N814QS
Service difficulty reports not matched to an aircraft · 18
They name N814QS, 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 = 'N814QS' 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 = 'N814QS' 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 DXTA2016072706273Actuator · unserviceableRIGHT MAIN GEAR INDICATOR DID NOT ACTUATE NORMALLY. RIGHT MAIN GEAR DOWN LIGHT WAS NOT ON. LANDING GEAR WILL NOT EXTEND CHECKLIST COMPLETED AND RIGHT MAIN GEAR EXTENDED LIGHT CAME ON. R & R THE RT SIDE BRACE ACTUATOR. OPS CHECKS GOOD, REF MM 32-31-04. R SDR DXTA2016031906205Seal · leakingRT ENG FIRE LIGHT ILLUMINATED IN FLT. DISCHARGED LT FIRE BOTTLE. FIRE LIGHT EXTINGUISHED. NO SIGN OF FIRE ON PREFLIGHT. CRASH & FIRE CREWS REPORTED NO HOT SPOTS. INSP ENG FOR EVIDENCE OF FIRE WITH NO FINDINGS. PERFORMED RESISTANCE CHECK OF RT FIRE DETECTSDR DXTR2015040901Skin · damagedANOMALY FOUND AT BS 205 AND WL 94-96 SKIN JOINT DURING PHASE 49 INSPECTION WHICH APPEARS TO BE A SCRATCH APPROXIMATELY 2" IN LENGTH. COMPLIED WITH MFG ENGINEERING MEMO: M150403DK DATED 04/02/2015 AND COMPLIED WITH ALL OF THE REQUIRED STEPS. THE SEAM WAS FILLESDR DXTA2014032405697Unknown · malfunctionedON LANDING ROLL BELOW 60 KNOTS, PILOTS RT BRAKE PEDAL WENT TO THE FLOOR. RIGHT PILOT GOT THE AIRPLANE SLOWED TO TAXI SPEED, THEN HIS RT PEDAL WAS INTERMITTENTLY SPONGY. AFTER CLEARING THE RUNWAY, TRIED THE BRAKES AGAIN & THE PILOT RIGHT WENT ALMOST TO THE FLSDR DXTA2014013005632Seal · damagedRIGHT ENG FIRE LIGHT ON IN FLIGHT. PERFORMED ENG FIRE LIGHT ON MEMORY ITEMS LIGHT EXTINGUISHED AFTER APPROXIMATELY 3 SECONDS AFTER EFFECTED ENG THROTTLE WAS REDUCED TO IDLE. REMOVED UPPER & LOWER COWLS ON RT ENG FOR FURTHER INSPECTION STARTED INSPECTING RT ESDR DXTA2013100705528Fire Loop · misroutedDURING CLIMB THRU FL230, RT ENGINE FIRE LIGHT AND WARNING BELL CAME ON. RETARDED RT THROTTLE TO IDLE IAW THE CHECKLIST AND BELL AND LIGHT EXTINGUISHED. FOUND LEFT ENGINE FIRE LOOP ROUTED INCORRECTLY. ROUTED FIRE LOOP PER DRAWING 6555660. DWG.0003. OPS CHECKSDR DXTA2013091105498Seal · leakingIN FLIGHT, RT ENGINE FIRE LIGHT AND WARNING BELL ACTIVATED. RETARDED THROTTLE TO IDLE AND BELL AND LIGHT EXTINGUISHED. LANDED WITH ENGINE IN IDLE, NO OTHER ABNORMAL INDICATIONS. PERFORMED HIGH POWER RUN UP AND VERIFIED NO BLEED AIR LEAKS. PERFORMED HIGH POWSDR DXTA2013082605484Seal · leakingAT 25,000 FT, RT ENGINE FIRE BELL AND LIGHT SOUNDED AND ILLUMINTED. PERFORMED ENGINE FIRE CHECK LIST DECLARED EMERGENCY AND LANDED WITHOUT FURTHER EVENT. INSPECTED RT ENGINE FOR SIGNS OF FIRE, NO DAMAGE FOUND. PERFORMED RUN UP AND FOUND FOUR BLEED AIR COUPLISDR DXTA2010110504290Gps · failedRT CIRCUIT BREAKER PANEL "WARN" CIRCUIT BREAKER POPPED IN FLIGHT. FOUND GPS TO BE CAUSE OF PROBLEM. R & R GPS. OPS CHECKED GOOD AT THIS TIME. ALL WORK DONE IAW MM 34-50-05, 53-50-02
