# Service difficulty reports: N619QS, cancelled Aug 31, 2026

A list on [N619QS, cancelled Aug 31, 2026](https://openairdocs.org/deregistered/N619QS-2026-08-31.md).

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

- [SDR DXTA2025110705596](https://openairdocs.org/sdr/DXTA2025110705596.md): Wire · disconnected · Nov 6, 2025 · N619QS · Cessna 560XL · Light System Wiring
  > THE LAV EMERGENCY SIGN BELOW LAV SEST ( FWD FACING PANEL) DOES NOT ILLUMINTATE. RECONNECTED WIRES. OPS CHECK GOOD. IAW AMM 33-50-02
- [SDR DXTA2025050903377](https://openairdocs.org/sdr/DXTA2025050903377.md): Bellcrank · defective · May 6, 2025 · N619QS · Cessna 560XL · Passenger/Crew Doors
  > MAIN DOOR: MAIN CABIN DOOR EXTREMELY DIFFICULT TO OPEN. REQUIRED BOTH CREW MEMBERS PUSHING WITH THEIR FEET. IT DOES NOT APPEAR THAT EITHER SEAL WAS INFLATED. CORRECTIVE ACTION; REPLACED FITTING ASSEMBLY IN DOOR PIN BELLCRANK IAW SUPPORT BRACKET ASSY AND DETAIL
- [SDR DXTA2025050603377](https://openairdocs.org/sdr/DXTA2025050603377.md): Door · binding · May 6, 2025 · N619QS · Cessna 560XL · Passenger/Crew Doors
  > MAIN DOOR: MAIN CABIN DOOR EXTREMELY DIFFICULT TO OPEN. REQUIRED BOTH CREW MEMBERS PUSHING WITH THEIR FEET. IT DOES NOT APPEAR THAT EITHER SEAL WAS INFLATED.
- [SDR DXTA2025032102744](https://openairdocs.org/sdr/DXTA2025032102744.md): Solenoid Valve · defective · Mar 18, 2025 · N619QS · Cessna 560XL · Passenger/Crew Doors
  > MAIN DOOR SECONDARY SEAL: WITH APU ON AND BLEED AIR OFF THE ACOUSTIC SEAL IN DOOR FRAME INTERFERES WITH OPENING AND CLOSING MAIN CABIN DOOR. BINDING BETWEEN THE DOOR HARDWARE AND THE INFLATED SEAL. THE SEAL APPEARS DAMAGED IN ALL OF THE AREAS WHERE THERE IS B
- [SDR DXTA2024112001186](https://openairdocs.org/sdr/DXTA2024112001186.md): Precatch · loose · Nov 17, 2024 · N619QS · Cessna 560XL · Passenger/Crew Doors
  > MAIN DOOR PRECATCH: INSIDE HANDLE OF PRECATCH SPINS FREELY AND CATCHES ON SIDE WALL. GAINED ACCESS TO MAIN ENTRY DOOR TRIM PANELS AND FOUND JAM NUT LOOSE TIGHTENED JAM NUT AND PRECATCH OPS CHECKS GOOD. RESECURED ALL MED TRIM PANELS NO FURTHER DEFECTS NOTED AT
- [SDR DXTA2024110401007](https://openairdocs.org/sdr/DXTA2024110401007.md): Circuit Breaker · defective · Oct 30, 2024 · N619QS · Cessna 560XL · Landing Gear System Wiring
  > DURING TAXING OUT TO THE ACTIVE RUNWAY, WHILE ON A TAXIWAY, WE HAD A MASTER CAUTION, RESET ILLUMINATE ALONG WITH A LOW PRESSURE/ANTISKID INOP ILLUMINATE. THE BRAKE PEDALS WENT ALL THE WAY TO THE FLOOR AND WOULD NOT STOP THE AIRPLANE. WE STOPPED THE AIRCRAFT WI
- [SDR DXTA2024102300913](https://openairdocs.org/sdr/DXTA2024102300913.md): Motor · faulted · Oct 20, 2024 · N619QS · Cessna 560XL · Landing Gear Brake System
  > POWER BRAKE CB: ABOUT 5 MINUTES INTO OUR TAXI FROM SIGNATURE TO RUNWAY 30 AT DULLES, JUST AS WE TURNED ON TAXIWAY ZULU GOT AN ANTI SKID ANNUNCIATOR ALONG WITH THE POWER BRAKE CIRCUIT BREAKER POPPED. WE ASKED TO GO TO RUNUP PAD AND AS WE PULLED IN GOT LOW BREAK
