# Service difficulty reports: N359QS

A list on [N359QS](https://openairdocs.org/aircraft/N359QS.md).

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

- [SDR DXTA2026061808489](https://openairdocs.org/sdr/DXTA2026061808489.md): G Switch · tripped · Jun 17, 2026 · N359QS · Cessna 680SOV · Emergency Lighting
  > ON POST FLIGHT DISCOVERED THE AFT OVER WING EMERGENCY LIGHT, THE BULK HEAD EXIT SIGN, EXIT SIGN, AND LIGHT OVER LAV REMAIN ON WITH THE EMER SWITCH OFF. RESET EMERGENCY LIGHTING INERTIA SWITCH NR 4. PERFORMED MULTIPLE SATISFACTORY OPS CHECKS WITH NO DEFECTS N
- [SDR DXTA2026042707766](https://openairdocs.org/sdr/DXTA2026042707766.md): Battery Pack · defective · Apr 24, 2026 · N359QS · Cessna 680SOV · Emergency Lighting
  > WHILE TESTING THE EMERGENCY LIGHTS DURING PRE-FLIGHT, SEVERAL INTERIOR OVERHEAD LIGHTS AND 3 EXTERIOR LIGHTS FAILED TO ILLUMINATE WITH THE EMERGENCY SWITCH IN ARM. REPEAT WRITE-UP. GAINED ACCESS TO ALL 4 EMEGENCY BATTERIES REMOVED DEFECTIVED ONES AND INSTALL
- [SDR DXTA2026042407749](https://openairdocs.org/sdr/DXTA2026042407749.md): Battery Pack · no test · Apr 23, 2026 · N359QS · Cessna 680SOV · Emergency Lighting
  > DURING THE EMERGENCY LIGHT PRE-FLIGHT, SEVERAL INTERIOR OVERHEAD LIGHTS AND EXTERIOR LIGHTS FAILED TO ILLUMINATE. PERFORMED EMERGENCY LIGHTING POWER SUPPLY BATTERY EXERCISE PROCEDUREA CHARGED EMERGENCY BATTERY'S AS REQUEST IN TC FOR 60 MINS LONG, WITH EMERGE
- [SDR DXTA2025111005606](https://openairdocs.org/sdr/DXTA2025111005606.md): Door Seal · worn · Nov 6, 2025 · N359QS · Cessna 680SOV · Passenger/Crew Doors
  > DOOR SEAL HAS AN AUDIBLE FREQUENCY THAT PRESENTS ON CLIMB STARTING AT FL200 THROUGH FL320 WITH PRESSURE DIFFERENTIALS OF 7.5-9.2 RESPECTIVELY. AIRSPEED IN CLIMB WAS 240 KIAS AND.68M. ABOVE FL320 WITH HIGHER TAS AND P DIF, THE NOISE STOPS. GAINED ACCESS TO AND
- [SDR JGVR20251024001](https://openairdocs.org/sdr/JGVR20251024001.md): Hinge · corroded · Oct 24, 2025 · N359QS · Cessna 680CE · Rudder Structure
  > FOUND UPPER HINGE UPPER HALF AND CENTER HINGE LOWER HALF ON THE RUDDER CORRODED BEYOND REPAIR. REPLACED PARTS WITH NEW TEXTRON P/N 6931050-46 AND 6931050-52.
- [SDR JGVR20251022002](https://openairdocs.org/sdr/JGVR20251022002.md): Hinge Bracket · corroded · Oct 22, 2025 · N359QS · Cessna 680CE · Rudder Structure
  > REMOVED CORRODE AREAS ON THE LOWER RUDDER HINGE BRACKET AND RUDDER TRIM BRACKET, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED BLENDED AREAS IAW NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.
- [SDR JGVR20251022001](https://openairdocs.org/sdr/JGVR20251022001.md): Skin · corroded · Oct 22, 2025 · N359QS · Cessna 680CE · Fuselage Main, Plate/Skin
  > REMOVED 10 AREAS OF CORROSION LOCATED ON EMERGENCY EXIT DOOR AROUND CONTOUR RINGS ON OUTER E-EXIT SKIN, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED BLENDED AREAS IAW NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.
