# Service difficulty reports: N397QS, cancelled Jul 21, 2026

A list on [N397QS, cancelled Jul 21, 2026](https://openairdocs.org/deregistered/N397QS-2026-07-21.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR 2026FA0000015](https://openairdocs.org/sdr/2026FA0000015.md): Spar Cap · corroded · Jan 9, 2026 · N397QS · Cessna 680SOV · Horizontal Stabilizer, Spar/Rib
  > CORROSION, RH HORIZONTAL STABILIZER, AFT SPAR UPPER CAP AND LOWER SKIN, APPROX. HSS 86.00 AND HSS 156.80
- [SDR DXTA2025092305039](https://openairdocs.org/sdr/DXTA2025092305039.md): Door · vibration · Sep 21, 2025 · N397QS · Cessna 680SOV · Air Distribution System
  > MAIN CABIN DOOR ACOUSTIC SEAL GENERATES LOUD, HARMONIC VIBRATION WHEN DOOR IS OPERATED --PARTICULARLY WHEN IT IS BEING OPENED. THE DOOR JETTISONED OUTWARD UNDER CABIN PRESSURE. ALSO ACCOMPANIED BY CABIN VERTICAL SPEED RATES EXCEEDING 3000 FT./MIN. PRESSURI
- [SDR DXTA2025091204907](https://openairdocs.org/sdr/DXTA2025091204907.md): Elec Connector · damaged · Sep 10, 2025 · N397QS · Cessna 680SOV · Light System Wiring
  > DURING PREFLIGHT IT WAS DISCOVERED THAT THE EMERGENCY LIGHTING SYSTEM IS INOPERATIVE. CORRECTIVE ACTION: DURING INITIAL INSPECTION AND OPERATION OF THE EMERGENCY LIGHT SYSTEM THE ONLY EMERGENCY LIGHT! INOP FOUND WAS THE CABIN DOORSTEP LIGHT (EXTERIOR AT MAIN E
- [SDR 3J7R2025061400001](https://openairdocs.org/sdr/3J7R2025061400001.md): Light · dim · Jun 14, 2025 · N397QS · Cessna 680CE · Emergency Lighting
  > EXTERIOR EMERGENCY EXIT LIGHT NEAR MAIN CABIN DOOR VERY DIM. ALSO DIM WHEN BEING USED AS PAX SAFETY LIGHT.
- [SDR 2024FA0000690](https://openairdocs.org/sdr/2024FA0000690.md): Skin · corroded · Sep 5, 2024 · N397QS · Cessna 680CE · Wing, Plate/Skin
  > REMOVED CORROSION ON THE WING SKINS AT THE FOUR AILERON SECTOR BUTTON PLUGS LH AND RH WING LOWER SURFACE, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, PRIMED AND TOPCATED REPAIR AREAS IAW NETJETS REQUEST FOR TECHNICAL SERVICES RTS-1116
- [SDR DXTA2024090500689](https://openairdocs.org/sdr/DXTA2024090500689.md): Skin · corroded · Sep 5, 2024 · N397QS · Cessna 680CE · Horizontal Stabilizer, Plate/Skin
  > REMOVED 2 AREAS OF CORROSION ON TOP SIDE OF LH HORIZONTAL STAB UPPER SKIN, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, PRIMED AND TOPCATED REPAIR AREAS IAW NETJETS REQUEST FOR TECHNICAL SERVICES RFTS-111665 REV. 0.
