# Service difficulty reports: N783NC, cancelled Dec 6, 2018 A list on [N783NC, cancelled Dec 6, 2018](https://openairdocs.org/deregistered/N783NC-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 · 56 reports - [SDR DALA1200419874](https://openairdocs.org/sdr/DALA1200419874.md): Battery · discharged · Dec 31, 2011 · N783NC · Doug DC951 · Emergency Lighting > EMERGENCY EGRESS OVERHEAD AISLE LIGHT INOP AT MID CABIN. REPLACED BATTERIES IN POWER SUPPLY B5-26. CHECKS OK. - [SDR DALA1125609874](https://openairdocs.org/sdr/DALA1125609874.md): Connector · loose · Apr 11, 2011 · N783NC · Doug DC951 · Light System Wiring > DURING LINE CHECK, MX FOUND THAT ALL OF THE EMERGENCY PATHWAY LIGHTS FOR THE CATWALK IN THE TAIL COMPARTMENT WERE INOPERATIVE. MX FOUND A CONNECTOR IN THE WIRE HARNESS LOOSE, RESECURED IT, RE-LAMPED EACH LIGHT, AND FUNCTIONALLY CHECKED THE SYS. - [SDR DALA1113739874](https://openairdocs.org/sdr/DALA1113739874.md): Structure · damaged · Feb 23, 2011 · N783NC · Doug DC951 · Leading Edge Devices > ON PREFLIGHT EXTERIOR INSPECTION, FOUND AREA BETWEEN SLATS 3 AND 4 ON THE RIGHT WING BINDING/DAMAGED UNDER DIRECTION OF MC COMPLIED WITH REPAIR INSTRUCTION ERA 48992 6-14. AIRCRAFT OK FOR SERVICE. - [SDR DALA1029189874](https://openairdocs.org/sdr/DALA1029189874.md): Pan · cracked · Oct 24, 2010 · N783NC · Doug DC951 · Fuselage Miscellaneous Structure > DURING L-CHECK FOUND CRACK ON AFT CARGO PAN AT DOOR CUTOUT LOWER JAMB. REPAIRED PER DWG 5910158 & SRM 53-13-3. - [SDR DALA1029169874](https://openairdocs.org/sdr/DALA1029169874.md): Attach Angle · damaged · Oct 24, 2010 · N783NC · Doug DC951 · Fuselage, Stabilizer Attach Fittings > DURING L-CHECK FOUND SEVERAL ELONGATED FASTENER HOLES IN VERTICAL STABILIZER LT SIDE FUSELAGE TO STABILIZER ATTACH ANGLE. REPAIRED PER SRM 55-31-0 FIGURE 1 SHEET 2, SRM 51-60-0 FIGURE 1 SHEET 1, SRM 55-01 FIGURE 4 & SRM 51-30-01 PAGE 127, - [SDR DALA1029159874](https://openairdocs.org/sdr/DALA1029159874.md): Skin · cracked · Oct 24, 2010 · N783NC · Doug DC951 · Fuselage Main, Plate/Skin > DURING L-CHECK FOUND CRACK IN FUSELAGE SKIN AT BS 1247 L2L. REPAIRED PER SRM 53-04 FIGURE 38. - [SDR DALA1028569874](https://openairdocs.org/sdr/DALA1028569874.md): Pan · corroded · Oct 24, 2010 · N783NC · Doug DC951 · Fuselage Miscellaneous Structure > DURING L-CHECK FOUND CORROSION ON DOOR PAN OF FORWARD CARGO COMPARTMENT DOOR CUTOUT LOWER JAMB. REPAIRED PER SRM 53-01 FIGURE 1 & SRM 53-05 FIGURE 44. - [SDR DALA1028549874](https://openairdocs.org/sdr/DALA1028549874.md): Gusset · damaged · Oct 24, 2010 · N783NC · Doug DC951 · Fuselage Miscellaneous Structure > DURING L-CHECK FOUND SEVERAL ELONGATED FASTENER HOLES ON GUSSET AT BS 1247 L2L. REPAIRED PER SRM 51-30-2, SRM 51-30-5 & DWG 5911432. - [SDR DALA1028529874](https://openairdocs.org/sdr/DALA1028529874.md): Attach Fitting · damaged · Oct 24, 2010 · N783NC · Doug