# Service difficulty reports: N617QS, cancelled Dec 31, 2024

A list on [N617QS, cancelled Dec 31, 2024](https://openairdocs.org/deregistered/N617QS-2024-12-31.md).

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

- [SDR DXTA2023092095960](https://openairdocs.org/sdr/DXTA2023092095960.md): Actuator · defective · Sep 19, 2023 · N617QS · Cessna 560XL · Elevator Control System
  > WHILE CLIMBING THROUGH FL 390 WE RECEIVED PIT TRIM ANNUCIATION ON BOTH PFDS. THE TRIM WHEEL WAS TRYING TO TRIM BUT WAS BINDING AND NOT MOVING AND HAD AN AUDIBLE BINDING SOUND. NEITHER ELECTRIC OR MANUAL TRIM WERE WORKING. THE TRIM NEVER COULD GO PAST THE WOR
- [SDR DXTA2023070690360](https://openairdocs.org/sdr/DXTA2023070690360.md): Motor · damaged · Jul 5, 2023 · N617QS · Cessna 560XL · Landing Gear Brake System
  > POWER BRAKE CB: BRAKE CB TRIPPED, ANTI SKID AND LOW BRAKE PRESSURE ENNUNCIATED DURING TAXI IN. PNEUMATIC BRAKE APPLIED TO STOP AIRCRAFT AT RAMP PARKING. REMOVED PWR BRAKE MOTOR AND INSTALLED AN OVERHAULED MOTOR IAW CE-560XL AMM 32-44-20 RE-SET CB AND PERFOR
- [SDR DXTA2022122676980](https://openairdocs.org/sdr/DXTA2022122676980.md): Pin · lack of lube · Dec 26, 2022 · N617QS · Cessna 560XL · Passenger/Crew Doors
  > MAIN CABIN DOOR HANDLE REQUIRES EXCESSIVE FORCE TO OPEN AND CLOSE DOOR. CLEANED AND LUBED ALL MAIN CABIN DOOR PINS. ADJUSTED UPPER AFT LATCH PLATE INNER ECCENTRIC IAW MM 52-10-00. OPENED AND CLOSED MAIN CABIN DOOR SEVERAL TIMES. OPS CHECK GOOD AT THIS TIME.
- [SDR DXTA2022012455550](https://openairdocs.org/sdr/DXTA2022012455550.md): Socket · defective · Jan 21, 2022 · N617QS · Cessna 560XL · Emergency Lighting
  > EMERG LIGHT SWITCH: AMBER LIGHT FOR THE EMERGENCY LIGHT SWITCH IS INOP // SIGNOFF// REMOVED AND RELNSTALLED NEW LAMP P/N 6838. REMOVED AND REPLACED SOCKET P/N MS90308·4, OPERATIONAL CHECK OF LIGHT FOUND SATISFACTORY. REFERENCE: 560XL AMM 33·10·01 AND SPM 20-30
- [SDR DXTA2021071945410](https://openairdocs.org/sdr/DXTA2021071945410.md): Light · shorted · Jul 17, 2021 · N617QS · Cessna 560XL · Light System Wiring
  > CABIN EMERG LIGHT: CIRCUIT BREAKER HT 043 POPPED ON THE AFT CIRCUIT BREAKER PANEL IN THE APU COMPARTMENT. WE EXPERIENCED HEAVY ELECTRICAL SMELL AND SMOKE IN THE CABIN IN FLIGHT. THE SMOKE DISSIPATED AFTER ABOUT 10 MINUTES. FOUND SEVERAL DROP AISLE LIGHTS
- [SDR DXTA2020071503863](https://openairdocs.org/sdr/DXTA2020071503863.md): Strut · out of adjust · Jul 14, 2020 · N617QS · Cessna 560XL · Passenger/Crew Doors
  > CABIN ENTRY DOOR SPRING TORQUE COUNTERBALANCE HANDLE BAR EXCESSIVELY LOOSE. BARELY MAKES OVER CENTER LOCK. ADJUSTED CABIN DOOR SUPPORT STRUT ASSEMBLY REF AMM 52-10-01 AND OPS CKD NORMAL FOR POSITIVE OVERCENTER ACTION.