- [SDR 3J7R2024082600001](https://openairdocs.org/sdr/3J7R2024082600001.md): Light · dim · Aug 25, 2024 · N397QS · Cessna 680SOV · Emergency Lighting
  > CABIN DOOR EMERGENCY EXIT LIGHT DIM
- [SDR DXTA2023111310038](https://openairdocs.org/sdr/DXTA2023111310038.md): Unknown · unknown · Nov 12, 2023 · N397QS · Cessna 680CE · Passenger/Crew Doors
  > SPADE DOOR SEPARATED FROM ATTACH RODS PASSING 2,500 FEET ON DEPARTURE. MAINTAINED 140KTS TO REDUCE VIBRATIONS ON THE RETURN. REMOVED AND REPLACE PUSHROD. ACCOMPLISHED THE SPADE DOOR REPAIRS AND SYSTEM CHECKS. NO DEFECTS FOUND. IAW CE680 52-10-60, 52-10-40,
- [SDR JGVR20230913002](https://openairdocs.org/sdr/JGVR20230913002.md): Unknown · unknown · Sep 13, 2023 · N397QS · Cessna 680CE · Wing, Plate/Skin
  > REPAIRED CORRODED AREAS OF THE UPPER INBOARD SKINS OF THE LH & RH WINGS ALONG AND UNDERNEATH THE DRAG ANGLES (WING-TO-FUSELAGE FAIRING ATTACH ANGLES) BY R&R THE DRAG ANGLES, BLENDING CORRODED AREAS, PERFORMING NDT AND REPORTING RESULTS FOR REPAIR DISPOSITION.
- [SDR JGVR20230913001](https://openairdocs.org/sdr/JGVR20230913001.md): Unknown · unknown · Sep 13, 2023 · N397QS · Cessna 680CE · Vertical Stabilizer
  > REPAIRED CORRODED AREAS OF THE VERTICAL STABILIZER AFT SPAR CAPS BY MECHANICALLY BLENDING PERFORMING NDT AND REPORTING FOR REPAIR DISPOSITION. CLEANED TREATED AND PRIMED AREAS FOUND ACCEPTABLE AND TRIMMED THE LH SKIN BOND ASSEMBLY, FABRICATED AND INSTALLING RE
- [SDR JGVR20230714004](https://openairdocs.org/sdr/JGVR20230714004.md): Unknown · unknown · Jul 14, 2023 · N397QS · Cessna 680CE · Wing, Plate/Skin
  > BLENDED SEVERAL CORRODED AREAS ON LH AND RH WING UPPER SKINS AT THE AT THE AILERON BELLCRANK ACCESS BUTTON PLUGS, PERFORMED NDT AND REPORTED RESULTS FOR REPAIR DISPOSITION. TREATED, PRIMED, AND TOP COATED REPAIR AREAS PER TEXTRON REPAIR MEMO.
- [SDR JGVR20230714003](https://openairdocs.org/sdr/JGVR20230714003.md): Unknown · unknown · Jul 14, 2023 · N397QS · Cessna 680CE · Vertical Stabilizer
  > BLENDED SEVERAL CORRODED AREAS ON THE RH SIDE OF THE VERTICAL STABILIZER JUST UNDER THE TIP CAP, PERFORMED NDT AND REPORTED RESULTS FOR REPAIR DISPOSITION. TREATED, PRIMED, AND TOP COATED REPAIR AREAS PER TEXTRON FIELD REPAIR.
- [SDR JGVR20230714002](https://openairdocs.org/sdr/JGVR20230714002.md): Unknown · unknown · Jul 14, 2023 · N397QS · Cessna 680CE · Horizontal Stabilizer, Plate/Skin
  > BLENDED SEVERAL CORRODED AREAS ON THE LOWER SKIN TRAILING EDGE OF THE RH HORIZONTAL STABILIZER, PERFORMED NDT AND REPORTED RESULTS FOR REPAIR DISPOSITION. TREATED, PRIMED, AND TOP COATED REPAIR AREAS PER TEXTRON REPAIR MEMO.
