WAS TURNED OFF ODOR WENT AWAY. ACM WAS STILL ON, CLEANED BOTH COCKPIT AND CABIN FILTERS FOR FREON BLOWERS, NO OTHER DEFECTS NOTSDR DXTA200601550Fan · odorDURING FLIGHT FROM CAE TO PWK, NOTICE ODOR IN COCKPIT SIMILAR TO CIGARETTE LIGHTING UP. TURNED OFF DEFOG FAN, ODOR STOPPED, 15 MIN LATER ODOR RETURNED. TURNED OFF FWD FREON FAN, ODOR STOPPED. NO INCREASE OF AMPERAGE DRAW DURING ODOR TIME. ODOR DID NOT RETUSDR DXTA200601185Rheostat · burnedDURING ENGINE START OF THE NR 2 ENGINE A STRONG ELECTRICAL ODOR WAS SMELLED BY THE CREW AT 38 PERCENT N2. AN ELECTRICAL ARC CLOSE TO LEFT KNEE, WENT TO IDLE CUTOFF ON THE NR 2 ENGINE AND SHUT THE BATTERY SWITCH OFF, LOTS OF SMOKE AND ODOR IN COCKPIT. T/S FOU
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