- [SDR DXTA2024101400817](https://openairdocs.org/sdr/DXTA2024101400817.md): Pressure Valve · defective · Oct 11, 2024 · N619QS · Cessna 560XL · Hydraulic System, Main
  > MAIN HYDRAULICS: UPON APPROACH INTO CHO WE ATTEMPTED TO BRING THE FLAPS TO 15° AND THEY DID NOT MOVE. WE ATTEMPTED TO LOWER THE LANDING GEAR. THE HANDLE CAME DOWN. WE HAD A RED UNLOCK LIGHT AND DID NOT GET ANY LANDING GEAR THREE GREEN LIGHTS. WE ELECTED TO DI
- [SDR DXTA2024100100718](https://openairdocs.org/sdr/DXTA2024100100718.md): Indicator · out of adjust · Sep 30, 2024 · N619QS · Cessna 560XL · Passenger/Crew Doors
  > CABIN DOOR LOCKED FLAG THAT IS IN THE STEP IS EXACTLY OPPOSITE TO DOOR FUNCTION. WHEN CABIN DOOR IS UNLOCKED FLAG INDICATES DOOR LOCKED. WHEN DOOR IS LOCKED, FLAG DISAPPEARS FROM WINDOW. CORRECTIVE ACTION: ADJUSTED RAG ARM IAW CE560XLS AMM 52-10-01. OPS CHECKE
- [SDR 2TJR202405147481](https://openairdocs.org/sdr/2TJR202405147481.md): Stringer · cracked · May 14, 2024 · N619QS · Cessna 560XL · Fuselage Main, Longeron/Stringer
  > DURING INSPECTION FOUND FUSELAGE STRINGER 15L IS CRACKED ON THE AFT END OF THE TAIL CONE SECTION AT F.S. 580.00. TRIMMED DAMAGED STRINGER AND PERFORMED A DOUBLER REPAIR IAW APPROVED DATA.
- [SDR DXTA2023103099300](https://openairdocs.org/sdr/DXTA2023103099300.md): Switch · defective · Oct 30, 2023 · N619QS · Cessna 560XL · Passenger/Crew Doors
  > AFTER SHUTTING MAIN CABIN DOOR, THE CABIN DOOR LIGHT REMAINS ILLUMINATED. INTTERMINTLY THE TOP CENTER AND BOTTOM CENTER LIGHTS ON THE CABIN DOOR INDICATORS REMAIN ON. REMOVED DEFECTIVE CABIN DOOR HANDLE LOCK SWITCH P/N G06-221-M-015 NSN. INSTALLED CUSTOMER SUP
- [SDR DXTA2023070590320](https://openairdocs.org/sdr/DXTA2023070590320.md): Unknown · unknown · Jul 3, 2023 · N619QS · Cessna 560XL · Emergency Lighting
  > MAIN ENTRANCE DOOR AFT "EXIT" LIGHT IS INOP. ALL OTHER LIGHTS WORK. ARRIVED AT AC. POWERED ON AC AND CONFIRMED DISCREPANCY. GAINED ACCESS TO LIGHT ASSEMBLY. FOUND WIRE BUNDLE HAS A WIRE TORN FROM SOCKET. CONNECTOR CONTACT WILL REQUIRE REPLACEMENT. TECH CONFIR
- [SDR DXTA2023053187420](https://openairdocs.org/sdr/DXTA2023053187420.md): Unknown · unknown · May 31, 2023 · N619QS · Cessna 560XL · Emergency Lighting
  > LAV EXIT SIGN/LIGHT: THE SMALL LIGHTED EXIT SIGN MOUNTED ON THE FRONT FASCIA IS INOP.//CORRECTIVE ACTION//FOUND MOLEX PIN 1 OF CONNECTOR J964V PUSHED OUT.RE-TERMINATED PIN 1 AND INSTALLED IT IN CONNECTOR J964V. WORK PERFORMED IAW CESSNA 560XL SPM TASK 20-30-20
- [SDR EBVR202305180002](https://openairdocs.org/sdr/EBVR202305180002.md): Flap · debonded · May 18, 2023 · N619QS · Cessna 560XL · Trailing Edge Flaps
  > ON LH OB FLAP 1.6 INCHES FROM INBOARD EDGE NEAR DATA TAG, THERE WAS A SPOT OF DISBONDING 7.6 INCHES SQUARE. AQRD REPAIRED AND REPAINTED THE FLAP IAW AQRD RS-825274 REV B DATED 10/31/22 & AQRD 912781 REV A DATED 04/11/2022. THIS WAS A MAJOR REPAIR.