- [SDR JGVR20230714001](https://openairdocs.org/sdr/JGVR20230714001.md): Unknown · unknown · Jul 14, 2023 · N397QS · Cessna 680CE · Empennage Structure
  > BLENDED CORRODED AREAS LOCATED ON THE UPPER AND LOWER SKINS OF THE LH & RH HORIZONTAL STABILIZERS LOCATED NEAR THE HORIZONTAL STABILIZER “PIE FAIRINGS” (ACCESS PANELS 351AC AND 352AC), PERFORMED NDT AND REPORTED RESULTS FOR REPAIR DISPOSITION. TREATED, PRIMED,
- [SDR 2023FA0000100](https://openairdocs.org/sdr/2023FA0000100.md): Spar · corroded · Feb 18, 2023 · N397QS · Cessna 680CE · Wing Spar
  > CORROSION - EXFOLIATION FOUND ON THE WING AFT SPAR IN THE LH AND RH MLG WHEEL WELLS
- [SDR DXTA2022101972380](https://openairdocs.org/sdr/DXTA2022101972380.md): Fuse · failed · Oct 18, 2022 · N397QS · Cessna 680CE · Emergency Lighting
  > CABIN EMERG LIGHT: FOLLOWING POWER ON CHECLIST, STEP 5 EMER LTS - ARM, NONE OF THE EMERGENCY LIGHTS COME ON. THEY DO TURN ON WITH SWITCH IN ON POSSITION (YES, MAIN BATTERIES ARE OFF DURING TEST). THIS IS POSSIBLE INDICATION A RELAY IS STUCK OR BURNED OUT BA
- [SDR DXTA2022092170810](https://openairdocs.org/sdr/DXTA2022092170810.md): None · none · Sep 20, 2022 · N397QS · Cessna 120 · Emergency Lighting
  > CABIN EMERG LIGHT: EMERGENCY LIGHTS DO NOT COME ON WITH THE PAX SAFETY ON OR WITH THE EMERGENCY LIGHTS IN ARM POSITION WITH NO DC POWER APPLIED. WITH THE EMERGENCY LIGHTS IN THE ON POSITION, ALL EMERGENCY LIGHTS ILLUMINATE EXCEPT FOR THE GALLEY READING LIGHT A
- [SDR DXTA2022091370340](https://openairdocs.org/sdr/DXTA2022091370340.md): None · none · Sep 13, 2022 · N397QS · Cessna 120 · Emergency Lighting
  > EMERGENCY LIGHTING: WHEN BATTERY SWITCHES ARE OFF AND EMER LIGHT SWITCH IS ON, THE GALLEY LIGHT, THE LIGHT BETWEEN SEATS 1 AND 3, LIGHT BETWEEN SESTS 5 AND 7, AISLE LIGHTS, LEFT EGRESS LIGHT AND MAIN CABIN DOOR EXIT SIGN ARE ALL INOP. THEN: WHEN BATTERIES ARE
- [SDR DXTA2022050961500](https://openairdocs.org/sdr/DXTA2022050961500.md): Wire · damaged · May 8, 2022 · N397QS · Cessna 680CE · DC Generating System
  > DC EMER BUS R AMBER CAS: IN FLIGHT DC EMER BUS R DC GEN OFF R DU 4 OFF DU 3 RED X'S FMS 2 INITIALLY TRIED TO USE DC GEN OFF R QRH THE BUS TIE WOULD NOT CLOSE. CHECKED RH ENGINE GENERATOR WIRES AND FOUND HIGH RESISTANCE GROUND COMING FROM ONE OF THE WIRES ON
- [SDR DXTA2021051041760](https://openairdocs.org/sdr/DXTA2021051041760.md): Control Valve · defective · May 7, 2021 · N397QS · Cessna 680CE · Cabin Temperature Control System
  > COCKPIT ODOR: DESCENDING THROUGH 5000 FEET WITH THE APU OFF, WE STARTED TO FEEL LIKE BURNED OIL ODOR IN THE COCKPIT, NO SMOKE ASSOCIATED WITH IT. SIGNOFF. INSPECTED SYSTEM AND FOUND TEMP CONTROLLER VALVE VT009 STICKING. FOUND WATER SERPERATOR CONDENSER SOCK
- [SDR DXTA2021011904622](https://openairdocs.org/sdr/DXTA2021011904622.md): Spring · defective · Jan 19, 2021 · N397QS · Cessna 680A · Passenger/Crew Doors
  > TECH HEARD NOISE WHEN HE OPENED MED, NOTICED COUNTER BALANCE CABLE LOOSE. REMOVED AND REPLACED MED AFT COUNTERBALANCE SPRING P/N: S3194-6, IAW CE680 AMM, 52-10-20. NO DEFECTS NOTED.
- [SDR JGVR20200819001](https://openairdocs.org/sdr/JGVR20200819001.md): Spar · corroded · Aug 7, 2020 · N397QS · Cessna 680A · Vertical Stabilizer, Spar/Rib
  > BLENDED AREA OF CORROSION ON RT SIDE OF VERTICAL STABILIZER AFT SPAR AT VFS 118.79. PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED AND TREATED BLENDED AREA THEN PRIMED, APPLIED TOP COAT, AND CORROSION INHIBITING COMPOUND PER TEXTRON FIELD REPAIR.
