# Service difficulty reports: N769NC, cancelled Dec 6, 2018 A list on [N769NC, cancelled Dec 6, 2018](https://openairdocs.org/deregistered/N769NC-2018-12-06.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 · 54 reports - [SDR DALA1142639860](https://openairdocs.org/sdr/DALA1142639860.md): Battery Pack · discharged · Jul 5, 2011 · N769NC · Doug DC951 · Emergency Lighting > MAINTENANCE FOUND THE EMERGENCY LIGHTS IN THE AFT STAIRWELL AND ABOVE THE TAIL CONE SLIDE NOT FUNCTIONING DURING SERVICE CHECK. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACKS B5-27 & B5-28 PER WIRING DIAGRAM AND THE SUBSEQUENT OPERATIONAL CHECK WAS GO - [SDR DALA1138329860](https://openairdocs.org/sdr/DALA1138329860.md): Inlet · contaminated · Jun 4, 2011 · N769NC · Doug DC951 · APU Core Engine > FLIGHT ATTENDANT REPORTED A BURNING SMELL AFTER TAKEOFF. RIGHT PACK IMMEDIATELY SECURED AND SMELL DISSIPATED. FOUND RIGHT PACK TEMPERATURE VALVE AT FULL HOT AND REPOSITIONED TO MID. RE-ACTIVATED RIGHT PACK AND SMELL RETURNED. HIGH PRESSURE BLEED VALVE SEC - [SDR DALA1137559860](https://openairdocs.org/sdr/DALA1137559860.md): Power Supply · inoperative · Jun 2, 2011 · N769NC · Doug DC951 · Emergency Lighting > MAINTENANCE FOUND EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT ROWS 1 THROUGH 4. MAINTENANCE REPLACED POWER SUPPLY. OPERATIONAL CHECK WAS GOOD PER AMM (2011-00379) ATL 340504. - [SDR DALA1100949860](https://openairdocs.org/sdr/DALA1100949860.md): Lamp · inoperative · Jan 6, 2011 · N769NC · Doug DC951 · Emergency Lighting > DURING LINE CHECK, MX FOUND THE RT OVERWING EMERGENCY EXIT SIGN WAS INOPERATIVE. MX REPLACED THE ASSOCIATED BALLAST AND INSTALLED A NEW LAMP. OPS CHECK WAS GOOD. - [SDR DALA1023549860](https://openairdocs.org/sdr/DALA1023549860.md): Skin Panel · dented · Sep 21, 2010 · N769NC · Doug DC951 · Trailing Edge Flaps > DURING GROUND INSP FOUND DENT IN LT INBD FLAP OTBD SKIN PANEL JUST AFT OF L/E. REPLACED IAW DWG 5910134. - [SDR DALA1023539860](https://openairdocs.org/sdr/DALA1023539860.md): Access Panel · damaged · Sep 21, 2010 · N769NC · Doug DC951 · Trailing Edge Flaps > DURING GROUND INSP FOUND DAMAGE TO LT INBD FLAP ACCESS PANEL. REPLACED IAW SRM 53-00-00. - [SDR DALA1023519860](https://openairdocs.org/sdr/DALA1023519860.md): Wedge · damaged · Sep 21, 2010 · N769NC · Doug DC951 · Trailing Edge Flaps > DURING GROUND INSP, FOUND DAMAGE TO LT FLAP T/E WEDGE OTBD OF AFT INBD SPOILER. REPAIRED IAW SRM 57-03-10. - [SDR DALA103729860](https://openairdocs.org/sdr/DALA103729860.md): Battery Pack · inoperative · Feb 14, 2010 · N769NC · Doug DC951 · Emergency Lighting > DURING LINE CHECK, MX FOUND THAT THE EMERGENCY CEILING LIGHTS IN THE FIRST CLASS SECTION OF THE CABIN HAD FAILED. MX REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION. - [SDR NWAA092569860](https://openairdocs.org/sdr/NWAA092569860.md): Battery Pack · discharged · Jul 20, 2009 · N769NC · Doug DC951 · Emergency Lighting > DURING LINE CHECK MAINTENANCE