DC951 · Vertical Stabilizer, Attach Fittings > DURING L-CHECK FOUND DRILLED HOLE ON LT ON VERTICAL TO FUSELAGE SKIN ATTACH DOUBLER AT BS 1275. REPAIRED PER ERA 486780-14. - [SDR DALA1028559874](https://openairdocs.org/sdr/DALA1028559874.md): Skin · bent · Oct 23, 2010 · N783NC · Doug DC951 · Fuselage Main, Plate/Skin > DURING L-CHECK FOUND SKIN BENT AT AFT CARGO DOOR CUTOUT PREVIOUS REPAIR AT BS 1100 BETWEEN L23R AND L 26R. REPAIRED PER SRM 53-30-0 FIGURE 3, SRM 51-10-2, SRM 51-10-04, SRM 51-30-2 & SRM 51-10-3 PAGE 239. - [SDR DALA1028539874](https://openairdocs.org/sdr/DALA1028539874.md): Attach Fitting · cracked · Oct 23, 2010 · N783NC · Doug DC951 · Fuselage, Stabilizer Attach Fittings > DURING L-CHECK FOUND CRACK IN VERTICAL STABILIZER RIGHT ATTACH ANGLE APPROXIMATELY.25 INCH FROM TRAILING EDGE. REPAIRED 53-05 FIGURE 23 & SRM 51-10-3B. - [SDR DALA1030509874](https://openairdocs.org/sdr/DALA1030509874.md): Skin · cracked · Oct 22, 2010 · N783NC · Doug DC951 · Fuselage Main, Plate/Skin > DURING LCK AT DHN, WHILE ACCOMPLISHING AN AD RELATED INSPECTION PER EM5330-01142, AD2000-23-22, A 0.25 INCH LONG CRACK WAS FOUND ON THE AFT EDGE OF THE NR 1 DOOR STOP HOLE REPAIRED PER ERA 486585-14AD SECTION I, SECTION II - ON OR BEFORE 3,000 CYCLES OR 24 MON - [SDR DALA1098742840](https://openairdocs.org/sdr/DALA1098742840.md): Frame · cracked · Oct 21, 2010 · N783NC · Doug DC951 · Fuselage Main, Frame > DURING M-CHECK FOUND CRACK IN FUSELAGE EXTERIOR CANTED FRAME AT BS 1303 BETWEEN L14L & L15L. REPAIRED PER SRM 53-01 FIGURE 9 SHEET 4. - [SDR DALA1027359874](https://openairdocs.org/sdr/DALA1027359874.md): Intercostal · cracked · Oct 19, 2010 · N783NC · Doug DC951 · Fuselage Miscellaneous Structure > DURING L-CHECK FOUND CRACK AND CORROSION ON AFT CARGO DOOR JAMB FORWARD INTERCOSTAL BELOW WEB. REPAIRED PER SRM 51-30-2, SRM 51-30-5 & DWG 5910158. - [SDR DALA1028579874](https://openairdocs.org/sdr/DALA1028579874.md): Web · corroded · Oct 16, 2010 · N783NC · Doug DC951 · Fuselage Miscellaneous Structure > DURING L-CHECK FOUND CORROSION ON LOWER WEB OF FORWARD CARGO DOOR CUTOUT. REPAIRED PER SRM 51-10-4, SRM 51-30-2, SRM 51-30-5 & SRM 51-30-3. - [SDR DALA1028589874](https://openairdocs.org/sdr/DALA1028589874.md): Web · corroded · Oct 15, 2010 · N783NC · Doug DC951 · Fuselage Miscellaneous Structure > DURING L-CHECK FOUND CORROSION ON LOWER WEB OF AFT CARGO COMPARTMENT DOOR JAMB. REPAIRED PER SRM 53-13-2 FIGURE 3 SHEET 3 ITEM 6. - [SDR DALA1029179874](https://openairdocs.org/sdr/DALA1029179874.md): Step · corroded · Oct 11, 2010 · N783NC · Doug DC951 · Entrance Stairs > DURING L-CHECK FOUND CORROSION ON AIR STAIR STEP NR 2. REPLACED STEP PER SRM 52-60-0. - [SDR DALA1022949874](https://openairdocs.org/sdr/DALA1022949874.md): Battery Pack · inoperative · Sep 15, 2010 · N783NC · Doug DC951 · Emergency Lighting > DURING LINE CHECK, MX FOUND THAT