- [SDR EBVR202305090451](https://openairdocs.org/sdr/EBVR202305090451.md): Unknown · unknown · May 9, 2023 · N619QS · Cessna 560XL · Emergency Exits
  > EMERGENCY EXIT DOOR SURROUND DOUBLER WAS CHAFFED BY SCREWS ON THE INTERIOR OF THE EMERGENCY EXIT INTERIOR REVEAL PANEL. TWO OF THESE CHAFES WERE IN AN AREA WHERE A PREVIOUS REPAIR HAD BEEN ACCOMPLISHED FOR THE SAME ISSUE. REPAIR DOUBLERS WERE FABRICATED AND IN
- [SDR EBVR20230509450](https://openairdocs.org/sdr/EBVR20230509450.md): Rudder · cracked · May 9, 2023 · N619QS · Cessna 560XL · Rudder, Tab Structure
  > ON VISUAL INSPECTION DRIVEN OFF OF AAIP, FOUND CRACK IN LOWER TRAILING EDGE SKIN APPROXIMATELY 0.6 INCHES IN LENGTH. PERFORMED AN EXTERNAL DOUBLER REPAIR OVER THE DAMAGED AREA PER AQRD ERO-108091 REV IR DATED 5/3/23. CHECKED BALANCE OF FLIGHT CONTROL PRIOR TO
- [SDR DXTA2023041484200](https://openairdocs.org/sdr/DXTA2023041484200.md): Solenoid · defective · Apr 13, 2023 · N619QS · Cessna 560XL · Cabin Pressure Control System
  > PRIOR TO DEPARTURE, GOT A CABIN DOOR ANNUNCIATOR & RED 6 PACK LIGHT. BOTTOM ROW MIDDLE LIGHT FOR THE VENT DOOR. COMPLIED WITH MEL O PROCEDURES MEL 52-70-01-06. RESETTING VENT DOOR IAW MEL & CONFIRMING ALL 9 FLAGS. ON CLIMB OUT NOTICED THAT CABIN MATCHED OUR R
- [SDR DXTA2023030682070](https://openairdocs.org/sdr/DXTA2023030682070.md): None · none · Mar 8, 2023 · N619QS · Cessna 560XL · Air Conditioning System
  > WITH APU RUNNING WE RECEIVED AN AIR DUCT O'HEAT CAB CAUTION. CABIN TEMP WAS EXCESSIVE AND THE CABIN STARTED TO FILL WITH AN UNKNOWN SMOKE/ODOR THAT WAS EASILY VISIBLE. UNABLE TO CONTROL THE CABIN TEMP IN BOTH AUTO & MANUAL MODES. REMOVED CABIN TEMP CONTROL V
- [SDR DXTA2022031458440](https://openairdocs.org/sdr/DXTA2022031458440.md): Engine · damaged · Mar 13, 2022 · N619QS · Cessna 560XL · Engine Fuel Distribution
  > RIGHT ENGINE FUEL FLOW: IN FLIGHT AFTER ACTUATING THE CROSSFEED FROM LEFT TANK TO RIGHT ENGINE THE RIGHT FUEL BOOST PUMP AMBER ANNUNCIATOR ILLUMINATED STEADY AND REMAINED ILLUMINATED. CROSSFEED WAS TURNED OFF AND R FUEL BOOST AMBER REMAINED ILLUMINATED. APPR
- [SDR DXTA2021061743820](https://openairdocs.org/sdr/DXTA2021061743820.md): Bolt · unsecure · Jun 17, 2021 · N619QS · Cessna 560XL · Passenger/Crew Doors
  > MAIN DOOR HARDWARE: BOLT ON THE AFT MAIN CABIN DOOR SUPPORT IS ALMOST UNSECURED. THE END ATTATCHED TO THE DOOR NOT THE AIRCRAFT DOOR FRAME. "CORRECTIVE ACTION" SECURED SCREW IAW CE-560XL AMM 52-10-01
- [SDR DXTA2021051442030](https://openairdocs.org/sdr/DXTA2021051442030.md): Brake · weak · May 14, 2021 · N619QS · Cessna 560XL · Landing Gear Brake System
  > RIGHT MLG BRAKE: AT SLOW SPEED WITH MINIMUM RIGHT SEAT PILOT BRAKE APPLICATION THE RIGHT LANDING GEAR BRAKE LOCKED UP AND RELEASED TWICE IN RAPID SUCCESSION.///SIGN-OFF///ARRIVED AT AIRCRAFT AND PERFORMED GVI OF BRAKES. SERVICED SYSTEM AS REQUIRED. PERFORMED
- [SDR DXTA2018061101059](https://openairdocs.org/sdr/DXTA2018061101059.md): Unknown · odor · Jun 9, 2018 · N619QS · Cessna 560XL · Air Distribution System
  > DESCENDING OUT OF 23000 FEET, DETECTED A DIRTY SOCK/BURNT OIL ODOR ALL THE WAY DOWN TO LANDING. REMOVED AND REPLACED THE CONDENSER BAG. RAN APU, NR 1 AND 2 ENGINES. OPS CHECKED GOOD. WORK PERFORMED IAW AMM 21-51-00, FOUND CONDENSER BAG TO HAVE NORMAL WE
- [SDR DXTR2017050201](https://openairdocs.org/sdr/DXTR2017050201.md): Channel · cracked · May 1, 2017 · N619QS · Cessna 560XL · Passenger/Crew Doors
  > MAIN CABIN DOOR FRAME STRUCTURE CRACKED BENEATH AFT SUPPORT ROD LOWER FITTING. ACCOMPLISHED MAJOR REPAIR IAW 5562/05RD.