- [SDR DXTA2019082102781](https://openairdocs.org/sdr/DXTA2019082102781.md): Condenser · odor · Aug 20, 2019 · N617QS · Cessna 560XL · Air Conditioning System
  > CABIN ODOR OIL SMELL - DISTINCT OIL SMELL IN CABIN AND COCKPIT. STRONGER IN LAV AREA AND CABIN, LESS STRONG ON COCKPIT. NOTICEABLE ON GROUND WITH APU AIR ON AND IN-FLIGHT WITH APU AIR OFF. CLEANED THE WATER SEPARATOR REMOVED AND REPLACED WATER SEPARATOR CONDE
- [SDR DXTA2018060501036](https://openairdocs.org/sdr/DXTA2018060501036.md): Unknown · odor · Jun 4, 2018 · N617QS · Cessna 560XL · Air Distribution System
  > CLIMBING THRU 10K, PAX NOTIFIED CREW OF A SMOKE ODOR IN THE CABIN. CREW CONFIRMED AND FO WENT BACK TO CHECK WHILE CAPTAIN SHUT DOWN APU. ODOR IMMEDIATELY DISSIPATED. GROUND VISUAL CHECK REVEALED NO EVIDENCE OF A PROBLEM. PERFORMED BOROSCOPE APU INLET INSPEC
- [SDR DXTA201711105HQ2T](https://openairdocs.org/sdr/DXTA201711105HQ2T.md): Motor · failed · Nov 11, 2017 · N617QS · Cessna 560XL · Brake Anti-Skid Section
  > COMPLETE BRAKE FAILURE DURING TAXI OUT. ANTI-SKID LIGHT AND POWER PRESSURE CIRCUIT BREAKER TRIPPED. THEN LOW BRAKE PRESSURE LIGHTS. HYD FLUID ON NOSE GEAR DURING POST FLIGHT. INSPECTED BRAKE SYSTEM FOR SIGNS OF DAMAGE, NONE FOUND. OPS CHECKED BRAKES, COULD NOT
- [SDR DXTAT2PL6D005BQW8](https://openairdocs.org/sdr/DXTAT2PL6D005BQW8.md): Water Separator · odor · Aug 22, 2017 · N617QS · Cessna 560XL · Cabin Temperature Control System
  > ODORS IN THE COCKPIT DURING FLIGHT WITH APU RUNNING. SMELLS LIKE BURNED OIL. INSPECTED THE APU INLET AND EXHAUST, APU BLEED AIR DUCT AND HEAT EXCHANGER DUCT, WATER SEPERATOR AND CLEANED WATER SEPARATOR SOCK IAW MM 12-19-02. REINSTALLED WATER SEPERATOR AND
- [SDR DXTA2016012406172](https://openairdocs.org/sdr/DXTA2016012406172.md): Steering Sys · corroded · Jan 28, 2016 · N617QS · Cessna 560XL · Landing Gear Steering System
  > AFTER DEPARTURE THE LG UNLOCK LIGHT REMAINED ON. DURING CLIMB OUT THE HYD PRESS LIGHT REMAINED ILLUMINATED. COMPLETED THE LG WILL NOT RETRACT CHECKLIST. LG EXTENDED NORMALLY. JACKED ACFT & PERFORMED GEAR OPERATIONAL CHECKS, NO PROBLEMS FOUND. SLIGHTLY TUR
- [SDR DXTA2015110706119](https://openairdocs.org/sdr/DXTA2015110706119.md): Selector · malfunctioned · Nov 7, 2015 · N617QS · Cessna 560XL · Cabin Pressure Control System
  > DURING TAKEOFF, A LOUD SOUND OF RUSHING AIR & CABIN PRESSURIZING RAPIDLY. ACCOMPANIED BY A STRONG BURNING ODOR. ANNUNCIATOR WITH FLASHING MASTER CAUTION ILLUMINATED BUT WENT OUT. TROUBLESHOT AND VERIFIED ODOR IN COCKPIT & CABIN. PERFORMED ENGINE RUNS & OPS
- [SDR DXTA2015031105992](https://openairdocs.org/sdr/DXTA2015031105992.md): Pressure Switch · failed · Mar 10, 2015 · N617QS · Cessna 560XL · Landing Gear Brake System