FOUND THAT THE RIGHT SIDE EXTERIOR EMERGENCY FLOOD LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND THE LIGHT. RETURNED TO AN OPERATIONAL CONDITION. - [SDR NWAA092389860](https://openairdocs.org/sdr/NWAA092389860.md): Battery Pack · discharged · Jul 5, 2009 · N769NC · Doug DC951 · Emergency Lighting > DURING LINE CHECK MAINTENANCE FOUND THAT THE RIGHT EXTERIOR EMERGENCY FLOOD LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION. - [SDR NWAA081619860](https://openairdocs.org/sdr/NWAA081619860.md): Battery Pack · inoperative · Apr 16, 2008 · N769NC · Doug DC951 · Emergency Lighting > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE TAILCONE AND FOR THE VENTRAL STAIRWAY WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK (B5-28) AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION. - [SDR NWAA080469860](https://openairdocs.org/sdr/NWAA080469860.md): Light · inoperative · Feb 12, 2008 · N769NC · Doug DC951 · Emergency Lighting > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE VENTRAL STAIRWAY WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHTS AND OPERATIONAL CHECKED THE SYSTEM. THE AIRCRAFT RETURNED TO SERVICE. - [SDR NWAA074319860](https://openairdocs.org/sdr/NWAA074319860.md): Engine · failed · Dec 28, 2007 · N769NC · Doug DC951 · Engine (Turbine/Turboprop) > DURING TAKEOFF ROLL FLIGHT CREW HEARD A LOUD "POP" AND NOTICED N1 ROLLBACK. FLIGHT CREW ABORTED THE TAKEOFF AT 110 KNOTS. MAINTENANCE FOUND METAL IN THE TAILPIPE AND REPLACED ENGINE NR 2. - [SDR 0500529860](https://openairdocs.org/sdr/0500529860.md): Computer · malfunctioned · Apr 15, 2005 · N769NC · Doug DC951 · Rudder Tab Control System > DURING TAKEOFF ROTATION, THE AIRCRAFT YAWED TO THE LT EVENTUALLY REQUIRING FULL RT RUDDER TRIM AND RT WING DOWN. COMPLIED WITH COM PROCEDURES AND FLT WAS ABLE TO CONTINUE TO SCHEDULED DESTINATION. CREW STATED THE LT RUDDER PEDAL WAS ABOUT 5 INCHES FORWARD AN - [SDR 0402009860](https://openairdocs.org/sdr/0402009860.md): Door Frame · cracked · Sep 16, 2004 · N769NC · Doug DC951 · Fuselage Main, Structure > DURING L-CHECK, FOUND CRACK IN FORWARD SERVICE DOOR JAMB AT LOWER FORWARD AND AFT CORNERS. REPAIRED PER EA 98-200689. - [SDR 0400349860](https://openairdocs.org/sdr/0400349860.md): Actuator · malfunctioned · Feb 28, 2004 · N769NC · Doug DC951 · Leading Edge Slat Actuator > DURING APPROACH FOR LANDING, THE RIGHT LEADING EDGE SLAT DID NOT COME FULLY OUT ON EXTENSION. THE AIRCRAFT DID EXPERIENCE AN UNCOMMANDED ROLL TO THE RIGHT. THE SLAT DISAGREEMENT ANNUNCIATOR LIGHT DID ILLUMINATE AND THE BLUE SLAT EXTEND INDICATOR DID NOT. AS - [SDR 0400359860](https://openairdocs.org/sdr/0400359860.md): Actuator · malfunctioned · Feb 28, 2004 · N769NC · Doug DC951 · Leading Edge Slat Actuator > ON APPROACH WHEN SLATS WERE EXTENDED, THE AIRCRAFT ROLLED TO THE RIGHT. THE BLUE SLAT EXTEND LIGHT DID NOT ILLUMINATE BUT NO MENTION OF SLAT DISAGREEMENT ANNUNCIATOR STATUS. AS THE AIRCRAFT SLOWED TO 190 