# Service difficulty reports: N587QS

A list on [N587QS](https://openairdocs.org/aircraft/N587QS.md).

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

- [SDR DXTA2026051808088](https://openairdocs.org/sdr/DXTA2026051808088.md): Brake Sys · faulted · May 14, 2026 · N587QS · Cessna 560XL · Landing Gear Brake System
  > DURING LANDING AT APPROX 80KTS, ANTISKID INOP ANNUNCIATION ILLUMINATED. CLEARED & CAME BACK ON. BRAKES WERE INOP DURING BRIEF TAXI OFF OF RUNWAY. THE BRAKES DID GRAB SLIGHTLY JUST BEFORE ACFT CAME TO A FULL STOP. ON POST FLT, ANTI SKID WIRING HARNESS ON R
- [SDR DXTA2025120105872](https://openairdocs.org/sdr/DXTA2025120105872.md): Wire Harness · faulted · Nov 27, 2025 · N587QS · Cessna 560XL · Landing Gear System Wiring
  > DURING FLIGHT ANTISKID LIGHT WOULD ILLUMINATE AND EXTINGUISH BEFORE COMPLETION OF AMBER C1 ANTISKID INOP CHECKLIST. DURING TAXI, ANTISKID INOP LIGHT ILLUMINATED (TAXIWAY WAS CLEAR OF ICE CONTAMINATION), LT BRAKE WOULD FAIL CAUSING ACFT TO AGGRESSIVELY TURN RT
- [SDR DXTA2025101305277](https://openairdocs.org/sdr/DXTA2025101305277.md): Wire Splice · damaged · Oct 10, 2025 · N587QS · Cessna 560XL · Light System Wiring
  > THE LEFT FLOOR EMERGENCY LIGHTS ARE EXTREMELY DIM. ALL OTHER LIGHTS ARE BRIGHT. WHEN THE FLOOR LIGHTS ARE TAPPED, THEY GET BRIGHT FOR A SECOND THEN RETURNS TO BEING DIM. NSPECTED THE LIGH CONNECTION AND FOUND SPLICE END TO BE DAMAGED. RE-SPLICED THE DAMAGED
- [SDR DXTA2025072304334](https://openairdocs.org/sdr/DXTA2025072304334.md): Handle · binding · Jul 22, 2025 · N587QS · Cessna 560XL · Passenger/Crew Doors
  > MAIN CABIN DOOR HANDLE REQUIRES EXCESSIVE FORCE TO OPEN OR CLOSE DOOR FROM INSIDE CABIN. INSPECTED AND NOTED TWO DOOR PINS ADJUSTED TO TIGHT AND BINDING IN THE ECCENTRIC HOLES CLOSE DOOR FROM INSIDE CABIN. ON DOOR FRAME. PERFORMED LATCH PLATE ADJUSTMENT TO THE
- [SDR 2025FA0000203](https://openairdocs.org/sdr/2025FA0000203.md): Strake · corroded · Mar 24, 2025 · N587QS · Cessna 560XL · Empennage Structure
  > LH AND RH STRAKES HAVE SEVERAL AREAS OF CORROSION ON UPPER AND LOWER SURFACES. PERFORMED 4 EACH DOUBLER REPAIRS TO LH STRAKE AND PERFORMED 6 EACH DOUBLER REPAIRS TO RH STRAKE. ALL WORK WAS ACCOMPLISHED IN ACCORDANCE WITH EO NO: C56-53-0001 TITLED: MINOR REPAIR
- [SDR 2025FA0000201](https://openairdocs.org/sdr/2025FA0000201.md): Strake · corroded · Mar 22, 2025 · N587QS · Cessna 560XL · Empennage Structure
  > LH STRAKE TRAILING EDGE WEDGE FITTING
- [SDR DXTA2024092500648](https://openairdocs.org/sdr/DXTA2024092500648.md): Door · out of adjust · Sep 23, 2024 · N587QS · Cessna 560XL · Passenger/Crew Doors
  > MAIN CABIN DOOR NEEDS ADJUSTED. AFTER LANDING WITH COLD SOAKED AIRCRAFT, MAIN CABIN DOOR WILL NOT STAY IN DOWN LOCKED POSITION USING CABIN DOOR HANDLE. CORRECTIVE ACTION: ADJUSTED SUPPORT STRUT ASSY AS NEEDED. NO DEFECTS FOUND AT THIS TIME OPS CHECKS GOOD. PER
- [SDR DXTA2024071712372](https://openairdocs.org/sdr/DXTA2024071712372.md): Light · inoperative · Jul 16, 2024 · N587QS · Cessna 560XL · Emergency Lighting
  > AISLE EMERGENCY LIGHTING ON LEFT, FRONT HALF OF THE AISLE ONLY LIGHTS FROM THE GALLEY TO JUST FORWARD OF SEAT 3 (AFT FACING SEAT ON LEFT SIDE). IT IS INOP FROM THAT POINT BACK TO MID -FUSELAGE. UPON INITIAL INVESTIGATION FOUND AISLE LIGHTING WAS COVERED BY F
- [SDR DXTA2024040211384](https://openairdocs.org/sdr/DXTA2024040211384.md): Battery · inoperative · Apr 2, 2024 · N587QS · Cessna 560XL · Emergency Lighting
  > EMERGENCY LIGHTS BATTERY INOP ON PRE-FLIGHT. REMOVED FAULTY FWD BATTERY PACK & INSTALLED OVERHAULED BATTERY PACK IAW MM 33-50-01. REMOVED FAULTY AFT BATTERY PACK & INSTALLED OVERHAULED BATTERY PACK IAW MM 33-50-01. CONNECTED EXTERNAL POWER & CHARGED FOR 1.