- [SDR DXTA2025012702087](https://openairdocs.org/sdr/DXTA2025012702087.md): Fuse · inoperative · Jan 23, 2025 · N359QS · Cessna 680SOV · Emergency Lighting
  > EMERGENCY LIGHTS DO NOT WORK IN THE ARM POSITION WITH ALL POWER SHUT DOWN. ALSO, EMERGENCY EXIT LIGHT OVER MAIN CABIN DOOR AND EMERGENCY LIGHT OVER SEAT FOUR DO NOT ILLUMINATE IN THE ON POSITION. ALL OTHER INTERIOR/EXTERIOR EMERGENCY LIGHTS ILLUMINATE IN THE O
- [SDR DXTA2024122401671](https://openairdocs.org/sdr/DXTA2024122401671.md): Fuse · blown · Dec 22, 2024 · N359QS · Cessna 680SOV · Emergency Lighting
  > POST-FLIGHT - DURING AN EXTERIOR LIGHT INSPECTION (APU ON, EMER LTS-ARM, PAX SAFETY-ON) AFTER FLYING FOR 7 HOURS, NONE OF THE THREE OVER/FRONT WING LIGHTS ILLUMINATED. AFTER RETURNING INSIDE THE CABIN, NONE OF THE INTERIOR EMERGENCY LIGHTING WAS ILLUMINATED E
- [SDR 2024F00255](https://openairdocs.org/sdr/2024F00255.md): Spar Splice · cracked · Oct 18, 2024 · N359QS · Cessna 680SOV · Wing Spar
  > CRACK INDICATIONS, CENTER WING, CENTER SPAR SPLICE W.S 37 REF FIELD REPAIR FR680-0126-13812 REV-
- [SDR DXTA2024010810540](https://openairdocs.org/sdr/DXTA2024010810540.md): Battery · faulted · Jan 6, 2024 · N359QS · Cessna 680CE · Emergency Lighting
  > SUSPECT BATTERY PACK 4 FOR CABIN AND OVERWING PAX EMERGENCY LIGHTING CONTROLLING MECH DOES NOT ILLUMINATE LIGHTS OVER SEAT 8 & FWD OVERWING EGRESS LIGHT WITH ONLY EMERGENCY BATTERY PACK PROVIDING POWER TO LIGHTS. INSPECTED, PERFORMED OPS CK IAW MM 33-50-00 E
- [SDR DXTA2023122610435](https://openairdocs.org/sdr/DXTA2023122610435.md): Unknown · unknown · Dec 25, 2023 · N359QS · Cessna 680SOV · Emergency Lighting
  > EMERGENCY LIGHTS FAILED PREFLIGHT INSPECTION TEST. DURING TEST WE ONLY GOT THREE LIGHTS TOTAL THAT CAME ON, THE EXIT LIGHT ABOVE THE MAIN ENTRY DOOR, THE READING LIGHT OVER THE GALLEY, AND THE EXTERIOR LIGHT LEFT-HAND SIDE NEXT TO MAIN ENTRY DOOR. ALL OTHER LI
- [SDR 2023F00318](https://openairdocs.org/sdr/2023F00318.md): Spar Cap · corroded · Oct 29, 2023 · N359QS · Cessna 680SOV · Vertical Stabilizer, Spar/Rib
  > CORROSION FOUND ON AFT RH OUTBOARD VERTICAL SPAR CAP VFS 168.94. ACCOMPLISHED FIELD REPAIR-CORROSION, VERTICAL STABILIZER, RH VERTICAL SPAR CAP IAW TEXTRON AVIATION FIELD REPAIR FR-680-0126-12539 DATED 10/23/2023.