THE EMERGENCY EXIT SIGN AT THE MAIN CABIN DOOR WAS INOPERATIVE. MX REPLACED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPS CONDITION. - [SDR DALA1022939874](https://openairdocs.org/sdr/DALA1022939874.md): Battery Pack · inoperative · Sep 15, 2010 · N783NC · Doug DC951 · Emergency Lighting > DURING LINE CHECK, MX FOUND THAT THE EMERGENCY EXIT SIGN AT THE AFT BULKHEAD EMERGENCY EXIT DOOR WAS INOPERATIVE. MX REPLACED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPS CONDITION. - [SDR DALA1014939874](https://openairdocs.org/sdr/DALA1014939874.md): Power Supply · inoperative · Jun 25, 2010 · N783NC · Doug DC951 · Emergency Lighting > DURING LINE CHECK, MX FOUND EMERGENCY LIGHTS AT ROW 9 TO 13 INOP. MX REPLACED POWER SUPPLY AND OVER WING LIGHT ASSY IAW MM 33-50-01. OPS CHECK OF LIGHTS, NOW CHECK GOOD. - [SDR DALA108399874](https://openairdocs.org/sdr/DALA108399874.md): Battery Pack · inoperative · Apr 22, 2010 · N783NC · Doug DC951 · Emergency Lighting > DURING A LINE CHECK FOUND TAIL COMPARTMENT EMERGENCY LIGHTS INOP. CHANGED BATTERY, FUSE, POWER SUPPLY AND REPAIRED WIRING HARNESS IN TAIL COMPARTMENT CATWALK. OPS CHECK OF EMERGENCY LIGHTS NOW CHECK NORMAL. - [SDR DALA108389874](https://openairdocs.org/sdr/DALA108389874.md): Power Supply · inoperative · Apr 22, 2010 · N783NC · Doug DC951 · Emergency Lighting > DURING A LINE CHECK FOUND EMERGENCY LIGHTS ROWS 9 THRU 13 AND LT FWD OVER WING EMERGENCY LIGHTS ARE INOP. MSP MX CHANGED BAD POWER SUPPLY IAW 33-53-01. OPERATIONS OF LIGHTS NOW OK. - [SDR NWAA093509874](https://openairdocs.org/sdr/NWAA093509874.md): Battery · discharged · Oct 8, 2009 · N783NC · Doug DC951 · Emergency Lighting > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 23-26 AND THE LEFT SIDE EMERGENCY EXIT SIGN WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. OPERATIONAL CHECK WAS GOOD. - [SDR NWAA093189874](https://openairdocs.org/sdr/NWAA093189874.md): Seal · blown · Sep 9, 2009 · N783NC · Doug DC951 · Engine Fuel Distribution > DURING CLIMB AT APPROX 800FT ENGINE NR 2 FLAMED OUT. FLIGHT CREW RETURNED AIRCRAFT TO DEPARTURE AIRPORT PERFORMING AN UNEVENTFUL LANDING. MAINTENANCE FOUND BLOWN SEALS AT THE FUEL IN LINE TO THE P&D VALVE. - [SDR NWAA092119874](https://openairdocs.org/sdr/NWAA092119874.md): Skin · damaged · May 27, 2009 · N783NC · Doug DC951 · Fuselage Main, Plate/Skin > DURING GROUND OPERATIONS LT FUSELAGE SKIN WAS DAMAGED BETWEEN BS 446-BS 503 L25L AND L28L. REPAIRED PER EA 98-215559. - [SDR NWAA09949874](https://openairdocs.org/sdr/NWAA09949874.md): Power Supply · inoperative · Mar 25, 2009 · N783NC · Doug DC951 · Emergency Lighting > DURING LINE CHECK, MX FOUND THAT THE EMERGENCY FLOOD LIGHT FOR THE AFT EVACUATION SLIDE WAS NOT FUNCTIONAL. MX REPLACED THE EMERGENCY LIGHT POWER SUPPLY AND OPERATIONALLY CHECKED THE SYSTEM. (K) - [SDR NWAA09389874](https://openairdocs.org/sdr/NWAA09389874.md): Wire · shorted · Jan 29, 2009 · N783NC · Doug DC951 · Light System Wiring > DURING LINE CHECK, MX FOUND THAT BOTH OF THE EXTERIOR EMERGENCY OVERWING EMERGENCY FLOOD LIGHTS WERE INOPERATIVE. MX FOUND A SHORTED WIRE AT THE OVERWING EMERGENCY LIGHT AND REPAIRED IT. ALSO, REPLACED BATTERY PACK B5-49. (K) - [SDR NWAA09269874](https://openairdocs.org/sdr/NWAA09269874.md): Floorbeam · cracked · Jan 28, 2009 · N783NC · Doug DC951 · Fuselage Main, Floor Beam > DURING LINE CHECK FOUND WEAK SPOT IN FLOOR BETWEEN SEAT 4B AND 4C. FOUND CRACK IN THE FLOOR SUPPORT T-CAP AT BS 427. REPAIRED PER EA 98-215295. (K) - [SDR NWAA083469874](https://openairdocs.org/sdr/NWAA083469874.md): Crank Assy · worn · Jul 27, 2008 · N783NC · Doug DC951 · Aileron Control System > FLIGHT RETURNED TO DTW AFTER TAKEOFF DUE TO UNRESPONSIVE OR SLOW TO RESPOND FLIGHT CONTROLS (AILERONS). CREW NOTICED 2 TO 3 INCHES OF YOKE TRAVEL BEFORE ANY FLIGHT CONTROL INPUT RESULTED IN AIRCRAFT CONTROL. PER DISPATCH REPORT MAINTENANCE CONTROL WAS CONTAC - [SDR 0601099874](https://openairdocs.org/sdr/0601099874.md): Tire · separated · May 27, 2006 · N783NC · Doug DC951 · Tire > AT 125KTS ON THE TAKEOFF ROLL THE CREW HEARD A LOUD BANG AS THE NR 1 TIRE BLEW AND SHREDDED IT`S RECAP. THE TAKEOFF WAS SAFELY ABORTED WITH THE AIRCRAFT REMAINING ON RUNWAY CENTERLINE. AFTER THE AIRCRAFT WAS TOWED TO THE GATE, MAINTENANCE FOUND FOD IN THE NR - [SDR 0600639874](https://openairdocs.org/sdr/0600639874.md): Doubler · corroded · Mar 3, 2006 · N783NC · Doug DC951 · Fuselage Main, Structure > DURING "H" CHECK, FOUND CORROSION ON THE FORWARD FUSELAGE LT KIDNEY PANEL CUTOUT DOUBLER ON INTERIOR SIDE. REPAIRED PER EA 98-199178. - [SDR 0400859874](https://openairdocs.org/sdr/0400859874.md): Warning Light · illuminated · May 17, 2004 · N783NC · Doug DC951 · Leading Edge Slat Control System > DURING SLAT EXTENSION FOR LANDING AT BUF, THE AIRCRAFT ROLLED WITH BOTH THE SLAT DISAGREEMENT AND SLAT EXTEND LIGHTS ILLUMINATED. COMPLIED WITH COM PROCEDURES AND FIRST OFFICER WENT BACK TO VISUALLY CHECK THAT BOTH SLATS WERE EXTENDED PRIOR TO LANDING. THE SLA - [SDR 0400789874](https://openairdocs.org/sdr/0400789874.md): Duct · damaged · May 15, 2004 · N783NC · Doug DC951 · Leading Edge Slat Control System > DURING SLAT EXTENSION ON APPROACH, THE AIRCRAFT ROLLED RIGHT WITH THE SLAT DISAGREEMENT LIGHT ILLUMINATED. INITIATED COM PROCEDURES WHEN CREW HEARD A THUD AND THE LIGHT EXTINGUISHED. LANDING AT MSP WAS NORMAL. MAINTENANCE REPLACED THE T-DUCT, O-RINGS, SLIDE - [SDR 0100609874](https://openairdocs.org/sdr/0100609874.md): Duct · binding · Feb 17, 2001 · N783NC · Doug DC951 · Leading Edge Slat Position Indicating System > DURING APPROACH, THE SLAT DISAGREEMENT LIGHT ILLUMINATED AND AIRCRAFT HAD A NOTICEABLE ROLL THE THE RIGHT WHEN SLATS EXTENDED. FOLLOWED COM PROCEDURES. FLAP/SLAT HANDLE WAS SPLIT. FLIGHT