- [SDR DXTA2024011510611](https://openairdocs.org/sdr/DXTA2024011510611.md): Unknown · unknown · Jan 13, 2024 · N587QS · Cessna 560XL · Passenger/Crew Doors
  > MAIN DOOR WILL NOT LOCK IN DOWN PISITION FROM INSIDE CABIN. IT WILL LATCH DOWN FRIM OUTSIDE HANDLE. OP'S CHECKED DOOR COMFRIMED THAT IT WASNT LOCKING. ADJUSTED THE MAIN DOOR PUSH PULL ROD AND OP'S CHECKED IT MULTIPLE TIMES UNTIL I ADJUSTED IT ONE TURN FWD FR
- [SDR DXTA2023110299510](https://openairdocs.org/sdr/DXTA2023110299510.md): Unknown · unknown · Nov 1, 2023 · N587QS · Cessna 560XL · Passenger/Crew Doors
  > THE MAIN DOOR IS HEAVILY WEIGHTED TOWARDS THE CLOSED POSITION. WHEN INSIDE & CLOSING THE DOOR IT SLAMS SHUT. WHEN ON THE OUTSIDE WITH A CLOSED DOOR, VERY DIFFICULT TO OPEN. PERFORMED A GVI IAW AMM 52-10-00. A COMPLETE DOOR INTERNAL STRUCTURE DETAILED INSP
- [SDR 3J7R2023061300001](https://openairdocs.org/sdr/3J7R2023061300001.md): Battery Pack · discharged · Jun 13, 2023 · N587QS · Cessna 560XL · Emergency Lighting
  > EXTERIOR EMERGENCY LIGHTS AND AFT LEFT BULKHEAD EXIT SIGN ARE INOP WHEN THE MAIN BATTERY IS OFF. CHARGED FOR 1.5 HOURS AND HAD THE SAME RESULT.
- [SDR DXTA2023010978130](https://openairdocs.org/sdr/DXTA2023010978130.md): Switch · out of adjust · Jan 8, 2023 · N587QS · Cessna 560XL · Landing Gear Position and Warning
  > ON TAKE OFF, RECEIVED A FLASHING HYD PRESS WITH A MASTER CAUTION AFTER FLAP RETRACTION. GEAR & FLAPS RETRACTED ON SCHEDULE. HYD PRESS, NLG UNLOCK LIGHT, & STAB MISCOMP. RAN HYD PRESS QRH. PULLED & RESET HYD CONTROL CB IAW QRH. MAINTAINED 200KTS & FL 310
- [SDR DXTA2022121976520](https://openairdocs.org/sdr/DXTA2022121976520.md): Battery · defective · Dec 17, 2022 · N587QS · Cessna 560XL · Emergency Lighting
  > MAIN EXIT SIGN/LIGHT: FORWARD EMERGENCY POWER BATT PACK WILL NOT TAKE CHARGE - LIGHTS ARE OUT. // SIGNOFF // REMOVED AND REPLACED THE FWD EMERGENCY BATTERY PACK IAW CB60XLS MM 33-51-01, OPERATIONAL CHECK IS GO0D AT THIS TIME
- [SDR DXTA2021052442490](https://openairdocs.org/sdr/DXTA2021052442490.md): Seal · defective · May 22, 2021 · N587QS · Cessna 560XL · Passenger/Crew Doors
  > MAIN DOOR: MAIN CABIN DOOR OPEN WITH EXTREME DIFFICULTY AFTER BEING AT ALTITUDE FOR ANYTHING OVER ONE HOUR. I.E. ONCE OPEN ON THE GROUND IT OPERATES FINE. REPEAT WRITE UP///SIGN-OFF///REPLACED SHEARED OFF BOLT AND ALL 3 ACCOUSTIC LINER SEALS IAW CE-560XLS AMM
- [SDR DXTA2021033040270](https://openairdocs.org/sdr/DXTA2021033040270.md): Control Valve · defective · Mar 30, 2021 · N587QS · Cessna 560XL · Cabin Cooling System