- [SDR DXTA2016102506323](https://openairdocs.org/sdr/DXTA2016102506323.md): Control Unit · defective · Oct 25, 2016 · N619QS · Cessna 560XL · Landing Gear Brake System
  > EXPERIENCED COMPLETE FAILURE OF NORMAL BRAKE SYSTEM WITH ILLUMINATION OF MASTER CAUTION AND ANTI-SKID INOP ANNUNCIATOR. THERE IS NO EVIDENCE OF FLUID LEAK. BRAKE ACCUMULATOR IS FULL WITH CORRECT PRESSURE. ANTI-SKID WIRING HARNESSES SEEM TO BE INTACT. THER
- [SDR DXTA2015051506018](https://openairdocs.org/sdr/DXTA2015051506018.md): Brake Sys · contaminated · May 14, 2015 · N619QS · Cessna 560XL · Landing Gear Brake System
  > WHEN DOING STATIC TAKEOFF AROUND 88% N1 WITH FULL APPLICATION OF BRAKES, ACFT MOVES FWD. PERFORMED BRAKE SYS BLEED IAW MM 32-44-00. PERFORMED ACFT POWER RUN, OBSERVER OUTSIDE OF ACFT. NOTED THAT TIRES WERE NOT ROLLING BUT SLIDING.
- [SDR DXTA212021304871](https://openairdocs.org/sdr/DXTA212021304871.md): Unknown · vapor · Feb 10, 2012 · N619QS · Cessna 560XL · Air Distribution System
  > WITH APU RUNNING AND BLEED AIR ON WE NOTICED LIGHT SMOKE OR VAPOR IN CABIN AND A MUSTY ODOR. TURNED BLEED AIR OFF AND SMOKE/VAPOR SEEMED TO GET WORST. SHUTDOWN APU AND STARTED ENGINES AND SMOKE/VAPOR WENT AWAY.
- [SDR DXTA2010112404319](https://openairdocs.org/sdr/DXTA2010112404319.md): Connector · burned · Nov 23, 2010 · N619QS · Cessna 560XL · Communications System Wiring
  > WHEN VIDEO SCREEN AT SEAT NR3 WAS INSTALLED, SMOKE BEGAN COMING FROM SOCKET AND SHORTLY THEREAFTER FROM BEHIND CLUB TABLE. SCREEN WAS REMOVED AND SMOKE DISSIPATED. SCREEN CONNECTOR PLUG IS BURNED. REMOVED DEFECTIVE SOCKET & INSTALLED A NEW SOCKET IAW IMM 25-2
- [SDR DXTA2010082304201](https://openairdocs.org/sdr/DXTA2010082304201.md): Yoke · binding · Aug 21, 2010 · N619QS · Cessna 560XL · Control Column Section
  > FROM THE RT YOKE, IN FLIGHT WITH THE AUTOPILOT ON THERE IS A VIBRATION IN THE RT YOKE AND YOU CAN FEEL A VIBRATION IN THE FLOORBOARDS AT THE BASE OF THE YOKE. YOU CAN ALSO FEEL A GRINDING WITH FORE/AFT MOVEMENT OF THE RT YOKE.
