N785NC, cancelled May 14, 2015

Service difficulty reports · 76

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

Query with SQL
duckdb -csv -c "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 = 'N785NC' AND deregistration_id = 'N785NC-2015-05-14'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR DALA1019909876Attach Angle · crackedDURING LINE CHECK FOUND CRACK IN LT ENGINE PYLON INSP PANEL 8103 ATTACH ANGLE. REPAIRED IAW SRM 54-01.Aug 21, 2010 · N785NC · Doug DC951 · Nacelle/Pylon, Attach FittingsSDR DALA1019899876Attach Fitting · crackedDURING LINE CHECK FOUND CRACK IN LT PYLON CLOSURE WEB UPPER CLIP INBD SIDE. REPAIRED IAW SRM 54-20-0.Aug 21, 2010 · N785NC · Doug DC951 · Nacelle/Pylon, Attach FittingsSDR DALA1019889876Attach Angle · crackedDURING LINE CHECK FOUND CRACK IN LT PYLON FAIRING SUPPORT RIB ATTACH ANGLE. REPAIRED IAW DWG 9915500.Aug 21, 2010 · N785NC · Doug DC951 · Nacelle/Pylon, Attach FittingsSDR DALA1018249876Skin · damagedDURING LINE CHECK FOUND DAMAGE TO FUSELAGE SKIN AT BS 427 AFT OF FORWARD CARGO DOOR AREA. REPAIRED PER SRM 53-05-82.Aug 3, 2010 · N785NC · Doug DC951 · Fuselage Main, Plate/SkinSDR DALA102609876Frame · crackedDURING "H" CHECK FOUND CRACK IN FRAME AT BS 465 L26R. REPAIRED IAW 53-03-02 AND SRM 51-30-05.Feb 2, 2010 · N785NC · Doug DC951 · Fuselage Main, FrameSDR DALA102519876Pan · corrodedDURING "H" CHECK FOUND DOOR PAN CORRODED AT BS 1079. REPAIRED IAW SRM 51-30-2, 51-30-5.Feb 1, 2010 · N785NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA102509876Frame · crackedDURING "H" CHECK FOUND CRACK IN FRAME AT BS 465 L26R. REPAIRED IAW SRM 53-03,51-10-4,51-10-3,51-30-5,51-10-2.Feb 1, 2010 · N785NC · Doug DC951 · Fuselage Main, FrameSDR DALA102239876Structure · crackedDURING "H" CHECK FOUND CRACK IN RT VERTICAL STRUT IN FWD CARGO BS 598. REPAIRED IAW SRM 51-30-2 & 53-01.Jan 31, 2010 · N785NC · Doug DC951 · Fuselage Main, StructureSDR DALA102229876Skin · corrodedDURING "H" CHECK FOUND CORROSION ON DOOR CUTOUT INNER SKIN. REPAIRED IAW SRM 51-30-2 & 51-30-5.Jan 31, 2010 · N785NC · Doug DC951 · Fuselage Main, Plate/SkinSDR DALA102249876Cargo Track · corrodedDURING "H" CHECK FOUND CORROSION ON CARGO TIEDOWN TRACK AT BS 1167 BETWEEN L27R AND L28R. REPAIRED IAW SRM 51-30-1.Jan 29, 2010 · N785NC · Doug DC951 · Fuselage, Seat/Cargo Attach FittingsSDR DALA102049876Floor Panel · corrodedDURING "H" CHECK FOUND COCKPIT FLOOR PANEL NR 15 BETWEEN STA 148 AND 160 HAS CORROSION. REPAIRED IAW SRM 51-10-04, SRM 51-30-01, AND SRM 51-30-02.Jan 28, 2010 · N785NC · Doug DC951 · Fuselage Floor PanelSDR DALA101989876Floor Panel · corrodedDURING "H" CHECK FOUND CORROSION ON FLOOR PANEL NR 37. REPAIRED IAW SRM 51-30-2.Jan 27, 2010 · N785NC · Airbus A330323 · Fuselage Floor PanelSDR DALA101749876Channel · crackedDURING "H" CHECK FOUND FLOOR PANEL NR37 HAS A CRACKED HAT CHANNEL. REPAIRED IAW SRM 51-30-2.Jan 26, 2010 · N785NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA101739876Floor Panel · corrodedDURING "H" CHECK FOUND COCKPIT FLOOR PANEL NR 13 HAS CORROSION AT STA 148 AND 160. REPAIRED IAW SRM 51-30-2, SRM 51-10-2, AND SRM 51-10-4.Jan 26, 2010 · N785NC · Doug DC951 · Fuselage Floor PanelSDR DALA101679876Intercostal · crackedDURING "H" CHECK FOUND CRACK IN INTERCOSTAL AT BS 579-598 BL0. REPAIRED IAW SRM 51-30-1.Jan 25, 2010 · N785NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA101669876Cusp Web · crackedDURING H-CHECK FOUND CUSP WEB CRACKED AT BS 1135 RBL 54. REPAIRED PER SRM 53-10-16.Jan 25, 2010 · N785NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA101659876Frame · crackedDURING "H" CHECK FOUND FRAME CRACKED AT BS 332 L26L-L27L. REPAIRED IAW SRM 53-03-02.Jan 25, 2010 · N785NC · Doug DC951 · Fuselage Main, FrameSDR DALA101339876Attach Bracket · crackedDURING H" CHECK FOUND CRACK IN LT TIE DOWN TRACK ATTACH BRACKET AT BS 427. REPAIRED IAW SRM 51-30-05.Jan 22, 2010 · N785NC · Doug DC951 · Fuselage, Seat/Cargo Attach FittingsSDR DALA100779876Stiffener · crackedDURING "H" CHECK FOUND CRACK IN AFT PRESSURE BULKHEAD NR 4 STIFFENER CLIP AT RT BS 1167. REPAIRED IAW SRM 51-30-5 & SRM 53-10-25.Jan 19, 2010 · N785NC · Doug DC951 · Fuselage Main, BulkheadSDR DALA100769876Stiffener · crackedDURING "H" CHECK FOUND CRACK IN AFT PRESSURE BULKHEAD NR 2 STIFFINER CLIP, AT LT BS 1167. REPAIRED IAW SRM 51-30-5, SRM 53-10-25, AND SRM 51-10-4.Jan 19, 2010 · N785NC · Doug DC951 · Fuselage Main, BulkheadSDR DALA100759876Stiffener · crackedDURING "H" CHECK FOUND CRACK IN AFT PRESSURE BULKHEAD NR 5 STIFFENER CLIP. REPAIRED IAW SRM 53-10-25.Jan 19, 2010 · N785NC · Doug DC951 · Fuselage Main, BulkheadSDR DALA100729876Floorbeam · damagedDURING "H" CHECK FOUND CHAFING DAMAGE TO FLOORBEAM AT BS 408, RBL 22 - BL 0. REPAIRED IAW SRM 53-01-20, SRM 51-10-4 & 51-10-3.Jan 18, 2010 · N785NC · Doug DC951 · Fuselage Main, Floor BeamSDR DALA100709876Intercostal · crackedDURING "H" CHECK FOUND CRACK ON INTERCOSTAL AT BS 408 BL 0. REPAIRED IAW SRM 51-10-2, SRM 51-10-3, SRM 51-10-4 AND SRM 51-30-5.Jan 18, 2010 · N785NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA100689876Floorbeam · crackedDURING "H" CHECK FOUND CRACK IN ATTACH ANGLE AT BS 1167. REPAIRED IAW SRM 51-01.Jan 17, 2010 · N785NC · Doug DC951 · Fuselage Main, Floor BeamSDR DALA100739876Stiffener · crackedDURING "H" CHECK FOUND 6 EACH BULKHEAD STIFFENERS, AND ATTACH CLIPS CRACKED, AT LT OTBD STA 1167. REPAIRED IAW SRM 53-10-25.Jan 16, 2010 · N785NC · Doug DC951 · Fuselage Main, BulkheadSDR DALA100719876Floor Support · crackedDURING "H" CHECK FOUND CRACK IN FLOOR SUPPORT AT BS 1154, LBL 20. REPAIRED IAW SRM 51-72-01, SRM 51-10-2, SRM 51-10-4, AND SRM 51-10-3 & 51-30-2.Jan 16, 2010 · N785NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA100699876Floor Panel · corrodedDURING "H" CHECK FOUND CORROSION ON FLOOR PANEL NR 26. REPAIRED IAW SRM 53-01, SRM 51-10-2, SRM 