N641QS
Service difficulty reports not matched to an aircraft · 20
They name N641QS, 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 = 'N641QS' 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 = 'N641QS' 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 JGVR20171121001Skin · crackedFOUND A FOUR INCH CRACK IN THE LT LOWER WING SKIN, JUST INBOARD OF WHEEL WELL OPENING. REPAIRED THE SKIN IAW ERO-911328, REV IR.SDR JGVR20171117001Cotter Pin · missingRUDDER TRIM TAB HINGE PIN, RETAINING COTTER PIN WAS MISSING WHICH CAUSED THE HINGE PIN TO MIGRATE AND CHAFE A HOLE INTO LOWER RUDDER RIB BENEATH RUDDER TRIM TAB. REMOVED AND REPLACED THE RIB IAW 51-40-03, 51-40-04, 51-40-06, AND MM 20-32-00.SDR DXTA2017012506366Tire · out of balanceAC EXPERIENCED STRONG VIBRATIONS ON NOSE FLOOR AND RUDDER PEDALS AFTER GEAR RETRACTION. INDICATIONS NORMAL. LOWERED GEAR AND LANDED. VIBRATIONS STOPPED PRIOR TO LOWERING GEAR. FOUND NOSE TIRE/WHEEL UNBALANCED AND NOT TORQUED TO PROPER SPECS. BALANCED NOSE WHEESDR DXTA2016113006335Circuit Breaker · failed3 - 5 MINUTES AFTER TAKEOFF, POWER BRAKE CIRCUIT BREAKER TRIPPED & ANTISKID INOP ANNUNCIATOR ILLUMINATED. CIRCUIT BREAKER WOULD NOT RESET. AFTER 30 MINUTES, CIRCUIT BREAKER RESET. AT LANDING THE BRAKES WORKED, FELT SOFT. BRAKE FLUID LEVELS NORMAL. NO LEAKS NOSDR DXTA2014030305672Actuator · lack of lubeDURING CLIMB OUT, THE ELEVATOR TRIM WOULD NOT TRIM FWD AS NEEDED. AIRPLANE WAS BEING HAND FLOWN AT THE TIME. UPON LEVEL OFF WE TRIED TO TRIM MANUALLY & THE TRIM MOMENTARILY WOULD MOVE IN REVERSE BUT NOTHING FWD OF WHERE IT STOPPED WORKING PREVIOUSLY. ONCE SSDR DXTA2012070505027Motor · burnedAFTER TAKEOFF, CLIMBING THROUGH 10000 FT, COCKPIT RECIRC FAN WAS SWITCHED ON HI. A STRONG ODOR OF BURNING AND MELTED PLASTIC WAS NOTED. FAN WAS TURNED OFF, BUT ODOR CONTINUED AND SEEMED TO GET STRONGER. NO SMOKE WAS NOTED. CO-PILOT NOTED A RATTLING SOUND CSDR DXTA2012060404991Bearing · wornEXCESSIVE VIBRATION IN CONTROL WHEEL COLUMN. MORE PRONOUNCED AT SPEEDS ABOVE 250 IAS. INSPECTED PRIMARY AND SECONDARY FLIGHT CONTROLS FOR SECURITY AND FREE PLAY. FOUND BOTH ELEVATOR TRIM TABS HAD SOME PLAY IN THEM. DISCONNECTED ELEVATOR TRIM TABS FROM PUSH SDR DXTR20120209001Bolt · looseFOUR VERTICAL ATTACH BOLTS ARE LOOSE AT THE VERTICAL STAB AFT SPAR ASSY TO WEB/RIB ASSY FS 588 - WL161.5. RETORQUED TO STANDARD PRACTICES.SDR DXTR20120206001Rib · crackedRT WING T/E RIB CRACKED AT WS 167.07. R & R RT T/E RIB.SDR DXTA2011082404709Bungee · bindingBINDING IN RUDDER PEDALS WHEN TURNING. MORE PROMINENT IN RIGHT HAND TURNS. FEELS LIKE SOMETHING BINDS MOMENTARILY THEN RELEASES. CAN HEAR "POP" AND FEEL IT IN BOTH PEDALS. PERFORMED TAXI CHECK. BINDING SOUND APPEARED TO BE LOUDER ON PILOT SIDE. INSPECTSDR DXTA2009100203805Actuator · inoperativeHYDRAULIC PRESS LIGHT WOULD NOT EXTINGUISH AFTER