# Service difficulty reports: N260JS, cancelled Dec 9, 2025

A list on [N260JS, cancelled Dec 9, 2025](https://openairdocs.org/deregistered/N260JS-2025-12-09.md).

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

Page 1 of 2 · 63 reports

- [SDR VNAA2019111521102](https://openairdocs.org/sdr/VNAA2019111521102.md): Tube · contaminated · Nov 12, 2019 · N260JS · Cndair CL6002B19 · Pitot/Static System
  > DURING TAKEOFF ROLL ON RWY 01, THE CREW INDICATED A FAULTY AIRSPEED INDICATOR BETWEEN 80-100 KIAS. THE CREW THEN REJECTED THE TAKEOFF AND WAS ABLE TO TAXI BACK INTO THE GATE. MX INSPECTED AND DRAINED WATER FROM RH ADC COLLECTOR TUBE. PERFORMED PITOT STATIC CHE
- [SDR VNAA2019110111103](https://openairdocs.org/sdr/VNAA2019110111103.md): Sensor · failed · Nov 1, 2019 · N260JS · Cndair CL6002B19 · Engine EGT/TIT Indicating System
  > WHILE CLIMBING OUT OF CAK, LEFT HAND ENGINE HAD N1 FLUCTUATIONS. THEY DECLARED AN EMERGENCY BUT DID NOT SHUT DOWN THE ENGINE AND LANDED SAFELY BACK IN CAK. THEY WERE ABLE TO TAXI TO GATE WITHOUT ISSUE. MX REPLACED THE INLET TEMP SENSOR. OPS CHECK GOOD.
- [SDR VNAA2019090211102](https://openairdocs.org/sdr/VNAA2019090211102.md): Wire Harness · failed · Sep 2, 2019 · N260JS · Cndair CL6002B19 · Landing Gear System Wiring
  > CREW GOT WOW INPUT CAUTION MSG ON WHEELS-UP OUT OF TYS, THAT WENT AWAY AS SOON AS MLG WAS UP. CREW RAN QRH. DETERMINED NO ISSUE AS LONG AS MSG WENT AWAY. CREW NOTIFIED ATC OF SLIGHT POSSIBILITY OF NO NOSE STEERING ON LANDING IF MSG CAME BACK ON GEAR DOWN. A
- [SDR VNAA2019083081101](https://openairdocs.org/sdr/VNAA2019083081101.md): Warning Message · false activation · Aug 28, 2019 · N260JS · Cndair CL6002B19 · Landing Gear Position and Warning
  > CREW RECEIVED A WEIGHT ON WHEEL MESSAGE. INFORMED AIR TRAFFIC CONTROL THAT THEY WOULD NEED A QUICK TURN OFF THE RUNWAY TO IN CASE THEY LOST THEIR NOSE WHEEL STEERING. AIR TRAFFIC CONTROL DECLARED AN EMERGENCY FOR THE CREW. MX PERFORMED PSEU SYSTEM TEST AND TH
- [SDR VNAA2019081631102](https://openairdocs.org/sdr/VNAA2019081631102.md): Ballast · failed · Aug 13, 2019 · N260JS · Cndair CL6002B19 · Passenger Compartment Lighting
  > REPORTED ELECTRICAL BURNING SMELL COMING FROM ROW 10 IN CABIN. R&R BALLAST IN ROW 10 IAW CRJ 200 AMM 33-21-04-000/400-801. NO SMELL DETECTED AT THIS TIME, OP CHECK GOOD.
- [SDR VNAA2018083111101](https://openairdocs.org/sdr/VNAA2018083111101.md): Unknown · odor · Aug 31, 2018 · N260JS · Cndair CL6002B19 · Air Distribution System
  > CREW REPORTED AN ELECTRIC SMELL IN COCKPIT WHEN SWITCHING POWER FROM APU TO GROUND POWER. MX INSPECTED FLIGHT DECK AND SURROUNDING AREA FOR ELECTRIC SMELL. NO SMELL NOTED. PERFORMED OPS CHECKS OF GROUND POWER AND APU POWER WITH NO DEFECTS NOTED.
