# Service difficulty reports: N441JS, cancelled Feb 7, 2006

A list on [N441JS, cancelled Feb 7, 2006](https://openairdocs.org/deregistered/N441JS-2006-02-07.md).

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

- [SDR VNAA0408009](https://openairdocs.org/sdr/VNAA0408009.md): Proximity Sensor · out of adjust · Aug 16, 2004 · N441JS · Dorner DO328100 · Door Warning System
  > DURING FLIGHT, THE DOORS LIGHT ON THE RED WARNING PANEL CAME ON. THE CREW THEN DIVERTED TO ELM. THE AIRCRAFT WAS THEN FERRIED TO PIT. MAINTENANCE THEN ADJUSTED THE PROXI SENSOR AND THE OVERCENTER LEVER IN ACCORDANCE WITH DORNIER MAITNENANCE MANUAL 52-00-00.
- [SDR VNAA0407009](https://openairdocs.org/sdr/VNAA0407009.md): Smoke Detector · failed · Jul 31, 2004 · N441JS · Dorner DO328100 · Smoke Detection
  > THE CREW REPORTED RECEIVING A LAV SMOKE MESSAGE. MAINTENANCE CONTROL DEFERRED THE LAV SMOKE DETECTOR IN ACCORDANCE WITH MEL 26-3 CODE-C. THE MEL WAS CLEARED BY REPLACING THE LAV SMOKE DETECTOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 26-00-00. OPERATI
- [SDR VNAA0406007](https://openairdocs.org/sdr/VNAA0406007.md): Power Supply · failed · Jun 13, 2004 · N441JS · Dorner DO328100 · Emergency Lighting
  > THE CREW REPORTED THAT THE EMERGENCY POWER SUPPLIES FAILED TO TEST. MAINTENANCE HAD THE CREW RUN THE ENGINES FOR 10 MINUTES AND PERFORM AN OPERATIONAL CHECK IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.
- [SDR VNAA0405004](https://openairdocs.org/sdr/VNAA0405004.md): Door · open · May 3, 2004 · N441JS · Dorner DO328100 · Passenger/Crew Doors
  > AFTER TAKEOFF, THE MAIN CABIN DOOR OPENED, AND FLIGHT 2447 RETURNED TO ABE, AIRCRAFT N441JS WAS THEN FERRIED TO CAK. THIS IS CURRENTLY STILL UNDER INVESTIGATION. AN UPDATED ODR WILL BE PROCESSED WHEN THE INVESTIGATION HAS BEEN COMPLETED.
- [SDR VNAA0403009](https://openairdocs.org/sdr/VNAA0403009.md): Fitting · failed · Mar 9, 2004 · N441JS · Dorner DO328100 · Fuel Controlling System
  > DURING FLIGHT, THE LEFT HAND ENGINE TORQUE WAS FLUCUATING AND FLIGHT 2434 RETURNED TO DAY. MAINTENEANCE INSPECTED AND FOUND A P-3 LINE FITTING LOOSE THEN TIGHTENED THE FITTING IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 71-00-00. OPERATIONAL CHECKS WERE PE
- [SDR VNAA0401008](https://openairdocs.org/sdr/VNAA0401008.md): Terminal · loose · Jan 19, 2004 · N441JS · Dorner DO328100 · Propeller/Rotor Anti-Ice/De-Ice System
  > DURING FLIGHT, THE CREW RECEIVED A LT PROPELLER HEAT FAIL BOTH MODES AND RETURNED TO PIT. MAINTENANCE CLEANED SLIP RING AND TIGHTENED TERMINAL ENDS ON BRUSH BLOCK IN ACCORDANCE WITH DORNER MAINTENANCE MANUAL 30-00. OPERATIONAL CHECKS WERE PERFORMED AND THE A
