# Service difficulty reports: N765NC, cancelled Dec 6, 2018 A list on [N765NC, cancelled Dec 6, 2018](https://openairdocs.org/deregistered/N765NC-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 · 67 reports - [SDR DALA1149559856](https://openairdocs.org/sdr/DALA1149559856.md): Fuse · blown · Aug 20, 2011 · N765NC · Doug DC951 · Emergency Lighting > MAINTENANCE FOUND ROWS 1 THROUGH 4 EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE FUSE AT THE SERVICE DOOR POWER SUPPLY PER AMM AND WPM. OPERATIONAL CHECK WAS OK. - [SDR DALA1132769856](https://openairdocs.org/sdr/DALA1132769856.md): Battery Pack · discharged · Apr 29, 2011 · N765NC · Doug DC951 · Emergency Lighting > ON PREFLIGHT, FOUND EMERGENCY LIGHTS ILLUMINATED WITH SWITCH IN THE EMERGENCY LIGHTS ARM POSITION. ASSOCIATED CIRCUIT BREAKERS WERE POPPED ON OVERHEAD PANEL. MX REMOVED AND REPLACED BATTERY PACKS B23 AND B24 BEHIND FWD LAV MIRROR. NO HELP. REMOVED AND REPL - [SDR DALA1126889856](https://openairdocs.org/sdr/DALA1126889856.md): Shear Tie · cracked · Apr 18, 2011 · N765NC · Doug DC951 · Fuselage Internal Mounting Structure > AFT ACCESSORY COMPARTMENT STATION 1190 JUST BELOW LONGERON 14 RIGHT FRAME SHEAR TIE CRACKED. REMOVED AND REPLACED SHEAR TIE WITH NEW SHEAR TIE P/N 9958239U12, FOUND FRAME CHAFED. CUT AND REMOVED DAMAGE SECTION OF FRAME AT L14R RE-INSTALLED NEW SECTION OF FRA - [SDR DALA1127039856](https://openairdocs.org/sdr/DALA1127039856.md): Fairing · cracked · Apr 17, 2011 · N765NC · Doug DC951 · Engine Thrust Reverser > ENGINE NR 2 LOWER T/R BUCKET OTBD FAIRING CRACKED. STOP DRILLED CRACK, FABRICATED DOUBLER FROM 2024T3.050 PO NR 1130701, INSTALLED DOUBLER IAW SRM 54-01, F2, P106 17APR11. REQUIRED INSP COMPLETED. - [SDR DALA1125579856](https://openairdocs.org/sdr/DALA1125579856.md): Skin · cracked · Apr 12, 2011 · N765NC · Doug DC951 · Fuselage Main, Plate/Skin > FUSELAGE EXTERIOR, STA 1303, L15L, SKIN IS CRACKED. GAINED ACCESS TO SKIN CRACK. CUT OUT CRACKED SKIN 1"X 1". HFEC VERIFIED CRACK CONTAINMENT. FABRICATED 1EA FILLER & 1EA DOUBLER OF 040" 7075-T6 PO NR 1023415. ALODINED, PRIMED AND INSTALLED DOUBLER & FILL - [SDR DALA1125109856](https://openairdocs.org/sdr/DALA1125109856.md): Channel · broken · Apr 10, 2011 · N765NC · Doug DC951 · Fuselage Floor Panel > MAIN CABIN FLOOR PANEL 60-C HAS 4EA HAT CHANNELS BROKEN OUT FROM PANEL. REMOVED HATS FROM SKIN, REMOVED CORR FROM SKIN IAW SRM 51-10-3 ORIG MAT.025" REMOVED.010" FOUND TO BE OUT OF LIMITS IAW SRM 53-01 FIG 1. FABBED NEW SKIN.025" 7075-T6 AND HATS P/N S291 - [SDR DALA1125069856](https://openairdocs.org/sdr/DALA1125069856.md): Floor Panel · corroded · Apr 10, 2011 · N765NC · Doug DC951 · Fuselage Floor Panel > FLIGHT DECK METAL SKIN FLOOR PANEL 14B HAS CORROSION. CPCP TASK 46-53303. REMOVED CORR FROM FLOOR PANEL. ORIG MAT.025" LOSS.010".015 REMAINING. FOUND TO BE OUT OF LIMITS IAW SRM 53-01 FIG 1. REPLACED SKIN AND HAT CHANNELS.025 7075-T6 AND P/N 1120080 A - [SDR DALA1125059856](https://openairdocs.org/sdr/DALA1125059856.md): Floor Panel · corroded · Apr 