N982QS
Service difficulty reports not matched to an aircraft · 35
They name N982QS, 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 = 'N982QS' 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 = 'N982QS' 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 2017F00197Skin · corrodedFUSELAGE SKIN CORRODED.SDR 2017F00196Skin · corrodedFUSELAGE AND TAILCONE SKIN CORRODED REPAIRED IAW ENGINEERING DQ8835M1, REV A.SDR 2017F00195Skin · corrodedREPAIR OF LT WING SKIN CORROSION IAW ENGINEERING DQ8751M1.SDR DXTA2016061406258Downlock Switch · unserviceableWHEN LANDING GEAR WAS EXTENDED WE GOT 3 GREEN AND 1 RED UNLOCKED LIGHT. AURAL WARNINGS CAME ON WHEN FLAPS FULLY EXTENDED AND WHEN TLA WAS BROUGHT TO IDLE. REMOVED RT MAIN LANDING GEAR DOWN LOCK SWITCH P/N 6-0407-1. INSTALLED AND RIGGED NEW DOWN LOCK SWITCH SDR DXTA2015082706066Indicator · out of limitsAFTER TAKEOFF & DURING CLIMB, CONTROL COLUMN, CAPTAIN'S SIDE, HAD A DEAD SPOT IN PITCH, ALLOWING PLUS OR MINUS 3 INCHES OF COLUMN MOVEMENT, WITH NO CONTROL FEEL OR ELEVATOR MOVEMENT. CONTINUED TO LANDING. FOUND GOOD, NO DEFECTS NOTED IAW IAW MM 27-32-00. PERSDR DXTA2014021205650Skin · corrodedCORROSION FOUND ON LOWER WING SKIN. REPAIRED CORROSION IAW S-750-ATA57 09RD, S-750-ATA 07RD REV A & S-750-0182 15RD.SDR DXTA2013103005551Acm · odorODOR IN COCKPIT & CABIN NOTICED BY CREW AND PASSENGERS. UNABLE TO DETERMINE WHETHER ENVIRONMENTAL OR ELECTRICAL. ODOR SLOWLY DISSIPATED DURING DESCENT. VERIFIED COCKPIT FILLS WITH SMOKE WITH ACM OPERATION. ACCOMPLISHED TROUBLESHOOTING PROCEDURES FOR AN ODOSDR DXTA2013012405260Turbocharger · inoperativeON INITIAL START UP OF APU A STRONG BURNING ODOR WAS OBSERVED FOLLOWED BY A VISABLE MIST IN THE COCKPIT ONLY. THIS OCCURED AS THE ISOLATION VALVE WAS OPENED. PERFORMED APU RUN DUPLICATED DISCREPANCY. NOTED BURNING SMELL FROM COCKPIT WEMAC. RELOCATED ACFT TOSDR DXTA2011082604711Rudder Pedal · bindingWHEN AIRPLANE IS TURNED TO THE LEFT IN FLIGHT THE RUDDER SEEMS TO GET STUCK. PROBLEM HAPPENS WITH AUTOPILOT ENGAGED AND DISENGAGED. DIDN'T MATTER WHAT ALTITUDE/AIRSPEED. HAPPENED MULTIPLE TIMES. CYCLED RUDDER SEVERAL TIMES. OPS CHECKED GOOD. CHECKED PCU BSDR DXTA2011080904695Unknown · odorON THE GROUND WITH JUST THE APU RUNNING, TURNED ON THE BLEED AIR MAX COOL SWITCH AND ISOLATION VALVE TO OPEN AND SMELLED A BURNING RUBBER ODOR. NO SMOKE OBSERVED.SDR DXTA2011032104517Float Valve · fodAT FL390, RECEIVED RT FUEL IMBALANCE. USED CHECKLIST, ABLE TO BALANCE FUEL & RETURNED SWITCHES TO NORMAL. CRUISE, NOTICED FUEL CONTINUED TO UNBALANCE. APPEARED NO FUEL TRANSFERING FROM CENTER TANK TO RT WING. TURNED OFF LT CENTER TO WING PUMP. DECENT, RECEISDR DXTA2011021804470Oil System · failedDURING DESCENT CREW SMELLED SULPHUR ODOR IN ACFT. UPON DEBARKATION OF PASSENGERS, CABIN FILLED WITH SMOKE, STARTING FROM THE REAR OF THE ACFT. ON INSPECTION OF A/C PACKS, IT APPEARS BOTH "ACM OIL RESERVOIRS" WERE BLACK - WHICH AT THE