  > DURING LANDING, LOWERING THE LANDING GEAR THE LOW BRAKE PRESSURE & ANTI-SKID INOPERATIVE ANNUNCIATOR LIGHTS CAME ON. RAN THE CHECKLIST & USED THE EMERGENCY BRAKE AFTER LANDING. TROUBLESHOT TO A BAD PRESSURE SWITCH. REPLACED THE PRESSURE SWITCH WITH AN OVE
- [SDR DXTA2015021705978](https://openairdocs.org/sdr/DXTA2015021705978.md): Unknown · unknown · Feb 16, 2015 · N617QS · Cessna 560XL · Landing Gear Brake System
  > DURING LANDING ROLL OUT AT SPEEDS ABOVE NORMAL TAXI SPEED, THE LT BRAKE GRABS EXCESSIVELY & PULLS THE ACFT TO THE LEFT. THE RT BRAKE APPEARED TO RELEASE & REAPPLY THE BRAKE 5 OR 6 TIMES DURING THE ROLL OUT. NO ANTI-SKID RELEASE MARKERS WERE NOTED AFTER LANDI
- [SDR DXTA2013111205563](https://openairdocs.org/sdr/DXTA2013111205563.md): Brake Assy · malfunctioned · Nov 11, 2013 · N617QS · Cessna 560XL · Landing Gear Brake System
  > LT BRAKE GRABS. R & R LT BRAKE ASSY IAW MM 32-42-01. BLED SYS AND PERFORMED OPS CHECKS. OPS CHECKS SATISFACTORY AT THIS TIME. TAXI, OPS, & LEAK CHECKED GOOD.
- [SDR DXTA2013103105553](https://openairdocs.org/sdr/DXTA2013103105553.md): Unknown · odor · Oct 30, 2013 · N617QS · Cessna 560XL · Air Distribution System
  > DURING CRUISE FLIGHT, A LOUD CLICK OR POP WAS HEARD. CREW NOTICED A STRONG ELECTRICAL BURNING ODOR IN THE COCKPIT THAT QUICKLY WENT AWAY. NO SMOKE WAS NOTED. NO CIRCUIT BREAKERS WERE TRIPPED. PERFORMED COCKPIT LIGHTING CHECK IAW MM 33-10-00, NO DEFECTS NOT
- [SDR DXTA2013070105426](https://openairdocs.org/sdr/DXTA2013070105426.md): Bearing · failed · Jun 30, 2013 · N617QS · Cessna 560XL · Elevator Control System
  > DURING DESCENT AT 35000 FT, ELEVATOR PITCH TRIM FROZE. PITCH TRIM LIGHT ILLUMINATED ON THE PFD. THE ELEVATOR PITCH TRIM WAS IMMOVABLE USING BOTH MANUAL AND ELECTRIC TRIM. PITCH TRIM BEGAN OPERATING NORMALLY AT APPROX. 20,000 FT AND OPERATED NORMALLY THEREAF
- [SDR DXTA2013050605373](https://openairdocs.org/sdr/DXTA2013050605373.md): Apu · fod · May 5, 2013 · N617QS · Cessna 560XL · APU Core Engine
  > AFTER STARTING APU, A BURNING ODOR CAME FROM APU. WENT OUTSIDE AND FOUND FLAMES COMING FROM EXHAUST ALONG WITH DEBRIS FROM A BIRDS NEST. SOME OF THE STICKS AND GRASS WENT INTO THE INTAKE. SHUTDOWN APU AND DISCHARGED A PORTABLE FIRE EXTINGUISHER. CLEANED O
- [SDR 2013F00002](https://openairdocs.org/sdr/2013F00002.md): Bolt · worn · Dec 12, 2012 · N617QS · Cessna 560XL · Nacelle/Pylon Miscellaneous Structure
  > ON PERFORMING AN INSPECTION-B, FOUND LT ENGINE FORWARD COWLING STRUT UPPER ATTACH BOLT SEVERELY WORN. SUSPECT VIBRATION CAUSING EXCESSIVE WEAR. THIS CONDITION HAS BEEN FOUND ON SEVERAL OF THIS MODEL ACFT.