- [SDR DXTA2020030203531](https://openairdocs.org/sdr/DXTA2020030203531.md): Squat Switch · defective · Mar 2, 2020 · N397QS · Cessna 680CE · Landing Gear Position and Warning
  > LANDING GEAR HANDLE STUCK - REPEAT WRITE-UP: GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION AFTER TAKEOFF. GEAR REMAINED DOWN AND LOCKED (3 GREEN) WOW MISCOMPARE AMBER CAS ILLUMINATED. ///SIGN-OFF///REMOVED DEFECTIVE NLG SQUAT SWITCH ASSY PN: 6948001-2 AND
- [SDR JGVR20200150001](https://openairdocs.org/sdr/JGVR20200150001.md): Spar · corroded · Jan 15, 2020 · N397QS · Cessna 680CE · Vertical Stabilizer, Spar/Rib
  > 6 SPOTS OF CORROSION ON THE VERTICAL STAB AFT SPAR.
- [SDR 2019F00148](https://openairdocs.org/sdr/2019F00148.md): Doubler · chafed · Mar 11, 2019 · N397QS · Cessna 680CE · Fuselage Main, Plate/Skin
  > GOUGES, AFT CABIN ESCAPE HATCH SURROUND, 6911166-2, DOUBLER AND 6911121-5 UPPER FRAME SEGMENT, MULTIPLE LOCATIONS. ACCOMPLISHED FIELD REPAIR FR-680-0144-5312, REV-, FAA FORM 8100-9 DATED 3/8/2019; FIELD REPAIR- GOUGES, AFT CABIN ESCAPE HATCH SURROUND, 6911166
- [SDR 2019F00143](https://openairdocs.org/sdr/2019F00143.md): Spar Cap · corroded · Mar 7, 2019 · N397QS · Cessna 680CE · Wing Spar
  > CORROSION, RT WING, SPAR CAP AND WEB, BETWEEN WS 37 AND WS 52. ACCOMPLISHED ENGINEERING FIELD REPAIR FR-680-0144-5291 REV- FAA FORM 8100-9 DATED 3/01/2019; FIELD REPAIR - CORROSION, RT WING, SPAR CAP AND WEB, BETWEEN WS 37 AND WS 52.
- [SDR 2019F00142](https://openairdocs.org/sdr/2019F00142.md): Gusset · chafed · Mar 7, 2019 · N397QS · Cessna 680CE · Fuselage Miscellaneous Structure
  > LEFT AND RIGHT GUSSETS ABOVE COCKPIT SIDE WINDOW DAMAGE (CHAFE MARKS). ACCOMPLISHED LETTER DQ18665M1 DATED MARCH 6, 2019; 680-0144 LEFT AND RIGHT GUSSETS ABOVE COCKPIT SIDE WINDOW DAMAGE (CHAFE MARKS).
- [SDR 2019F00136](https://openairdocs.org/sdr/2019F00136.md): Truss Fitting · corroded · Feb 28, 2019 · N397QS · Cessna 680CE · Airborne Auxiliary Power Unit (APU) System
  > APU TRUSS MOUNT (FLANGE) CORROSION. ACCOMPLISHED ENGINEERING LETTER DQ18604M1 DATED FEB. 26, 2019; 680-0144 (N397QS) APU TRUSS MOUNT (FLANGE) CORROSION.
- [SDR DXTA2018100801515](https://openairdocs.org/sdr/DXTA2018100801515.md): Squat Switch · out of rig · Oct 7, 2018 · N397QS · Cessna 680SOV · Landing Gear Position and Warning
  > ALL LANDING GEAR RETRACTION DID NOT RETRACT - AFTER LIFTOFF GEAR HANDLE MOVED TO RETRACT POSITION. GEAR DID NOT RETRACT. INDICATORS HAD 3 GREEN AND ONE RED UNLOCK LIGHT ILLUMINATED AT SAME TIME. AMBER WOW MISCOMPARE CAS ILLUMINATED. SUPPLEMENTAL INFORMATION:
- [SDR 2018FA0000389](https://openairdocs.org/sdr/2018FA0000389.md): Channel · corroded · Sep 26, 2018 · N397QS · Cessna 680CE · Fuselage Miscellaneous Structure
  > REPAIRED CORRODED AREA ON THE NOSE WHEEL WELL FORWARD CHANNEL P/N 6731051-57 LOWER FLANGE, JUST FORWARD OF THE NLG UPLOCK, BY BLENDING, PERFORMING EDDY CURRENT AND ULTRASONIC THICKNESS INSPECTIONS, CLEANING, TREATING, AND PRIMING PER REPAIR MEMO.
