N505QS
Service difficulty reports · 20
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. 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 = 'N505QS' AND registry_match = 'registration' 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 = 'N505QS' AND registry_match = 'registration' 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 DXTA2026012106608Battery Pack · faultedEMER LIGHTS DO NOT COME ON IN THE ARM POSITION ON PREFLIGHT. REMOVED NR 1 EMERGENCY LIGHT POWER SUPPLY AND INSTALLED A NEW #1 OUTRIGHT EMERGENCY LIGHT POWER SUPPLY IAW MM 33-50-06. OPS TEST IS GOOD AND NO DEFECTS NOTED.SDR DXTA2025121106072Battery Pack · failedINTERIOR REAR EMERGENCY LIGHT ON LAV BULKHEAD & EXIT LIGHT BELOW LAV SEAT INOP WHEN USING BATTERY PACK. BOTH FUNCTION ON SHIPS MAIN BATTERY POWER. POSITIONED THE ACFT INSIDE HANGAR. APPLIED POWER & ALLOWED ACFT TO BOOT UP & VERIFIED THE WRITE-UP. REMOVED THE SDR DXTA2025120405949Light · inoperativeEMERGENCY FLOOR LIGHT BELOW LAV SEAT INOPERATIVE. REMOVED AND REPLACED LAV SEAT TOEKICK LIGHT ASSEMBLY IAW SPM 20-30-0A PERFORMED OPS CHECK OF THE EMERGENCY LIGHTS YAW IAW AMM 33-50-00, OPS CHECKED GOOD.SDR DXTA2024041711529Battery · no testON PREFLIGHT EMER LIGHTS WERE ARMED AND FAILED TO ILLUMINATE. PER MCC PROCEDURE, THE APU WAS STARTED AND GIVEN 30MIN TO CHARGE. THEN, THE AIRCRAFT POWERED DOWN AND EMER LIGHT FAILED TO ILLUMINATE AGAIN. REMOVED AND REPLACED EMERGENCY BATTERY PACKS 1,2,3 AND 4SDR DXTA2024011110581Battery · faultedLAV OVERHEAD LIGHT. LAV EMER LIGHT UNDER TOILET. LAV FLOOR LIGHT. AND REAR BULKHEAD EXIT SIGN ARE ALL INOP IN ARM MODE. IN ON MODE ALL EMER LIGHTS ARE INOP. TRIED TO CHARGE SYSTEM PER NOTE WITH LIGHT SWITCH IN OFF POSITION FOR 30 MINUTES WITH NO CHANGES. REMOVSDR DXTA2023120710252Unknown · unknownUPON 1ST FLIGHT CHECKS, FOUND MULTIPLE CABIN (+ 1 EXTERIOR) EMERGENCY LIGHTS INOP: EXIT SIGNS: BULKHEAD ABOVE SEAT 7, ABOVE LAV SEAT & BELOW LAV SEAT; PATH LIGHTING: BELOW SEATS 5, 8 & LAV; OVERHEAD SEAT LIGHT: LAV; EXTERIOR OVERWING LIGHT (OVER RIGHT WING). NSDR DXTA2023021580530Wire Harness · defectiveNLG LANDING GEAR RETRACTION: ON APPROACH, AFTER GEAR HAD BEEN EXTENDED FOR A WHILE AND FLAPS HAD BEEN SELECTED TO FULL, WE GOT THE AMBER WOW MISCOMPARE CAS. WE INITIATED A MISSED APPROACH, DURING WHICH WE BROUGHT THE GEAR HANDLE UP, BUT GEAR WOULD NOT RETRACT.SDR DXTA2022120575440Door · unknownMAIN DOOR: CABIN DOOR INTERMITTENTLY CLOSES HALF WAY THEN STOPS AND FALLS OPEN WITH EXTERIOR AMBER CHECK DOOR HANDLE LIGHT ILLUMINATED. TURNING DOOR SWITCH OFF, AMBER LIGHT EXTINGUISHES AND DOOR CLOSES NORMALLY. OPS CHECKED THE DOOR MULTIPLE TIMES AND WE WERSDR 2022FA0000418Skin · gougedR/H INBOARD FLAP HAS A GOUGE ON THE UPPER SURFACE APPROXIMATELY 14" FROM OUTBOARD EDGE AND 1" FROM TRAILING EDGE, MEASURING .5" IN LENGTH AND .03 IN WIDTH, FROM A TOOL FALLING ON THE FLAP. ACCOMPLISHED TEXTRON AVIATION ENGINEERING ORDER, DQ35433M1, DATED: JULYSDR 