N951U, cancelled Jan 6, 2011

Service difficulty reports · 57

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 = 'N951U' AND deregistration_id = 'N951U-2011-01-06'
  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 AALA20090609TUL41Seat Track · corrodedCORROSION BEYOND LIMITS ON SEAT TRACK NR 5. INSTALLED PLUG PER AARD 53-20-00-10.May 20, 2009 · N951U · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR AALA20090609TUL44Support Angle · crackedNR 2 SEAT TRACK SUPPORT ANGLE CRACKED AT STATION 927 BELOW FLOORBEAM. REMOVED CRACKED ANGLE, INSTALLED NEW ANGLE PER SRM 51-01.May 15, 2009 · N951U · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR AALA20090609TUL43Longeron · crackedLONGERON 20L CRACKED AT STATION 1003. STOP DRILLED CRACK AND INSTALLED DOUBLER PER AARD 53-10-00-18.May 15, 2009 · N951U · Doug DC982 · Fuselage Main, Longeron/StringerSDR AALA20090609TUL47Pressure Panel · crackedCRACK IN RIGHT WHEEL WELL PRESSURE DECK AT STATION 990 IN AREA OF FUEL LINE SHROUD. STOP DRILLED CRACK, INSTALLED TITANIUM DOUBLER PER AARD 53-30-00-13.May 14, 2009 · N951U · Doug DC982 · Fuselage Main, BulkheadSDR AALA20090512TUL49Battery Pack · dischargedCEILING EMERGENCY LIGHTS ARE INOP FROM SEAT 7 TO 16. REMOVED AND REPLACED BATTERY PACKS IN RT BIN PER MM 33-60-98-4.Apr 29, 2009 · N951U · Doug DC982 · Emergency LightingSDR AALA20090512TUL38Skin · damagedLT ALT STATIC PORT, 7 INCH WAVINESS CHECK IS OUT OF LIMITS. INSTALLED DOUBLER PER SRM 51-30-2.Apr 24, 2009 · N951U · Doug DC982 · Fuselage Main, Plate/SkinSDR AALA20090513TUL15Skin · dentedDENT IN FUSELAGE STA 333 ABOVE LONG 23L. INSTALLED DOUBLER PER SRM 53-04 FIG 38.Apr 23, 2009 · N951U · Doug DC982 · Fuselage Main, Plate/SkinSDR AALA20090513TUL14Skin · dentedDENT IN FUSELAGE BETWEEN LONG 17L-18L. REPAIRED PER SRM 53-04 FIG 38 SHEET 30 VIEW P.Apr 23, 2009 · N951U · Doug DC982 · Fuselage Main, Plate/SkinSDR AALA20090513TUL13Channel · crackedNOSE LANDING GEAR WHEEL WELL C-CHANNEL IS CRACKED AT SPRAY DEFLECTOR GUIDE LT SIDE. REPAIRED PER AARD 53-10-00-4 REPAIR NR 4.Apr 23, 2009 · N951U · Doug DC982 · Fuselage Miscellaneous StructureSDR AALA20090513TUL10Skin · dentedDENT IN FUSELAGE AT STA 254 AND LONG 18L-19L. INSTALLED DOUBLER PER SRM 53-04 FIG 12B.Apr 22, 2009 · N951U · Doug DC982 · Fuselage Main, Plate/SkinSDR AALA20090513TUL11Cusp Web · crackedRT CUSP CRACKED UNDER NUMBER 5 SEAT TRACK. CUT OUT CRACKED AREA AND INSTALLED DOUBLER PER 53-20-00-16.Apr 21, 2009 · N951U · Doug DC982 · Fuselage Miscellaneous StructureSDR AALA20090513TUL07Skin · corrodedLT ALTERNATE STATIC PORT HAS CORROSION. INSTALLED NEW DOUBLER PER SRM 51-30-2.Apr 21, 2009 · N951U · Doug DC982 · Fuselage Main, Plate/SkinSDR AALA20090513TUL09Skin · dentedDENT IN FUSELAGE AT RT STA 355 ABOVE LONG 21R. COLD WORK DENT AND INSTALLED DOUBLER PER SRM 53-04 FIG 38.Apr 16, 2009 · N951U · Doug DC982 · Fuselage Main, Plate/SkinSDR AALA20050807Oil System · leakingORD - COMING IN FOR LANDING AT ABOUT 2000 FEET SMELLED AN UNIDENTIFIED ODOR. AFTER LANDING FLIGHT ATTENDANTS INFORMED CREW OF A LITE HAZY SMOKE IN THE CABIN. SHUT OFF THE WING AND ENGINE ANTI-ICE AND THE SMOKE SUBSIDED. SUSPECT OIL LEAKING INTO