- [SDR 2018F00126](https://openairdocs.org/sdr/2018F00126.md): Angle · corroded · Sep 26, 2018 · N397QS · Cessna 680CE · Wing Spar
  > FOUND THE LT WING AFT SPAR LOWER CAP FORWARD ANGLE CORRODED AT WS 30.36 AND WS 41.54, AND CENTER SPAR WEB CORRODED JUST IB OF THE TRUNNION SUPPORT AT WS 56.36. REPAIRED THE LT WING REAR SPAR LOWER CAP FORWARD ANGLE AT WS 30.36 (SITE L134), AND WS 41.54 (SITE L
- [SDR JGVR20180621003](https://openairdocs.org/sdr/JGVR20180621003.md): Skin · corroded · Jun 21, 2018 · N397QS · Cessna 680CE · Wing, Plate/Skin
  > CORROSION FOUND ON THE OUTBOARD EDGE AND UNDERNEATH THE RT WING UPPER AFT DRAG ANGLE, WING TO FUSELAGE FAIRING. BLENDED THE CORROSION, PERFORMED AN EDDY CURRENT AND ULTRASONIC INSPECTIONS AND SUBMITTED FOR DISPOSITION. REPLACED THE BLENDED FASTENERS AS REQUIR
- [SDR JGVR20180621002](https://openairdocs.org/sdr/JGVR20180621002.md): Skin · corroded · Jun 21, 2018 · N397QS · Cessna 680CE · Fuselage Main, Plate/Skin
  > REMOVED AIRCRAFT DATA TAG AND MECHANICALLY BLENDED CORROSION ON AIRCRAFT SKIN. PERFORMED EDDY CURRENT AND ULTRASONIC INSPECTIONS AND REPORTED RESULTS TO ENGINEERING FOR DISPOSITION. REPAIRED CORROSION BLENDS FOUND UNDERNEATH IAW MEMO BY TREATING AND PRIMING TH
- [SDR JGVR20180621001](https://openairdocs.org/sdr/JGVR20180621001.md): Skin · corroded · Jun 21, 2018 · N397QS · Cessna 680CE · Fuselage Main, Plate/Skin
  > REMOVED AIRCRAFT DATA TAG AND MECHANICALLY BLENDED CORROSION ON AIRCRAFT SKIN. PERFORMED EDDY CURRENT AND ULTRASONIC INSPECTIONS AND REPORTED RESULTS TO ENGINEERING FOR DISPOSITION. REPAIRED CORROSION BLENDS FOUND UNDERNEATH IAWMEMO BY TREATING AND PRIMING THE
- [SDR DXTA2014070705812](https://openairdocs.org/sdr/DXTA2014070705812.md): Brake Assy · dirty · Jul 6, 2014 · N397QS · Cessna 680CE · Landing Gear Brake System
  > AFTER A LANDING CYCLE, BRAKES SHUDDER & GRAB WHEN STOPPING ACFT. THIS OCCURS UNDER 3 KTS TO PARK. ACCOMPLISHED BRAKE BLEEDING PROCEDURE IAW MM 32-42-10. CLEANED ALL BRAKE ASSEMBLIES, PERFORMED HIGH SPEED TAXI WITH SEVERAL STOPS. NO DEFECTS NOTED AT THIS TIM
- [SDR DXTA2014012805627](https://openairdocs.org/sdr/DXTA2014012805627.md): Warning System · activated · Jan 27, 2014 · N397QS · Cessna 680CE · Landing Gear Position and Warning
  > AFTER TAKEOFF NOSE GEAR RED LIGHT REMAINED ILLUMINATED.