- [SDR VNAA0308014](https://openairdocs.org/sdr/VNAA0308014.md): Probe · failed · Aug 21, 2003 · N441JS · Dorner DO328100 · Outside Air Temperature Indicator/Sensor
  > DURING FLIGHT, THE CREW RECEIVED A TAT HEAT FAIL CAS MESSAGE AND RETURNED TO DAY. MAINTENANCE INSPECTED AND REPLACED THE TAT PROBE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 30-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SER
- [SDR VNAA0305004](https://openairdocs.org/sdr/VNAA0305004.md): Hmu · failed · May 2, 2003 · N441JS · Dorner DO328100 · Fuel Controlling System
  > AT 13,000, THE CREW BEGAN GETTING A LEFT HAND ENGINE SURGE. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND CONTACTED MAINTENANCE CONTROL. THE CREW THEN DIVERTED TO PHL. NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED SAFELY AT PHL. TWO MECHANICS FROM P
- [SDR VNAA0212035](https://openairdocs.org/sdr/VNAA0212035.md): Fan · failed · Dec 28, 2002 · N441JS · Dorner DO328100 · Air Distribution Fan
  > THE CREW REPORTED A BURNING SMELL IN THE COCKPIT AREA. THEN THE AVIONICS FAN FAILED. MAINTENANCE INSPECTED THE AVIONICS FAN AND FOUND IT DID FAIL. MAINTENANCE CONTROL THEN DEFERRED THE AVIONICS FAN WITH THE CREW USING CODE 21-6 B.
- [SDR VNAA0212034](https://openairdocs.org/sdr/VNAA0212034.md): Valve · failed · Dec 26, 2002 · N441JS · Dorner DO328100 · Master Cylinder/Brake Valve
  > EN ROUTE, THE CREW RECEIVED A PARKING BRAKE ACCUMULATOR PRESSURE LOW CAS MESSAGE. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND DIVERTED TO ROC. THE AIRCRAFT WAS THEN FERRIED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE PARKING BRAKE VALVE IN ACCORDA
- [SDR VNAA0212014](https://openairdocs.org/sdr/VNAA0212014.md): Pseu · failed · Dec 9, 2002 · N441JS · Dorner DO328100 · Landing Gear System
  > THE CREW RECEIVED A PROXY SYSTEM AMBER CAS MESSAGE AND RETURNED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE PSEU IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA0212005](https://openairdocs.org/sdr/VNAA0212005.md): Screw · Dec 4, 2002 · N441JS · Dorner DO328100 · Ice/Rain Protection System
  > WHILE ENROUTE TO EVV, THE CREW RECEIVED A CAPTAIN'S WINDSHIELD HEAT FAIL CAS MESSAGE AND RETURNED TO PIT. MAINTENANCE INSPECTED AND CLEANED THE WINDSHIELD SCREWS AND RESEALED THE WINDSHIELD IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 30-00-00. OPERATIONAL
- [SDR VNAA0212006](https://openairdocs.org/sdr/VNAA0212006.md): Windshield · Dec 4, 2002 · N441JS · Dorner DO328100 · Ice/Rain Protection System
  > DURING THE CLIMB OUT, THE CREW RECEIVED A CAPTAIN'S WINDSHIELD HEAT FAIL AND RETURNED TO PIT. THE AIRCRAFT WAS FERRIED TO DAY WHERE MAINTENANCE WILL REPLACE THE WINDSHIELD AND COMPLY WITH SERVICE BULLETIN 328-30-206.