BEGINNING OF THE FLIGHT SDR DXTA2010020503972Coalescer Bag · odorBAD ODOR FROM PAC'S. R & R BOTH RT & LT COALESCER SOCKS.SDR DXTA2009051103644Actuator · malfunctionedRUDDER LIMIT FAIL B AMBER CAS MESSAGE ILLUMINATED ON CLIMBOUT. RUDDER LIMITED TO 32 PERCENT. TROUBLESHOT SYSTEM. REMOVED AND REPLACED RUDDER LIMIT ACTUATOR "B" IAW MM 27-23-00. OPERATIONAL AND RIG CHECK GOOD.SDR DXTA200803012Acm · odorWITH APU ON AN OILY MUSTY ODOR IS PRESENT WITH THE CABIN AND COCKPIT PAC'S COOLING THE AC. REMOVED AND REPLACED AFT ACM IAW MM CHAPTER 21-51-00. OPERATIONAL AND LEAK CHECK GOOD.SDR DXTA200802990Seal · smokeIMMEDIATELY AFTER TAKEOFF SMELLED AND SAW SMOKE IN THE COCKPIT MOVING FROM LT TO RT ACROSS THE PILOT'S SEAT. REMOVED AND REPLACED LT ENGINE IAW 750 MM 71-00-03 & MM 72-00-00. OPS & LEAK CHECKED GOOD. CHANGED ENGINE AND APU, OIL LEAK OF CARBON SEAL CREATING SDR DXTA200802988O-Ring · leakingCKPT PAC NOTICEABLE FUMES DURING TAKEOFF POWER. M2B-LT ENGINE N1A AND N1B SPEED SENSORS LEAKING OIL PAST O-RINGS. INSTALLED NEW O-RINGS AND LEAK CHECK GOOD PER ENG MM 72-00-00.SDR DXTA20082903Apu · overservicedON TAKEOFF, COCKPIT AND CABIN BEGAN FILLING WITH SMOKE. AN IMMEDIATE RETURN FOR LANDING WAS ACCOMPLISHED. FOUND APU OVER SERVICED AND REMOVED EXCESS OIL. INSPECTED ENGINE AND AIRFRAME. INSPECTED BOTH WATER SEPARATOR AND CLEANED. OPERATIONAL AND LEAK CHECKESDR DXTA200802841Acm · leakingSMOKE IN COCKPIT, SMELLED AND SEEN AS A LIGHT MIST, IMMEDIATELY AFTER TAKE OFF. RETURNED (M-2B) T/S AND REMOVED AND REPLACED COCKPIT ACM WITH A NEW UNIT. PERFORMED OPERATIONAL AND LEAK CHECKS. IAW MM 21-51-00. REMOVED AND REPLACED CABIN AND COCKPIT WATERSDR DXTA200702689Bulb · burned outGREEN NOSE GEAR DOWN AND LOCKED LIGHT IS INOP, LANDING GEAR BLOW DOWN BOTTLE AND NOSE GEAR UPLOCK MANUAL RELEASE (D-RING) WAS USED. INSTALLED NEW BULBS IN NOSE DOWNLOCK LIGHT IAW MM 31-10-00. OPS CHECKED GOOD. RESECURED D-RING AND EMERGENCY KNOB AND RESET BUTTSDR DXTA200702383Brake · weakRIGHT BRAKE PEDAL IS VERY SPONGY ON BOTH PILOTS AND COPILOTS SIDE. PEDAL GOES ALMOST TO THE BOTTOM BEFORE SOLID BRAKING OCCURS. BLED BRAKES IAW 750 MM 32-42-00. TAXI CHECK GOOD.SDR DXTA200702333Strut · underservicedCOULD NOT RETRACT GEAR AFTER DEPARTURE. GEAR HANDLE WAS LOCKED IN THE DOWN POSITION AND COULD NOT BE MOVED. JACKED A/C, FOUND NLG STRUT DID NOT EXTEND. SERVICED STRUT AND OLEO IAW MM CH 12-10-38. PERFORMED GEAR SWING IAW MM CH 32-30-00. NO DEFECTS NOTED. DOWSDR DXTA200702111A/C Pack · odorSTRONG BURN SMELL FROM COCKPIT PACK. PAC TURNED OFF. NO DIVERSION. REMOVED & REPLACED COCKPIT ACM IAW CESSNA 750 MM CHPT 21-51-00. OPS & LEAK CHECKS GOOD.SDR DXTA200702102Brake Assy · damagedBRAKES ARE HARD TO PUSH AND MAKE EXCESSIVE NOISE. [SUP 4-19-07] PERFORMED TESTS AS IAW CE750 MM 32-42-00, NO FAULTS WERE FOUND IN EITHER POWER BRAKE FUNCTIONAL OR ANTI-SKID FUNCTIONAL TESTS. REMOVED ALL 4 MLG TIRES AND CLEANED OUT THE ACCUMULATIONS OF BRAKE