- [SDR 2023FA0000675](https://openairdocs.org/sdr/2023FA0000675.md): Spar Cap · corroded · Oct 24, 2023 · N359QS · Cessna 680SOV · Vertical Stabilizer
  > CORROSION, VERTICAL STABILIZER, RH VERTICAL SPAR CAP, VFS 168.94: REMOVED CORROSION AND ACCOMPLISHED ULTRASONIC THICKNESS CHECK. VERIFIED NO CRACK INDICATIONS. REAPPLIED PROTECTIVE FINISH AND CIC. ALL WORK ACCOMPLISHED IAW TEXTRON AVIATION FIELD REPAIR: FR-68
- [SDR DXTA2023092196050](https://openairdocs.org/sdr/DXTA2023092196050.md): Unknown · unknown · Sep 20, 2023 · N359QS · Cessna 680CE · Emergency Lighting
  > UPON CHECKING AIRCRAFT LIGHTS ON POST FLIGHT INSPECTION, WE FOUND THE AFT CABIN EXIT SIGN LIGHT BURNT OUT. REPAIRED BROKEN WIRE FOR AFT LEFT EXIT SIGN ON LAV BULKHEAD IA W SPM 20-30-25, OPS CHECK GOOD IAW CE680 AMM 33-50-00.
- [SDR DXTA2023092196070](https://openairdocs.org/sdr/DXTA2023092196070.md): Unknown · unknown · Sep 20, 2023 · N359QS · Cessna 680CE · Emergency Lighting
  > UPON CHECKING AIRCRAFT LIGHTS ON POST FLIGHT INSPECTION, WE FOUND THE AFT CABIN EXIT SIGN LIGHT BURNT OUT. PAIRED BROKEN WIRE FOR AFT LEFT EXIT SIGN ON LAV BULKHEAD IA W SPM 20-30-25, OPS CHECK GOOD IAW AMM 33-50-00.
- [SDR DXTA2023062689570](https://openairdocs.org/sdr/DXTA2023062689570.md): Unknown · unknown · Jun 26, 2023 · N359QS · Cessna 680SOV · Engine (Turbine/Turboprop)
  > ON CLIMB OUT THE RT ENG WAS ABOUT 50 DEG HOTTER THAN LT. PASSING FL 380 ENG TEMP SPIKED UP THROUGH AMBER RANGE & TO RED AT 928 DEGREES. PULLED THROTTLE BACK & ENG BACK TO NORMAL TEMP. ON DESCENT, RT ENG STARTED ABOUT 40 DEG HOTTER THAN LT FLUCTUATING 5-15 DEG
- [SDR JGVR20230531004](https://openairdocs.org/sdr/JGVR20230531004.md): Unknown · unknown · May 31, 2023 · N359QS · Cessna 680CE · Vertical Stabilizer
  > MECHANICALLY REMOVED 2 AREAS OF CORROSION LOCATED ON VERTICAL STAB AFT SPAR RUDDER COVE LOCATED JUST ABOVE RUDDER FAIRING PANEL LH SIDE ON SPAR CLIP, PERFORMED NDT AND SUBMITTED FOR REPAIR DISPOSITION. TREATED AND PRIMED BLENDED AREAS IAW TEXTRON FIELD REPAIR
- [SDR JGVR20230531003](https://openairdocs.org/sdr/JGVR20230531003.md): Unknown · unknown · May 31, 2023 · N359QS · Cessna 680CE · Wing Main, Frame Structure
  > MECHANICALLY BLENDED 1 AREA OF CORROSION IN LH GEAR WELL, AFT LOWER SPAR WS 21 TO 23 AND MECHANICALLY BLENDED 1 AREA OF CORROSION IN RH GEAR WELL, AFT LOWER SPAR WS 30 TO 33. NDT VERIFIED CORROSION REMOVAL AND REMAINING THICKNESS. EVALUATED FINDINGS AND SUBMIT
- [SDR JGVR20230531002](https://openairdocs.org/sdr/JGVR20230531002.md): Unknown · unknown · May 31, 2023 · N359QS · Cessna 680CE · Empennage Structure
  > MECHANICALLY BLENDED MULTIPLE AREAS OF CORROSION APX 3 INCHES IN LENGTH LOCATED ON LH HORIZONTAL STAB, AFT SPAR ELEVATOR COVE, APX 12 INCHES INBD OF STAB TIP UPPER SPAR CLIP. MECHANICALLY REMOVED MULTIPLE AREAS OF SURFACE CORROSION APX 12 INCHES IN LENGTH LOCA
- [SDR JGVR20230531001](https://openairdocs.org/sdr/JGVR20230531001.md): Unknown · unknown · May 31, 2023 · N359QS · Cessna 680CE · Empennage Structure
  > REPLACED THE CORRODED RUDDER TORQUE TUBE WITH NEW TEXTRON P/N 6933025-55 ON RUDDER ASSEMBLY P/N 6933000-20 S/N CE0187 PER CESSNA 680 SRM 55-40-09.