- [SDR VNAA0211002](https://openairdocs.org/sdr/VNAA0211002.md): Shim · Nov 1, 2002 · N441JS · Dorner DO328100 · Engine Oil System (Airframe Furnished)
  > JUST PRIOR TO DESCENDING, THE CREW RECEIVED A HIGH OIL PRESSURE INDICATION. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND FEATHERED THE PROP WHILE PASSING THROUGH 24,000 FEET. FLIGHT 4055 LANDED AT YUL WITH NO FURTHER INCIDENTS. OUTSTATION MAINTENANCE
- [SDR VNAA0210029](https://openairdocs.org/sdr/VNAA0210029.md): Proximity Sensor · dirty · Oct 30, 2002 · N441JS · Dorner DO328100 · Door Warning System
  > EN ROUTE TO EVV AT 18,000 FEET, THE CREW RECEIVED A DOORS INDICATION ON THE RED WARNING PANEL AND DESCENDED TO 10,000 FEET AND THE LIGHT EXTINGUISHED. FLIGHT 4029 LANDED AT EVV WITH NO FURTHER INCIDENTS. OUTSTATION MAINTENANCE INSPECTED AND FOUND GREASE TO B
- [SDR VNAA0209007](https://openairdocs.org/sdr/VNAA0209007.md): Blade · out of adjust · Sep 5, 2002 · N441JS · Dorner DO328100 · Propeller Blade Section
  > DURING CLIMBOUT, THE CREW REPORTED THAT THE LEFT HAND FUEL SHUT OFF VALVE IS CLOSED AND THERE WAS A TORQUE SPLIT OF 5 PERCENT. THE CREW ELECTED TO RETURN TO YOW. THE AIRCRAFT WAS THEN FERRIED TO PIT WHERE MAINTENANCE PERFORMED OPERATIONAL CHECKS ON THE FUEL
- [SDR VNAA0207032](https://openairdocs.org/sdr/VNAA0207032.md): Clamp · failed · Jul 22, 2002 · N441JS · Dorner DO328100 · Air Conditioning System
  > THE CREW REPORTED A HOT SMELL IN THE CABIN APPROXIMATELY UNDER THE PACK AREA. MAINTENANCE INSPECTED AND FOUND A LOOSE CLAMP AROUND THE HOT AIR DUCT. MAINTENANCE RESECURED THE CLAMP IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 21-00-00. OPERATIONAL CHECKS W
- [SDR VNAA0204007](https://openairdocs.org/sdr/VNAA0204007.md): Lamp · Apr 13, 2002 · N441JS · Dorner DO328100 · Indicating/Recording System
  > AFTER SELECTING GEAR DOWN, THE CREW RECEIVED NO NOSE GEAR DOWN AND LOCK INDICATION. A LAMP TEST THEN INDICATED THAT THERE WAS A BURNED OUT LIGHT. AS A PRECAUTION, THE CREW DECLARED AN EMERGENCY AND REQUESTED A FLY BY FROM ATC. THE TOWER CONFIRMED THAT THE G
- [SDR VNAA0110009](https://openairdocs.org/sdr/VNAA0110009.md): Boot · failed · Oct 14, 2001 · N441JS · Dorner DO328100 · Airfoil Anti/De-ice System
  > DURING CLIMBOUT, THE LEFT HAND INBOARD DE-ICE BOOT FAILED AND FLIGHT 4075 RETURNED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE LEADING EDGE ASSEMBLY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 30-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT
- [SDR VNAA0105015](https://openairdocs.org/sdr/VNAA0105015.md): Control Valve · failed · May 24, 2001 · N441JS · Dorner DO328100 · Airfoil Anti/De-ice System
  > AFTER DEPARTURE, THE CREW RECEIVED A AIRFOIL DE-ICE SYSTEM FAIL. THE CAPTAIN CONTACTED MAINTENANCE CONTROL AND WAS INSTRUCTED TO DIVERT TO CAK. FLIGHT 4135 DIVERTED TO CAK WHERE MAINTENANCE INSPECTED AND REPLACED THE EJECTOR FLOW CONTROL VALVE IN ACCORDANCE