APU INLET. RDec 8, 2005 · N951U · Doug DC982 · APU Oil SystemSDR AALA20041036Battery Pack · inoperativeDFW - TAIL CONE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK B527 FOR TAIL CONE EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.Oct 10, 2004 · N951U · Doug DC982 · Emergency LightingSDR AALA20041035Battery Pack · inoperativeDFW - AFT ENTRY OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK B527 FOR AFT ENTRY OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.Oct 10, 2004 · N951U · Doug DC982 · Emergency LightingSDR ZW0A0301302Frame · corrodedDURING CHECK-C, IN THE AFT CARGO COMPT FOUND BULKHEAD FRAME CORRODED AT STRINGER 1320, RBL 6, LBL 40. REMOVED OLD FRAME AND REPLACED PER SPM 6-70-01.Jan 27, 2003 · N951U · Doug DC982 · Fuselage Main, FrameSDR ZW0A0301104Bracket · crackedDURING CHECK-C CRACKED BRACKET FOR LOWER AFT DOOR STOP FORWARD CARGO DOOR. REPLACED BRACKET PER SRM 52-03.Jan 17, 2003 · N951U · Doug DC982 · Cargo/Baggage DoorsSDR ZW0A0301103Door Frame · crackedDURING CHECK-C MAINT FORWARD CARGO DOOR FORWARD SIDE AT SECOND DOOR STOP FROM BOTTOM PIN AREA CRACKED. INSTALLED DOUBLER REPAIR PER SRM 52-05 PAGE 291.Jan 16, 2003 · N951U · Doug DC982 · Cargo/Baggage DoorsSDR ZW0A0300811Bracket · corrodedDURING CHECK-C MAINT FOUND FWD SERVICE DOOR AFT SILL BRACKET CORRODED, STA 197 AND RBL 53. REPLACED BRACKET PER DOUGLAS DRAWING 9911516 AND SPM 6-70-01 FASTENER SUBSTITUTION, 51-50-01 SRM.Jan 13, 2003 · N951U · Doug DC982 · Fuselage Miscellaneous StructureSDR ZW0A0300810Web · corrodedDURING CHECK-C MAINT IN THE FWD ENTRY FOUND CORROSION ON WEB, BELOW FLOOR AT STA 168 TO 200, LBL 54. CLEANED AREA OF CORROSION. CUT OUT AREA BEYOND LIMITS AND INSTALLED REPAIR PER SRM 53-01, PAGE 9.Jan 13, 2003 · N951U · Doug DC982 · Fuselage Miscellaneous StructureSDR ZW0A0300809Fitting · corrodedDURING CHECK-C MAINT IN THE FWD CABIN AT THE FWD SERVICE DOOR WAY, FOUND SILL BRACKET (GIRT BAR FITTING) CORRODED AT STA 172, RBL 53. REMOVED AND REPLACED FITTING PER SPM 6-70-01.Jan 13, 2003 · N951U · Doug DC982 · Emergency EquipmentSDR ZW0A0300808Floor Support · corrodedDURING CHECK-C MAINT IN THE FWD CABIN, FOUND CORROSION ALONG THE FLOOR SUPPORT AT STA 148 TO 200, 8 INCHES LBL, UNDER NUMBER 5 FLOOR PANEL. INSTALLED NEW FLOOR SUPPORT PER SPM 6-70-01.Jan 10, 2003 · N951U · Doug DC982 · Fuselage Miscellaneous StructureSDR ZW0A0300807Door Frame · crackedDURING CHECK-C MAINT FOUND CRACK IN LOWER DOOR BEAM AT LOWER HINGE CUTOUT. FWD SERVICE DOOR. REPLACED FRAME PER SRM SPM 6-70-01.Jan 10, 2003 · N951U · Doug DC982 · Fuselage Main, StructureSDR ZW0A0300806Floor Support · corrodedDURING CHECK-C MAINT FOUND CORROSION ALONG FLOOR SUPPORT AT STA 148 TO 200, 8 INCHES RBL, UNDER NUMBER 4 FLOOR PANEL. INSTALLED NEW FLOOR SUPPORT, FABRICATED FROM EXTRUSION PER SPM 6-70-01.Jan 10, 2003 · N951U · Doug DC982 · Fuselage Miscellaneous StructureSDR ZW0A0300805Floor Support · damagedDURING CHECK-C MAINT FOUND CABIN FLOOR SUPPORT DAMAGED AT STA 905, LBL 12. REMOVED AND REPLACED FLOOR SUPPORT PER SPM 6-70-01.Jan 8, 2003 · N951U · Doug DC982 · Fuselage Miscellaneous StructureSDR ZW0A0300804Floor Support · corrodedDURING CHECK-C