51-10-3, SRM 51-10-4 AND SRM 51-30-2.Jan 16, 2010 · N785NC · Doug DC951 · Fuselage Floor PanelSDR DALA100679876Cusp Web · crackedDURING "H" CHECK FOUND CRACK IN LT CUSP WEB AT BS 1126. REPAIRED IAW SRM 53-13-3 AND SRM 53-10-16.Jan 16, 2010 · N785NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA100669876Cusp Web · crackedDURING "H" CHECK FOUND CRACK IN LT OTBD CUSP WEB AT BS 1102. REPAIRED IAW SRM 53-13-3 AND SRM 53-10-16.Jan 16, 2010 · N785NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA100659876Cusp Web · crackedDURING "H" CHECK FOUND CRACK IN RT OTBD CUSP WEB AT BS 1134. REPAIRED IAW SRM 53-10-16.Jan 16, 2010 · N785NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA100649876Bulkhead · crackedDURING "H" CHECK FOUND CRACK IN BULKHEAD STRINGER NR 16 AT RT BS 1136. REPAIRED IAW SRM 51-30-2 AND SRM 51-30-5.Jan 16, 2010 · N785NC · Doug DC951 · Fuselage Main, BulkheadSDR DALA100399876Seat Track · corrodedDURING "H" CHECK FOUND LT INBD SEAT TRACK CLIP CORRODED AT BS 1136. REPAIRED IAW SRM 51-30-1.Jan 14, 2010 · N785NC · Doug DC951 · Fuselage, Seat/Cargo Attach FittingsSDR DALA100389876Floor Support · crackedDURING "H" CHECK FOUND CRACK IN FLOOR SUPPORT HAT CHANNEL OTBD LEG AT BS 1136 RBL 20. REPAIRED IAW SRM 51-30-1, SRM 51-10-3, SRM 51-30-2.Jan 14, 2010 · N785NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA100379876Floor Panel · crackedDURING "H" CHECK FOUND CORROSION AND CRACKS IN FLOOR PANEL NR 16. FLOOR PANEL REPLACED IAW SRM 51-10-3, SRM 51-10-4 & 51-30-2.Jan 14, 2010 · N785NC · Doug DC951 · Fuselage Floor PanelSDR DALA100369876Floor Support · corrodedDURING "H" CHECK FOUND CORROSION ON FLOOR SUPPORT BETWEEN BS 218 TO 304 BL 0. REPAIRED IAW SRM 51-30-5,SRM 51-30-2 & SRM 51-10-4.Jan 14, 2010 · N785NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA100359876Stringer · crackedDURING "H" CHECK FOUND CRACK IN BULKHEAD STRINGER NR 17 AT BS 1136. REPAIRED IAW EA SRM 51-30-02.Jan 14, 2010 · N785NC · Doug DC951 · Fuselage Main, Longeron/StringerSDR DALA100329876Floor Support · corrodedDURING "H" CHECK FOUND LEVEL 2 CORROSION AT RBL 44, BETWEEN STA 160 AND 200 FLOOR SUPPORT. REPAIRED IAW SRM 51-30.Jan 11, 2010 · N785NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA109876032Floor Support · corrodedDURING "H" CHECK FOUND LEVEL 2 CORROSION AT RBL44, BETWEEN STA 160 AND 200 FLOOR SUPPORT. REPAIRED IAW SRM 51-30-5.Jan 11, 2010 · N785NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA100299876Floor Support · corrodedDURING "H" CHECK FOUND CORROSION ON FLOOR SUPPORT BETWEEN BS 160 TO BS 200 RBL 44. REPAIRED IAW SRM 51-30-5.Jan 11, 2010 · N785NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA100229876Floorbeam · corrodedDURING "H" CHECK FOUND CORROSION ON FLOORBEAM AT BS 200 BL0-L20L. REPAIRED IAW SRM 51-10-03.Jan 9, 2010 · N785NC · Doug DC951 · Fuselage Main, Floor BeamSDR DALA100219871Floorbeam · corrodedDURING "H" CHECK FOUND CORROSION