- [SDR DXTA2009070203713](https://openairdocs.org/sdr/DXTA2009070203713.md): Sensor · inoperative · Jul 1, 2009 · N619QS · Cessna 560XL · Cabin Cooling System
  > ACM OVERHEAT LIGHT ILLUMINATES DURING TAKEOFF ROLL BETWEEN 70KTS AND V1. ALSO EXPERIENCED RUSH OF AIR IN CABIN AND COCKPIT WITH HOT AIR RUBBER ODOR. TROUBLESHOT BLEED AIR SYSTEM PER MM 36-11-00. FOUND NO FLOW FROM LT PRECOOLER EXHAUST. REMOVED AND REPLACED LT
- [SDR DXTA200702574](https://openairdocs.org/sdr/DXTA200702574.md): Metering Unit · intermittent · Oct 25, 2007 · N619QS · Cessna 560XL · Landing Gear Brake System
  > AT TAXI SPEEDS OF 15 MPH AND LESS, BOTH BRAKES GRAB INTERMITTENTLY AND INDEPENDENTLY OF EACH OTHER. THE BRAKES CAUSED THE AIRCRAFT TO LURCH AND SHUDDER. REMOVED & REPLACED FAULTY BRAKE METERING VALVE IAW C560XL M.M. 32-44-20. OPS & LEAK CHECK GOOD.
- [SDR DXTA200702427](https://openairdocs.org/sdr/DXTA200702427.md): O-Ring · cut · Jul 29, 2007 · N619QS · Cessna 560XL · Hydraulic System, Main
  > WITH AIR COMING OUT OF SIDE VENTS. UPPER DUCTS A BURNED ACRID SMELL AND BLUE-ISH SMOKE LIKE HAZE WAS OBSERVED IN CABIN (APU RUNNING, ENGINES OFF) FOUND HYD RESERVOIR LEAKING AT FWD UNION REPLACED CUT O-RING AND SVCD HYDRAULIC SYS. I/A/W CE560XL AMM 29-11-
- [SDR DXTA200601700](https://openairdocs.org/sdr/DXTA200601700.md): Switch · stuck · Oct 30, 2006 · N619QS · Cessna 560XL · Landing Gear Actuator
  > LT GEAR INDICATED UNSAFE W/ASSOC UNLOCKED LIGHT AND NO AOA INDEXERS. ROTARY TEST LIGHTS CHECK 4.0 FOLLOWED ALL EMERGENCY PROCEDURES INCLUDING BLOW DOWN, UNSAFE CONDITION REMAINED ON LANDING TO FULL STOP AND ROLL OUT ON ALL GEAR. FOUND LT GEAR DOWNLOCK SWITCH
- [SDR DXTA200601416](https://openairdocs.org/sdr/DXTA200601416.md): Engine · oil consumption · Jun 1, 2006 · N619QS · Cessna 560XL · Engine (Turbine/Turboprop)
  > LT ENGINE OIL PRESSURE ANNUNCIATOR ILLUMINATED, MASTER WARNING ILLUMINATED. OIL PRESSURE FELL BELOW 20 PSI THEN CAME BACK UP AND HOVERED AT 40 PSI, SHUT ENGINE DOWN NOTICED NO OIL IN SIGHT GAUGE. DETERMINED THAT THE LT ENGINE WAS BURNING OIL INTERNALLY, REPL
- [SDR DXTA200601295](https://openairdocs.org/sdr/DXTA200601295.md): Actuator · malfunctioned · Mar 13, 2006 · N619QS · Cessna 560XL · Landing Gear Actuator
  > ON APPROACH WITH FLAPS AT 15 (DEG) AND 175 KTS, GEAR DOWN WAS SELECTED. LEFT MAIN AND NOSE GEAR INDICATED GREEN LIGHTS. RIGHT MAIN DID NOT LIGHT UP. NO RED UNLOCKED LIGHT WAS SEEN. RECYCLED GEAR, GOT ALL THREE GREEN. BOTTLE WAS NOT BLOWN. REPEAT WRITE UP
- [SDR DXTA200601289](https://openairdocs.org/sdr/DXTA200601289.md): Warning Light · no indication · Mar 10, 2006 · N619QS · Cessna 560XL · Landing Gear Position and Warning
  > RIGHT MAIN LANDING GEAR LIGHT DID NOT ILLUMINATE WITH GEAR EXTENSION. CONDITION REPEATS AFTER CYCLING. BULBS CHECKED GOOD WITH ROTORY TEST. COMPLETED EMERGENCY GEAR EXTENSION CHECKLIST AND LIGHT CAME ON. RESET EMERGENCY GEAR PNUEMATIC BOTTLE VALVE. JACKED

## 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 = 'N619QS' AND deregistration_id = 'N619QS-2026-08-31'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N619QS-2026-08-31/reports

---
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