N14063, cancelled Jun 11, 2013

Service difficulty reports · 64

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 = 'N14063' AND deregistration_id = 'N14063-2013-06-11'
  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 CALA0100162Spoiler · delaminatedINSPECTION FOUND LT WING SPOILER NR 2 DELAMINATED WITH LOWER SKIN CORRODED. THE NR 2 LT SPOILER WAS REMOVED AND REPLACED IAW MM 27-60-01.Feb 24, 2001 · N14063 · Doug DC1030 · SpoilersSDR CALA0100161Skin · crackedINSPECTION FOUND A 1.2 INCH CRACK IN APU DOOR SKIN. A NEW DOOR WAS INSTALLED IAW DRAWING AHL7008 AND SRM 51-31-01.Feb 24, 2001 · N14063 · Doug DC1030 · Auxiliary Power Unit (APU) DoorsSDR CALA0100160Spoiler · delaminatedINSPECTION FOUND RT WING SPOILER PANELS NR 3, 4, & 5 DELAMINATED ON UPPER SURFACE. THE SPOILERS WERE REMOVED AND REPLACED IAW MM 27-60-01.Feb 24, 2001 · N14063 · Doug DC1030 · SpoilersSDR CALA0100159Spoiler · delaminatedINSPECTION FOUND RT WING NR 1 AND 2 SPOILER PANELS DELAMINATED ON UPPER SURFACE. THE NR 1 AND 2 SPOILERS WERE REMOVED AND REPLACED IAW MM 27-60-01.Feb 24, 2001 · N14063 · Doug DC1030 · SpoilersSDR CALA0100157Angle · crackedINSPECTION FOUND A 1 INCH CRACK IN CENTER CARGO LT ANGLE AT STA 1721. THE ANGLE WAS REPLACED IAW SRM 51-31-01.Feb 23, 2001 · N14063 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA0001998Battery Pack · inoperativeTHE EMERGENCY LIGHT TEST FUNCTION WOULD NOT GIVE A VALID TEST. THE L-2 DOOR EMERGENCY LIGHT BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-51-01. OPERATIONAL CHECKS WERE GOOD.Dec 26, 2000 · N14063 · Doug DC1030 · Emergency LightingSDR CALA0000420Spar · crackedINSPECTION FOUND A 1.3 INCH CRACK IN LT HORIZONTAL STABILIZER REAR SPAR CAP AFT BARREL NUT BORE. THE LT HORIZONTAL STABILIZER UPPER AFT SPAR CAP SECTION WAS REPLACED IAW ECRA 5511-01015.Apr 6, 2000 · N14063 · Doug DC1030 · Elevator, Spar/RibSDR CALA0000327Floorbeam · corrodedINSPECTION FOUND FLOORBOARD SUPPORT BEAM CORRODED AT STA 420, X=28L. A SPLICE REPAIR WAS INSTALLED IAW SRM 53-70-00, FIGURE 13.Mar 22, 2000 · N14063 · Doug DC1030 · Fuselage Main, Floor BeamSDR CALA9900419Channel · damagedINSPECTION FOUND DAMAGED CHANNEL SECTION IN CENTER CARGO BAY AT STA 1801-1841. THE CHANNEL WAS REPLACED WITH A NEW CHANNEL IAW MM 25-52-01.Apr 16, 1999 · N14063 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9900415Sill · corrodedINSPECTION FOUND CENTER CARGO BAY DOOR SILL LOWER AFT FRAME AND LOWER FORWARD FRAME CORRODED. THE LOWER AFT AND LOWER FORWARD FRAMES WERE REPAIRED IAW SRM 53-50-00, PAGES 119-130.Apr 15, 1999 · N14063 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9900414Beam · corrodedINSPECTION FOUND SUPPORT BEAM CORRODED AT CENTER CARGO BAY CENTER ROLLER CHANNEL ADJOINING BULK CARGO AREA. THE SUPPORT BEAM WAS REMOVED AND REPLACED IAW SRM 53-42-00.Apr 15, 1999 · N14063 