# Service difficulty reports: N14063, cancelled Jun 11, 2013 A list on [N14063, cancelled Jun 11, 2013](https://openairdocs.org/deregistered/N14063-2013-06-11.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 · 64 reports - [SDR CALA0100162](https://openairdocs.org/sdr/CALA0100162.md): Spoiler · delaminated · Feb 24, 2001 · N14063 · Doug DC1030 · Spoilers > INSPECTION 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. - [SDR CALA0100161](https://openairdocs.org/sdr/CALA0100161.md): Skin · cracked · Feb 24, 2001 · N14063 · Doug DC1030 · Auxiliary Power Unit (APU) Doors > INSPECTION FOUND A 1.2 INCH CRACK IN APU DOOR SKIN. A NEW DOOR WAS INSTALLED IAW DRAWING AHL7008 AND SRM 51-31-01. - [SDR CALA0100160](https://openairdocs.org/sdr/CALA0100160.md): Spoiler · delaminated · Feb 24, 2001 · N14063 · Doug DC1030 · Spoilers > INSPECTION FOUND RT WING SPOILER PANELS NR 3, 4, & 5 DELAMINATED ON UPPER SURFACE. THE SPOILERS WERE REMOVED AND REPLACED IAW MM 27-60-01. - [SDR CALA0100159](https://openairdocs.org/sdr/CALA0100159.md): Spoiler · delaminated · Feb 24, 2001 · N14063 · Doug DC1030 · Spoilers > INSPECTION 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. - [SDR CALA0100157](https://openairdocs.org/sdr/CALA0100157.md): Angle · cracked · Feb 23, 2001 · N14063 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION FOUND A 1 INCH CRACK IN CENTER CARGO LT ANGLE AT STA 1721. THE ANGLE WAS REPLACED IAW SRM 51-31-01. - [SDR CALA0001998](https://openairdocs.org/sdr/CALA0001998.md): Battery Pack · inoperative · Dec 26, 2000 · N14063 · Doug DC1030 · Emergency Lighting > THE 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. - [SDR CALA0000420](https://openairdocs.org/sdr/CALA0000420.md): Spar · cracked · Apr 6, 2000 · N14063 · Doug DC1030 · Elevator, Spar/Rib > INSPECTION 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. - [SDR CALA0000327](https://openairdocs.org/sdr/CALA0000327.md): Floorbeam · corroded · Mar 22, 2000 · N14063 · Doug DC1030 · Fuselage Main, Floor Beam > INSPECTION FOUND FLOORBOARD SUPPORT BEAM CORRODED AT STA 420, X=28L. A SPLICE REPAIR WAS INSTALLED IAW SRM 53-70-00, FIGURE 13. - [SDR CALA9900419](https://openairdocs.org/sdr/CALA9900419.md): Channel · damaged · Apr 16, 1999 · N14063 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION 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. - [SDR CALA9900415](https://openairdocs.org/sdr/CALA9900415.md): Sill · corroded · Apr 15, 1999 · N14063 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION 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. - [SDR CALA9900414](https://openairdocs.org/sdr/CALA9900414.md): Beam · corroded · Apr 15, 1999 · N14063 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION 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. - [SDR CALA9900413](https://openairdocs.org/sdr/CALA9900413.md): Bracket · cracked · Apr 15, 1999 · N14063 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION 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. - [SDR CALA9900408](https://openairdocs.org/sdr/CALA9900408.md): Bolt · sheared · Apr 14, 1999 · N14063 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION FOUND LT MLG BAY TRAPEZOIDAL FRAME UPPER FLANGE BOLT SHEARED. THE BOLT, NUT AND WASHERS WERE REPLACED IAW MM 20-20-01. - [SDR CALA9900404](https://openairdocs.org/sdr/CALA9900404.md): Sill · corroded · Apr 14, 1999 · N14063 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION 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. - [SDR CALA9900388](https://openairdocs.org/sdr/CALA9900388.md): Rib · cracked · Apr 12, 1999 · N14063 · Doug DC1030 · Wing, Rib/Bulkhead > INSPECTION 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. - [SDR CALA9900360](https://openairdocs.org/sdr/CALA9900360.md): Door · cracked · Apr 6, 1999 · N14063 · Doug DC1030 · Landing Gear Doors > INSPECTION 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. - [SDR CALA9900359](https://openairdocs.org/sdr/CALA9900359.md): Angle · cracked · Apr 6, 1999 · N14063 · Doug DC1030 · Vertical Stabilizer > INSPECTION 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. - [SDR CALA9900193](https://openairdocs.org/sdr/CALA9900193.md): Wire · shorted · Feb 25, 1999 · N14063 · Doug DC1030 · Light System Wiring > INSPECTION 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. - [SDR CALA9801957](https://openairdocs.org/sdr/CALA9801957.md): Wire · broken · Oct 14, 1998 · N14063 · Doug DC1030 · Light System Wiring > ROW 33 AND 34 L AND K EMERGENCY LIGHTS INOP. RESECURED BROKEN WIRE FOR EMERGENCY LIGHTS. - [SDR CALA9801855](https://openairdocs.org/sdr/CALA9801855.md): Duct · ruptured · Sep 20, 1998 · N14063 · Doug DC1030 · Pneumatic Distribution System > THE 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 DU - [SDR CALA9800645](https://openairdocs.org/sdr/CALA9800645.md): Support · corroded · Apr 8, 1998 · N14063 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION 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. - [SDR CALA9800644](https://openairdocs.org/sdr/CALA9800644.md): Jamb · corroded · Apr 7, 1998 · N14063 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION 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. - [SDR