10, 2011 · N765NC · Doug DC951 · Fuselage Floor Panel > MAIN CABIN FLOOR PANEL 21 HAS CORROSION SPOTS ON TOP SKIN SIDE FROM FWD END TO AFT END OF PANEL FLOOR PANEL HAS 100 PERCENT MAT LOSS, OUT OF LIMITS IAW SRM 53-01 FIG 1. FABBED NEW SKIN.032" 7075-T6 AND NEW HAT CHANNEL P/N S2912282. INSTALLED NEW SKIN AND HA - [SDR DALA1125099856](https://openairdocs.org/sdr/DALA1125099856.md): Support Channel · cracked · Apr 8, 2011 · N765NC · Doug DC951 · Fuselage Miscellaneous Structure > NOSE WHEEL WELL STA 37 RBL 6 SUPPORT CHANNEL CRACKED AT FASTENER. REMOVED CRACKED SUPPORT ANGLE FROM NOSE WHEEL WELL STA 37 RBL 6 IAW DC9 SRM 51-30-2. FABRICATED NEW ANGLE FROM.050 2024-T IAW DC9 SRM 53-13-1 AND DC9 SRM 51-10-2 & 51-10-4. TREATED AND PRIME - [SDR DALA1125559856](https://openairdocs.org/sdr/DALA1125559856.md): Frame · cracked · Apr 6, 2011 · N765NC · Doug DC951 · Fuselage Main, Frame > AFT ACCESSORY COMPARMENT, L4L, CANTED FRAME CRACKED BS 1245. R & R CANTED FRAME 1245 PN 09-5300-3-0606IAW SRM 51-30-5 & 51-30-2. REQUIRED INSP COMPLETED. - [SDR DALA1112719856](https://openairdocs.org/sdr/DALA1112719856.md): Light · inoperative · Feb 18, 2011 · N765NC · Doug DC951 · Emergency Lighting > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING FOR THE CATWALK IN THE TAIL COMPARTMENT AND THE TAIL SLIDE LIGHT WERE INOPERATIVE. MAINTENANCE REPLACED THE CATWALK LIGHT ASSEMBLIES AND INSTALLED THE PROPER BULBS IN THE SLIDE FLOOD LIG - [SDR DALA1035489855](https://openairdocs.org/sdr/DALA1035489855.md): Angle · cracked · Nov 23, 2010 · N765NC · Doug DC951 · Fuselage Miscellaneous Structure > DURING M-CHECK, FOUND BS 110, BULKHEAD LBL4, 7 IN ABOVE BELLY ANGLE CRACKED. REMOVED CRACKED ANGLE IAW SRM 51-30-2. FABRICATED NEW ANGLE IAW DWG 9915600. TREATED AND PRIMED ANGLE IAW SRM 51-10-3. INSTALLED NEW ANGLE IAW SRM 51-30-5. - [SDR DALA1035499855](https://openairdocs.org/sdr/DALA1035499855.md): Strut · cracked · Nov 22, 2010 · N765NC · Doug DC951 · Fuselage Main, Structure > DURING M-CHECK, FOUND BS 560 RT STRUT CRACKED AT LOWER END. REMOVED FASTENERS IAW SRM 51-30-2, STOP DRILLED CRACK IAW SRM 53-01, FIG 2, FABRICATED REPAIR DOUBLER IAW SRM 51-10-2 & 53-01 FIG 2. LOCATED,DRILLED & DEBURRED IAW SRM 51-10-4 INSTALLED REPAIR DOUBL - [SDR DALA1035479855](https://openairdocs.org/sdr/DALA1035479855.md): Floor Panel · corroded · Nov 14, 2010 · N765NC · Doug DC951 · Fuselage Floor Panel > DURING M-CHECK, FOUND COCKPIT FLOOR PANEL NR15 HAS CORROSION. REMOVED CORROSION, ORIGINAL THICKNESS WAS.020. REMOVED.005 OUT OF LIMITS IAW SRM 53- 01 FIG.1. RECEIVED NEW PANEL DRILLED IAW SRM 51-10-4. TRANSFERRED ATTACH BRACKETS FROM OLD PANEL TO NEW PANE - [SDR DALA1035469855](https://openairdocs.org/sdr/DALA1035469855.md): Seat Track · broken · Nov 12, 2010 · N765NC · Doug DC951 · Fuselage, Seat/Cargo Attach Fittings > DURING M-CHECK FOUND MAIN CABIN FS 597 LBL 45 SEAT TRACK LUGS ARE BROKEN. R & R LBL 45, SEAT TRACK STA 570-654 LOCATED DRILLED AND INSTALLED SPLICE ACA7413-505 & SPLICE PLATE ACA7414-3 IAW SRM 51-30-2,51-30-5 53-23-0 FIG 