KTS, THE SLAT EXTEND LIGHT ILLUMINATED. IT WAS NOTED - [SDR 0400029860](https://openairdocs.org/sdr/0400029860.md): Engine · failed · Jan 2, 2004 · N769NC · Doug DC951 · Turbine Engine Compressor Section > DURING TAKEOFF, THE NR 1 ENGINE EXPERIENCED A COMPRESSOR STALL AND LOSS OF POWER AT 105 KNOTS. FLIGHT CREW ABORTED TAKEOFF. MAINTENANCE FOUND METAL IN THE TAILPIPE. REPLACED THE NR 1 ENGINE. - [SDR 0301219860](https://openairdocs.org/sdr/0301219860.md): Fuel Control · malfunctioned · Jun 29, 2003 · N769NC · Doug DC951 · Turbine Engine Compressor Section > DURING TAKEOFF ROLL, FLIGHT CREW OBSERVED A FLOCK OF BIRDS PASS CLOSE TO THE AIRCRAFT AND THEN HEARD A POSSIBLE ENGINE COMPRESSOR STALL. FLIGHT CREW ABORTED TKAEOFF AT 118 KNOTS. MAINTENANCE INSPECTED BOTH ENGINES FOR EVIDENCE OF A BIRD STRIKE, NONE FOUND. - [SDR 0203129860](https://openairdocs.org/sdr/0203129860.md): Regulator Valve · malfunctioned · Sep 22, 2002 · N769NC · Doug DC951 · Cabin Cooling System > AT FL330, CABIN WAS CLIMBING 800-1000 FPM. CREW WAS UNABLE TO CONTROL PRESSURE MANUALLY. PERFORMED COM PROCEDURES AND MADE AN EMERGENCY DESCENT. AUTO PRESSURE CONTROLLER BEGAN WORKING AGAIN AT 18,000 FT. CABIN ALTITUDE HAD REACHED 12,500 FT MAXIMUM. FLIGH - [SDR 0203119860](https://openairdocs.org/sdr/0203119860.md): Line · leaking · Sep 19, 2002 · N769NC · Doug DC951 · Landing Gear Brake System > DURING DESCENT, THE RIGHT HYDRAULIC PRESSURE LOW LIGHT ILLUMINATED. THE RIGHT HYDRAULIC PRESSURE DROPPED TO ZERO. COMPLIED WITH COM PROCEDURES AND FLIGHT CONTINUED WITH AN UNEVENTFUL APPROACH AND LANDING. MAINTENANCE FOUND THE LEFT OUTBOARD BRAKE LINE DAMAG - [SDR 0202739860](https://openairdocs.org/sdr/0202739860.md): Duct · slow · Aug 8, 2002 · N769NC · Doug DC951 · Leading Edge Slat Control System > WHEN SLATS WERE DEPLOYED AT 250 KTS, THE AIRCRAFT ROLLED TO THE RIGHT AND THERE WAS NO BLUE SLAT EXTEND LIGHT. CREW CYCLED THE SLATS BACK UP NORMALLY, RE-DEPLOYED AND THE AIRCRAFT ROLLED AGAIN. AFTER A FEW SECONDS THE BLUE LIGHT ILLUMINATED AND THERE WAS LES - [SDR 0104059860](https://openairdocs.org/sdr/0104059860.md): Skin · cracked · Aug 8, 2001 · N769NC · Doug DC951 · Fuselage Main, Plate/Skin > During Line MTC in Atl, the fwd fuselage upper nose skin between the cut outs for the nose radome hinge sustained crack damage when the radome was raised.Repaired per EA98-185035. Material 2024-t3.050" - [SDR 9901619860](https://openairdocs.org/sdr/9901619860.md): Guide · lack of lube · Apr 22, 1999 · N769NC · Doug DC951 · Leading Edge Slat Control System > SLAT DISAGREEMENT OCCURRED ON LANDING INTO ALB. FLIGHT CREW REQUESTED EMERGENCY EQUIPMENT ON STANDBY AND AIRCRAFT LANDED WITHOUT INCIDENT USING FLAPS ONLY. MAINTENANCE LUBRICATED THE LEFT AND RIGHT ANTI-ICE TELESCOPING DUCTS IN ALB. OPERATIONAL CHECK NORMAL - [SDR 9810339860](https://openairdocs.org/sdr/9810339860.md): Control Unit · inop · Nov 9, 1998 · N769NC · Doug DC951 · Landing Gear Position and Warning > AFTER