- [SDR DXTA2022101071840](https://openairdocs.org/sdr/DXTA2022101071840.md): Switch · tripped · Oct 9, 2022 · N359QS · Cessna 680CE · Emergency Lighting
  > EMERGENCY LIGHTS BATTERY: 5G SWITCH TRIPPED ON ONE OF THE EMERGENCY LIGHT BATTERIES. LIGHT OVER SEAT 8 AS WELL AS THE FORWARD OVER-WING LIGHT AND SHARK LIGHT REMAIN ON WITH EMER LIGHTS SWITCH OFF AND POWER REMOVED FROM THE AIRCRAFT. GAINED ACCESS TO AND RESET
- [SDR DXTA2022081567970](https://openairdocs.org/sdr/DXTA2022081567970.md): Water Separator · odor · Aug 15, 2022 · N359QS · Cessna 680SOV · APU Cowling/Containment
  > APU BLEED AIR: UPON STARTING THE APU AND THE BLEEDS THERE WAS A SMELL OF OIL IN THE AIR//CORRECTIVE ACTION// COMPLETED BORESCOPE INSP OF APU IAW TC-C68-49-1001 AND PROVIDED PHOTOS TO CUSTOMER. NDN. COMPLETED ECS DUT BURN OUT RUN IAW TC-680-21-120905M NDN. R/R
- [SDR DXTA2021112952660](https://openairdocs.org/sdr/DXTA2021112952660.md): None · none · Nov 28, 2021 · N359QS · Cessna 680CE · Passenger/Crew Doors
  > MAIN DOOR HANDLE: THE MAIN DOOR HANDLE IS VERY STIFF AND HARD TO ACTUATE AT THE VERY END OF CLOSING AS WELL AS THE START OF OPENING THE DOOR. // SIGN OFF // REMOVED ENTRY DOOR STEP COVER, REMOVED ACCESS PANEL TO INSPECT LATCHING MECHANISM, V!SUAUY INSPECTED LA
- [SDR 2020F00472](https://openairdocs.org/sdr/2020F00472.md): Skin · corroded · Nov 24, 2020 · N359QS · Cessna 680A · Wing, Plate/Skin
  > CORROSION ON WING SKIN. ACCOMPLISHED TEXTRON AVIATION ENGINEERING LETTER DQ11111 DATED NOV 2020.
- [SDR 2020F00455](https://openairdocs.org/sdr/2020F00455.md): Skin · out of alignment · Nov 23, 2020 · N359QS · Cessna 680A · Wing, Plate/Skin
  > MISALIGNED HOLES COMMON TO THE HEATED LEADING EDGE SKIN AND THE REPLACEMENT DIFFUSERS. ACCOMPLISHED TEXTRON AVIATION LETTER DQ27749 DATED NOV 8, 2020; 680-0126, N359QS, REPAIR RECOMMENDATION.
- [SDR 2020F00454](https://openairdocs.org/sdr/2020F00454.md): Spar Cap · damaged · Nov 23, 2020 · N359QS · Cessna 680A · Vertical Stabilizer, Spar/Rib
  > VERTICAL FIN AFT SPAR CAP (LEFT SIDE) DAMAGE. ACCOMPLISHED TEXTRON AVIATION LETTER DQ27908M1 DATED NOV 19, 2020; 680-0126 (N359QS) VERTICAL FIN AFT SPAR CAP (LEFT SIDE) DAMAGE.
- [SDR 2020F00453](https://openairdocs.org/sdr/2020F00453.md): Door · corroded · Nov 23, 2020 · N359QS · Cessna 680CE · Engine Thrust Reverser
  > CORROSION ON THE RT LOWER THRUST REVERSER LOWER DOOR ASSEMBLY, PART NUMBER 07ND78004-5. ACCOMPLISHED NORDAM FIELD ENGINEERING DISPOSITION DATED 6 NOV 2020 NTRSD-20TP-241. LOWER DOOR CORROSION REMOVAL.