- [SDR VNAA2018051599912](https://openairdocs.org/sdr/VNAA2018051599912.md): Intercostal · cracked · May 15, 2018 · N260JS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL BETWEEN FS 621 AND FS 625 AT LBL45 WL 94 IS CRACKED. REMOVED AND REPLACED OBLIQUE ANGLE IAW SRM 51-42-06.
- [SDR VNAA2018051599911](https://openairdocs.org/sdr/VNAA2018051599911.md): Intercostal · cracked · May 15, 2018 · N260JS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL BETWEEN FS 621 AND FS 625 AT RBL45 WL 94 IS CRACKED. REMOVED AND REPLACED OBLIQUE ANGLE IAW SRM 51-42-06.
- [SDR VNAA2018051599910](https://openairdocs.org/sdr/VNAA2018051599910.md): Bulkhead · cracked · May 15, 2018 · N260JS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > REPAIRED FS621 BULKHEAD IAW REO 601R-53-61-1240 REV D DATED 10/31/16. AND INCORPORATED DEVIATION REPAIR IAW REO 601R-53-61-6554 REV-- DATED 5/8/18 AT RBL 27.5 WL76-77, LBL27.5 WL 78-79, AND LBL9.5 WL76-79.
- [SDR VNAA2018051599909](https://openairdocs.org/sdr/VNAA2018051599909.md): Rib · cracked · May 15, 2018 · N260JS · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > RIGHT WING BATT RIB CAP ANGLE AT WS 48.30 IS CRACKED. REMOVED AND REPLACED CAP ANGLE IAW SRM 51-42-21.
- [SDR VNAA2018051599908](https://openairdocs.org/sdr/VNAA2018051599908.md): Rib · cracked · May 15, 2018 · N260JS · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > LEFT WING BATT RIB CAP ANGLE AT WS 48.30 IS CRACKED. REMOVED AND REPLACED CAP ANGLE IAW SRM 51-42-21
- [SDR VNAA2018051599907](https://openairdocs.org/sdr/VNAA2018051599907.md): Angle · cracked · May 15, 2018 · N260JS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CLIP ANGLES AT FS 200 LBL6 AND RBL6 WL79 ARE CRACKED. REMOVED AND REPLACED CLIP ANGLES PN: 600-33101-89 AND CLIP ANGLE PN 600-33101-90 IAW SRM 51-42-06.
- [SDR VNAA2018051599906](https://openairdocs.org/sdr/VNAA2018051599906.md): Crossbeam · cracked · May 15, 2018 · N260JS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 280 CROSSBEAM IS CRACKED JUST O/B OF LBL 9. REPAIRED FS 280 CROSSBEAM IAW REO 601R-53-11-926 REV B DATED 2006/05/10.
- [SDR VNAA2018051599905](https://openairdocs.org/sdr/VNAA2018051599905.md): Door Sill · corroded · May 15, 2018 · N260JS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT FLOOR SILL HAS AREA OF CORROSION AND SOME CHAFING, DAMAGE FROM FLOOR BOARD BETWEEN FS 559+112 TO FS 621. REMOVED AND REPLACED SILL IAW EO CL-600-2B19-53-L05666.
- [SDR VNAA2018051599904](https://openairdocs.org/sdr/VNAA2018051599904.md): Stringer · corroded · May 15, 2018 · N260JS · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STGR 27 IS CORRODED BETWEEN FS 559+112 AND FS 574. REMOVED AND REPLACED ANGLE CLIP IAW SRM 200 51-42-06.
- [SDR VNAA2018051599903](https://openairdocs.org/sdr/VNAA2018051599903.md): Stringer · cracked · May 15, 2018 · N260JS · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > PAX DOOR UPPER SILL (STR 3L) IS CRACKED JUST AFT OF FS 379.00. REPAIRED CRACKED STRINGER IAW REO 601R-53-21-2976. REV-- DATED 2018-04-28.