  > ACM OVERHEAT ON TAKEOFF. THERE WAS A HOT/BURN SMELL IN THE AIRCRAFT. COMPLETED CHECKLIST AND LANDED. DID NOT DECLARE AN EMERGENCY. DID NOT LAND OVER WEIGHT. COMPLIED WITH OPERATIONAL PROCEDURE. REMOVED AND REPLACED RH FLOW CONTROL VALVE. IAW 560XL MM 21
- [SDR DXTA2020122404515](https://openairdocs.org/sdr/DXTA2020122404515.md): Door · frozen · Dec 24, 2020 · N587QS · Cessna 560XL · Passenger/Crew Doors
  > MAIN CABIN DOOR FROZEN SHUT. OPENED EMERGENCY EXIT DOOR TO EGRESS AIRCRAFT. EMERGENCY EXIT DOOR REQUIRES REINSTALLATION. COMPLIED WITH TASK T2PL6D007YVC5. INSPECTED THE CABIN EMERGENCY EXIT DOOR AND SURROUNDING AREAS FOR DEFECTS. NO DEFECTS NOTED. INSTAL
- [SDR DXTA2020111304353](https://openairdocs.org/sdr/DXTA2020111304353.md): Relief Valve · abnormal · Nov 13, 2020 · N587QS · Cessna 560XL · Landing Gear Brake System
  > WHILE TAXIING IN, THE "LOW BRAKE PRESSURE" AND "ANTI SKID INOP" AMBER MESSAGES ILLUMINATED. A FEW SECONDS LATER, THE BRAKE PEDALS WENT TO THE FLOOR AND WE HAD ALMOST NO BRAKES. NO BREAKERS WERE TRIPPED. SIGN OFF. REMOVED POWER BRAKE RELIEF VALVE CAUSING LO
- [SDR DXTA2020072903913](https://openairdocs.org/sdr/DXTA2020072903913.md): Counterbalance · out of adjust · Jul 28, 2020 · N587QS · Cessna 560XL · Passenger/Crew Doors
  > THE MAIN CABIN DOOR IS OUT OF ADJUSTMENT. IT IS HARD TO OPEN FROM THE INSIDE AND IT SLAMS SHUT WHEN CLOSING.ADJUSTED CABIN ENTRY DOOR COUNTERBALANCE ASSEMBLY IAW CE-560XLS AMM.
- [SDR 2019F00003](https://openairdocs.org/sdr/2019F00003.md): Skin · cracked · May 1, 2018 · N587QS · Cessna 560XL · Landing Gear Doors
  > RIGHT NOSE LG DOOR SKIN CRACKED AT THE LATCH.
- [SDR DXTA2017051706404](https://openairdocs.org/sdr/DXTA2017051706404.md): Windshield · damaged · May 17, 2017 · N587QS · Cessna 560XL · Flight Compartment Windows
  > DURING CRUISE FLIGHT AT FL400 AFTER 25 MINUTES AT FL400 A STRONG SMELL OF BURNING WIRES. THAT SMELL CONTINUED ON THE FLIGHT DECK THEN AFTER 15 MINUTES OF THE BURNING SMELL THE RIGHT WINDSHIELD HEAT FAULT LIGHT ANNUNCIATOR ILLUMINATED. WE THEN DECLARED AN EMERG
- [SDR DXTR2016122901](https://openairdocs.org/sdr/DXTR2016122901.md): Skin · dented · Dec 29, 2016 · N587QS · Cessna 560XL · Wing, Plate/Skin
  > RIGHT LOWER WING SKIN AT RWS 143.07 DENTED, REPAIRED IAW ERO-877762.
- [SDR DXTR2016122801](https://openairdocs.org/sdr/DXTR2016122801.md): Structure · corroded · Dec 28, 2016 · N587QS · Cessna 560XL · Fuselage Main, Structure
  > CORROSION FOUND UNDER THE DATA PLATE ON THE TAILCONE. REPAIRED CORROSION IAW DQ6626.