ON FLOORBEAM AT BS 237 L22L-L44L. REPAIRED IAW SRM 53-10-03.Jan 9, 2010 · N785NC · Doug DC951 · Fuselage Main, Floor BeamSDR NWAA083429876Battery · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 23-26 OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE ASSOCIATED FUSE AND INSTALLED NEW BATTERIES IN THE POWER SUPPLY. OPERATIONAL CHECK WAS GOOD. (A)Jul 26, 2008 · N785NC · Doug DC951 · Emergency LightingSDR NWAA082789876Connector · disconnectedDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGN LIGHT FOR THE FWD RT OVERWING HATCH WAS INOPERATIVE. MAINTENANCE FOUND THE WIRE RECEPTACLE UNPLUGGED. AFTER CONNECTOR WAS RE-SECURED THE LIGHTS FUNCTIONED WITHOUT PROBLEM. (A)Jun 16, 2008 · N785NC · Doug DC951 · Light System WiringSDR NWAA081289876Hose · separatedTHE FLIGHT ATTENDANT REPORTED A THIN HAZE OF SMOKE AND A BURNING RUBBER SMELL IN THE CABIN. FLIGHT CREW NOTED THE SAME IN THE COCKPIT. THE SMOKE QUICKLY DISSIPATED SO THE FLIGHT CONTINUED TO SCHEDULED DESTINATION. LANDING AT DTW WAS NORMAL AND PASSENGERS DEMar 29, 2008 · N785NC · Doug DC951 · Cabin Cooling SystemSDR 0203109876Duct · looseLOST CABIN PRESSURE AT FL310 AND PERFORMED AN EMERGENCY DESCENT TO 10,000 FEET. THE OUTFLOW VALVE WAS FULLY CLOSED AND BOTH SUPPLY PRESSURES INDICATED 25 PSI. FLIGHT LANDED WITHOUT INCIDENT AT GFK. AFTER LANDING, THE CREW DETERMINED THERE WAS NO AIRFLOW FROM TSep 22, 2002 · N785NC · Doug DC951 · Cabin Pressure Control SystemSDR 0202889876Control Valve · failedDURING CRUISE AT FL330, THE MASTER WARNING AND RED CABIN PRESSURE LIGHTS ILLUMINATED AND CABIN PRESSURE INDICATED 1000 FEET. COMPLIED WITH COM PROCEDURES. AIRCRAFT DESCENDED TO 10,000 FEET BUT CREW COULD NOT CONTROL THE CABIN PRESSURE. MASKS DEPLOYED AUTOMASep 12, 2002 · N785NC · Doug DC951 · Cabin Pressure Control SystemSDR 0200199876Rod · brokenWHEN SLATS WERE EXTENDED, THE AIRCRAFT ROLLED TO THE RIGHT. SLAT DISAGREEMENT LIGHT ILLUMINATED AND BLUE SLAT EXTEND LIGHT DID NOT ILLUMINATE. COMPLIED WITH COM PROCEDURES AND AIRCRAFT LANDED UNEVENTFULLY WITH SLATS RETRACTED AND FLAPS EXTENDED. MAINTENANCE REJan 7, 2002 · N785NC · Doug DC951 · Leading Edge Slat ActuatorSDR 0003689876Battery Pack · inoperativeDURING LINE CHECK, FOUND FORWARD SECTION OF EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. OPERATIONAL CHECK NORMAL.Sep 27, 2000 · N785NC · Doug DC951 · Emergency LightingSDR 0001339973Battery Pack · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT EMERGENCY LIGHTS DIM. REPLACED BATTERY PACK.Apr 7, 2000 · N785NC · Doug DC951 · Emergency LightingSDR 9902859876Wire · crossedDURING LINE MAINTENANCE INSPECTION, FORWARD COCKPIT AND FORWARD ENTRY CEILING EMERGENCY LIGHTS WOULD NOT SHUT OFF, NO OTHER POWER AVAILABLE. FOUND WIRES CROSSED AT TERMINALS 4 AND 7. REPAIRED WIRING, OPERATIONAL CHECK NORMAL.Jul 14, 1999 · N785NC · Doug DC951 · Light System Wiring
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