N983QS
Service difficulty reports not matched to an aircraft · 26
They name N983QS, 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 = 'N983QS' 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 = 'N983QS' 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 DXTA2010041204065Engine · malfunctionedDURING T/O, PASSING THRU 4000 FT, HEARD A THUMP FROM ENGINE 1 AND SAW RED TURB PERCENT AND INDICATIONS OF 102 PERCENT. EXCEED PAGE SHOWS N2 102 PERCENT FOR 2 SECONDS TRIGGERED BY L N2. R & R LT ENGINE "B" BARRIERS. OPS CHECKS SATISFACTORY. WORK WAS ACCOMPLISSDR 2010F00051Engine · oscillatesWITH POWER IN T/O DETENT, FADEC B CONTROLLING BOTH ENGINES, CLIMBING THROUGH 7000 FT THE NR 1, LT ENG POWER BEGAN OSCILLATING. LE N2 WENT TO 102 PERCENT. REDUCED L POWER SLOWLY OUT OF T/O EVENTUALLY TO IDLE. UPON BRINGING L POWER BACK TO CRUISE SETTING, AMBERSDR DXTA2010021803992Engine · surgesCLIMBING THROUGH 15,000 FT, LT N2 STARTED SURGING BETWEEN 93-98. SHORTLY AFTER, AMBER "FAN DAMAGE L" CAS MESSAGE ILLUMINATED. INSPECTED LT ENGINE INLET, FAN AND 1ST STAGE STATORS. NO DEFECTS NOTED. REMOVED BYPASS ACCESS PANELS INNER AND OUTER. REMOVED CVG ASDR DXTA2009081403757Igniter · failedDURING DESCENT TRIED TO START THE APU. GOT THE "APU FAIL" LIGHT AFTER HITTING THE START SWITCH. VISUAL INSP SHOWS SIGN OF A FIRE NEAR THE INTAKE OF THE APU. GAINED ACCESS TO APU EXTERIOR AND ACCOMPLISHED VISUAL INSP OF EXTERIOR COMPONENTS AND ACCESSORIES IASDR DXTA2009020503491Actuator · inoperativeAFTER TAKEOFF AT GEAR RETRACTION THE MAIN GEAR CAME UP BUT THE NOSE GEAR STAYED DOWN AND LOCKED. REMOVED AND REPALCED NOSE GEAR ACTUATOR IAW MM 32-30-03. OPS CHECK LEAK CHECKED SATISFACTORY. SERVICED NOSE GEAR STRUT PER 750 MM CH 12-10-38SDR DXTA2008122903450Actuator · inoperativeEXCESSIVE LT RUDDER TRIM NEEDED TO MAINTAIN COORDINATED STRAIT LEVEL FLIGHT. REMOVED AND REPLACED LINEAR ACTUATOR FOR RUDDER TRIM SYS. COMPLETED FULL RUDDER SYS RIG IAW MM CHAPTER 27-26-00. OPS CHECK GOOD.SDR DXTA2008123003450Unknown · unknownEXCESSIVE LEFT RUDDER TRIM NEEDED TO MAINTAIN COORDINATED STRAIT LEVEL FLIGHT.SDR DXTA2008122503440Strut · dischargedAFTER TAKEOFF THE LANDING GEAR TOOK ABOUT 1 MIN TO FULLY RETRACT. INITIALLY ALL 3 GREEN INDICATORS EXTINGUISHED, BUT THE RED UNLOCK LIGHT REMAINED ILLUMINATED. FOUND NOSE STRUT TO NOT BE FULLY EXTENDING WHEN ACFT WAS OFF THE GROUND. SERVICED NOSE STRUT IAW MSDR DXTA2008122603440Indicator · malfunctionedTHE LANDING GEAR TOOK ABOUT 1 MIN TO FULLY RETRACT. THE RED UNLOCK LIGHT REMAINED ILLUMINATED.SDR DXTA200808173225Lock Pin · missingSEVERE NOSE WHEEL SHIMMY OCCURRED DURING TAKEOFF ROLL AT APPROX 60 KNOTS REQUIRING AN ABORT. WAS ABLE TO CLEAR RUNWAY USING DIFFERENTIAL POWER AND BRAKING, BUT TILLER SPINS 360 DEGREES AS IF IT IS SPINNNG ON THE SHAFT. T/S AND INSPECTED NOSE GEAR AND TIRES NO SDR DXTA200803225Wheel · vibrationSEVERE NOSE WHEEL SHIMMY OCCURRED DURING TAKEOFF ROLL AT APPROX 60 KNOTS REQUIRING AN ABORT. (S)SDR DXTA200803021Coalescer Bag · odorDURING CRUISE, AC HAS A SMELL OF DIRTY SOCKS. REMOVED AND CLEANED AND INSTALLED WATER SOCKS IAW CE750 MM CHAPTER 12-10-01-160. REMOVED CLEANED AND INSTALLED OZONE CONVERTER IAW CE 750 MM CHAPTER 12-10-01-161. OPERATIONAL AND LEAK CHECK GOOD.SDR DXTA200702687Coalescer Bag · dirtyBAD SMELL IN CABIN 7 LARGE ANOUNTS OF MOISTURE COMING FROM WEEMACS AND FLOOR VENTS. REMOVED AND REPLACED BOTH ACM FILTER SOCKS WITH NEW SOCKS, RAN APU OPS AND LEAK CHECK GOOD AT THIS TIME IAW CE-750 MM 21-51.SDR DXTA200702342Coalescer Bag · dirtyTHE CABIN PAC TEMP IS UNCONTROLLABLE AND ALSO PRODUCING AN OILY SMELL IN THE CABIN. INSPECTED ACM, OIL, AND SERVICED, REPLACED COALESCER SOCKS PERFORMED APU AND ENGINE RUNS, NO OIL SMELL PRESENT. PERFORMED OPS CHECK OF CABIN TEMP CONTROLER WITH APU AND ENGINSDR DXTA200701925Indicator · no indicationNOSE WHEEL DOWN GREEN LIGHT DID NOT ILLUMINATED WITH GEAR SELECTED TO DOWN/ EXTENDED POSITION. EMERG CHECK LIST COMPLETED AND GEAR WAS BLOWN DOWN. LIGHT STILL FAILED TO ILLUMINATE NO OTHER NEGATIVE INDICATIONS NOTES. LIGHT TESTED SATISFACTORY W/ ROTARY TEST. SDR DXTA200701901Indication Sys · malfunctionedNOSE WHEEL UNSAFE INDICATION. NOSE LIGHT NOT ILLUMINATED WITH GEAR HANDLE DOWN. COMPLETED EMERGENCY PROCEDURES AND BLEW GEAR DOWN. LIGHT STILL NOT ILLUMINATED. LIGHT ILLUMINATED APPOX 20 MIN AFTER LANDING. TIGHTENED BACKSHELL ON NOSEGEAR ACTUATOR DOWNLOCK SWISDR DXTA200701864Logic Card · inoperativeRUDDER LIMITER FAIL B EICAS MESSAGE RUDDER LIMIT 90%.GAINED ACCESS TO THE RUDDER LIMITER PCB NK124. REMOVED RUDDER LIMITER PCB NK124 AND INSTALLED A NEW RUDDER LIMITER PCB. CONNECTED THE AIR DATA TEST SET AND APPLIED ELECTRICAL POWER. APPLIED HYDRAULICS AND PESDR DXTA200601329Uplock Switch · out of adjustDURING CLIMB OUT PHASE OF FLIGHT, NOSE GEAR APPEARS TO BE MAKING "BUMPING NOISE". ADJUSTED RT MLG UPLOCK SWITCH, WAS .05 OUT OF SPEC. WORK DONE REF CE 750 MM CH 32-30-00. ALSO, FOUND UPLOCK AREA DIRTY AND GUMMED UP. CLEANED AND LUBED UPLOCK COMPONENTS. SESDR DXTA200601238Apu · malfunctionedUPON DESCENT INTO BCT, ATTEMPTED TO START THE APU TWICE. WHILE ATTEMPTING A SECOND START, SMELLED AN ELECTRICAL ODOR COMING FROM THE OVERHEAD GASPER. ABANDONED ALL FURTHER ATTEMPTS TO START APU. PERFORMED OPERATIONAL CHECKS OF THE APU AND INSPECTED APU, NO SDR DXTA200501128Warning Light · illuminatedDURING TAKEOFF AROUND 50 KTS THE FADEC FAULT R A-B CAS MESSAGE CAME ON. TAKEOFF WAS ABORTED. THE FAULT WOULD NOT RESET. ITEM IS UNDER INVESTIGATION.SDR DXTA200500955Actuator · failedAT FL 320 AND .88 MACH THE UPPER RUDDER YD STARTED BOUNCING OFF THE LEFT SIDE OF THE RUDDER LIMITER WITH THE UPPER YD IN THE B-CHANNEL, IT WOULD NOT HAPPEN ON THE A-CHANNEL. AT SPEED & ALTITUDE THE RUDDER HAD TO BE TRIMMED TO THE LEFT EXCESSIVELY. REMOVED UPSDR DXTA200500555Line · leakingUPON LOWERING GEAR HANDLE A/C LOST ALL -A- SYSTEM FLUID. FOLLOWED EMERGENCY CHECKLIST, POST FLIGHT DISCOVERED FLUID IN NOSE WHEEL WELL. ITEM IS UNDER INVESTIGATION.SDR DXTA200400423Actuator · failedUPON GEAR RETRACTION ALL GREEN LIGHTS OUT RED UNLOCK LIGHT ON. RECYCLED GEAR AND GOT THE SAME RESULT. A LOT OF AIR/WIND NOISE FROM NOSE OF PLANE, SOUNDED LIKE NOSE GEAR WAS EXTENDED. REMOVED & REPLACED NOSE GEAR ACTUATOR WITH RENTAL UNIT. SENT LINE NOSE GESDR DXTA200400281Warning Light · illuminatedDURING TAKE-OFF ROLL BELOW 80 KTS, NO TAKE-OFF CAS MESSAGE ILLUMINATED, MACH TRIM OFF, PRIMARY STAB TRIM FAILED, YAW DAMPER FAIL LOWER, YAW DAMPER NOT CENTERED, FGC A FAIL CAS MESSAGES ILLUMINATED. NOSE WHEEL SHIMMY VERY STRONG ALSO, ABORTED TAKE-OFF. PERFOSDR DXTA200300055Acm · seizedAT TEB DURING GROUND OPS OF APU NORMAL APU BLEED SELECTED WITH NORMAL APU EGT TEMPS, ISOLATION VALVE OPEN, PILOTS NOTED GRINDING NOISE. ACM SEIZED CAUSING CABIN TO FILL WITH SMOKE. REMOVED SEIZED FORWARD ACM AND INSTALLED OVERHAULED UNIT, OPS & LEAK CHECK GOSDR DXTA200300001Circuit Board · failedON APPROACH TO GSO, (LT TR AUTOSTOW) AMBER CAS MESSAGE ILLUMINATED AND THROTTLE ROLLED BACK TO IDLE.
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