- [SDR DXTR2016122702](https://openairdocs.org/sdr/DXTR2016122702.md): Structure · corroded · Dec 27, 2016 · N587QS · Cessna 560XL · Wing Main, Frame Structure
  > CORROSION FOUND IN MULTIPLE LOCATIONS ON THE UPPER SIDE OF THE LT AND RT WINGS. REPAIRED IAW REPAIR S-560XL-5805/06RD.
- [SDR DXTR2016122701](https://openairdocs.org/sdr/DXTR2016122701.md): Structure · corroded · Dec 27, 2016 · N587QS · Cessna 560XL · Wing Main, Frame Structure
  > CORROSION FOUND IN MULTIPLE LOCATIONS ON THE UPPER SIDE OF THE LT AND RT WINGS. REPAIRED IAW REPAIR S-560XL-5805/06RD.
- [SDR DXTR2015092901](https://openairdocs.org/sdr/DXTR2015092901.md): Spar · gouged · Sep 26, 2015 · N587QS · Cessna 560XL · Vertical Stabilizer, Spar/Rib
  > GOUGES ON LT AND RT FWD SIDE OF THE VERTICAL SPAR. GOUGE DAMAGE WAS FOUND ON THE FWD SURFACE OF THE LOWER AFT VERTICAL STABILIZER SPAR WEB. REPAIRED IAW SR 5805/05RD.
- [SDR DXTR2015092301](https://openairdocs.org/sdr/DXTR2015092301.md): Bulkhead · gouged · Sep 23, 2015 · N587QS · Cessna 560XL · Fuselage Main, Bulkhead
  > A GOUGE & A SCRATCH WERE FOUND ON THE AFT SIDE OF THE 6611371-1 AFT PRESS BULKHEAD BOND ASSEMBLY AT FS 373.75, RBL 29.63, WL 114.27, NEAR STRINGER 11R. THE GOUGE WAS APPROX 0.173 INCHES IN DIAMETER & 0.013 INCHES DEEP. THE SCRATCH WAS 0.75 INCHES LONG & NEGL
- [SDR DXTA2015042706011](https://openairdocs.org/sdr/DXTA2015042706011.md): Bulb · inoperative · Apr 26, 2015 · N587QS · Cessna 560XL · Landing Gear Position and Warning
  > WHEN LANDING, LEFT MAIN GEAR DIDN'T HAVE GREEN LIGHT. PERFORMED EMERGENCY GEAR EXTENSION. FOUND THE LT GEAR DOWN & LOCK LIGHT BULBS INOPERATIVE. REMOVED THE FAILED INDICATOR BULBS & INSTALLED NEW BULBS. JACKED ACFT & CYCLED THE GEAR SEVERAL TIMES WITH NO F
- [SDR 2011FA0000397](https://openairdocs.org/sdr/2011FA0000397.md): Bolt · worn · Jun 14, 2011 · N587QS · Cessna 560XL · Elevator Control System
  > TWO PUSH/PULL TUBES THAT ATTACH TO THE AFT ELEVATOR BELLCRANK, WHEN TORQUING ATTACHING HARDWARE, THE NUT SHANKS OUT ON THE BOLT, ALLOWING THE BOLT TO BE ROTATED BY AND AND CAUSING WEAR IN THE BELLCRANK ATTAHCH HOLE. THIS WEAR CAUSES EXCESSIVE PLAY AT THE ATT
- [SDR 2011FA0000396](https://openairdocs.org/sdr/2011FA0000396.md): Shaft · worn · Jun 14, 2011 · N587QS · Cessna 560XL · Rudder Control System
  > FOUND GROOVES WORN INTO SHAFT OF THE 2 SCREWS THAT ENTER INTO THE RUDDER ACTUATOR ASSEMBLY. ACFT IS SET FOR CRUISE CONFIGURATION: DURING FLIGHT, TAIL VIBRATES CAUSING GROOVES TO WEAR INTO SHAFT OF SCREWS AT POINT WHERE SCREWS ENTER INTO ACTUATOR.