4, 51-10-4, 53-05, FIG 4F 51-10-3, 51- - [SDR DALA1035459855](https://openairdocs.org/sdr/DALA1035459855.md): Seat Track · gouged · Nov 12, 2010 · N765NC · Doug DC951 · Fuselage, Seat/Cargo Attach Fittings > DURING M-CHECK FOUND MAN CABIN FS 891 RBL 24 SEAT TRACK LUG IS GOUGED OUT OF LIMITS. REMOVED SEAT TRACK FACTORY SPLICE STA 842 RBL 24 AND CUT AT BS 936.5, RBL 24 RECEIVED NEW TRACK AND SPLICE,TRIMMED LOCATED, DRILLED, DEBURRED, TREATED AND PRIMED IAW SRM 53- - [SDR DALA1032059856](https://openairdocs.org/sdr/DALA1032059856.md): Support · gouged · Nov 12, 2010 · N765NC · Doug DC951 · Fuselage, Landing Gear Attach Fittings > DURING LINE CHECK FOUND NOSE GEAR SUPPORT WEB LT DAMAGED (GOUGED). PERFORMED PERMANENT REPAIR PER ERA 487318-14 REVISION ORIGINAL. INSTALLED REPAIR PARTS PER SRM 53-05 FIG 36. - [SDR DALA1025739856](https://openairdocs.org/sdr/DALA1025739856.md): Panel · delaminated · Oct 6, 2010 · N765NC · Doug DC951 · Spoilers > DURING LINE CHECK FOUND DELAMINATION ON LT WING OTBD SPOILER PANEL. REPLACED SPOILER PANEL IAW AMM 21-61-01-401 AND CARD 2760-9901M-LO. - [SDR DALA1020579856](https://openairdocs.org/sdr/DALA1020579856.md): Battery Pack · inoperative · Aug 26, 2010 · N765NC · Doug DC951 · Emergency Lighting > DURING LINE CHECK, MX FOUND LT AND RT AUX EMERGENCY EXIT LIGHTS INOP. MX REPLACED BATTERIES IN POWER SUPPLY B5-25 REF WDM 33-51-01. OPERATION OF LIGHTS NOW CHECK GOOD. - [SDR DALA1020569856](https://openairdocs.org/sdr/DALA1020569856.md): Battery Pack · inoperative · Aug 26, 2010 · N765NC · Doug DC951 · Emergency Lighting > DURING LINE CHECK MX FOUND FIRST CLASS CEILING EMERGENCY LIGHTS INOP. MX REPLACED BATTERIES IN POWER SUPPLY B5-24 REF WDM 33-51-01. OPERATION OF LIGHTS NOW CHECK GOOD. - [SDR DALA1017569856](https://openairdocs.org/sdr/DALA1017569856.md): Splice · corroded · Jul 26, 2010 · N765NC · Doug DC951 · Emergency Lighting > DURING LINE CHECK, MAINTENANCE FOUND THAT THE FORWARD AND MIDDLE OF THE EMERGENCY PATHWAY LIGHTS FOR THE CATWALK IN THE TAIL COMPARTMENT WERE INOPERATIVE. MAINTENANCE FOUND THE CATWALK AFT SPLICE PACK WERE CORRODED AND REPLACED THEM BOTH. - [SDR DALA108879856](https://openairdocs.org/sdr/DALA108879856.md): Battery · discharged · Apr 27, 2010 · N765NC · Doug DC951 · Emergency Lighting > INBOUND CREW WROTE LEFT AFT OVERWING EMERGENCY EXIT SIGN LIGHT OUT. SET EMERGENCY EXIT LIGHTS TO ARM TO CHARGE BATTERIES FOR 20 MINUTES. LIGHT NOW CHECKS OK. - [SDR DALA107589856](https://openairdocs.org/sdr/DALA107589856.md): Wire · broken · Apr 9, 2010 · N765NC · Doug DC951 · Light System Wiring > ON FLIGHT CHECK MX FOUND SEAT 26D EMERGENCY PATH LIGHT INOP. REPAIRED BROKEN WIRE IAW AMDS 33-51-04. OPS CHECK OF LIGHT IS NOW GOOD. - [SDR DALA105409856](https://openairdocs.org/sdr/DALA105409856.md): Power Supply · inoperative · Mar 10, 2010 · N765NC · Doug DC951 · Emergency Lighting > DURING LINE CHECK, MAINTENANCE FOUND THAT THE RIGHT SIDE LOWER OVERWING EMERGENCY EXIT SIGN WAS INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND THE LIGHT RETURNED TO