- [SDR DXTA2011091504727](https://openairdocs.org/sdr/DXTA2011091504727.md): Motor · failed · Sep 15, 2011 · N617QS · Cessna 560XL · Landing Gear Brake System
  > ACFT WAS TAXIING TO THE RUNWAY, WHEN THE POWER BRAKES AND ANTI SKID SYSTEMS FAILED. THE CREW STOPPED THE ACFT ON THE TAXIWAY. REMOVED FAULTY MOTOR PN MP50B-1, SN 2728. FOUND COUPLER BETWEEN PUMP AND MOTOR WORN EXCESSIVELY. REPLACED COUPLER WITH NEW PN 6517
- [SDR DXTA2010100604257](https://openairdocs.org/sdr/DXTA2010100604257.md): Brake Assy · malfunctioned · Oct 4, 2010 · N617QS · Cessna 560XL · Landing Gear Brake System
  > BRAKES NOT FUNCTIONING PROPERLY. GRINDING AND GRABBING. TAXIED ACFT & VERIFIED PROBLEM, BUT WENT AWAY DURING TAXI. LET BRAKES COOL DOWN & RETAXIED & BRAKE FUNCTIONED NORMALLY. BLED LT & RT BRAKES IAW MM 32-44-00 & NEW BLEEDING PROCEDURE. TAXI CHECKED ACFT
- [SDR DXTA2009111003857](https://openairdocs.org/sdr/DXTA2009111003857.md): Nose Cone · damaged · Nov 10, 2009 · N617QS · Cessna 560XL · Engine Air Intake System
  > POSSIBLE BIRD STRIKE ON RT ENGINE AT 7 O`CLOCK POSITION. DENT FOUND ON ENGINE LIP AND BLOOD WITH FEATHERS AROUND INTAKE. PERFORMED A BIRD STRIKE INSP ON RT ENG AND BOROSCOPRED AND FOUND NO RESIDUE OF BIRD FID INGESTION. REMOVED AND REPLACED NOSE CONE LIP WIT
- [SDR DXTA2009111103853](https://openairdocs.org/sdr/DXTA2009111103853.md): Structure · dented · Nov 10, 2009 · N617QS · Cessna 560XL · Nacelle/Pylon, Main Frame
  > POSSIBLE BIRD STRIKE ON RT ENGINE AT 7 OCLOCK POSITION. DENT FOUND ON ENGINE LIP AND BLOOD WITH FEATHERS AROUND INTAKE.
- [SDR DXTA2009071703731](https://openairdocs.org/sdr/DXTA2009071703731.md): Seal · leaking · Jul 17, 2009 · N617QS · Cessna 560XL · Turbine Engine Oil System
  > DURING TAKEOFF APPROX 500FT, CREW GOT A RT 'LO OIL PRESS' INDICATION LIGHT. CREW FOLLOWED CHECKLIST AND LANDED THE ACFT SAFELY. OIL PRESSURE WAS AT APPROX 30 PSI. ALL OTHER INDICATIONS WERE NORMAL. RAN ACFT AT TAKEOFF PWR AND FOUND GARLOCK SEAL ON FCU LEAKIN
- [SDR DXTA200702508](https://openairdocs.org/sdr/DXTA200702508.md): Actuator · inoperative · Sep 28, 2007 · N617QS · Cessna 560XL · Engine Bleed Air System
  > RT EEC INOP ON TAKEOFF ROLL AND COULD NOT REACH TAKEOFF POWER SETTING IN MANUAL POSITION. REMOVED & REPLACED R/H BLEED TORQUE MOTOR. RAN A/C FOR LEAK & OPS CHECKS. SYSTEM OP'S CHECKS SATISFACTORY AT THIS TIME. ENG MAKES POD IN BOTH MANUAL & AUTO. ALL WORK DON
- [SDR DXTA200601474](https://openairdocs.org/sdr/DXTA200601474.md): Adc · fluctuates · Jul 1, 2006 · N617QS · Cessna 560XL · Air Data Computer
  > EXPERIENCED PITCH OSCILLATIONS IN CLIMB WITH KP/FD COUPLED TO AUTO PILOT. VIS FLUCTUATED FROM 500FPM TO +5000 FPM. GOT RED X ON VSI AND ALT AND A/S YELLOW FLAGS. APPEARS TO BE NR 1 ADC. REPLACED NR 1 ADC WITH REPAIR UNIT CERTIFIED TO AN ALTITUED OF 59,500
- [SDR DXTA200601437](https://openairdocs.org/sdr/DXTA200601437.md): Windshield · cracked · Jun 14, 2006 · N617QS · Cessna 560XL · Flight Compartment Windows