- [SDR VNAA0009005](https://openairdocs.org/sdr/VNAA0009005.md): Apu · odor · Sep 11, 2000 · N441JS · Dorner DO328100 · Airborne Auxiliary Power Unit (APU) System
  > AS FLIGHT 4169 DEPARTED THE CREW SMELLED AN UNUSUAL ODOR IN THE COCKPIT AND BECAME LIGHT HEADED. THE CREW IMMEDIATELY RETURNED TO THE FIELD AND PROCEEDED TO THE GATE. MAINTENANCE INSPECTED THE AIRCRAFT AND DEFERRED THE AUXILARY POWER UNIT, FLIGHT 4169 THEN D
- [SDR VNAA0008008](https://openairdocs.org/sdr/VNAA0008008.md): Sensor · failed · Aug 10, 2000 · N441JS · Dorner DO328100 · Pneumatic Distribution System
  > AFTER DEPARTURE THE CREW WAS GETTING A LEFT HAND BLEED VALVE FAIL MESSAGE. AFTER A MAINTENANCE CALL AND DIFFERENT PROCEDURES, MAINTENANCE CONTROL ADVISED THE CREW TO RETURN TO PIT. MAINTENANCE INSPECTED AND REPLACED THE LEFT HAND HIGH PRESSURE TEMPERATURE SE
- [SDR VNAA0006009](https://openairdocs.org/sdr/VNAA0006009.md): Battery · failed · Jun 21, 2000 · N441JS · Dorner DO328100 · Emergency Lighting
  > THE FLIGHT CREW REPORTED THAT THE EMERGENCY LIGHTING AT THE 5 LK POSITION WAS NOT WORKING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE 5 LK POSITION IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-01. OPERATIONAL CHECKS WERE PERFORMED
- [SDR VNAA0005010](https://openairdocs.org/sdr/VNAA0005010.md): Battery · failed · May 16, 2000 · N441JS · Dorner DO328100 · Emergency Lighting
  > THE CREW REPORTED THAT THE EMERGENCY LIGHTING IN ROW 6 WOULD NOT ILLUMINATE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE 5LK POSITION IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-01. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRA
- [SDR VNAA0004007](https://openairdocs.org/sdr/VNAA0004007.md): Warning Light · illuminated · Apr 5, 2000 · N441JS · Dorner DO328100 · Instrument Panel
  > DURING TAKEOFF, THE CREW RECEIVED A TAKEOFF CONFIGURATION WARNING INDICATION. THE CREW REFERENCED THE QUICK REFERENCE HANDBOOK AND ATTEMPTED ANOTHER DEPARTURE. FLIGHT 4063 DEPARTED PIT WITH NO FURTHER INCIDENTS.
- [SDR VNAA0004023](https://openairdocs.org/sdr/VNAA0004023.md): Bleed Valve · malfunctioned · Mar 27, 2000 · N441JS · Dorner DO328100 · Cabin Cooling System
  > THE RIGHT HAND HIGH PRESSURE VALVE HAD BEEN PREVIOUSLY ON THE MEL LIST. DURING CLIMBOUT THE CABIN ALTITUDE STARTED TO CLIMB. THE CREW REFERRED TO THE QUICK REFERENCE HANDBOOK, FOLLOWED THE PROCEDURES AND ASKED FOR A LOWER ALTITUDE. THE CREW RESET THE BLEED
- [SDR VNAA0003026](https://openairdocs.org/sdr/VNAA0003026.md): Shutoff Valve · failed · Mar 25, 2000 · N441JS · Dorner DO328100 · Pneumatic Distribution System
  > THE RIGHT HAND MAIN DUCT PRESSURE REDUCING SHUTOFF VALVE FAILED IN THE CLOSED POSITION. MAINTENANCE INSPECTED AND REPLACED THE MAIN DUCT PRESSURE REDUCING SHUTOFF VALVE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 36-11-03. FUNCTIONAL CHECKS WERE COMPLETED
- [SDR VNAA0002004](https://openairdocs.org/sdr/VNAA0002004.md): Horn Assy · failed · Feb 3, 2000 · N441JS · Dorner DO328100 · Elevator Structure