MAINT FOUND A CORRODED CABIN FLOOR SUPPORT CAP AT STA 1250, LBL 22 TO 44. REMOVED CORRODED CAP. CLEANED AREA AND FABRICATED AND INSTALLED NEW CAP PER SPM 6-70-01.Jan 7, 2003 · N951U · Doug DC982 · Fuselage Miscellaneous StructureSDR ZW0A0300803Floor Support · corrodedDURING CHECK-C IN THE CABIN A CORRODED FLOOR SUPPORT CAP WAS FOUND AT STA 1155, LBL 22 TO 44. REMOVED CORRODED CAP. CLEANED AREA AND INSTALLED NEW FABRICATED CAP PER SPM 6-70-01.Jan 7, 2003 · N951U · Doug DC982 · Fuselage Miscellaneous StructureSDR ZW0A0300802Angle · crackedDURING CHECK-C IN THE NLG WHEEL WHEEL A CRACK WAS FOUND ON RT SIDE OF NOSE GEAR WHEEL WELL JUST ABOVE THE RT FWD NOSE GEAR DOOR FWD HINGE, 8 INCHES AFT OF STA 37 ON WHEEL WELL CUTOUT SUPPORT ANGLE ON THE RT SIDE. CRACK WAS THROUGH FASTENER. TWO STACKED DOUBLJan 6, 2003 · N951U · Doug DC982 · Fuselage Miscellaneous StructureSDR ZW0A0210203Control Cable · out of rigWHEN FLAPS EXTENDED TO 15 DEGREES THE SLAT DISAGREE LIGHT ILLUMINATED. DURING APPROACH SLAT DISAGREE LIGHT CONTINUED TO INTERMITTENTLY CHANGE BETWEEN OFF AND DISAGREE. NO ASYMMETRY IN FLIGHT CONTROLS WAS NOTICED. RIGGED SLAT FOLLOW UP CABLES PER MM 27-81-02Sep 29, 2002 · N951U · Doug DC982 · Leading Edge Slat Control SystemSDR ZW0A0201002CableFOUND FLAP BUS TRAVEL CABLE BROKEN. REPLACED THE CABLE. CHECK-C 8-25-01 STL. --CLOSED--Jan 22, 2002 · N951U · Doug DC982 · Leading Edge Slat Control SystemSDR ZW0A0201001CableFOUND FLAP BUS TRAVEL CABLE BROKEN. REPLACED THE CABLE. CHECK-C 8-25-01 STL. ---CLOSED---Jan 22, 2002 · N951U · Doug DC982 · Leading Edge Slat Control SystemSDR TWAA0105602Battery · dischargedTHE COCKPIT EMERGENCY FLOOD LIGHTS WERE INOPERATIVE. REPLACED THE BATTERIES. CHECK-C 9-8-00 STL.Mar 28, 2001 · N951U · Doug DC982 · Emergency LightingSDR TWAA0105601Light · inoperativeTHE AFT ACCESSORY COMPT EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE LAMPS. CHECK-C 9-8-00 STL.Mar 28, 2001 · N951U · Doug DC982 · Emergency LightingSDR TWAA0017603Wire · wornTHE FIRST CLASS FLOOR EGRESS LIGHTS WERE INOPERATIVE. REPAIRED WIRING, WORN DUE TO WEAR AND TEAR. CHECK-C 9-8-00 STL.Nov 8, 2000 · N951U · Doug DC982 · Light System WiringSDR TWAA0008602Gyro · failedDURING CRUISE, F/O''S RMI AND CAPT''S HSI BECAME ERRATIC THEREAFTER VG NUMBER 1 FAILED AND WOULD NOT RESET. REPLACED VG (PN 19911-C1) (S/N 45145) AND DG (P/N 17265-2A) (S/N 55485). AC03 04-04-00 JFK.May 31, 2000 · N951U · Doug DC982 · Attitude and Direction Data SystemSDR TWAA9911303Intercostal · crackedDURING OP 16 MAINT CHECK, FOUND AFT CARGO COMPT TRACK SUPPORT INTERCOSTAL CRACKED AND CORRODED AT STA 1309, LONGERON 27R TO 28R. REMOVED INTERCOSTAL AND REPLACED PER SPM 6-70-01, PAGE 3.Aug 13, 1999 · N951U · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA9911304Support · corrodedDURING OP 16 MAINT CHECK, FOUND CABIN FLOOR SUPPORT CORRODED AT STA 198, RBL 9 TO RBL44. FABRICATED ANGLE FROM 7075 T-6 PER SPM 6-70-01.Aug 11, 1999 · N951U · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA9911302Support · corrodedDURING OP 16 MAINT CHECK, THE CABIN O/B FLOOR SUPPORT RAIL WAS CORRODED AT STA 160 TO 198 AT FWD GALLEY DOOR. REMOVED THE CORROSION BY