  > RIGHT FRONT WINDSHIELD HAS MULTIPLE CRACKS BROKE AT FLIGHT LEVEL 390 AND APPEARS TO BE THE OUTER LAYER ONLY. VERIFIED CO-PILOTS WINDSHIELD SHATTERED. REMOVED & REPLACED RT WINDSHIELD. C/W EDGE SEAL. C/W FUNCTIONAL TEST, CHECK GOOD. C/W RETAINER SCREW TORQ
- [SDR DXTA200601367](https://openairdocs.org/sdr/DXTA200601367.md): Position Switch · out of adjust · Apr 28, 2006 · N617QS · Cessna 560XL · Stabilizer Position Indicating
  > AFTER TAKEOFF, GEAR RAISED WITH NORMAL INDICATIONS. AT 400FT WHEN FLAPS RAISED TO (0) DEGREE, GOT A STEADY HYD PRESS AND STAB MISCOMPARE LIGHT. AFTER RUNNING CHECKLIST, FLAPS WERE LOWERED TO 15 DEGREES RESULTING IN HYD PRESS AND STAB MISCOMPARE LIGHTS. ADJUS
- [SDR DXTA200601359](https://openairdocs.org/sdr/DXTA200601359.md): Position Switch · contaminated · Apr 23, 2006 · N617QS · Cessna 560XL · Central Warning
  > SHORTLY AFTER TAKEOFF POWER APPLIED NO TAKE OFF LIGHT ILLUMINATES AND AUARAL WARNING. AFTER CLEARING RUNWAY LIGHT GOES OUT. TROUBLESHOT SYSTEM. CLEANED LT AND RT SPEED BRAKE SWITCHES AND CONNECTORS, CHECKED OPERATION OF FLAP POS SWITCH, RT STAB SWITCH, ELEV
- [SDR DXTA200500740](https://openairdocs.org/sdr/DXTA200500740.md): Wire Harness · faulty · May 22, 2005 · N617QS · Cessna 560XL · Turbine Engine System Wiring
  > DURING TAKEOFF ROLL LEFT ENGINE PRODUCED 80% N1. SCHEDULED TAKEOFF POWER WAS 90.1% - REMOVED AND REPLACED ENGINE WIRING HARNESS PER P&WC M/M CH 76-20-02 OPERATIONAL CHECKS SATISFACTORY. BOTH AUTO AND MANUAL MODES.
- [SDR DXTA200500626](https://openairdocs.org/sdr/DXTA200500626.md): Uplock Cable · out of adjust · Mar 12, 2005 · N617QS · Cessna 560XL · Landing Gear Retraction/Extension System
  > WHILE IN CRUISE AT FL410, CREW HEARD CLUNK SOUND FROM GEAR AREA, RED GEAR UNSAFE LIGHT ILLUMINATED AND HYD PRESS LIGHT ILLUMINATED STEADY. PULLED HYD CONTROL CB, HYD PRESS EXTINGUISHED, GEAR UNSAFE REMAINED ILLUMINATED. FOUND NOSE GEAR FREEFALL CABLE TO BE T
- [SDR DXTA200500603](https://openairdocs.org/sdr/DXTA200500603.md): Landing Gear · malfunctioned · Feb 20, 2005 · N617QS · Cessna 560XL · Main Landing Gear
  > AFTER ROTATION, GEAR SELECTED UP, AFTER 3-4 SEC GEAR MADE A CYCLING THUMPING NOISE FOR APPROX 3 SECONDS. RECEIVED A HYD FLOW & A HYD LOW CAUTION LIGHT. CYCLING STOPPED, GEAR LOCKED UP & HYD FLOW LIGHT WENT OUT. KEPT FLAPS AT 15 DEG AND RE-EXTENDED GEAR. HY
- [SDR DXTA200400500](https://openairdocs.org/sdr/DXTA200400500.md): Switch · malfunctioned · Dec 27, 2004 · N617QS · Cessna 560XL · Landing Gear Retraction/Extension System
  > AFTER GEAR UP/FLAPS UP HAD HYD PRESS, STAB MISCOMPARE ANNUNCIATORS AND UNLOCK GEAR LIGHT. PULL HYD C/B, AND LOUD THUMP HEARD AND FELT IN NOSE GEAR AREA. PUSH HYD C/B IN GET SAME NOISE. ALL LIGHTS OUT AND SYSTEMS WORKED FINE WITH GEAR DOWN AND FLAPS FULL AT

## 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 = 'N617QS' AND deregistration_id = 'N617QS-2024-12-31'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N617QS-2024-12-31/reports

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