  > WHILE CLIMBING THROUGH 11,000 FEET, THE CREW RECEIVED A RIGHT HAND ELEVATOR HORN HEAT FAIL CAS MESSAGE. THE CREW TRIED TWICE TO RESET THE CIRCUIT BREAKER BUT WOULD NOT RESET. MAINTENANCE CONTROL ADVISED THEM TO RETURN TO PIT. MAINTENANCE INSPECTED AND REPLA
- [SDR VNAA9911012](https://openairdocs.org/sdr/VNAA9911012.md): Bleed Valve · failed · Nov 15, 1999 · N441JS · Dorner DO328100 · Pneumatic Distribution System
  > THE FLIGHT CREW RECEIVED A LEFT HAND LOW PRESSURE BLEED VALVE FAIL CAS MESSAGE DURING THE TAKEOFF ROLL. WHILE TALKING TO MAINTENANCE CONTROL THE CAS MESSAGE CLEARED. THE FLIGHT CREW AGAIN ATTEMPTED TO TAKEOFF AND RECEIVED THE SAME LEFT HAND LOW PRESSURE BLEE
- [SDR VNAA9911001](https://openairdocs.org/sdr/VNAA9911001.md): Pcu · failed · Nov 1, 1999 · N441JS · Dorner DO328100 · Propeller Controlling System
  > WHILE PREPARING TO TAXI, FLIGHT 4097 COULD NOT GET THE RIGHT HAND PROPELLER OUT OF FEATHER. MAINTENANCE INSPECTED AND REPLACED THE PROPELLER CONTROL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 61-21-06. OPERATIONAL CHECKS WERE COMPLETED AND AIRCRAFT W
- [SDR VNAA9905010](https://openairdocs.org/sdr/VNAA9905010.md): Control Box · inoperative · May 26, 1999 · N441JS · Dorner DO328100 · Landing Gear Position and Warning
  > THE LANDING GEAR FAILED TO INDICATE DOWN AND LOCKED WHEN SELECTED ON FINAL APPROACH. THE CREW FOLLOWED QRH PROCEDURES AND DECLARED AN EMERGENCY. THE AIRCRAFT MADE A TOWER FLY BY, AND HAD THE TOWER VERIFY THE GEAR POSITION. AFTER THE GEAR WAS VERIFIED DOWN
- [SDR VNAA9812021](https://openairdocs.org/sdr/VNAA9812021.md): Power Supply · failed · Dec 22, 1998 · N441JS · Dorner DO328100 · Emergency Lighting
  > THE EMERGENCY LIGHTS AT 9DF AND 7DF WERE NOTED TO BE INOPERATIVE, DURING THE PREFLIGHT INSPECTION. MAINTENANCE INSPECTED AND REPLACED THE POWER SUPPLY AT THE 5LK POSITION. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR VNAA9812016](https://openairdocs.org/sdr/VNAA9812016.md): Connector · dirty · Dec 22, 1998 · N441JS · Dorner DO328100 · Propeller Controlling System
  > DURING TAXI, THE LEFT HAND PROPELLER OVERSPEED TEST FAILED TO OPERATE WHEN SELECTED. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND CLEANED THE OVERSPEED GOVERNOR CANNON PLUG. MAINTENANCE THEN PERFORMED OPERATIONAL CHECKS IN ACCORDANCE WITH DO
- [SDR VNAA9810003](https://openairdocs.org/sdr/VNAA9810003.md): Pcu · failed · Oct 5, 1998 · N441JS · Dorner DO328100 · Propeller Controlling System
  > THE LEFT PROPELLER FAILED TO UNFEATHER WHEN SELECTED, DURING THE PUSHBACK FOR DEPARTURE. THE AIRCRAFT WAS RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE LEFT PROPELLER CONTROL UNIT, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 61-21-06. OPERA
- [SDR VNAA9808024](https://openairdocs.org/sdr/VNAA9808024.md): Deice Boot · defective · Aug 24, 1998 · N441JS · Dorner DO328100 · Airfoil Anti/De-ice System