MADE AN UNEVENTFUL LANDING AT MSP. MAINTENANCE INSPECTION OF SLATS DE - [SDR 0003369874](https://openairdocs.org/sdr/0003369874.md): Drain Valve · clogged · Sep 3, 2000 · N783NC · Doug DC951 · Aileron Control System > ROLL CONTROL RESTRICTED IN FLIGHT IN BOTH AUTOPILOT AND MANUAL. THE FLIGHT CREW PERFORMED ROLL CONTROL RESTRICTION COM PROCEDURE. DESCENDED TO WARMER TEMPERATURES AND PROBLEM CLEARED. FLIGHT LANDED AT DESTINATION WITHOUT INCIDENT. MAINTENANCE REPLACED THE - [SDR 0001459874](https://openairdocs.org/sdr/0001459874.md): Check Valve · clogged · Apr 22, 2000 · N783NC · Doug DC951 · Autopilot System > EN ROUTE FROM BDL TO DTW, THE AIRCRAFT BEGAN AN UNCOMMANDED GRADUAL BANK. DISCONNECTED AUTOPILOT AND FOLLOWED COM PROCEDURES. REGAINED COMPLETE FREEDOM OF MOVEMENT OF CONTROLS PRIOR TO APPROACH AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND CHECK VALVE FOR - [SDR 9904249874](https://openairdocs.org/sdr/9904249874.md): Batteries · discharged · Oct 6, 1999 · N783NC · Doug DC951 · Emergency Lighting > DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL. - [SDR 9901859874](https://openairdocs.org/sdr/9901859874.md): Seal · leaking · Jun 1, 1999 · N783NC · Doug DC951 · Pneumatic Distribution System > AFTER TAKEOFF, THE TAIL COMPARTMENT HIGH TEMPERATURE INDICATOR LIGHT ILLUMINATED WITH POWER SET AT CLIMB AND AT TAKEOFF EPR. INDICATION EXTINGUISHED AT LOWER POWER SETTING. FLIGHT CREW DECLARED YELLOW EMERGENCY, RETURNED TO ATL AND LANDED WITHOUT INCIDENT. - [SDR 9808309874](https://openairdocs.org/sdr/9808309874.md): Battery · inoperative · May 5, 1998 · N783NC · Doug DC951 · Emergency Lighting > DURING LINE CHECK, FOUND EMERGENCY LIGHTING IN TAIL COMPARTMENT VERY DIM. MAINTENANCE REPLACED BATTERIES, OPERATIONAL CHECK NORMAL. - [SDR 9802799874](https://openairdocs.org/sdr/9802799874.md): Adc · failed · Feb 17, 1998 · N783NC · Doug DC951 · Air Data Computer > DURING CLIMBOUT, THE FIRST OFFICER'S ALTIMETER OFF FLAG AND THE ALTITUDE ALERTER OFF FLAG CAME INTO VIEW. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE AIR DATA COMPUTER AND ALTITUDE ALERTER INDICATOR, OPERATIONAL CHECK OK. - [SDR 9801929874](https://openairdocs.org/sdr/9801929874.md): Batteries · discharged · Jan 29, 1998 · N783NC · Doug DC951 · Emergency Lighting > DURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD MOUNTED CENTER AISLE EMERGENCY LIGHTS BETWEEN ROWS 21 THROUGH 23 WOULD NOT TEST. REPLACED BATTERIES. OPERATIONAL CHECK NORMAL. - [SDR 9713969874](https://openairdocs.org/sdr/9713969874.md): Turbine · damaged blades · Jul 21, 1997 · N783NC · Doug DC951 · Turbine Section > DURING TAXI OUT, THE RIGHT ENGINE WAS REPORTED BY A FOLLOWING AIRCRAFT TO HAVE SPARKS EXITING THE TAIL OF THE ENGINE. CREW SHUTDOWN THE RIGHT ENGINE AND RETURNED TO GATE. MAINTENANCE REPLACED THE RIGHT ENGINE. ENGINE OPERATIONAL CHECK OK. AIRCRAFT RETURNE - [SDR 9707399874](https://openairdocs.org/sdr/9707399874.md): Tcas Computer · failed · Apr 9, 1997 · N783NC · Doug DC951 · Air Collision Avoidance System > AFTER TAKEOFF, CAPTAIN'S GYRO FLAG APPEARED AND GYRO TUMBLED. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED TCAS COMPUTER. TCAS AND ATTITUDE OPERATION CHECKED OK. - [SDR 9706479874](https://openairdocs.org/sdr/9706479874.md): Oil Press Trans · malfunctioned · Mar 27, 1997 · N783NC · Doug DC951 · Engine Oil Pressure > DURING CRUISE FLIGHT, THE RIGHT ENGINE OIL PRESSURE INDICATION DECREASED TO 32 PSI. AIRCRAFT DIVERTED TO ATL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT ENGINE OIL PRESSURE TRANSMITTER. OPERATIONAL CHECK OK. - [SDR 9706299874](https://openairdocs.org/sdr/9706299874.md): Battery Pack · discharged · Mar 25, 1997 · N783NC · Doug DC951 · Emergency Lighting > DURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT EMERGENCY LIGHTS DIM. REPLACED BATTERY PACK AND CLEANED CONTACTS, OPERATIONAL CHECK NORMAL. - [SDR 9708049874](https://openairdocs.org/sdr/9708049874.md): Pressure Panel · cracked · Mar 17, 1997 · N783NC · Doug DC951 · Fuselage Miscellaneous Structure > DURING H-CHECK, FOUND CRACK IN NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE PANEL AT FRAME FITTING, LEFT SIDE, FS 83. REPAIRED PER EA 98-111877. - [SDR 9627309874](https://openairdocs.org/sdr/9627309874.md): Power Pack · inoperative · Dec 31, 1996 · N783NC · Doug DC951 · Emergency Lighting > DURING LINE CHECK, FOUND TAIL COMPARTMENT EMERGENCY LIGHT INOPERATIVE. REPLACED AFT POWERPACK IN RIGHT LAV CEILING, OPERATIONAL CHECK OK. - [SDR 9625059874](https://openairdocs.org/sdr/9625059874.md): Batteries · discharged · Nov 18, 1996 · N783NC · Doug DC951 · Emergency Lighting > DURING LINE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE AT ROW 16 EXIT SIGN FOR OVERWING DOOR. REPLACED BATTERIES AND OPERATIONAL CHECKS GOOD. - [SDR 9612209874](https://openairdocs.org/sdr/9612209874.md): Alignment Blocks · out of position · May 29, 1996 · N783NC · Doug DC951 · Leading Edge Slat Control System > DURING DESCENT INTO GRR, SLAT DISAGREEMENT LIGHT ILLUMINATED. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. FOUND RIGHT LEADING EDGE SLAT T-DUCT ALIGNMENT BLOCKS BINDING ON TELESCOPIC TUBE. REPOSITIONED UPPER AND LOWER BLOCKS AND CYCLED SLATS NUMEROUS - [SDR 9607649874](https://openairdocs.org/sdr/9607649874.md): Battery Pack · discharged · Apr 2, 1996 · N783NC · Doug DC951 · Emergency Lighting > DURING LINE CHECK, FOUND AFT WALKWAY EMERGENCY LIGHTS OUT. RESEATED BULBS AND REPLACED THE BATTERY PACK, OPERATIONAL CHECK GOOD. Next page: https://openairdocs.org/deregistered/N783NC-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 = 'N783NC' AND deregistration_id = 'N783NC-2018-12-06' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N783NC-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.