- [SDR VNAA2018051599902](https://openairdocs.org/sdr/VNAA2018051599902.md): Frame · corroded · May 15, 2018 · N260JS · Cndair CL6002B19 · Fuselage Main, Frame
  > FUSELAGE FRAME FS574 IS CORRODED BETWEEN STGR 25L AND STGR 18R. REMOVED AND REPLACED FRAME SECTOR P/N 601R36024-61 IAW SRM 51-40-11, 51-42-06 AND 51-42-21.
- [SDR VNAA2018051599901](https://openairdocs.org/sdr/VNAA2018051599901.md): Skin · cracked · May 15, 2018 · N260JS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FORWARD FUSELAGE SKIN IS CRACKED AT THE LT TRU DOOR AFT LATCH LOCATION. REMOVED AND REPLACED DOOR LANDING IAW SRM 51-42-06 AND 51-42-13.
- [SDR VNAA2018032311102](https://openairdocs.org/sdr/VNAA2018032311102.md): Windshield · failed · Mar 23, 2018 · N260JS · Cndair CL6002B19 · Flight Compartment Windows
  > WHILE IN CRUISE FLIGHT, THE CREW NOTICED A CRACK ON THE CAPTAIN`S WINDSHIELD AND NOTICED A FEW SPARKS WHILE THE WINDSHIELD HEAT WAS ON. DECLARED AN EMERGENCY AND DIVERTED. REPLACED THE WINDSHIELD.
- [SDR VNAA2017112811101](https://openairdocs.org/sdr/VNAA2017112811101.md): Target · loose · Nov 28, 2017 · N260JS · Cndair CL6002B19 · Landing Gear Position and Warning
  > CREW RECEIVED GEAR DISAGREE MESSAGE AFTER DEPARTING CAE, DUE TO THE RIGHT MAIN GEAR NOT RETRACTING. MX INSPECTED AND FOUNG THE RT MAIN GEAR UPLOCK PROXIMITY SENSOR TARGET WAS LOOSE. SECURED THE TARGET, LANDING GEAR RETRACTION AND EXTENSION SYSTEM OPS CHECKED G
- [SDR VNAA2017040900010](https://openairdocs.org/sdr/VNAA2017040900010.md): Carbon Seal · defective · Apr 9, 2017 · N260JS · Cndair CL6002B19 · Turbine Engine Oil System
  > RED RIGHT ENGINE OIL PRESSURE WARNING. REMOVED AND REPLACED THE ACCESSORY DRIVE GEARBOX’S CARBON SEAL ASSEMBLIES.
- [SDR VNAA2016091300012](https://openairdocs.org/sdr/VNAA2016091300012.md): Proximity Sensor · inoperative · Sep 13, 2016 · N260JS · Cndair CL6002B19 · Door Warning System
  > AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R THE PASSENGER DOOR OUTER HANDLE PROXIMITY SENSOR PS2MB AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2016041200012](https://openairdocs.org/sdr/VNAA2016041200012.md): Control Unit · failed · Apr 12, 2016 · N260JS · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL MESSAGE, MAINTENANCE TROUBLESHOT, R & R THE FLAPS ELECTRONIC CONTROL UNIT, AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2015042400040](https://openairdocs.org/sdr/VNAA2015042400040.md): Sensor · failed · Apr 24, 2015 · N260JS · Cndair CL6002B19 · Pneumatic Indicating System
  > CREW REPORTED RT 14TH DUCT, RED WARNING MESSAGE ON TAKEOFF. QRH WAS RUN AND MESSAGE PERSISTED. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R RT 14TH STAGE PYLON SENSING ELEMENT AND PERFORMED CHECKS IAW AMM. ACFT RELEASED
- [SDR VNAA2014081100007](https://openairdocs.org/sdr/VNAA2014081100007.md): Skin · cracked · Aug 11, 2014 · N260JS · Cndair CL6002B19 · Wing, Plate/Skin