  > DURING TAXI FOR TAKEOFF, CREW RECEIVED AIRFRAME DEICE FAIL MESSAGE. AIRCRAFT RETURNED TO GATE. MAINTENANCE INSPECTED AIRCRAFT AND DEFERRED RT MIDDLE WING DEICE BOOT. AIRCRAFT WAS RELEASED AND FLOWN TO PIT. PIT MAINTENANCE REPLACED RT MIDDLE AIRFRAME LEADIN
- [SDR VNAA9807007](https://openairdocs.org/sdr/VNAA9807007.md): Control Panel · failed · Jul 16, 1998 · N441JS · Dorner DO328100 · Ice Detection
  > DURING THE TAXI PRIOR TO TAKEOFF, A PITOT HEAT FAIL WARNING MESSAGE ILLUMINATED. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE ICE SYSTEMS CONTROL PANEL (17VE), IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 31-12-13. OPERATIONAL
- [SDR VNAA9806013](https://openairdocs.org/sdr/VNAA9806013.md): Valve · failed · Jun 24, 1998 · N441JS · Dorner DO328100 · Pneumatic Distribution System
  > A CROSSBLEED WARNING MESSAGE OCCURED DURING THE TAXI FOR TAKEOFF. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE CROSSBLEED VALVE, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 36-11-10. OPERATION CHECKS WERE COMPLETED, AND THE AI
- [SDR VNAA9803026](https://openairdocs.org/sdr/VNAA9803026.md): Connector · dirty · Mar 24, 1998 · N441JS · Dorner DO328100 · Propeller Controlling System
  > THE RIGHT HAND PROPELLER OVERSPEED TEST FAILED WHEN SELECTED, DURING TAXI CHECKS. THE AIRCRAFT RETURNED TO THE GATE. OUTSTATION MAINTENANCE INSPECTED, CLEANED AND SECURED THE RIGHT HAND OVERSPEED GOVERNOR CANNON PLUG. OPERATIONAL CHECKS WERE COMPLETED IN ACC
- [SDR VNAA9712020](https://openairdocs.org/sdr/VNAA9712020.md): Control Unit · tripped · Dec 31, 1997 · N441JS · Dorner DO328100 · Trailing Edge Flap Control System
  > DURING TAXI, CREW RECEIVED FLAP CONTROL FAIL INDICATION. CREW RETURNED TO GATE. MAINTENANCE RESET FLAP CONTROL UNIT. OPERATIONAL CHECK GOOD. AIRCRAFT APPROVED FOR RETURN TO SERVICE.
- [SDR VNAA9707005](https://openairdocs.org/sdr/VNAA9707005.md): Smoke Detector · activated · Jul 20, 1997 · N441JS · Dorner DO328100 · Smoke Detection
  > SHORTLY AFTER TAKEOFF, THE CREW NOTED LAV SMOKE WARNING ILLUMINATED. CREW ALSO BELIEVED TO HAVE SMELLED A SLIGHT ODOR IN THE AIRCRAFT AT THAT TIME. THE AIRCRAFT RETURNED TO FIELD AND ON SHORT FINAL APPROCH THE LAV SMOKE WARNING WENT OUT. MAINTENANCE INSPECT
- [SDR VNAA9707004](https://openairdocs.org/sdr/VNAA9707004.md): Overtemp Switch · defective · Jul 20, 1997 · N441JS · Dorner DO328100 · Cabin Cooling System
  > DURING TAKEOFF ROLL, RT ECS OVERHEAT CAS MESSAGE ILLUMINATED. ABORTED T/O AND RETURNED TO GATE. INSPECTED SYSTEM AND DEFERRED RT AIR CYCLE MACHINE IN ACCORDANCE WITH MEL. LATER TROUBLE SHOT SYSTEM AND FOUND OVER TEMP SWITCH TO BE DEFECTIVE. REMOVED AND RE
- [SDR VNAA9703005](https://openairdocs.org/sdr/VNAA9703005.md): Brush Block · failed · Mar 18, 1997 · N441JS · Dorner DO328100 · Propeller/Rotor Anti-Ice/De-Ice System
  > LEFT PROP HEAT CAS MESSAGE ILLUMINATED AFTER PROP HEAT WAS SELECTED ON. AIRCRAFT RETURNED TO THE FIELD. MAINTENANCE REMOVED AND REPLACED THE LEFT PROP DE-ICE BRUSH BLOCK, OPERATIONAL CHECK GOOD.