- [SDR 2020F00447](https://openairdocs.org/sdr/2020F00447.md): Door · delaminated · Nov 16, 2020 · N359QS · Cessna 680A · Nacelle/Pylon, Main Frame
  > REPAIR OF RIGHT ENGINE UPPER COWL DOOR DAMAGE. TEXTRON AVIATION ENGINEERING REPAIR LETTER DQ27776M1 DATED NOV 10, 2020.
- [SDR 2020FA0000495](https://openairdocs.org/sdr/2020FA0000495.md): Diffuser · elongated · Nov 11, 2020 · N359QS · Cessna 680SOV · Leading Edge Devices
  > REPAIR TO LEADING EDGE DIFFUSER. TEXTRON AVIATION REPAIR LETTER DQ27749 DATED NOV 8, 2020. 680-0126 N359QS REPAIR RECOMMENDATION.
- [SDR JGVR20190523001](https://openairdocs.org/sdr/JGVR20190523001.md): Doubler · damaged · May 23, 2019 · N359QS · Cessna 680CE · Fuselage Main, Plate/Skin
  > REPAIRED SIX AREAS OF CHAFES /GOUGES IN THE DOUBLER BOND ASSEMBLY OF THE EMERGENCY EXIT OPENING SURROUND P/N 6911166-2 AND FRAME SEGMENT 6911122-3 BETWEEN FS 405.4 AND FS 432 BY REPLACING FRAME SEGMENT 6911122-3 WITH NEW, AND BLENDING, PERFORMING NDT, TREATING
- [SDR DXTA2019031102152](https://openairdocs.org/sdr/DXTA2019031102152.md): Controller · defective · Mar 11, 2019 · N359QS · Cessna 680CE · Cabin Pressure Controller
  > CABIN ALTITUDE AMBER CAS ILLUMINATED - CLIMBING THROUGH FL 180 AMBER CAS CABIN ALTITUDE ILLUMINATED AND CABIN SHOWED 9000 FEET. CABIN ALTITUDE CHECKLIST WAS COMPLETED AND THE MAX CABIN WAS 9500 FEET. PASSENGER MASKS WERE NOT DEPLOYED. DESENDING THROUGH FL 180
- [SDR JGVR20171221001](https://openairdocs.org/sdr/JGVR20171221001.md): Skin · corroded · Dec 21, 2017 · N359QS · Cessna 680CE · Vertical Stabilizer, Plate/Skin
  > REMOVED FIRST LOCK FASTENER COLLAR, JUST ABOVE APU STINGER, ON LT SIDE OF VERTICAL STAB AFT SPAR FACE. MECHANICALLY BLENDED CORROSION APX 3 INCHES ABOVE APU STINGER PANEL 342AB. SUBMITTED FINDINGS TO CESSNA ENGINEERING AND PERFORMED BLEND TREAT REPAIR PER TEXT
- [SDR DXTA2013061005414](https://openairdocs.org/sdr/DXTA2013061005414.md): Warning Light · false activation · Jun 8, 2013 · N359QS · Cessna 680CE · Landing Gear Position and Warning
  > IN CRUISE AT FL 410, OBSERVED AN FMS MESSAGE OF "GEAR SPEED LIM 210". OBSERVED RT MAIN GEAR LIGHT ON. GEAR HAD BEEN VERIFIED UP AFTER TAKE OFF. RIGHT GEAR DOWN INDICATION & NO RED UNLOCKED LIGHT. LAV DOOR OPEN CASS MESSAGES SHORTLY BEFORE WHEN THE LAV WAS
- [SDR CWQR20130321026](https://openairdocs.org/sdr/CWQR20130321026.md): Rib · cracked · Mar 21, 2013 · N359QS · Cessna 680CE · Horizontal Stabilizer, Plate/Skin
  > DURING A SCHEDULED INSPECTION, FOUND THE RT STABILIZER RIB CLOSE-OUT PANEL CRACKED ON THE UPPER ATTACH FLANGE TO SKIN ATTACH AREA, 4.5" LONG.
- [SDR CWQR20130321025](https://openairdocs.org/sdr/CWQR20130321025.md): Rib · cracked · Mar 21, 2013 · N359QS · Cessna 680CE · Horizontal Stabilizer, Spar/Rib
  > DURING A SCHEDULED INSPECTION, WE FOUND THE RT INBD STABALIZER RIB CRACKED ON THE INBD LOWER FLANGE TO SKIN ATTACH AREA IN A ZIZAG PATTERN AND 2.2 INCHES LONG.