AN OPERATIONAL CONDITION. - [SDR DALA105419856](https://openairdocs.org/sdr/DALA105419856.md): Power Supply · inoperative · Mar 10, 2010 · N765NC · Doug DC951 · Emergency Lighting > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 5-8 OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION. - [SDR NWAA093049856](https://openairdocs.org/sdr/NWAA093049856.md): Socket · dirty · Aug 28, 2009 · N765NC · Doug DC951 · Emergency Lighting > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE VENTRAL STAIRWAY WERE INOPERATIVE. MAINTENANCE FOUND THE STAIRS LIGHT SOCKETS WERE COMPROMISED AND CLEANED THEM. SUBSEQUENT FUNCTIONAL CHECKS WERE GOOD. - [SDR NWAA09449856](https://openairdocs.org/sdr/NWAA09449856.md): Unknown · leaking · Feb 13, 2009 · N765NC · Doug DC951 · Engine Fuel Distribution > DURING ROTATION AND CLIMB ENGINE NR1 FUEL FLOW WAS ERRATIC AND EPR DROPPED ABOUT 10 PERCENT. ADVANCED THROTTLE TO MATCH ENGINE NR2 BUT EPR DROPPED AGAIN TO 1.6 AND WOULD NOT RESPOND TO HIGHER THROTTLE SETTINGS. FLIGHT CREW RETURNED ACFT TO DEPARTURE AIRPORT. - [SDR NWAA074309856](https://openairdocs.org/sdr/NWAA074309856.md): Support Angle · cracked · Dec 26, 2007 · N765NC · Doug DC951 · Fuselage Miscellaneous Structure > DURING "L" CHECK, FOUND CRACK IN THE FORWARD FLANGE OF BULKHEAD SUPPORT ANGLE AT BS 851. REPAIRED PER EA 98-211053. - [SDR 0500809856](https://openairdocs.org/sdr/0500809856.md): Pump · leaking · Jun 1, 2005 · N765NC · Doug DC951 · Hydraulic Pump (Electric/Engine), Main > AFTER ACFT LEVELLED OFF AT FL 290, PILOT NOTICED DROP IN RT HYDRAULIC SYSTEM QUANTITY FROM 6 QTS TO 4 QTS. QUANTITY CONTINUED TO SLOWLY DECREASE AND WHEN REACHED 2 QTS COM PROCEDURES WERE COMPLIED WITH. CREW REQUESTED LONGEST RUNWAY. GEAR EXTENSION NORMAL BU - [SDR 0500749856](https://openairdocs.org/sdr/0500749856.md): Coalescer Bag · odor · May 12, 2005 · N765NC · Doug DC951 · Humidity Control System > SOON AFTER TAKEOFF, BOTH THE LEFT AND RIGHT AIR CONDITION SUPPLY TEMP HIGH LIGHTS ILLUMINATED. AT ABOUT THE SAME TIME THE FLIGHT ATTENDANT REPORTED VISIBLE SMOKE IN THE CABIN. THE CREW COMPLIED WITH COM PROCEDURES, RETURNED TO MSP, AND MADE AN UNEVENTFUL BUT - [SDR 0203289856](https://openairdocs.org/sdr/0203289856.md): Floor Panel · cracked · Aug 30, 2002 · N765NC · Doug DC951 · Fuselage Miscellaneous Structure > During Mck in ATL, the galley floor panel was found with a soft condition and a 4 inch crack in the aft floor panel web edge. Repaired per EA 98-190673. - [SDR 0203279856](https://openairdocs.org/sdr/0203279856.md): Skin · cracked · Aug 29, 2002 · N765NC · Doug DC951 · Fuselage Main, Plate/Skin > During Mck in ATL, a.5" skin crack was found at station 1135, 1 inch below L17. Also a dent was found at Sta 1135. Repaired per EA 98-190648. - [SDR 0203259856](https://openairdocs.org/sdr/0203259856.md): Bulkhead · cracked · Aug 2, 2002 · N765NC · Doug DC951 · Fuselage Main, Structure > During Mck in ATL, a 2" crack was found in the flight compartment horizontal pressure panel at station 105 X=35. Repaired per EA. 98-190618. - [SDR 0202399856](https://openairdocs.org/sdr/0202399856.md): Pump · failed · Jul 21, 2002 · N765NC · Doug DC951 · Engine Fuel Pump > DURING AIRCRAFT ROTATION FOR FLIGHT, THE RIGHT ENGINE EXPERIENCED A FLAME-OUT. AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE RIGHT ENGINE FUEL PUMP. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. - [SDR 0200049876](https://openairdocs.org/sdr/0200049876.md): Duct · lack of lube · Jan 5, 2002 · N765NC · Doug DC951 · Leading Edge Slat Control System > ON SLAT EXTENSION, THE AIRCRAFT ROLLED RIGHT ACCOMPANIED BY THE AMBER SLAT DISAGREEMENT AND BLUE SLAT EXTEND LIGHT DID NOT ILLUMINATE. THE CREW ACCOMPLISHED COM PROCEDURES AND LANDED WITHOUT SLATS UNEVENTFULLY. MAINTENANCE LUBRICATED THE RIGHT T-DUCT. OPERA - [SDR 0104849856](https://openairdocs.org/sdr/0104849856.md): Web · cracked · Nov 30, 2001 · N765NC · Doug DC951 · Nacelle/Pylon, Main Frame > During Line check in ATL, the LH pylon closure rib at STA yn164 was found cracked at the lightening hole lower edge. Repaired per EA 98-185355. - [SDR 0001809856](https://openairdocs.org/sdr/0001809856.md): Valve · failed · May 6, 2000 · N765NC · Doug DC951 · Leading Edge Slat Control System > DURING APPROACH INTO MSP UPON SLAT EXTENSION, THE AIRCRAFT ROLLED TO THE RIGHT. SLAT DISAGREEMENT LIGHT ILLUMINATED AND NO SLAT EXTEND INDICATION. PERFORMED COM PROCEDURES AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE HYDRAULIC SLAT VALVE BYPASSING IN - [SDR 0001799856](https://openairdocs.org/sdr/0001799856.md): Actuator · malfunctioned · May 5, 2000 · N765NC · Doug DC951 · Leading Edge Slat Actuator > DURING APPROACH INTO MSN UPON SLAT EXTENSION, THE AIRCRAFT ROLLED TO THE RIGHT. SLAT DISAGREEMENT LIGHT ILLUMINATED AND NO SLAT EXTEND INDICATION. PLACED FLAP SELECTOR TO 15 DEGREES AND SLATS EXTENDED NORMALLY. MAINTENANCE FOUND NO OBVIOUS PROBLEM BUT LUBED - [SDR 9903499856](https://openairdocs.org/sdr/9903499856.md): Batteries · discharged · Aug 23, 1999 · N765NC · Doug DC951 · Emergency Lighting > DURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL. - [SDR 9809119856](https://openairdocs.org/sdr/9809119856.md): Battery · discharged · May 12, 1998 · N765NC · Doug DC951 · Emergency Lighting > DURING LINE CHECK, FOUND CABIN CEILING EMERGENCY EXIT LIGHTS INOPERATIVE AT SEAT ROWS 16 THROUGH 20. MAINTENANCE REPLACED BATTERIES IN POWER SUPPLY. OPERATIONAL CHECK NORMAL. - [SDR 9807049856](https://openairdocs.org/sdr/9807049856.md): Battery · discharged · Apr 22, 1998 · N765NC · Doug DC951 · Emergency Lighting > DURING LINE CHECK, FOUND AFT OVERWING EMERGENCY EXIT SIGN LIGHTING INOPERATIVE. MAINTENANCE REPLACED BATTERIES. OPERATIONAL CHECK NORMAL. - [SDR 9804909856](https://openairdocs.org/sdr/9804909856.md): Latch · out of adjust · Mar 22, 1998 · N765NC · Doug DC951 · Landing Gear Door Retract Section > DURING CLIMBOUT, THE LEFT MAIN LANDING GEAR UNSAFE AND DOOR OPEN LIGHTS ILLUMINATED. FLIGHT CREW FOLLOWED COM PROCEDURES, RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE ADJUSTED THE LEFT