- [SDR VNAA9703003](https://openairdocs.org/sdr/VNAA9703003.md): Retract Mech · malfunctioned · Mar 10, 1997 · N441JS · Dorner DO328100 · Landing Gear Door Retract Section
  > LOUD NOISE COMING FROM NOSE GEAR AREA WHEN GEAR WAS RETRACTED, GOES AWAY WHEN GEAR IS EXTENDED. RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE LT NOSE GEAR DOOR OPENED. INSPECTED AND SECURED THE LT NOSE LANDING GEAR DOOR, AIRCRAFT APP
- [SDR VNAA9701002](https://openairdocs.org/sdr/VNAA9701002.md): Dau · failed · Jan 3, 1997 · N441JS · Dorner DO328100 · Air Data Computer
  > ENCOUNTERED LOSS OF DAU NR 1, DAU NR 2 AND ADC. THIS RESULTED IN THE LOSS OF THE PRIMARY FLIGHT INSTRUMENTATION AND ENGINE INSTUMENTATION. ALSO, LOSS OF FMS. NOTIFIED ATC. ENTIRE SYSTEM RESET ITSELF WHILE RETURNING TO FIELD. PERFORMED NORMAL LANDING. MAI
- [SDR VNAA9606008](https://openairdocs.org/sdr/VNAA9606008.md): Bulb · failed · Jun 17, 1996 · N441JS · Dorner DO328100 · Landing Gear Position and Warning
  > ON APPROACH AFTER SELECTING GEAR DOWN, THE CREW REPORTED LEFT MAIN LANDING GEAR DID NOT INDICATE DOWN AND LOCKED. CREW SHOT A MISSED APPROACH WHILE THE FIRST OFFICER REPLACED THE BULB IN THE LANDING GEAR POSITION INDICATOR. AFTER BULB REPLACEMENT LEFT MIAN G
- [SDR VNAA9600013](https://openairdocs.org/sdr/VNAA9600013.md): Control Unit · malfunctioned · Apr 6, 1996 · N441JS · Dorner DO328100 · Brake Anti-Skid Section
  > PIT - FLT 4169 - DURING TAKEOFF ROLL, THE CREW WAS ALERTED BY A C.A.S. MESSAGE THAT BRAKES WERE HOT. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. PIT MX RE-RACKED THE ANTI-SKID CONTROL UNIT IAW MM 32-43-10. ALSO, ALLOWED SEVERAL MINUTES FOR THE BRAKES TO
- [SDR 96ZZZX2117](https://openairdocs.org/sdr/96ZZZX2117.md): Warning Light · illuminated · Mar 7, 1996 · N441JS · Dorner DO328100 · Door Warning System
  > FLT 4165 - CREW REPORTED THE CARGO DOOR WARNING LIGHT ILLUMINATED DURING FLIGHT. AIRCRAFT RETURNED TO AZO, LANDED 400 POUNDS OVERWEIGHT. AIRCRAFT WAS FERRIED WHERE CAK MAINTENANCE CONDUCTED AN OVERWEIGHT LANDING INSPECTION IAW MM 05-00-00. NO DEFECTS NOTED.
- [SDR 96ZZZX2116](https://openairdocs.org/sdr/96ZZZX2116.md): Deice Boot · defective · Feb 3, 1996 · N441JS · Dorner DO328100 · Air Intake Anti/De-Ice System
  > BLD/IAD - FLT 4126 - EN ROUTE, CREW REPORTED A PROBLEM WITH THE LEFT ENGINE INLET DEICE BOOT. THEY WERE ALERTED BY AN AMBER CAS MESSAGE DEICE BOOT FAIL. AIRCRAFT DIVERTED TO PIT. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. PIT MAINTENANCE REPLACED THE LEFT E

## 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 = 'N441JS' AND deregistration_id = 'N441JS-2006-02-07'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N441JS-2006-02-07/reports

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