# Service difficulty reports: N436JS, cancelled May 5, 2006 A list on [N436JS, cancelled May 5, 2006](https://openairdocs.org/deregistered/N436JS-2006-05-05.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 · 72 reports - [SDR VNAA0311010](https://openairdocs.org/sdr/VNAA0311010.md): Ecu · failed · Nov 26, 2003 · N436JS · Dorner DO328100 · Fuel Controlling System > DURING TAKEOFF, WHEN THE CONTROL LEVERS WERE ADVANCED THE LT ENGINE ECU FAILED AND THE CREW ABORTED TAKEOFF. THE CREW RESET THE ECU AND WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT WHICH WAS SUCCESSFUL. - [SDR VNAA0309011](https://openairdocs.org/sdr/VNAA0309011.md): Light · inoperative · Sep 18, 2003 · N436JS · Dorner DO328100 · Emergency Lighting > THE CREW REPORTED THAT THE ROW 10 EMERGENCY FLOOR LIGHTING STRIP WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY FLOOR LIGHT STRIP IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCR - [SDR VNAA0308024](https://openairdocs.org/sdr/VNAA0308024.md): Battery · discharged · Aug 29, 2003 · N436JS · Dorner DO328100 · Emergency Lighting > THE CREW REPORTED THAT THE EMERGENCY LIGHTS AT 9A WERE NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE 6LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR - [SDR VNAA0308001](https://openairdocs.org/sdr/VNAA0308001.md): Smoke Detector · faulty · Aug 1, 2003 · N436JS · Dorner DO328100 · Smoke Detection > THE CREW RECEIVED A LAV SMOKE CAS MESSAGE AND CALLED MAINTENANCE. MAINTENANCE DEFERRED THE LAV SMOKE DETECTOR WITH THE CREW. UPON ARRIVAL AT PIT, MAINTENANCE INSPECTED AND REPLACED THE LAV SMOKE DETECTOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 26-00-00 - [SDR VNAA0301003](https://openairdocs.org/sdr/VNAA0301003.md): Light · inoperative · Jan 5, 2003 · N436JS · Dorner DO328100 · Emergency Lighting > THE CREW REPORTED THAT THE EMERGENCY FLOOR LIGHTING IN THE GALLEY AREA WAS NOT ILLUMINATING. THE AIRCRAFT WAS THEN FERRIED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY FLOOR LIGHTING STRIP IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. - [SDR VNAA0212032](https://openairdocs.org/sdr/VNAA0212032.md): Target · out of adjust · Dec 25, 2002 · N436JS · Dorner DO328100 · Door Warning System > EN ROUTE, THE CREW RECEIVED A GALLEY DOOR OPEN MESSAGE. THE CREW REFERENCED THE QUICK REFERENCE HANDBOOK AND LANDED BACK AT PIT. MAINTENANCE INSPECTED AND FOUND THE TARGET A 1/4 LOOSE. THE AIRCRAFT WAS THEN FERRIED TO CAK. MAINTENANCE THEN ADJUSTED THE TA - [SDR VNAA0203022](https://openairdocs.org/sdr/VNAA0203022.md): Flight Dir · malfunctioned · Mar 13, 2002 · N436JS · Dorner DO328100 · Integrated Flight System > DURING THE TAKEOFF, THE CREW RECEIVED A VNAV SYSTEM FAIL INDICATION AGAIN AND ABORTED TAKEOFF. FLIGHT 4092 RETURNED TO THE GATE. MAINTENANCE CONTROL THEN MEL'D THE SYSTEM. FLIGHT 4092 THEN ATTEMPTED ANOTHER TAKEOFF AND DEPARTED WITH NO FURTHER INCIDENTS. - [SDR