.SDR DXTA200810123302Fire Detector · false indicationRT ENG FIRE LIGHT ILLUMINATED IN FLT, DISCHARGED FIRST BOTTLE, LIGHT EXTINGUISHED. LIGHT RE-ILLUMINATED & WOULD NOT EXTINGUISH AFTER SECOND BOTTLE DISCHARGED. ACCOMPLISHED ALL MEMORY ITEMS & PROCEDURES FOR ENG FIRE LIGHT ILLUMINATED. REMOVED RT ENGINE TOPSDR DXTA2008101303302Warning Light · illuminatedRIGHT ENG FIRE LIGHT ILLUMINATED IN FLIGHT DISCHARGED FIRST BOTTLE, LIGHT EXTINGUISHED. LIGHT RE-ILLUMINATED AND WOULD NOT EXTINGUISH AFTER SECOND BOTTLE DISCHARGED.SDR DXTA200809193279Trim System · out of limitsAUTO PILOT KICKS OFF WHEN IN CLIMB OR TURN. ACFT CONTROLS APPEAR TO BE LOADED WHEN AUTOPILOT KICKS OFF. PERFORMED OPS CHECK OF AUTOPILOT DISENGAGEMENT SYS TO ENSURE PROPER OPERATION. ALL CHECK GOOD. PERFORMED AHRS FUNCTIONAL TEST. ALL AHRS OPS CHECK GOOD. GAINSDR DXTA200803279Autopilot Sys · malfunctionedAUTO PILOT KICKS OFF WHEN IN CLIMB OR TURN.SDR DXTA200803069Pressure Switch · inoperativeWHILE TAKING THE RUNWAY FOR DEPARTURE THE LOW BRAKE PRESSURE - ANTI-SKID ANNUNCIATOR LIGHT ILLUMINATED. REMOVED DEFECTIVE PUMP MOTOR PRESSURE SWITCH AND INSTALLED REPAIRED SWITCH. SYSTEM CHECKS GOOD REF MM 32-20-00. TAXI CHECKED GOOD IAW PILOTS HANDBOOK.SDR DXTA20082939Pcb · inoperativeLANDING GEAR DID NOT EXTEND WHEN GEAR HANDLE WAS PUT DOWN. REPLACED PCB NZ014 PER CE560 ENCORE & MM 24-51-01, REPLACED LANDING GEAR CONTROL HANDLE ASSY. PER CE560 ENCORE & MM 32-31-01. FUNCTIONAL CHECKED GOOD PER 560 ENCORE & MM 32-01-00.SDR DXTA20082912Indicator · looseELEVATOR TRIM POSITION INDICATOR INOP. INDICATES INCORRECT TRIM POSITION. FOUND TRIM LOOSE. SHIMMED & RESECURED INDICATOR IAW MM 27-31-00. OPERATIONAL AND TRAVEL CHECK NORMAL.SDR DXTA20082897Anti-Skid Sys · malfunctionedON TAXI OUT LOW BRAKE PRESS AND ANTI-SKID INOP LIGHT ILLUMINATED. NORMAL BRAKING WAS INEFFECTIVE. EMERGENCY BRAKE WAS USED TO STOP THE AC. GAINED ACCESS TO ANTI-SKID CONTROLLER AND FOUND NO FAULTS. EMERGENCY PNEUMATIC BOTTLE IS SERVICED TO TOP OF GREEN ARC. SDR DXTA200802743Warning Light · unknownWHEN THE GEAR WAS CYCLED DOWN NORMALLY (GEAR HANDLE TO DOWN POSITION) THERE WAS NONE OF THE 3 GREEN DOWN INDICATORS. JACKED ACFT, CONNECTED HYDRAULIC MULE. EXTEND & RETRACTED GEAR 13 TIMES. ALL GEAR OPS NORMAL. DISCONNECTED MULE. ALL WORK DONE IAW AMM 32-01
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