- [SDR DXTA2013080505468](https://openairdocs.org/sdr/DXTA2013080505468.md): Acm · failed · Aug 4, 2013 · N397QS · Cessna 680CE · Cabin Cooling System
  > WITH ENGINES AND APU RUNNING, AFTER START UP COULD NOT GET TEMPERATURE UNDER CONTROL. WENT TO MANUAL AND STILL COULDN'T CONTROL IT. HAD A STRONG BURNING ELECTRICAL ODOR AND SMOKE THROUGHOUT CABIN AND IN HELL HOLE. R & R THE ACM IAW MM 4-04. ACM OPS & LEAK
- [SDR DXTA2013080105462](https://openairdocs.org/sdr/DXTA2013080105462.md): Landing Gear · malfunctioned · Jul 31, 2013 · N397QS · Cessna 680CE · Landing Gear Retraction/Extension System
  > AFTER TAKEOFF, THE GEAR HANDLE WOULD NOT COME UP.
- [SDR CWQR20130528034](https://openairdocs.org/sdr/CWQR20130528034.md): Tube · cracked · May 28, 2013 · N397QS · Cessna 680CE · APU Cowling/Containment
  > DURING A SCHEDULED INSPECTION, FOUND THIS TUBE ASSEMBLY, CRACKED 50 PERCENT AROUND THE FIREWALL BULKHEAD ATTACH FLANGE. CRACK WAS FOUND RIGHT ON THE EDGE OF THE WELD BEAD. THIS WAS REPLACED WITH A NEW TUBE. AN SCR HAS BEEN SUBMITTED UNDER SCR REPORT 659412.
- [SDR DXTA2012101505145](https://openairdocs.org/sdr/DXTA2012101505145.md): Coalescer Bag · odor · Oct 14, 2012 · N397QS · Cessna 680CE · Humidity Control System
  > AFTER TAKEOFF, AT ALTITTUDE OF 20,000 MSL BOTH PILOTS OBSERVED SMOKE & FUMES IN THE ACFT. BOTH BLEEDS WERE TURNED OFF AND SMOKE SUBSIDED, AFTER LANDING ACFT TOWED, AIRCRAFT ENGINE RUN UP WITH LEFT BLEED OFF ALLOWED AIRCRAFT TO FILL UP WITH SMOKE/ FUMES AGAIN
- [SDR DXTA2011080204682](https://openairdocs.org/sdr/DXTA2011080204682.md): Wheel · worn · Aug 1, 2011 · N397QS · Cessna 680CE · Wheel/Ski/Float
  > ABNORMAL GEAR RETRACTION, GEAR UNSAFE LIGHT REMAINED ON FOR APPROX 7-10 SECONDS AFTER ALL GEAR INDICATED UP. HEARD NOSE WHEEL SPINNING ABNORMALLY LONG IN NOSE COMPARTMENT. GEAR EXTENDED NORMALLY, NOSE WHEEL MADE ABNORMAL NOISE UPON ROLLOUT. FOUND LOWER TORQ
- [SDR 2011FA0000134](https://openairdocs.org/sdr/2011FA0000134.md): Connector · damaged · Feb 9, 2011 · N397QS · Cessna 680CE · Fuel System Wiring
  > DURING FUEL TANK INSPECTIONS, FINDING ELECTRICAL BLANKING PINS IN WING ROOT OF FUEL TANKS. PINS FALLING OUT OF PLUGS PREVIOUSLY INSTALLED DURING ACFT MFG.
- [SDR DXTA2009062503702](https://openairdocs.org/sdr/DXTA2009062503702.md): Strut · discharged · Jun 25, 2009 · N397QS · Cessna 680CE · Nose/Tail Landing Gear Strut/Axle
  > DURING GEAR RETRACTION, NUMEROUS LOUD BANGING NOISES WERE HEARD FROM THE NOSE GEAR. SOUND AND BUMPS FELT IN THE FLOOR CONTINUED FOR 5 -10 SEC UNTIL THE NOSE GEAR COMPLETELY RETRACTED. THE "UNLOCK" LIGHT STAYED ILLUMINATED CONTINUOULY DURING THE MALFUNCTION AN

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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 = 'N397QS' AND deregistration_id = 'N397QS-2026-07-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N397QS-2026-07-21/reports

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