  > DURING SCHEDULED MAINTENANCE, LOWER WING PLANK AFT FASTENER WAS FOUND CRACKED. REPAIRED IAW AMM. ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2014081100006](https://openairdocs.org/sdr/VNAA2014081100006.md): Skin · cracked · Aug 11, 2014 · N260JS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DURING SCHEDULED MAINTENANCE, THE AFT RIGHT CORNER OF THE NLG CUTOUT SKIN, BS 235 WAS FOUND CRACKED. INSPECTED AND REPAIRED IAW AMM. ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2014081100005](https://openairdocs.org/sdr/VNAA2014081100005.md): Skin · damaged · Aug 11, 2014 · N260JS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DURING SCHEDULED MAINTENANCE A CREASE WAS FOUND BELOW THE BAGGAGE BAY SCUFF PLATE AT BS 605. REPAIRED IAW AMM. ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2014081100004](https://openairdocs.org/sdr/VNAA2014081100004.md): Post · cracked · Aug 11, 2014 · N260JS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING SCHEDULED MAINTENANCE THE RT VERTICAL POST BS 409+128 WAS FOUND CRACKED. VERTICAL POST R & R IAW AMM. ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2014081100003](https://openairdocs.org/sdr/VNAA2014081100003.md): Seat Track · corroded · Aug 11, 2014 · N260JS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > DURING SCHEDULED MAINTENANCE, CABIN SEAT TRACK BS 409+40 WAS FOUND CORRODED. SEAT TRACK R & R IAW AMM. ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2014062200020](https://openairdocs.org/sdr/VNAA2014062200020.md): Windshield · malfunctioned · Jun 22, 2014 · N260JS · Cndair CL6002B19 · Flight Compartment Windows
  > CREW REPORTED ICE ACCUMULATION INSIDE BLACK AREA OF LT SIDE ON CAPTAIN’S FRONT WINDSHIELD. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R LEFT FORWARD WINDSHIELD AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2013070100001](https://openairdocs.org/sdr/VNAA2013070100001.md): Idg · failed · Jul 1, 2013 · N260JS · Cndair CL6002B19 · AC Generator-Alternator
  > DURING CRUISE, NR 1 GENERATOR FELL OFF LINE. ACFT RETURNED TO AIRPORT AND LANDED WITHOUT INCIDENT. MX TROUBLESHOT, R & R NR 1 IDG IAW ACFT MANUALS. CHECKS WERE PERFOMED IAW THE ACFT MANUALS AND ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2013050400001](https://openairdocs.org/sdr/VNAA2013050400001.md): Rib · cracked · May 4, 2013 · N260JS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING SCHEDULED MAINTENANCE A CRACK WAS FOUND AT THE RIGHT RIB IN RIGHT WHEEL WELL. THE AREA WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2013013100015](https://openairdocs.org/sdr/VNAA2013013100015.md): Sensing Element · faulty · Jan 31, 2013 · N260JS · Cndair CL6002B19 · Bleed Air Indicating System
  > CREW REPORTED LEFT 14TH STAGE BLEED DUCT WARNING MESSAGE WITH ANTI-ICE TURNED ON AND APU STARTED. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MESSAGE WENT OFF 15 TO 20 MINUTES LATER. MAINTENANCE INSPECTED, REMOVED AND REPLACED LEFT ENGINE 14TH STAGE PYLON SE
- [SDR VNAA2013011100004](https://openairdocs.org/sdr/VNAA2013011100004.md): Tire · separated · Jan 11, 2013 · N260JS · Cndair CL6002B19 · Tire
  > ON CLIMBOUT, SHORTLY AFTER TAKEOFF, CREW HEARD THUMPING NOISE AROUND NOSE GEAR. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND TREAD SEPARATION ON RIGHT NOSE LANDING GEAR TIRE. MAINTENANCE REMOVED AND REPLACED RIGHT AND LEFT TIRE
- [SDR VNAA2012111800012](https://openairdocs.org/sdr/VNAA2012111800012.md): Smoke Detector · false activation · Nov 18, 2012 · N260JS · Cndair CL6002B19 · Smoke Detection