2022FA0000417Skin · gougedNDI REQUIRED ON FUSELAGE SKIN SCRATCH BEHIND RH FORWARD OVER WING FUSELAGE FAIRING SPLICE STRAP AT FS 354. COMPLIED WITH TEXTRON AVIATION ENGINEERING ORDER, DQ35681M1, FUSELAGE (RIGHT SIDE) DAMAGE (SCRATCH), DATED: JULY 28, 2022.SDR 2022FA0000416Skin · corrodedFOUND CORROSION AT LH HORIZONTAL UPPER SKIN AT TIP CAP. COMPLIED WITH TEXTRON AVIATION ENGINEERING ORDER, DQ35708M1, 680A-0042 (N505QS) HORIZONTAL STABILIZER (LEFT UPPER) SKIN DAMAGE (CORROSION).SDR 2022FA0000398Skin · gougedR/H INBOARD FLAP HAS A GOUGE ON THE UPPER SURFACE APPROXIMATELY 14" FROM OUTBOARD EDGE AND 1" FROM TRAILING EDGE, MEASURING .5" IN LENGTH AND .03 IN WIDTH, FROM A TOOL FALLING ON THE FLAP.SDR DXTA2022052362510Door · bindingMAIN DOOR: UPON ARRIVAL AND WHILE DEPARTING THE AIRCRAFT, THE MAIN CABIN DOOR WOULD NOT SELF-RELEASE WHEN DOOR HANDLE WAS SELECTED TO THE OPEN POSITION. REPEAT WRITE UP. COMPLETED 3 OPERATIONAL CHECKS OF MAIN CABIN DOOR. FOUND TO BE ACCEPATABLE IN OPERATION WSDR DXTA2022052362440Door · intermittentMAIN DOOR: NOTICED THAT WHEN OPENING THE MAIN CABIN DOOR, THE DOOR DOES NOT FREE-FALL OPEN REGULARLY ESPECIALLY FROM THE OUTSIDE. IT WILL POP THE SEAL BUT STAY IN THE SLIGHTLY AJAR POSITION. FOUND DOOR SUPPORT STRUT TO HAVE A STICKY SUBSTANCE ON IT. CLEANED SUSDR DXTA2022050261150Wire · pulledLAV EMERG LIGHT: LAV EMERGENCY LIGHT BELOW TOILET INOP. FOUND THE MOLEX CONNECTOR FOR THE LAV TOE KICK LIGHTING HAD THE WIRES PULLED OUT OF IT. RECONNECTED THE WIRES TO THE MOLEX CONNECTORS AND PERFORMED SATISFACTORY OPS CHECK. WORK PERFORMED IAW CE680A AMM 3SDR DXTA2022012755770Not Reported · not reportedMAIN DOOR: MAIN CABIN DOOR DOES NOT OPEN PROPERLY AND REQUIRES EXCESSIVE FORCE TO OPEN. ONCE LATCH IS RELEASED, DOOR OPENS ABOUT 3 INCHES THEN STOPS AND DOOR HAS TO BE PUSHED OR PULLED TO OPEN FULLY.
CORRECTIVE ACTION:
CONFIRMED DOOR SEAL WAS CAUSING THE SDR 2021F00007Web · crackedREPAIR OF NLG WHEEL WELL WEB AND UPPER MID FRAME CRACKS. TEXTRON AVIATION STANDARD REPAIR SR-680A-ATA53-25890 DATED 6/1/2020, CRACK DAMAGE, NOSE LANDING GEAR WHEEL WELL (NWW) FRAME WEB, AND DOUBLERS FS 75. WITH FAA FORM 8100-9 DATED 6/1/2020.SDR 2021F00009Web · crackedNLG WHEEL WELL WEB AND UPPER MID FRAME CRACKED. TEXTRON AVIATION STANDARD REPAIR SR-680A-ATA53-25890 DATED: 6-1-2020, CRACK DAMAGE, NOSE LANDING GEAR WHEEL WELL (NWW) FRAME WEB, AND DOUBLERS FS 75. WITH FAA FORM 8100-9 DATED: 6-1-2020.SDR 2020F00249Tip Cap · erodedREPAIR RIGHT-HAND HORIZONTAL TIP CAP DAMAGE (EROSION). TEXTRON AVIATION ENGINEERING REPAIR LETTER DQ25536M1 DATED APRIL 22, 2020.SDR DXTA2018041700850Strut · dischargedNLG VIBRATION AFTER RETRACTION, AFTER START AND DURING TAXI NWS OPERATED NORMALLY. TAKEOFF ROLL AND ROTATION ALSO NORMAL. RAISED THE LANDING GEAR AND IMMEDIATELY HAD A VERY PRONOUNCED 2 PER SECOND VERTICAL VIBRATION AND LOUD THUMPING NOISE. IT FELT LIKE THE
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