TAKEOFF, THE FLIGHT CREW PERFORMED A LANDING GEAR UPLATCH CHECK. THE LEFT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED. LANDING GEAR WAS RECYCLED WITH A NOSE LANDING GEAR UNSAFE LIGHT ILLUMINATION UPON LANDING GEAR RETRACTION. FLIGHT RETURNED T - [SDR 9809779860](https://openairdocs.org/sdr/9809779860.md): Telescoping Duct · lack of lube · Jul 6, 1998 · N769NC · Doug DC951 · Leading Edge Slat Control System > DURING APPROACH INTO RDU, SLAT DISAGREEMENT LIGHT ILLUMINATED WITH NO BLUE SLAT EXTEND LIGHT. AIRCRAFT ROLLED TO THE RIGHT AND FLIGHT ATTENDANT OBSERVED NO SLAT EXTENSION ON LEFT WING. CAPTAIN DECLARED A YELLOW EMERGENCY AND REQUESTED EQUIPMENT ON STANDBY AS - [SDR 9807259860](https://openairdocs.org/sdr/9807259860.md): Boost Pump · leaking · Apr 24, 1998 · N769NC · Doug DC951 · Fuel Boost Pump > DURING CLIMB-OUT, THE FLIGHT CREW NOTICED A STREAM OF FLUID LEAKING FROM THE LEFT WING. FLIGHT CREW DECLARED AN EMERGENCY, FOLLOWED COM PROCEDURES, RETURNED TO DFW, AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT SIDE AFT BOOST PUMP VOLUTE. OPER - [SDR 9805089860](https://openairdocs.org/sdr/9805089860.md): Battery Pack · discharged · Mar 26, 1998 · N769NC · Doug DC951 · Emergency Lighting > DURING LINE CHECK, FOUND ONE SECTION OF CEILING EMERGENCY EXIT LIGHTING INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. - [SDR 9804629860](https://openairdocs.org/sdr/9804629860.md): Transformer · inoperative · Mar 18, 1998 · N769NC · Doug DC951 · AC Regulator > DURING CLIMB-OUT, THE LEFT ENGINE DRIVEN GENERATOR TRIPPED OFF LINE WITH AN AC CROSSTIE LOCKOUT CONDITION. FLIGHT CREW PERFORMED COM PROCEDURES, RETURNED TO DTW, AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE DIFFERENTIAL PROTECTION CURRENT TRANSFORME - [SDR 9804509860](https://openairdocs.org/sdr/9804509860.md): Gen Contl Pnl · malfunctioned · Mar 18, 1998 · N769NC · Doug DC951 · AC Generation System > DURING CLIMBOUT, THE LEFT ENGINE DRIVEN GENERATOR TRIPPED OFF LINE TOGETHER WITH AN AC CROSSTIE LOCKOUT. THE FLIGHT CREW SUCCESSFULLY RESET THE LEFT ENGINE DRIVEN GENERATOR. RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE GENERATOR CON - [SDR 9804489860](https://openairdocs.org/sdr/9804489860.md): Valve · inoperative · Mar 17, 1998 · N769NC · Doug DC951 · Leading Edge Slat Control System > DURING DESCENT, THE SLAT DISAGREEMENT INDICATION ILLUMINATED WHEN LEADING EDGE SLAT DE-VICES WERE EXTENDED. FLIGHT CREW FOLLOWED COM PROCEDURES, DECLARED EMERGENCY AND LANDED AT DTW WITHOUT INCIDENT. MAINTENANCE REPLACED THE SLAT CONTROL VALVE, OPERATIONAL C - [SDR 9803109860](https://openairdocs.org/sdr/9803109860.md): Battery · discharged · Feb 20, 1998 · N769NC · Doug DC951 · Emergency Lighting > DURING LINE CHECK, FOUND FORWARD EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK, OPERATIONAL CHECK OK. - [SDR 9719459860](https://openairdocs.org/sdr/9719459860.md): Battery Pack · discharged · Oct 18, 1997 · N769NC · Doug DC951 · Emergency Lighting > DURING LINE CHECK, FOUND AFT LEFT EMERGENCY OVERWING FLOOD LIGHT INOPERATIVE. REPLACED OVERWING EMERGENCY LIGHT BATTERY PACK, OPERATIONAL CHECK OK. - [SDR 9713829860](https://openairdocs.org/sdr/9713829860.md): Casting · broken · Jul 15, 1997 · N769NC · Doug DC951 · Landing Gear Retraction/Extension System > RIGHT MAIN GEAR UNSAFE LIGHT AND GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR RETRACTION. CREW RECYCLED GEAR THREE TIMES WITH SAME RESULTS. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND RIGHT MAIN GEAR FOLLOW-UP CASTING BROKEN. ALSO - [SDR 9710159860](https://openairdocs.org/sdr/9710159860.md): Gear Pins · not removed · May 22, 1997 · N769NC · Doug DC951 · Landing Gear Retraction/Extension System > AFTER TAKEOFF, UNABLE TO RAISE LANDING GEAR. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED GEAR PINS. - [SDR 9708939860](https://openairdocs.org/sdr/9708939860.md): Clip · out of adjust · May 5, 1997 · N769NC · Doug DC951 · Aerodynamic Fairings > DURING TAIL CONE FUNCTIONAL CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL EXTERIOR HANDLE FROM CLIPS. CLEANED AND ADJUSTED CLIPS, OPERATIONAL CHECK OK. - [SDR 9704819860](https://openairdocs.org/sdr/9704819860.md): Release Mech · out of adjust · Mar 4, 1997 · N769NC · Doug DC951 · Aerodynamic Fairings > DURING H-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE TAILCONE. ALSO FOUND THAT TAILCONE DID NOT RELEASE WHEN LATCHES ROTATED. RIGGED TAILCONE RELEASE SYSTEM. - [SDR 9705229860](https://openairdocs.org/sdr/9705229860.md): Web · cracked · Feb 27, 1997 · N769NC · Doug DC951 · Fuselage Miscellaneous Structure > DURING H-CHECK, FOUND CRACK IN WEB AT FS 1209, LONGERON 10L. REPAIRED PER EA 98-112203. - [SDR 9705219860](https://openairdocs.org/sdr/9705219860.md): Web · cracked · Feb 27, 1997 · N769NC · Doug DC951 · Fuselage Miscellaneous Structure > DURING H-CHECK, FOUND CRACK IN WEB AT FRAME FS 1209, LONGERON 13R. REPAIRED PER EA 98-112203. - [SDR 9704139860](https://openairdocs.org/sdr/9704139860.md): Pressure Panel · cracked · Feb 26, 1997 · N769NC · Doug DC951 · Fuselage Miscellaneous Structure > DURING H-CHECK, FOUND CRACKS IN NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE PANEL EMANATEING FROM OUTBOARD FITTING LEFT HAND SIDE, FS 83. REPAIRED PER EA 99-112097. - [SDR 9704129860](https://openairdocs.org/sdr/9704129860.md): Pressure Panel · cracked · Feb 21, 1997 · N769NC · Doug DC951 · Fuselage Miscellaneous Structure > DURING H-CHECK, FOUND CRACK IN NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE PANEL AT RIGHT OUTBOARD FITTING AT FS 105. REPAIRED PER EA 99-112099. - [SDR 9701689860](https://openairdocs.org/sdr/9701689860.md): Jamb · corroded · Jan 25, 1997 · N769NC · Doug DC951 · Fuselage Miscellaneous Structure > DURING H-CHECK, FOUND CORROSION ON DOOR 1R LOWER AFT DOOR JAMB AREA. REPAIRED PER SABRE TECH EA DC9-53-092. - [SDR 9625399860](https://openairdocs.org/sdr/9625399860.md): Battery Charger · failed · Nov 26, 1996 · N769NC · Doug DC951 · Battery/Charger System > AT GATE, PUSH BACK DRIVER INFORMED COCKPIT OF SMOKE COMING FROM NOSE WHEEL WELL E AND E COMPARTMENT. PASSENGERS DEPLANED, FOUND BATTERIES AND CHARGER HOT TO TOUCH. REPLACED BATTERIES, CHARGER AND TEMP SENSOR AND OPERATION CHECKS GOOD. - [SDR 9619439860](https://openairdocs.org/sdr/9619439860.md): Light · inoperative · Sep 8, 1996 · N769NC · Doug DC951 · Emergency Lighting > DURING LINE CHECK, FOUND EMERGENCY LIGHTS ABOVE TAILCONE SLIDE INOPERATIVE. FOUND SOCKET LOOSE. RESECURED SOCKET AND INSTALLED NEW BULBS. OPERATIONAL CHECK OK. - [SDR 9615789860](https://openairdocs.org/sdr/9615789860.md): Acm Duct · loose · Jul 18, 1996 · N769NC · Doug DC951 · Cabin Cooling System > LOSS OF CABIN PRESSURIZATION OCCURRED DURING CRUISE FLIGHT AT 28,000 FEET. OXYGEN MASKS WERE AUTOMATICALLY DEPLOYED THROUGHOUT THE CABIN AND EMERGENCY DESCENT WAS MADE TO 10,000 FEET. PRESSURE WAS REGAINED AND AIRCRAFT CONTINUED TO DESTINATION. AN UNEVENTFU - [SDR 9612399860](https://openairdocs.org/sdr/9612399860.md): Battery Pack · discharged · Jun 6, 1996 · N769NC · Doug DC951 · Emergency Lighting > DURING LINE MAINTENANCE, FOUND LEFT AFT CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK OK. - [SDR 9607529860](https://openairdocs.org/sdr/9607529860.md): Anti-Skid Comp · failed · Apr 1, 1996 · N769NC · Doug DC951 · Brake Anti-Skid Section > DURING LANDING WITH ANTI-SKID ON MEL, THE NR 2 AND NR 3 TIRES BLEW, NO DAMAGE TO AIRFRAME. CHANGED NR 2 AND NR 3 TIRES. REPLACED NR 1 ANTI-SKID VALVE AND ANTI-SKID COMPUTER. ANTI-SKID SYSTEM OPERATIONALLY CHECKED GOOD. - [SDR 9604869860](https://openairdocs.org/sdr/9604869860.md): Strut · reqd service · Feb 27, 1996 · N769NC · Doug DC951 · Nose/Tail Landing Gear Strut/Axle > DURING CLIMBOUT, UNABLE TO RETRACT LANDING GEAR AND AIRCRAFT PLACED IN FLIGHT MODE MANUALLY. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. NOSE STRUT WAS FOUND FLAT ON RETURN TO GATE. SERVICED NOSE STRUT AND CHECKED GOOD. - [SDR 9602789860](https://openairdocs.org/sdr/9602789860.md): Prox Contl Unit · malfunctioned · Feb 20, 1996 · N769NC · Doug DC951 · Landing Gear Position and Warning > ON CLIMBOUT, GEAR DOOR OPEN LIGHT DID NOT GO OUT WHEN GEAR WAS RETRACTED. RECYCLED GEAR 3 TIMES, LIGHT REMAINED ON. LIGHT EXTINGUISHED NORMALLY WHEN GEAR EXTENDED FOR LANDING AT DTW. REPLACED THE PROXIMITY SWITCH CONTROL UNIT AND OPERATIONAL CHECK GOOD. - [SDR 9604089860](https://openairdocs.org/sdr/9604089860.md): Battery Pack · discharged · Feb 16, 1996 · N769NC · Doug DC951 · Emergency Lighting > DURING LINE CHECK, FOUND AFT OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK GOOD. Next page: https://openairdocs.org/deregistered/N769NC-2018-12-06/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 = 'N769NC' AND deregistration_id = 'N769NC-2018-12-06' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N769NC-2018-12-06/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.