  > CREW REPORTED LAVATORY SMOKE ALARM SOUNDED ABOUT 7 MINUTES INTO FLIGHT. NO SMELL OR SMOKE SEEN. NO MESSAGES WERE DISPLAYED. AIRCRAFT RETURNED TO AIRPORT LANDING WITHOUT ISSUE. MAINTENANCE TROUBLESHOT AND REMOVED AND REPLACED THE LAVATORY SMOKE DETECTOR. O
- [SDR VNAA2012091100008](https://openairdocs.org/sdr/VNAA2012091100008.md): Handle · open · Sep 11, 2012 · N260JS · Cndair CL6002B19 · Cargo/Baggage Doors
  > CREW REPORTED CARGO DOOR CAUTION MESSAGE IN FLIGHT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. HANDLE WAS CONFIRMED OPEN BY GROUND PERSONNEL. MAINTENANCE CLOSED CARGO DOOR HANDLE AND INSPECTED CARGO DOOR USING AIRCRAFT MAINTENANCE MANUALS. NO DEFE
- [SDR VNAA2011102700023](https://openairdocs.org/sdr/VNAA2011102700023.md): Sensing Element · faulty · Oct 21, 2011 · N260JS · Cndair CL6002B19 · Pneumatic Indicating System
  > CREW REPORTED RIGHT 14TH DUCT RED CAS MESSAGE IN FLIGHT EN ROUTE FROM DAY TO DCA. CREW RETURNED TO DAY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED RIGHT PYLON SENSING ELEMENT AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANU
- [SDR VNAA2011072700028](https://openairdocs.org/sdr/VNAA2011072700028.md): Beam · damaged · Jul 24, 2011 · N260JS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING SCHEDULED MAINTENANCE THE FS 280.0 FLOOR TRAVERSE BEAM WAS FOUND CRACKED AND CORRODED. THE FS 280.0 FLOOR TRAVERSE BEAM WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE. REVISED UNIQUE NUMBER.
- [SDR VNAA20110727](https://openairdocs.org/sdr/VNAA20110727.md): Beam · damaged · Jul 24, 2011 · N260JS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING SCHEDULED MAINTENANCE THE FS 280.0 FLOOR TRAVERSE BEAM WAS FOUND CRACKED AND CORRODED. THE FS 280.0 FLOOR TRAVERSE BEAM WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2011072700027](https://openairdocs.org/sdr/VNAA2011072700027.md): Post · cracked · Jul 24, 2011 · N260JS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING SCHEDULED MAINTENANCE FS409+128 RBL 18 AND LBL POST WERE CRACKED. REPAIRS WERE MADE. INSPECTION AND REPAIRS WERE ACCOMPLISHED USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2011072700026](https://openairdocs.org/sdr/VNAA2011072700026.md): Skin · corroded · Jul 24, 2011 · N260JS · Cndair CL6002B19 · Wing, Plate/Skin
  > DURING SCHEDULED MAINTENANCE LEFT WING LOWER PLANK ACCESS HOLE (540BB) WAS PITTED. REPAIRS WERE MADE. INSPECTION AND REPAIRS WERE ACCOMPLISHED USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2011060900004](https://openairdocs.org/sdr/VNAA2011060900004.md): Trim Switch · dirty · Jun 6, 2011 · N260JS · Cndair CL6002B19 · Stabilizer Control System
  > CREW REPORTED STAB TRIM CAS MESSAGE OCCURRED REPEATEDLY AFTER TAKEOFF FROM CVG. CREW RETURNED TO CVG AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, CLEANED FIRST OFFICER’S STAB TRIM DISCONNECT SWITCH AND PERFORMED CHECKS USING AIRCRAFT MANUALS. AIRCR
- [SDR VNAA2010112900018](https://openairdocs.org/sdr/VNAA2010112900018.md): Angle · cracked · Nov 26, 2010 · N260JS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING SCHEDULED MAINTENANCE A CRACK WAS FOUND AT FS 559 CAP ANGLE. CRACK WAS REPAIRED USING AIRCRAFT MANUALS AND AIRCRAFT RELEASED FOR SERVICE.