- [SDR CWQR20120318022](https://openairdocs.org/sdr/CWQR20120318022.md): Heat Exchanger · cracked · Mar 18, 2013 · N359QS · Cessna 680CE · Pneumatic Distribution System
  > DURING A SCHEDULED INSPECTION, PERFORMED A PRODUCT IMPROVEMENT. REPLACEMENT OF DUCT ASSY 6914070-67. NOTICED THAT THE HEAT EXCHANGER SIDE PLATE HAD TWO CRACKS ABOUT.30 INCHES LONG. OPPOSITE SIDE OF THE HEAT EXCHANGER WAS CRACKED IN NONE OF THE FOUR CORNER
- [SDR CWQR20120318021](https://openairdocs.org/sdr/CWQR20120318021.md): Heat Exchanger · cracked · Mar 18, 2013 · N359QS · Cessna 680CE · Pneumatic Distribution System
  > DURING A SCHEDULED INSPECTION, PERFORMED A PRODUCT IMPROVEMENT (REPLACEMENT OF DUCT ASSY 6914070-67) NOTICED THAT THE HEAT EXCHANGER SIDE PLATE HAD THREE CRACKS ABOUT.30 INCHES LONG. OPPOSITE SIDE OF THE HEAT EXCHANGER WAS CRACKED IN ONE OF THE FOUR CORNERS.
- [SDR DXTA2012021004869](https://openairdocs.org/sdr/DXTA2012021004869.md): Oil System · overserviced · Feb 9, 2012 · N359QS · Cessna 680CE · APU Oil System
  > WITH APU ON, NON-ELECTRICAL SMOKE STARTED TO FILL CABIN. WITH BLEED AIR TURNED ON, SMOKE INCREASED RAPIDLY. OIL FOUND LEAKING FROM APU COMPARTMENT. FOUND DEICE FLUID DRIPPING DOWN THE RUDDER, TRAILING INTO THE APU EXHAUST CONE. ALSO FOUND APU TO BE OVER S
- [SDR DXTA2010102804279](https://openairdocs.org/sdr/DXTA2010102804279.md): Strut · discharged · Oct 27, 2010 · N359QS · Cessna 680CE · Nose/Tail Landing Gear Strut/Axle
  > ON TAKEOFF, UNABLE TO RAISE GEAR. TAKE OFF + 20 SEC, WOW MISCOMPARE MESSAGE ILLUMINATED. THRUST REVERSERS & NOSEWHEEL STEERING WERE AVAILABLE ON LANDING. TROUBLESHOT LANDING GEAR RETRACTION PROBLEM. FOUND NOSE LANDING GEAR LOWER STRUT NITROGEN PRESSURE LOW.
- [SDR CWQR.2010.02](https://openairdocs.org/sdr/CWQR.2010.02.md): Bracket · misinstalled · Jun 15, 2010 · N359QS · Cessna 680CE · Fuselage Main, Attach Fittings
  > DURING MX THE TECH OPENED THE PILOT'S SIDE WINDOW, AFTER UN-LATCHING THE WINDOW IT SWUNG IN AND FELL OFF IT'S HINGE POINTS. UPON FURTHER INVESTIGATION, FOUND THAT THE LOWER HINGE POINT HAD COME LOOSE AT THE HINGE ATTACH BRACKET RIVETS. AND THAT THE UPPER HINGE
- [SDR DXTA200809123274](https://openairdocs.org/sdr/DXTA200809123274.md): Cable · loose · Sep 12, 2008 · N359QS · Cessna 680CE · Elevator Control System
  > ACFT HAS AN AIRFRAME FLUTTER- INCREASE W/SPEED ABOVE 250KTS. SOME INDICATIONS W/ AP AND YD ON OR OFF, NOT NOTICED IN RUDDER OR AILERON FLUTTER APPEARS TO BE IN ELEVATOR. BALANCED LT AND RT ELEVATORS. FOUND ELEVATOR SERVO CABLE TENSIONS LOW. ADJUSTED TENSIO

## 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 = 'N359QS' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N359QS/reports

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