SDR DXTA200601770Wheel · vibratesNOSE WHEEL SHIMMY DEVELOPED AT LOW SPEED ON TAKE-OFF ROLL. LESS THAN 50 KNOTS. FOUND LT NOSE WHEEL OB BEARING BURNED, IB BEARINGS DIRTY, LT AXLE UNDER TORQUED AND ALL SCISSOR ATTACH NUTS UNDER TORQUED. FOUND STEERING DUALBAND 2 DEGREES (4 DEGREES IS MAX), NLG SDR DXTA200601585Tire · failedDURING TAKEOFF ROLL, AIRCRAFT BEGAN TO SHUTTER ACCELERATING THRU 60 KIAS. TAKEOFF WAS ABORTED AND RETURNED TO NORMAL AS AIRCRAFT SLOWED THRU 60 KIAS. REMOVED AND INSTALLED LT & RT NOSE TIRES AND WHEELS, ALL WORK DONE IAW CESSNA 750 MM CHAPTER 32-41-01. RT WSDR DXTA200601358Pitot System · contaminatedYAW DAMP, MACH TRIM DISENGAGED TWICE ON TAKEOFF ROLL. PITOT HEAT WAS ON FOR 5 MINUTES PRIOR TO SECOND TAKEOFF ROLL. PERFORMED OPS CHECK OF YAW DAMPNER ON FGC A AND B SIDES, FOUND NO DISCRECPENCIES. DOWNLOAD AFCS FAULTS AND MADC FAULTS AND MAILED TO TEAM X PROSDR DXTA200501047Strut · dirtyDURING FLIGHT GEAR RETRACTS HEARD AND FELT BUMP IN THE NIGHT FOUR (4) TIMES DURING FLIGHT. MEASURED EXTENSION OF NOSE STRUT, MEASURED 9.80 INCHES DISASSEMBLED AND CLEANED LOWER BARREL ASSEMBLY. RESEALED AND REASSEMBLED. MEASUREMENT NOW 9.75 INCHES IAW MM. SDR DXTA200500971Acm · failedWHILE DESCENDING OUT OF 410, HEARD A LOUD BANG AND SMELLED SMOKE. THE SMOKE CLEARED, UNABLE TO CONTROL COCKPIT TEMP. SUSPECT COCKPIT ACM BROKEN. ITEM IS UNDER INVESTIGATION.SDR DXTA200500905Actuator · failedRUDDER LIMIT FAIL A EICAS MESSAGE. CONTROL PAGE SHOWS 43 PERCENT RUD LIMIT. REMOVED UPPER RUDDER -A- LINEAR ACTUATOR DUE TO INTERNAL FAILURE. INSTALLED OVERHAULED UNIT. OPERATIONAL CHECK WAS GOOD. WORK WAS DONE IAW CE-750 MM 27-23-00.SDR DXTA200500861Handle · lockedGEAR WOULD NOT RETRACT AFTER T/O HANDLE LOCKED IN DOWN POSITION T/O INDICATORS ON N1 STAYED ON AFTER POWER REDUCTION THEY WERE WHITE. ITEM IS UNDER INVESTIGATION.SDR DXTA200500767Light · smokeAT 41,000 FT WHITE PUFF OF SMOKE APPEARED FROM F/O CHART HOLDER LIGHT. THE LIGHT WAS OFF. THE MAP CB WAS PULLED AND THE SMOKE STOPPED. ITEM DEFERRED PER NJA CARRY OVER PROCEDURE AND MAINTENANCE CONTROLLER COLLARED AND INOP STICKER INSTALLED, CAT 99-9, CAT ASDR DXTA200500633Strut · underservicedAFTER DEPARTURE FROM MIDWAY, GEAR HANDLE WOULD NOT RELEASE FROM THE DOWN POSITION, COULD NOT BE RAISED, AIRCRAFT RETURNED FOR LANDING. JACKED ACFT AND FOUND THE NOSE STRUT NOT EXTENDING PROPERLY. CHECKED SERVICING AND FOUND THAT THE AIR PRESSURE WAS LOW. SESDR DXTA200300199Tire · failedON LANDING AT TXKF BOTH MAIN TIRES BLEW DAMAGING HARDWARE ON STRUT, GEAR DOOR AND FLAP TRACK FAIRINGS. ITEM IS UNDER INVESTIGATION.SDR DXTA200300019Controller · malfunctionedJUST AFTER STARTING A DESCENT FROM FL 410 CABIN RAPIDLY OVERPRESSURIZED . PRESSURE WENT TO BELOW ZERO AND CABIN DPSI WAS RIGHT AT REDLINE. DUE TO RATE AND PRESSURE, CHOSE TO CABIN DUMP. AS A RESULT OXYGEN MASKS DEPLOYED. OPS CHECKED PRESSURISATION SYSTEM O
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