- [SDR DXTA2011032104520](https://openairdocs.org/sdr/DXTA2011032104520.md): Actuator · binding · Mar 20, 2011 · N587QS · Cessna 560XL · Elevator Tab Control System
  > ELEVATOR TRIM TAB JAMMED AND COULD NOT BE MOVED ELECTRICALLY OR MANUALLY. FLIGHT WAS AT 41000' AND THE PITCH TRIM ANNUNCIATOR ILLUMINATED DESCENDING THROUGH 34000'. THE TRIM TAB REMAINED LOCKED IN POSITION UNTIL 19000' WERE ABLE TO MANUALLY BREAK IT LOOSE. RE
- [SDR DXTA2011010304386](https://openairdocs.org/sdr/DXTA2011010304386.md): Ahrs · illuminated · Jan 2, 2011 · N587QS · Cessna 560XL · Attitude and Direction Data System
  > RED HEADING AND ATTITUDE FAIL MESSAGE ON THE NR 2 PFD. REMOVED FAULTY NR 2 AHRS & INSTALLED. OPS CHECKED REPAIRED UNIT IAW MM 34-21-01. OPS CHECKED GOOD.
- [SDR DXTA2010120304345](https://openairdocs.org/sdr/DXTA2010120304345.md): Trim System · malfunctioned · Dec 2, 2010 · N587QS · Cessna 560XL · Stabilizer Position Indicating
  > DURING THE DESCENT FROM 39000' THE PITCH TRIM ANNUNCIATION ON THE PFDS CAME ON. WITH THE AUTOPILOT OFF THE TRIM WHEEL COULD NOT BE TRIMMED ANY FURTHER FWD. AT LOWER ALTITUDES THE TRIM WORKED FREELY. PURGED AND LUBRICATED THE ELEVATOR TRIM ACTUATORS, INSPECTED
- [SDR DXTA2010112904336](https://openairdocs.org/sdr/DXTA2010112904336.md): Strut · leaking · Nov 28, 2010 · N587QS · Cessna 560XL · Main Landing Gear Strut/Axle/Truck
  > ON FINAL APPROACH THE LT MLG FAILED TO FULLY EXTEND TO GIVE A GREEN DOWN AND LOCKED LIGHT INDICATION. THE LANDING GEAR WAS BLOWN DOWN IAW THE EMERGENCY CHECKLIST. WHEN PNEUMATIC PRESSURE WAS APPLIED, THE LT MAIN GEAR FULLY EXTENDED GIVING A GREEN LIGHT INDICAT
- [SDR 2010F00027](https://openairdocs.org/sdr/2010F00027.md): Tube · short · Mar 4, 2010 · N587QS · Cessna 560XL · Fuselage Miscellaneous Structure
  > THE RUDDER CONTROL CABLES PASS THROUGH A PLASTIC GUIDE TUBE BETWEEN WING AND FUSELAGE. THIS GUIDE TUBE IS NOT SUPPORTED AT AFT END. IT IS TOO SHORT TO PASS THROUGH THE SUPPLIED SUPPORT CLAMP. SB560XL-27-20 ADDRESSES THIS CONDITION BUT IS NOT APPLICABLE TO T
- [SDR DXTA20090908037](https://openairdocs.org/sdr/DXTA20090908037.md): Control Cable · out of adjust · Sep 6, 2009 · N587QS · Cessna 560XL · Elevator Control System
  > CHECKED ALL FLT. CONTROL CABLES (PRIMARY) IAW MM 27-10-00, 27-20-00 & 27-30-00. ADJUSTED & CHECKED AILERON WING, FUSELAGE & SERVO CABLE TENSION IAW MM 27-10-00. ADJUSTED & CHECKED ELEVATOR & RUDDER CABLES IAW MM 27-31-00 & 27-20-00.
- [SDR DXTA2009090803775](https://openairdocs.org/sdr/DXTA2009090803775.md): Control Column · vibration · Sep 6, 2009 · N587QS · Cessna 560XL · Control Column Section
  > EXCESSIVE VIBRATION IN CONTROL YOKE/COLUMN STARTING AT 230 KTS, APPROX 9-10K FT, CONTINUED AT ALL A/S AND ALTITUDES ABOVE THAT. REPEAT WRITE-UP. VIBRATES WITH AUTOPILOT ON OR OFF.
- [SDR DXTA200906043678](https://openairdocs.org/sdr/DXTA200906043678.md): Actuator · bypassing · Jun 4, 2009 · N587QS · Cessna 560XL · Stabilizer Control System
  > STAB MISCOMPARE ILLUMINATED AFTER TAKOFF, RAN CHECKLIST AND LIGHT WENT OUT AFTER THE HYD CONTROL C/B WAS CYCLED. FOUND HORIZ STAB ACTUATOR BYPASSING HYDRO FLUID. REMOVED AND REPLACED STAB ACTUATOR. LEAK AND OPS CHECK GOOD. IAW MM 27-40-00.

## 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 = 'N587QS' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N587QS/reports

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