MAIN LANDING GEAR DOOR LATCH MECHANISM, OPERATIONAL CHECK OK. - [SDR 9802249856](https://openairdocs.org/sdr/9802249856.md): Battery Pack · discharged · Feb 4, 1998 · N765NC · Doug DC951 · Emergency Lighting > DURING INSPECTION, THE AFT ATTENDANT EMERGENCY FLASHLIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED BATTERIES, OPERATIONAL CHECK OK. - [SDR 9720119856](https://openairdocs.org/sdr/9720119856.md): Battery · discharged · Oct 28, 1997 · N765NC · Doug DC951 · Emergency Lighting > DURING LINE CHECK, FOUND EMERGENCY CEILING LIGHTS OUT AT ROWS 10 TO 14. REPLACED EMERGENCY LIGHT BATTERIES, OPERATIONAL CHECK OK. - [SDR 9716069856](https://openairdocs.org/sdr/9716069856.md): Epr Indicator · malfunctioned · Aug 21, 1997 · N765NC · Doug DC951 · Engine Pressure Ratio (EPR) > AS TAKEOFF POWER WAS APPLIED, THE LEFT ENGINE EPR INDICATION WOULD NOT REACH TARGET EPR. MAINTENANCE REPLACED THE LEFT ENGINE EPR INDICATOR. ENGINE OPERATIONAL CHECK OK. - [SDR 9716109856](https://openairdocs.org/sdr/9716109856.md): Controller · inoperative · Aug 17, 1997 · N765NC · Doug DC951 · Cabin Pressure Controller > CABIN PRESSURE BECAME INOPERATIVE DURING CRUISE AT FL330. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURE AND CONTROLLED CABIN MANUALLY. FLIGHT DIVERTED TO STL AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE CABIN PRESSURE CONTROLLER, OPERATIONAL CHECK OK - [SDR 9703719856](https://openairdocs.org/sdr/9703719856.md): Seat Belt · out of position · Feb 21, 1997 · N765NC · Doug DC951 · Passenger Compartment Equipment > DURING CLIMB, THE AIRCRAFT WOULD NOT PRESSURIZE. AIRCRAFT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. REMOVED FLIGHT ATTENDANT SEAT BELT FROM UNDER AFT CABIN DOOR, DOOR SEAL AND FUNCTIONAL CHECK OK. - [SDR 9627369856](https://openairdocs.org/sdr/9627369856.md): Battery · discharged · Dec 28, 1996 · N765NC · Doug DC951 · Emergency Lighting > DURING LINE CHECK, FOUND AFT OVERWING EMERGENCY EXIT LIGHTS ABOVE DOOR DO NOT LIGHT. REPLACED BATTERIES IN PACK 85-25, OPERATION CHECKS GOOD. - [SDR 9625129856](https://openairdocs.org/sdr/9625129856.md): Nose Dome · malfunctioned · Nov 21, 1996 · N765NC · Doug DC951 · Engine Pressure Ratio (EPR) > AS POWER WAS APPLIED FOR TAKEOFF LEFT ENGINE EPR INDICATION WAS ABNORMALLY HIGH. CREW ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE REPLACED LEFT ENGINE NOSE DOME AND EPR TRANSMITTER. RAN ENGINES TO TAKEOFF AND PART POWER SETTINGS, ALL INDICATIONS WERE - [SDR 9622469856](https://openairdocs.org/sdr/9622469856.md): Lights · inoperative · Oct 19, 1996 · N765NC · Doug DC951 · Emergency Lighting > DURING LINE MAINTENANCE INSPECTION, FOUND AFT OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. CYCLED SWITCH SEVERAL TIMES, OPERATIONAL CHECK NORMAL. Next page: https://openairdocs.org/deregistered/N765NC-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 = 'N765NC' AND deregistration_id = 'N765NC-2018-12-06' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N765NC-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.