- [SDR VNAA20101129](https://openairdocs.org/sdr/VNAA20101129.md): Skin · damaged · Nov 26, 2010 · N260JS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DURING SCHEDULED MAINTENANCE DAMAGE WAS FOUND FROM FS605 TO FS621 SKIN. DAMAGE WAS REPAIRED USING AIRCRAFT MAINTENANCE MANUALS AND AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2010011500007](https://openairdocs.org/sdr/VNAA2010011500007.md): Oil System · low · Jan 8, 2010 · N260JS · Cndair CL6002B19 · APU Oil System
  > CREW REPORTED AN APU OIL TEMP AMBER MESSAGE DURING CRUISE EN ROUTE FROM CLT TO XNA. AIRCRAFT DIVERTED TO BNA BECAUSE THE RT ENGINE INTEGRATED DRIVE GENERATOR (IDG) WAS ALREADY DEFERRED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE SERVICED THE APU OIL LEVE
- [SDR VNAA2009092300006](https://openairdocs.org/sdr/VNAA2009092300006.md): Fan Blade · damaged · Sep 20, 2009 · N260JS · Cndair CL6002B19 · Turbine Engine Compressor Section
  > CREW REPORTED, INGESTED SMALL BIRD(S) IN LEFT ENGINE. AIRCRAFT RETURNED TO DAY WITHOUT INCIDENT. MAINTENANCE INSPECTED LT ENGINE PER THE MANUFACTURER MAINTENANCE MANUAL AND REPLACE FAN BLADES. CHECKS WERE MADE PER THE AIRCRAFT MAINTENANCE MANUAL AND AIRCRAF
- [SDR VNAA2009040200016](https://openairdocs.org/sdr/VNAA2009040200016.md): Indication Sys · malfunctioned · Mar 30, 2009 · N260JS · Cndair CL6002B19 · Fuel Indicating System
  > CREW REPORTED 10 MIN AFTER T/O AUTO XFLOW INHIBIT WHITE STATUS MSG APPEARED AND THE FUEL QTY INDICATORS LEFT SIDE AS WELL AS TOTAL FUEL WERE BLANK W/AMBER DASHES. AIRCRAFT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE DEFERRED SYSTEM PER MEL 28-41
- [SDR VNAA2009030900006](https://openairdocs.org/sdr/VNAA2009030900006.md): Probe · failed · Mar 6, 2009 · N260JS · Cndair CL6002B19 · Fuel Quantity Sensor
  > CREW REPORTED THE FUEL QUANTITY INDICATOR SHOWED DASHES ON LT SIDE AND TOTAL FUEL SYNOPTIC PAGE. AIRCRAFT RETURNED TO CLT WITHOUT INCIDENT. MAINTENANCE INSPECTED, REMOVED, AND REPLACED LT NR 6 FUEL QTY PROBE. CHECKS WERE MADE PER THE AIRCRAFT MAINTENANCE MA
- [SDR VNAA2008120900003](https://openairdocs.org/sdr/VNAA2008120900003.md): Apu · hung start · Dec 1, 2008 · N260JS · Cndair CL6002B19 · APU Core Engine
  > CREW REPORTED ON DESCENT INTO DAY, APU EXPERIENCED A HUNG START. MOMENTS LATER THE CREW TRIED TO START APU AND WAS SUCCESSFUL. BLEED AIR WAS SELECTED TO APU AND A STRONG FUEL SMELL WAS EVIDENT IN COCKPIT AND CABIN. APU WAS SHUTDOWN AND AIRCRAFT LANDED WITHO
- [SDR VNAA0807009](https://openairdocs.org/sdr/VNAA0807009.md): None · none · Jul 17, 2008 · N260JS · Cndair CL6002B19 · Standard Practices/Structures
  > CREW REPORTED THE PDF SHOWED FLAPS EXTENDED TO 2 DEG UNCOMMANDED AT 30,000FT WITH NO AURAL WARNING AT CRUISE. THE CREW DIVERTED TO TYS AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND NO DEFECTS. AIRCRAFT WAS RETURNED TO SERVICE. (

Next page: https://openairdocs.org/deregistered/N260JS-2025-12-09/reports.md?page=2

## 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 = 'N260JS' AND deregistration_id = 'N260JS-2025-12-09'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N260JS-2025-12-09/reports

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