TAKEOFF. GEAR WAS UP AND FLAPS WERE 0. WHEN FLAPS WERE PUT DOWN, LIGHT WENT OUT. AFTER LANDING, HYDRAULIC LIGHT CAME BACK ON AND REMAINED ON UNTIL SHUTDOWN. REMOVED SEVERAL ACCESS PANELS ON BELLY TO ACCESS CONNSDR 2008FA0000675Control Cable · brokenDURING ROUTINE INSP, FOUND BROKEN STRANDS ON ELEVATOR TRIM CABLE ASSY PN 666000134. DAMAGE FOUND WHERE CABLE PASSES THROUGH A SERIES OF "S" PULLEYS. (K)SDR DXTA200803087Light · unknownWHEN GEAR SELECTED DOWN THE RT SIDE GREEN LIGHT DIDN'T ILLUMINATE. VISUALLY INSPECTED LANDING GEAR SYSTEM. C/W LANDING GEAR FUNCTIONAL CHECK IAW THE CE-560XL MM CH 32-01-00 GEAR SWING & FUNCTIONAL CHECK GOOD. RESET AND SERVICED GARE BLOW DOWN BOTTLE IAW MMSDR DXTA200702323Actuator · inoperativeDURING LANDING GEAR EXTENSION THE RT MAIN GEAR WOULD NOT EXTEND AND THE (HYD PRESS) ANNUNCIATOR ILLUMINATED CONTINUOUSLY. THE LANDING GEAR EXTENDED AFTER COMPLETING THE LANDING GEAR WILL NOT EXTEND CHECKLIST. REMOVED AND REPLACED RT MAIN LANDING GEAR ACTUATORSDR DXTA200601725Unknown · leakingAFTER LANDING WHILE TAXIING TO RAMP, MASTER CAUTION ILLUMINATED ALONG WITH THE LO BRK PRESS/ANTI SKD INOP ANNUNCIATOR ILLUMINATION. AFTER ACFT WAS PARKED/CHOCKED, CREW DISCOVERED BRAKE FLUID POURING DOWN FROM NOSE COMPARTMENT ONTO NOSE GEAR. ACCOMPLISHED SB. SDR DXTA200601719Actuator · warning lightPLACED GEAR HANDLE IN DOWN POSITION GOT GEAR UNLOCKED LT AND NO ILLUMINATION OF RT GEAR BEING DOWN. HYD PRESS LIGHT ILLUMINATED CONTINUOUSLY. RAN CHECKLIST 23, GEAR CAME DOWN WHEN GEAR CONTROL CB RESET. CONT W/CHECKLIST. BLOW DOWN BOTTLE USED. REMOVED AND REPLSDR DXTA200601517Actuator · inoperativeAFTER LANDING GEAR EXTENSION - NOSE GEAR FAILED TO EXTEND. RED UNLOCK LIGHT ON. NO NOSE GEAR GREEN LOCK LIGHT. RECYCLED WITH SAME RESULT. AFTER APPROXIMATELY 30 SEC NOSE GEAR EXTENDED & LOCKED. TROUBLESHOT TO BAD ACTUATOR. REPLACED ACTUATOR IAW CESSNA 56SDR DXTA200601512Control Handle · inoperativeTHE RT LANDING GEAR LIGHT REMAINED ON FOR 15 MINUTES AFTER GEAR RETRACTION . THERE WERE NO OTHER INDICATIONS OF A PROBLEM. ADJUSTED MAIN GEAR DOORS IAW 560XL MM CHAPTER 32-10-00. REMOVED AND REPLACED GEAR CONTROL HANDLE ASSY IAW 560XL MM CHAPTER 32-01-00. ASDR DXTA200500997Indicator · no indicationON LANDING GEAR EXTENSION GREEN L/R MAIN WITH NO NOSE GEAR GREEN AND RED UNLOCK LIGHT. RECYCLED GEAR UP AND THEN DOWN WITH NO GREEN OR RED INDICATION. NO ANOMALIES ON LANDING ROLL OUT. JACKED AIRCRAFT, PERFORMED SEVERAL GEAR RETRACTIONS WITH NO DEFECTS NOTESDR DXTA200500530Warning Light · illuminatedON APPROACH WHEN FLAPS WERE SELECTED TO 15 DEG LOW HYD FLOW LT & RT CAUTION LIGHTS ILLUMINATED. THAT WAS FOLLOWED BY LOW HYD LEVEL AT AROUND THE SAME TIME THE FLAPS REACHED 15 DEG BECAUSE OF THE POTENTIAL FOR HYDRAULIC FLUID LOSS, AND EMERGENCY GEAR EXTENSION
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