REPLACEMENT OF THE PART PER SPM 6-70-01, SEALED AND USED 5/32 AD RIVETS.Aug 11, 1999 · N951U · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA9911210Support · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION ON CABIN FLOOR SUPPORT, STA 200, OTBD OF CHAIR TRACK AT RBL 44. REMOVED AND REPLACED SUPPORT MEMBER PER SPM 6-70-01, PAGE 2.Aug 10, 1999 · N951U · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA9911209Intercostal · corrodedDURING OP 16 MAINT CHECK, FOUND IN AFT CARGO COMPT AT STA 1212 TO 1216, INTERCOSTAL BETWEEN LONGERONS 29R AND 30 WITH CORROSION ON FOOT. REMOVED AND RELACED FOOT PER SPM 6-70-01.Aug 10, 1999 · N951U · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA9911208Seat Track · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION ON CHAIR TRACK FLANGE, STA 1271 TO 1307, LBL 44. REPLACED CHAIR TRACK PER SPM 6-70-01.Aug 10, 1999 · N951U · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA9911207Seat Track · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION ON CHAIR TRACK FLANGE AT STA 1212 TO 1250, LBL 44. REPLACED CHAIR TRACK PER SPM 6-70-01.Aug 10, 1999 · N951U · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA9911203Intercostal · corrodedDURING OP 16 MAINT CHECK, FOUND STA 1212 TO 1216 LONGERON 29R INTERCOSTAL CORRODED. REMOVED CORROSION BY REPLACEMENT OF PART PER SRM 51-10-3.Aug 4, 1999 · N951U · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA9816310Battery Pack · dischargedDURING MAINT CHECK, FOUND EMERGENCY CEILING LIGHT INOP AT AFT LAVS. REPLACED BATTERY PACK. CHECK-C 7-28-98 MCI.Oct 11, 1998 · N951U · Doug DC982 · Emergency LightingSDR TWAA9816309Battery Pack · dischargedDURING MAINT CHECK, FOUND EMERGENCY CEILING LIGHT INOPERATIVE AT CABIN ROWS 9 AND 11. REPLACED BATTERY PACK. CHECK-C 7-28-98 MCI.Oct 11, 1998 · N951U · Doug DC982 · Emergency LightingSDR TWAA9811802Connector · shortedDURING CHECK-C MAINTENANCE, WHILE OPERATING THE AUX HYD PUMP THE ELECTRICAL CONNECTOR ON THE PUMP SHORTED, BURNING THE CONNECTOR CONTACTS AND CAUSING A SMALL FIRE AT THE CONNECTOR. REPLACED THE AUX HYD PUMP CONN AND THE PUMP. (M)Jul 22, 1998 · N951U · Doug DC982 · Hydraulic Pump, AuxiliarySDR TWAA9809009Hyd Fluid · lostSTL - FLT 203 - DURING TAKEOFF, LOST RT SYSTEM HYDRAULIC FLUID. REPLACED RT NOSE TIRE MFG PN 3910097-535 DUE TO TREAD CAP MISSING. CC-010 7-20-97 LAX. (X)Jun 7, 1998 · N951U · Doug DC982 · Hydraulic System, MainSDR TWAA9804103Generator · wornJFK - FLT 8703 - THE LEFT GEN FAILED, NO VOLTS OR FREQS. APU STARTED AND RAN NORMALLY FOR 30 MINUTES THEN APU GEN FAILED, NO VOLTS OR FREQS RETURNED TO JFK. THE LEFT GEN WAS DEFERRED PER MEL, AND THE APU GENERATOR CONTROL UNIT WAS REPLACED. IN FLIGHT, THE AMar 19, 1998 · N951U · Doug DC982 · AC Generator-AlternatorSDR TWAA9713905Duct · crackedPBI - FLT 229 - DURING CLIMB, HAD A RECURRENCE OF TAIL COMPARTMENT HIGH LIGHT ILLUMINATION. LIGHT WENT OUT WITH POWER REDUCTION. REPAIRED RIGHT AND LEFT PACK Y DUCT MFG P/N 5953625-521. ACCOMPLISHED TAIL COMPARTMENT LEAK AND Y DUCT HIGH PRESSURE CHECKS. OPNov 27, 1997 · N951U · Doug DC982 · Pneumatic Distribution System
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