VNAA0203021](https://openairdocs.org/sdr/VNAA0203021.md): Flight Dir · malfunctioned · Mar 13, 2002 · N436JS · Dorner DO328100 · Integrated Flight System > DURING THE TAKEOFF, THE CREW RECEIVED A VNAV SYSTEM FAIL INDICATION AND ABORTED TAKEOFF. BEFORE THE AIRCRAFT CLEARED THE RUNWAY THE SYSTEM RESET ITSELF. THE CREW CALLED MAINTENANCE CONTROL AND WAS TOLD TO TRY ANOTHER TAKEOFF ATTEMPT IF ALL SYSTEMS WERE WORKI - [SDR VNAA0203019](https://openairdocs.org/sdr/VNAA0203019.md): Battery · discharged · Mar 13, 2002 · N436JS · Dorner DO328100 · Emergency Lighting > THE CREW REPORTED THAT THE EMERGENCY FLOOR LIGHTING STRIP WAS NOT WORKING. THE AIRCRAFT WAS FERRIED TO DAY. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY POWER SUPPLY AND THE EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERA - [SDR VNAA0201020](https://openairdocs.org/sdr/VNAA0201020.md): Battery · discharged · Jan 27, 2002 · N436JS · Dorner DO328100 · Emergency Lighting > THE CREW REPORTED THAT THE FIRST STRIP OF EMERGENCY LIGHTING WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE 4LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS REL - [SDR VNAA0201013](https://openairdocs.org/sdr/VNAA0201013.md): Battery · discharged · Jan 13, 2002 · N436JS · Dorner DO328100 · Emergency Lighting > THE CREW REPORTED THAT THE FORWARD EMERGENCY LIGHTING WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE 4LK POSITION IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAF - [SDR VNAA0112001](https://openairdocs.org/sdr/VNAA0112001.md): Control Unit · malfunctioned · Dec 1, 2001 · N436JS · Dorner DO328100 · Landing Gear Steering System > PULLING OFF THE GATE, THE NOSE WHEEL STEERING FAILED. AS SOON AS THE WHEEL WAS STRAIGHTENED THE FAIL LIGHT WENT OUT. AS FLIGHT 4106 TOOK THE RUNWAY THE NOSE WHEEL STEERING FAILED AGAIN. THE CREW CLEARED THE RUNWAY AND PERFORMED SEVERAL TURNS BUT COULD NOT D - [SDR VNAA0111004](https://openairdocs.org/sdr/VNAA0111004.md): Panel · failed · Nov 5, 2001 · N436JS · Dorner DO328100 · AC Power Distribution System > DURING CLIMBOUT, THE CREW RECEIVED A RIGHT HAND GENERATOR FAIL CAS MESSAGE AND RETURNED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE 1VE PANEL IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RE - [SDR VNAA0110004](https://openairdocs.org/sdr/VNAA0110004.md): Odor · detected · Oct 7, 2001 · N436JS · Dorner DO328100 · Air Distribution System > THE APU WAS RUNNING AND THE FLIGHT ATTENDANT REPORTED SMELLING SMOKE. MAINTENANCE INSPECTED THE AIRCRAFT AND COULD NOT DUPLICATE OR FIND ANY DISCREPANCIES. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. - [SDR VNAA0107016](https://openairdocs.org/sdr/VNAA0107016.md): Wheel · vibration · Jul 16, 2001 · N436JS · Dorner DO328100 · Wheel/Ski/Float > AFTER ROTATION, THE CREW FELT A VIBRATION COMING FROM THE NOSE GEAR. THE CREW LOWERED THE GEAR ASSUMING THAT THERE WAS A BLOWN TIRE. MAINTENANCE CONTROL REQUESTED FLIGHT 4169 CONTINUE TO PIT FOR MAINTENANCE BUT THE CREW FELT IT WOULD BE SAFER TO LAND BACK AT - [SDR VNAA0107014](https://openairdocs.org/sdr/VNAA0107014.md): Connector · dirty · Jul 11, 2001 · N436JS · Dorner DO328100 · Engine Indicating System > DURING THE TAKEOFF ROLL, THE CREW RECEIVED A ELECTRONIC CONTROL UNIT FAIL LIGHT AND A GENERATOR OFF LINE LIGHT. OUT STATION MAINTENANCE INSPECTED AND CLEANED THE ELECTRONIC CONTROL UNIT CANNON PLUG IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 77-00-00. OPER - [SDR VNAA0107008](https://openairdocs.org/sdr/VNAA0107008.md): Battery · defective · Jul 6, 2001 · N436JS · Dorner DO328100 · Battery/Charger System > THE CREW RECEIVED A BATTERY OVERHEAT INDICATION ON THE RED WARNING PANEL APPROXIMATELY TEN MINUTES OUT OF DAY. THE CREW CONTACTED MAINTENANCE CONTROL AND WAS ADVISED TO RETURN TO DAY. MAINTENANCE INSPECTED AND REPLACED THE NR 2 BATTERY IN ACCORDANCE WITH DOR - [SDR VNAA0107006](https://openairdocs.org/sdr/VNAA0107006.md): Harness · failed · Jul 4, 2001 · N436JS · Dorner DO328100 · Powerplant System > AFTER APPLYING POWER FOR TAKE OFF, THE AIRCRAFT LOST 50 PERCENT TORQUE AS THE AIRCRAFT ROTATED. THE POWER CAME BACK AND THE CREW DECIDED TO RETURN TO THE FIELD. THE CREW ALSO RECEIVED A LEFT HAND ELECTRONIC CONTROL UNIT FAILURE. MAINTENANCE INSPECTED AND FO - [SDR VNAA0105010](https://openairdocs.org/sdr/VNAA0105010.md): Fire Detector · malfunctioned · May 17, 2001 · N436JS · Dorner DO328100 · Fire Detection > FLIGHT 4044 WAS CLIMBING AND THE CREW RECEIVED A CARGO FIRE LIGHT INDICATION ACCOMPANIED BY THE TRIPLE CHIME. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK, MEMORY ITEMS, AND COMPANY PROCEDURES AND DECLARED AN EMERGENCY. THE AIRCRAFT LANDED OVERWEIGHT DUE T - [SDR VNAA0103012](https://openairdocs.org/sdr/VNAA0103012.md): Warning System · activated · Mar 14, 2001 · N436JS · Dorner DO328100 · Door Warning System > AS THE AIRCRAFT WAS TAXIING ONTO THE RUNWAY, THE FLIGHT RECEIVED A PROXI DOOR FAIL WARNING MESSAGE FOR THE MAIN CABIN DOOR. THE FLIGHT CREW EXITED THE RUNWAY AND RETURNED TO THE GATE. THE FLIGHT CREW CYCLED THE MAIN CABIN DOOR PROXI SENSOR CIRCUIT BREAKERS A - [SDR VNAA0103004](https://openairdocs.org/sdr/VNAA0103004.md): Anti-Ice System · failed · Mar 4, 2001 · N436JS · Dorner DO328100 · Airfoil Anti/De-ice System > DURING CLIMBOUT THE FLIGHT CREW RECEIVED A RIGHT WING MIDDLE AIRFOIL DEICE FAIL MESSAGE. THE FLIGHT CREW RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT MIDDLE LEADING EDGE ASSEMBLY IN ACCORDANCE WITH DORNIER - [SDR VNAA0102011](https://openairdocs.org/sdr/VNAA0102011.md): Bleed Valve · failed · Feb 18, 2001 · N436JS · Dorner DO328100 · Pneumatic Distribution System > AFTER CLIMB OUT, THE CREW RECEIVED A RIGHT HAND PACK OVERHEAT MESSAGE. THE CREW REFERENCED THE QUICK REFERENCE HANDBOOK THEN CONTACTED MAINTENANCE CONTROL WHO DIRECTED THEN TO RETURN TO PIT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT HAND HIGH PRESSURE BLE - [SDR VNAA0102003](https://openairdocs.org/sdr/VNAA0102003.md): Elevator · malfunctioned · Feb 7, 2001 · N436JS · Dorner DO328100 · Elevator Tab Control System > DURING CLIMB, THE CREW NOTICED THAT THE ELEVATOR TRIM WOULD NOT WORK WHEN SELECTED UP. FLIGHT 4061 RETURNED TO GSP. MAINTENANCE INSPECTED AND RECYCLED AIRCRAFT POWER AND PERFORMED OPERATIONAL CHECKS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 27-00-00. OP - [SDR VNAA0101022](https://openairdocs.org/sdr/VNAA0101022.md): Oxygen Mask · deployed · Jan 24, 2001 · N436JS · Dorner DO328100 · Passenger Oxygen System > WHILE CLIMBING THROUGH 10,000 FEET THE OXYGEN MASKS DEPLOYED INADVERTENTLY. THE FLIGHT LANDED IN PIT WITH NO FURTHER INCIDENTS. MAINTENANCE TROUBLESHOT THE WIRING, REPLACED THE SOLENOID AND OXYGEN PANEL, AND HAD A TEST FLIGHT. THE TEST FLIGHT WAS GOOD AND T - [SDR VNAA0011014](https://openairdocs.org/sdr/VNAA0011014.md): Door · not closed · Nov 16, 2000 · N436JS · Dorner DO328100 · Fluid Service Doors > DURING THE TAKEOFF RUN, THE FUEL DOOR CAS MESSAGE ILLUMINATED. THE CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. THE FUELER RETURNED AND SECURED THE FUEL DOOR. FLIGHT 4157 DEPARTED WITH NO FURTHER INCIDENT. - [SDR VNAA0011006](https://openairdocs.org/sdr/VNAA0011006.md): Bleed Valve · failed · Nov 10, 2000 · N436JS · Dorner DO328100 · Pneumatic System > DAY - FLT 4026 - AFTER TAKING THE RUNWAY AND AS POWER WAS ADVANCED THE PUT BLEED SHUTOFF VALVE FAILED. MAINTENANCE REPLACED THE RIGHT LP BLEED VALVE. THE AIRCRAFT DEPARTED WITH FURTHER INCIDENTS. (M) - [SDR VNAA0010008](https://openairdocs.org/sdr/VNAA0010008.md): Lever · failed · Oct 10, 2000 · N436JS · Dorner DO328100 · Landing Gear Selector > DURING THE TAKEOFF ROLL, THE UNSAFE GEAR LIGHT ILLUMINATED. THE CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE DECIDED TO FERRY THE PLANE TO DAYTON. MAINTENANCE AT DAY INSPECTED AND REPLACED THE GEAR CONTROL LEVER IN ACCORDANCE WITH DORNIER MAI - [SDR VNAA0010010](https://openairdocs.org/sdr/VNAA0010010.md): Pin · installed · Oct 10, 2000 · N436JS · Dorner DO328100 · Landing Gear System > DURING CLIMBOUT, THE CREW ATTEMPTED TO RETRACT THE GEAR AND RECEIVED ALL GEAR INDICATIONS. THE CREW CONTACTED MAINTENANCE CONTROL AND RETURNED TO THE FIELD. MAINTENANCE INSPECTED AND FOUND THE LANDING GEAR PINS INSTALLED IN THE LANDING GEAR. THE PINS WERE R - [SDR VNAA0009021](https://openairdocs.org/sdr/VNAA0009021.md): Structure · bird strike · Sep 23, 2000 · N436JS · Dorner DO328100 · Fuselage Main, Structure > DURING TAKEOFF, FLIGHT 4172 SUSTAINED MULTIPLE BIRD STRIKES. FLIGHT 4172 ABORTED TAKEOFF. MAINTENANCE INSPECTED THE AIRCRAFT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 53-00-00 AND FOUND NO DAMAGE TO THE AIRCRAFT. THE AIRCRAFT WAS RELEASED FOR SERVICE. - [SDR VNAA0008015](https://openairdocs.org/sdr/VNAA0008015.md): Ecu · failed · Aug 28, 2000 · N436JS · Dorner DO328100 · DC Power Distribution System > FLIGHT 4087 ABORTED TAKEOFF AFTER RECEIVING A LEFT HAND ELECTRONIC CONTROL UNIT FAIL MESSAGE. THE CREW WAS INSTRUCTED BY MAINTENANCE TO RESET THE ELECTRONIC CONTROL UNIT AND THE FAIL LIGHT EXTINGUISHED. THE CREW CONTINUED TO THE GATE WHERE MAINTENANCE CLEANE - [SDR VNAA0008014](https://openairdocs.org/sdr/VNAA0008014.md): Pressure Switch · failed · Aug 21, 2000 · N436JS · Dorner DO328100 · Propeller Controlling System > THE CREW RECEIVED A RIGHT HAND PROPELLER OIL PRESSURE CAS MESSAGE. THE CREW CALLED MAINTENANCE CONTROL AND ELECTED TO RETURN TO THE FIELD. MAINTENANCE INSPECTED AND REPLACED THE PRESSURE SWITCH IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 61-21-12. OPERATI - [SDR VNAA0008012](https://openairdocs.org/sdr/VNAA0008012.md): Connector · dirty · Aug 17, 2000 · N436JS · Dorner DO328100 · Propeller Indication System > FLIGHT 4066 PERFORMED AN AIR RETURN DUE TO RECEIVING A RIGHT HAND OIL PRESSURE CAS MESSAGE. MAINTENANCE INSPECTED BUT COULD NOT DUPLICATE THE PROBLEM. MAINTENANCE CLEANED THE CANNON PLUGS. A FUNCTIONAL CHECK FLIGHT WAS BUILT FOR THE AIRCRAFT AND THE AIRCRAF - [SDR VNAA0003004](https://openairdocs.org/sdr/VNAA0003004.md): Warning System · activated · Mar 6, 2000 · N436JS · Dorner DO328100 · Instrument Panel > THE FIGHT CREW RECEIVED A TAKEOFF CONFIGURATION WARNING AS THE TAKEOFF ROLL WAS INITIATED. THE FLIGHT CREW ABORTED THE TAKEOFF AND EXITED THE RUNWAY. A PITCH TRIM ASSYMETRY WARNING WAS DISPLAYED ON THE EICAS DISPLAY. AFTER THE POWER LEVERS WERE CYCLED THE W - [SDR VNAA0002017](https://openairdocs.org/sdr/VNAA0002017.md): Circuit Breaker · failed · Feb 22, 2000 · N436JS · Dorner DO328100 · Engine Oil Pressure > AFTER TAKEOFF CLIMBING THROUGH 500 FEET, THE CAPTAIN NOTICED THAT THE OIL PRESSURE IN THE LEFT HAND ENGINE READ ZERO POUNDS PER SQAURE INCH. THE AIRCRAFT RETURNED TO THE AIRFIELD WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND RESET THE CIRCUIT BREAKER. - [SDR VNAA0002006](https://openairdocs.org/sdr/VNAA0002006.md): Battery · discharged · Feb 3, 2000 · N436JS · Dorner DO328100 · Emergency Lighting > THE CREW NOTICED THAT THE EMERGENCY LIGHTS AT ROWS 3, 4, AND 5 WERE NOT WORKING. THE AIRCRAFT WAS THEN FERRIED TO PIT WHERE MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE 5LK POSITION IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-01. O - [SDR VNAA0001016](https://openairdocs.org/sdr/VNAA0001016.md): Battery · discharged · Jan 21, 2000 · N436JS · Dorner DO328100 · Emergency Lighting > THE CREW FOUND THAT THE EMERGENCY LIGHT ABOVE THE FLIGHT ATTENDENTS JUMPSEAT WAS NOT WORKING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY AT THE 5LK POSITION IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-01. OPERATIONAL CHECKS WERE PERFORMED AND T - [SDR VNAA9912012](https://openairdocs.org/sdr/VNAA9912012.md): Switch · failed · Dec 17, 1999 · N436JS · Dorner DO328100 · Propeller Controlling System > DURING CLIMBOUT FROM PIT, THE FLIGHT CREW RECEIVED A RIGHT HAND PROPELLER OIL PRESSURE CAS MESSAGE. MAINTENANCE CONTROL INSTRUCTED THE CREW TO RETURN TO THE FIELD. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE OIL PRES - [SDR VNAA9912011](https://openairdocs.org/sdr/VNAA9912011.md): Valve · failed · Dec 15, 1999 · N436JS · Dorner DO328100 · Cabin Temperature Controller > WHILE EN ROUTE TO CLARKSBURG, THE LEFT PACK OVERHEATED. THE FLIGHT CREW WAS INSTRUCTED TO RETURN TO THE FIELD. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE FLOW CONTROL AND SHUT OFF VALVE IN ACCORDANCE WITH DORNIER MA - [SDR VNAA9910008](https://openairdocs.org/sdr/VNAA9910008.md): Valve · failed · Oct 15, 1999 · N436JS · Dorner DO328100 · Landing Gear Brake System > AIRCRAFT WAS EN ROUTE TO PIT WHEN THE EMERGENCY PARKING BRAKE ACCUMULATOR CAS MESSAGE ILLUMINATED. THE FLIGHT CREW REFERENCED THE QRH AND ATTEMPTED TO CLEAR THE MESSAGE. THE WARNING DID NOT EXTINGUISH AND THE CREW DIVERTED TO CHO. THE AIRCRAFT LANDED WITHOU - [SDR VNAA9909003](https://openairdocs.org/sdr/VNAA9909003.md): Battery · discharged · Sep 15, 1999 · N436JS · Dorner DO328100 · Emergency Lighting > THE EMERGENCY FLOOR LIGHTING ADJACENT TO CABIN SEAT ROWS 5 THROUGH 7 WAS FOUND TO BE INOPERATIVE BY MAINTENANCE PERSONNEL. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK LOCATED AT POSITION 5LK IN ACCORDANCE WITH DORNIER MAINTENANCE MANUA - [SDR VNAA9908005](https://openairdocs.org/sdr/VNAA9908005.md): Structure · damaged · Aug 13, 1999 · N436JS · Dorner DO328100 · Fuselage Main, Structure > THE AIRCRAFT WAS STRUCK BY A PICKUP TRUCK WHILE SITTING STATIC AT THE GATE. OUTSTATION MAINTENANCE INSPECTED AND APPROVED THE AIRCRAFT FOR A FERRY FLIGHT TO PIT FOR REPAIR. THE FERRY TOOK PLACE WITHOUT INCIDENT. PIT MAINTENANCE INSPECTED AND RETURNED THE AI - [SDR VNAA9907002](https://openairdocs.org/sdr/VNAA9907002.md): Gearbox · lightning strike · Jul 7, 1999 · N436JS · Dorner DO328100 · Turbine Engine Reduction Gear > WHILE EN ROUTE TO DCA, THE AIRCRAFT WAS STRUCK BY LIGHTNING. THE FLIGHT CONTINUED ON TO DCA AND LANDED WITHOUT ANY FURTHER PROBLEMS. OUTSTATION MAINTENANCE INSPECTED THE AIRCRAFT AND A FERRY FLIGHT WAS APPROVED TO DAY FOR REPAIRS. DAY MAINTENANCE PERFORMED - [SDR VNAA9902018](https://openairdocs.org/sdr/VNAA9902018.md): Hub · cracked · Feb 27, 1999 · N436JS · Dorner DO328100 · Propeller Hub Section > A CRACK WAS FOUND ON THE RIGHT HAND PROPELLER HUB DURING COMPLIANCE OF HARTZELL ALERT SERVICE BULLETIN HD-ASB-61-021. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND PROPELLER, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 61-10-00. OPERATIONAL CHECKS WERE C - [SDR VNAA9902005](https://openairdocs.org/sdr/VNAA9902005.md): Pcu · failed · Feb 10, 1999 · N436JS · Dorner DO328100 · Propeller Controlling System > AFTER PUSHBACK, THE LEFT HAND PROPELLER FAILED TO UNFEATHER WHEN SELECTED. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE LEFT HAND PROPELLER CONTROL UNIT, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 61-21-06. OPERATIONAL CHECKS - [SDR VNAA9811024](https://openairdocs.org/sdr/VNAA9811024.md): Valve · failed · Nov 26, 1998 · N436JS · Dorner DO328100 · Pneumatic Distribution System > DURING THE TAXI PRIOR TO TAKEOFF, A CROSS-BLEED FAIL WARNING MESSAGE ILLUMINATED. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE CROSS-BLEED VALVE, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 36-11-10. OPERATIONAL CHECKS WERE CO - [SDR VNAA9811019](https://openairdocs.org/sdr/VNAA9811019.md): Windshield · bird strike · Nov 18, 1998 · N436JS · Dorner DO328100 · Flight Compartment Windows > SHORTLY AFTER TAKEOFF, THE AIRCRAFT TOOK A BIRD STRIKE ON THE LEFT HAND FORWARD WINDSHIELD. THE AIRCRAFT CONTINUED ON TO PIT AND PERFORMED A NORMAL LANDING. WHEN IN RANGE OF PIT, THE CREW REQUESTED MAINTENANCE. PIT MAINTENANCE INSPECTED THE AIRCRAFT FOR DAM - [SDR VNAA9810004](https://openairdocs.org/sdr/VNAA9810004.md): Ahru · failed · Oct 6, 1998 · N436JS · Dorner DO328100 · Integrated Flight System > A NUMBER TWO ATTITUDE/HEADING FAIL WARNING MESSAGE ILLUMINATED, DURING THE CLIMB-OUT PHASE OF THE FLIGHT. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED, WITHOUT ANY FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REPLACED THE NUMBER TWO ATTITUDE AND HEADING REFE - [SDR VNAA9809023](https://openairdocs.org/sdr/VNAA9809023.md): Pseu · tripped · Sep 26, 1998 · N436JS · Dorner DO328100 · Door Warning System > A CARGO DOOR WARNING INDICATION ILLUMINATED, DURING THE TAXI FOR DEPARTURE. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND RERACKED THE PROXY SWITCH ELECTRONIC UNIT (PSEU), IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-61-12. OPERATIONAL CH - [SDR VNAA9809022](https://openairdocs.org/sdr/VNAA9809022.md): Seat · loose · Sep 25, 1998 · N436JS · Dorner DO328100 · Passenger Compartment Equipment > THE FLIGHT ATTENDANT REPORTED THAT THE ATTENDANT SEAT CAME OFF TRACK, DURING THE TAXI OUT FOR DEPARTURE. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND RESECURED THE FLIGHT ATTENDANT SEAT, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 25-2-03. - [SDR VNAA9808005](https://openairdocs.org/sdr/VNAA9808005.md): Control Unit · failed · Aug 4, 1998 · N436JS · Dorner DO328100 · Brake Anti-Skid Section > AN ANTI-SKID FAIL WARNING MESSAGE OCCURRED, DURING TAXI OUT FOR TAKEOFF. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE ANTI-SKID CONTROL UNIT, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-42-11. OPERATIONAL CHECKS WERE COMPLET Next page: https://openairdocs.org/deregistered/N436JS-2006-05-05/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 = 'N436JS' AND deregistration_id = 'N436JS-2006-05-05' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N436JS-2006-05-05/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.