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9900413Bracket · crackedINSPECTION FOUND TAIL CONE CENTER RT, UPPER RT, AND UPPER LT SPIGOT MOUNTING BRACKETS CRACKED. EACH BRACKET HAD A 3 INCH CRACK. THE BRACKETS WERE REPAIRED IAW SRM 53-30-00, FIGURE 3.Apr 15, 1999 · N14063 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9900408Bolt · shearedINSPECTION FOUND LT MLG BAY TRAPEZOIDAL FRAME UPPER FLANGE BOLT SHEARED. THE BOLT, NUT AND WASHERS WERE REPLACED IAW MM 20-20-01.Apr 14, 1999 · N14063 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9900404Sill · corrodedINSPECTION FOUND THE FORWARD CARGO BAY FORWARD LOWER DOOR SILL CORRODED IN FORWARD CORNER. THE DOOR SILL WAS REPAIRED IAW SRM 53-50-00, FIGURE 9.Apr 14, 1999 · N14063 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9900388Rib · crackedINSPECTION FOUND A 1.5 INCH CRACK RT WING LEADING EDGE DOUBLER AND SUPPORT RIB AT STA XORS 795. THE LEADING EDGE DOUBLER AND SUPPORT RIB WERE REPAIRED IAW SRM 57-10-00, PAGE 163 AND SRM 57-31-01.Apr 12, 1999 · N14063 · Doug DC1030 · Wing, Rib/BulkheadSDR CALA9900360Door · crackedINSPECTION FOUND A 4 INCH CRACK IN Z SECTION AT FORWARD CORNER OF LT MLG DOOR. THE DOOR WAS REPAIRED IAW SRM 52-10-00, FIGURE 15.Apr 6, 1999 · N14063 · Doug DC1030 · Landing Gear DoorsSDR CALA9900359Angle · crackedINSPECTION FOUND A 3 INCH CRACK IN LT AND RT DRAG ANGLES BELOW NR 2 ENGINE AT THIRD BANJO FITTING. THE CRACKS WERE STOP DRILLED AND REPAIR ANGLES WERE INSTALLED IAW SRM 55-20-00, FIGURE 3.Apr 6, 1999 · N14063 · Doug DC1030 · Vertical StabilizerSDR CALA9900193Wire · shortedINSPECTION FOUND THE EMERGENCY AISLE PATH LIGHTING AT SEAT ROWS 29/36KL INOPERATIVE. A POWER WIRE WAS FOUND DAMAGED AND SHORTED UNDER SEAT 36L CAUSING POWER SUPPLY FUSES TO BLOW. THE WIRE WAS REPAIRED AND THE FUSES WERE REPLACED.Feb 25, 1999 · N14063 · Doug DC1030 · Light System WiringSDR CALA9801957Wire · brokenROW 33 AND 34 L AND K EMERGENCY LIGHTS INOP. RESECURED BROKEN WIRE FOR EMERGENCY LIGHTS.Oct 14, 1998 · N14063 · Doug DC1030 · Light System WiringSDR CALA9801855Duct · rupturedTHE NR 3 ENGINE FIRE WARNING LIGHT ILLUMINATED WHILE EN ROUTE. BOTH FIRE BOTTLES WERE DISCHARGED, BUT THE LIGHT REMAINED ILLUMINATED. THE AIRCRAFT WAS DIVERTED TO SNN WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 3 ENGINE 8TH STAGE PNEUMATIC DUSep 20, 1998 · N14063 · Doug DC1030 · Pneumatic Distribution SystemSDR CALA9800645Support · corrodedINSPECTION FOUND CORROSION ON FLOOR OMEGA SUPPORT AT STA 455, RBL 45. THE FLOOR SUPPORT WAS REMOVED. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-70-00, 51-20-00, AND 51-31-01.Apr 8, 1998 · N14063 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9800644Jamb · corrodedINSPECTION FOUND CORROSION ON ENTRY LOWER AFT CARGO JAMB BOX AT STA 1964 BETWEEN STRINGER 40-46. THE CORRODED AREAS WERE REMOVED. A STRAP, DOUBLERS, PLUG, ANGLE, AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-50-00, FIGURE 14.Apr 7, 1998 · N14063 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9800636Air Bottle · low pressureINSPECTION FOUND R-1 DOOR AIR BOTTLE PRESSURE LOW. THE AIR BOTTLE WAS FILLED IAW MM 52-11-06.Apr 7, 1998 · N14063 · Doug DC1030 · Passenger/Crew DoorsSDR CALA9800635Air Bottle · low pressureINSPECTION FOUND L-2 DOOR AIR BOTTLE PRESSURE LOW. THE AIR BOTTLE WAS FILLED IAW MM 52-12-06.Apr 7, 1998 · N14063 · Doug DC1030 · Passenger/Crew DoorsSDR CALA9800634Air Bottle · low pressureINSPECTION FOUND L-3 DOOR AIR BOTTLE PRESSURE LOW. THE AIR BOTTLE WAS FILLED IAW MM 52-12-06.Apr 7, 1998 · N14063 · Doug DC1030 · Passenger/Crew DoorsSDR CALA9800629Charger · inoperativeINSPECTION FOUND ZONE-A EMERGENCY LIGHT BATTERY PACK INOPERATIVE. THE EMERGENCY LIGHT CHARGER WAS REPLACED AND OPERATION CHECKED GOOD IAW MM 33-50-00.Apr 6, 1998 · N14063 · Doug DC1030 · Emergency LightingSDR CALA9800605Ribs · crackedINSPECTION FOUND A 1 INCH CRACK IN THREE RIBS OF NR 1 LT SLAT. THE CRACKED RIBS WERE REMOVED. NEW RIBS WERE FABRICATED AND INSTALLED IAW SRM 57-55-01 FIGURE 2 51-20-00 AND 51-31-01.Mar 30, 1998 · N14063 · Doug DC1030 · Leading Edge DevicesSDR CALA9800577Bracket · corrodedINSPECTION FOUND NR 2 PYLON UPPER PYLON TRAILING EDGE ATTACH BRACKET CORRODED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 54-32-02, 51-38-01, FIGURE 13, 51-21-01, 51-31-01.Mar 22, 1998 · N14063 · Doug DC1030 · Nacelle/Pylon StructureSDR CALA9800491Jamb · corrodedINSPECTION FOUND LOWER AFT CARGO DOOR JAMB CORRODED BETWEEN STA 1921 AND 1942. THE CORRODED AREA WAS REMOVED. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-21-01, 53-50-00, FIGURE 15A, AND 51-31-01.Mar 18, 1998 · N14063 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9800490T-Profile · crackedINSPECTION FOUND SEVERAL 1 CRACKS IN INBOARD AND OUTBOARD ATTACH FLANGES OF RT HORIZONTAL STABILIZER NR 3 LEADING EDGE T-PROFILE. THE STRAP AND T-PROFILE WERE REMOVED. A NEW T-PROFILE WAS FABRICATED AND INSTALLED IAW SRM 51-20-00 AND 51-31-01.Mar 18, 1998 · N14063 · Doug DC1030 · Horizontal Stabilizer StructureSDR CALA9800489Mount · crackedINSPECTION FOUND TAILCONE UPPER SECTION RT WORK PLATFORM FORWARD MOUNT RIVETS LOOSE AND CRACKED. THE MOUNT WAS REMOVED AND A NEW MOUNT WAS FABRICATED AND INSTALLED IAW SRM 51-20-00, 51-31-01, AND 53-52-01, FIGURE 2.Mar 18, 1998 · N14063 · Doug DC1030 · Aerodynamic FairingsSDR CALA9800488Floor Post · brokenINSPECTION FOUND CABIN FLOOR POST BROKEN IN FORWARD CARGO AREA AT STA 1100. THE AREA WAS TRIMMED AND BLENDED OUT. A REPAIR CHANNEL, ANGLE, AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 51-20-00 AND ENGINEERING ORDER MF MAN D10-53-86801.Mar 18, 1998 · N14063 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9800487Floor Web · crackedINSPECTION FOUND A 5 INCH CRACK ON FORWARD CARGO LOWER FLANGE OF FLOOR WEB AT STA 879 LBL 50. THE FLANGE WAS TRIMMED AND BLENDED OUT AND THE AREA WAS REWORKED. TWO ANGLES WERE INSTALLED IAW SRM 53-00-01, FIGURE 3, 51-20-00, AND 51-31-01.Mar 18, 1998 · N14063 · Doug DC1030 · Fuselage Floor PanelSDR CALA9800485Floorbeam · brokenINSPECTION FOUND INTERIOR UPPER LOBE CABIN FLOORBEAM BROKEN AT STA 1275, RBL 103. THE FLOORBEAM WAS REPAIRED IAW ECRA 5320-01511 AND ENGINEERING ORDER MF MAN D10-53-896798.Mar 17, 1998 · N14063 · Doug DC1030 · Fuselage Main, Floor BeamSDR CALA9800484Floorbeam · brokenINSPECTION FOUND INTERIOR UPPER LOBE CABIN FLOORBEAM BROKEN AT STA 1293, RBL 103. THE FLOORBEAM WAS REPAIRED IAW ECRA 5320-01511 AND ENGINEERING ORDER MF MAN D10-53-896798.Mar 17, 1998 · N14063 · Doug DC1030 · Fuselage Main, Floor BeamSDR CALA9800481Stringer · corrodedINSPECTION FOUND STRINGER 52 CORRODED IN CENTER CARGO AREA AT STA 1581-1601. THE STRINGER WAS REMOVED. A NEW PART WAS INSTALLED IAW SRM 51-21-01.Mar 17, 1998 · N14063 · Doug DC1030 · Fuselage Main, Longeron/StringerSDR CALA9800480Longeron · corrodedINSPECTION FOUND LONGERON 48L CORRODED IN CENTER CARGO AREA AT STA 1521-1541. THE CORRODED AREA WAS CLEANED AND BLENDED OUT. A NEW ANGLE WAS FABRICATED, THE AREA WAS REWORKED, AND REPAIR WAS INSTALLED IAW SRM 51-21-01 AND 51-31-01.Mar 17, 1998 · N14063 · Doug DC1030 · Fuselage Main, Longeron/StringerSDR CALA9800479Flange · corrodedINSPECTION FOUND LOWER FLANGE IN CENTER CARGO AREA CORRODED AT STA 1821, STRINGER 51. THE CORRODED AREA WAS TRIMMED AND BLENDED OUT, REWORKED, AND REINFORCED WITH SHEAR CLIP IAW SRM 53-30-00, FIGURE 9. NEW PARTS WERE FABRICATED AND INSTALLED USING RIVETS IAWMar 17, 1998 · N14063 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9800478Flange · corrodedINSPECTION FOUND LOWER FLANGE IN CENTER CARGO AREA CORRODED AT STA 1741, STRINGER 48. THE CORRODED AREA WAS TRIMMED AND BLENDED OUT. A NEW CHORD WAS FABRICATED IAW SRM 53-15-01, FIGURE. THE AREA WAS REWORKED, REINFORCED WITH SPLICE, AND INSTALLED USING RIVEMar 17, 1998 · N14063 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9800477Flange · corrodedINSPECTION FOUND LOWER FLANGE IN CENTER CARGO AREA CORRODED AT STA 1761, STRINGER 48. THE CORRODED AREA WAS TRIMMED AND BLENDED OUT. A NEW CHORD WAS FABRICATED IAW SRM 53-15-01, FIGURE 12. THE AREA WAS REWORKED AND REINFORCED WITH A SPLICE AND RIVETED IN PLMar 17, 1998 · N14063 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9800476Chord · corrodedINSPECTION FOUND LOWER CHORD IN CENTER CARGO AREA CORRODED AT STA 1761, STRINGER 51 TO 47L. THE CORRODED AREA WAS REMOVED. A NEW PART AND SHEAR CLIP WERE FABRICATED IAW SRM 51-20-00. THE AREA WAS REWORKED, REINFORCED, AND RIVETED IAW 53-30-00, FIGURE 9 AND Mar 17, 1998 · N14063 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9800475Chord · corrodedINSPECTION FOUND LOWER CHORD IN CENTER CARGO AREA CORRODED AT STA 1781, STRINGER 51. THE CORRODED AREA WAS REMOVED AND THE AREA WAS REWORKED. A NEW PART WAS INSTALLED USING RIVETS AND REINFORCED WITH SHEAR CLIP IAW SRM 53-30-00, FIGURE 9, 51-20-00, AND 51-31Mar 17, 1998 · N14063 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9800474Flange · corrodedINSPECTION FOUND LOWER FLANGE IN CENTER CARGO AREA CORRODED AT STA 1781, STRINGER 47-48R. THE CORRODED AREA WAS TRIMMED AND BLENDED OUT. A NEW CHORD WAS FABRICATED, THE AREA REWORKED AND REINFORCED WITH SPLICE AND RIVETED IAW SRM 53-15-01, FIGURE 12, 53-30-0Mar 17, 1998 · N14063 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9800462Vent Box · corrodedINSPECTION FOUND CORROSION ON VENT BOX AT STA 1480 AT ATTACHMENT TO LONGERON 27R. CORRODED TRUSS WAS REMOVED. A NEW PART WAS FABRICATED AND INSTALLED IAW SRM 51-20-00, 51-31-01, AND 53-14-01, FIGURE 5, ITEM 42.Mar 15, 1998 · N14063 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9800461Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 455, LBL 60. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-12-15, FIGURE 1 AND 26, 51-31-01, AND 51-20-00.Mar 15, 1998 · N14063 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9800460Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 492, RBL 30. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-12-15, FIGURE 1 AND 26, 51-20-00, AND 51-31-01.Mar 15, 1998 · N14063 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9800459Angle · crackedINSPECTION FOUND A 1 INCH CRACK ON FAIRING SUPPORT ANGLE AT STA 1421, STRINGER 32R. THE SUPPORT ANGLE WAS REMOVED. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-20-00, 51-31-01, AND 53-53-01, FIGURE 3.Mar 15, 1998 · N14063 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9800458Angle · crackedINSPECTION FOUND A 1 INCH CRACK ON FAIRING SUPPORT ANGLE AT STA 1381, STRINGER 32R. THE SUPPORT ANGLE WAS REMOVED. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-53-01, FIGURE 3, 51-20-00, AND 51-31-01.Mar 15, 1998 · N14063 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9800457Support · corrodedINTERIOR UPPER LOBE CABIN UNDER FLOOR LAV/GALLEY CORROSION ON FLOOR SUPPORT BETWEEN STA 824 AND 879, RBL 73. THE FLOOR SUPPORT WAS REMOVED. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-12-15, FIGURE 1 AND 26, 51-20-00, AND 51-31-01.Mar 15, 1998 · N14063 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9800456Floor Track · corrodedINTERIOR UPPER LOBE CABIN UNDER FLOOR LAV/GALLEY CORROSION ON FLOOR TRACK AT STA 840, RBL 27. THE FLOOR TRACK WAS REMOVED, A NEW TRACK WAS INSTALLED IAW SRM 53-70-00, 51-20-00, AND 51-31-01.Mar 15, 1998 · N14063 · Doug DC1030 · Fuselage, Seat/Cargo Attach Fittings
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