CALA9800636](https://openairdocs.org/sdr/CALA9800636.md): Air Bottle · low pressure · Apr 7, 1998 · N14063 · Doug DC1030 · Passenger/Crew Doors > INSPECTION FOUND R-1 DOOR AIR BOTTLE PRESSURE LOW. THE AIR BOTTLE WAS FILLED IAW MM 52-11-06. - [SDR CALA9800635](https://openairdocs.org/sdr/CALA9800635.md): Air Bottle · low pressure · Apr 7, 1998 · N14063 · Doug DC1030 · Passenger/Crew Doors > INSPECTION FOUND L-2 DOOR AIR BOTTLE PRESSURE LOW. THE AIR BOTTLE WAS FILLED IAW MM 52-12-06. - [SDR CALA9800634](https://openairdocs.org/sdr/CALA9800634.md): Air Bottle · low pressure · Apr 7, 1998 · N14063 · Doug DC1030 · Passenger/Crew Doors > INSPECTION FOUND L-3 DOOR AIR BOTTLE PRESSURE LOW. THE AIR BOTTLE WAS FILLED IAW MM 52-12-06. - [SDR CALA9800629](https://openairdocs.org/sdr/CALA9800629.md): Charger · inoperative · Apr 6, 1998 · N14063 · Doug DC1030 · Emergency Lighting > INSPECTION FOUND ZONE-A EMERGENCY LIGHT BATTERY PACK INOPERATIVE. THE EMERGENCY LIGHT CHARGER WAS REPLACED AND OPERATION CHECKED GOOD IAW MM 33-50-00. - [SDR CALA9800605](https://openairdocs.org/sdr/CALA9800605.md): Ribs · cracked · Mar 30, 1998 · N14063 · Doug DC1030 · Leading Edge Devices > INSPECTION 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. - [SDR CALA9800577](https://openairdocs.org/sdr/CALA9800577.md): Bracket · corroded · Mar 22, 1998 · N14063 · Doug DC1030 · Nacelle/Pylon Structure > INSPECTION 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. - [SDR CALA9800491](https://openairdocs.org/sdr/CALA9800491.md): Jamb · corroded · Mar 18, 1998 · N14063 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION 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. - [SDR CALA9800490](https://openairdocs.org/sdr/CALA9800490.md): T-Profile · cracked · Mar 18, 1998 · N14063 · Doug DC1030 · Horizontal Stabilizer Structure > INSPECTION 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. - [SDR CALA9800489](https://openairdocs.org/sdr/CALA9800489.md): Mount · cracked · Mar 18, 1998 · N14063 · Doug DC1030 · Aerodynamic Fairings > INSPECTION 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. - [SDR CALA9800488](https://openairdocs.org/sdr/CALA9800488.md): Floor Post · broken · Mar 18, 1998 · N14063 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION 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. - [SDR CALA9800487](https://openairdocs.org/sdr/CALA9800487.md): Floor Web · cracked · Mar 18, 1998 · N14063 · Doug DC1030 · Fuselage Floor Panel > INSPECTION 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. - [SDR CALA9800485](https://openairdocs.org/sdr/CALA9800485.md): Floorbeam · broken · Mar 17, 1998 · N14063 · Doug DC1030 · Fuselage Main, Floor Beam > INSPECTION 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. - [SDR CALA9800484](https://openairdocs.org/sdr/CALA9800484.md): Floorbeam · broken · Mar 17, 1998 · N14063 · Doug DC1030 · Fuselage Main, Floor Beam > INSPECTION 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. - [SDR CALA9800481](https://openairdocs.org/sdr/CALA9800481.md): Stringer · corroded · Mar 17, 1998 · N14063 · Doug DC1030 · Fuselage Main, Longeron/Stringer > INSPECTION 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. - [SDR CALA9800480](https://openairdocs.org/sdr/CALA9800480.md): Longeron · corroded · Mar 17, 1998 · N14063 · Doug DC1030 · Fuselage Main, Longeron/Stringer > INSPECTION 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. - [SDR CALA9800479](https://openairdocs.org/sdr/CALA9800479.md): Flange · corroded · Mar 17, 1998 · N14063 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION 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 IAW - [SDR CALA9800478](https://openairdocs.org/sdr/CALA9800478.md): Flange · corroded · Mar 17, 1998 · N14063 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION 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 RIVE - [SDR CALA9800477](https://openairdocs.org/sdr/CALA9800477.md): Flange · corroded · Mar 17, 1998 · N14063 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION 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 PL - [SDR CALA9800476](https://openairdocs.org/sdr/CALA9800476.md): Chord · corroded · Mar 17, 1998 · N14063 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION 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 - [SDR CALA9800475](https://openairdocs.org/sdr/CALA9800475.md): Chord · corroded · Mar 17, 1998 · N14063 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION 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 51-31 - [SDR CALA9800474](https://openairdocs.org/sdr/CALA9800474.md): Flange · corroded · Mar 17, 1998 · N14063 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION 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, 53-30-0 - [SDR CALA9800462](https://openairdocs.org/sdr/CALA9800462.md): Vent Box · corroded · Mar 15, 1998 · N14063 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION 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. - [SDR CALA9800461](https://openairdocs.org/sdr/CALA9800461.md): Support · corroded · Mar 15, 1998 · N14063 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION 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. - [SDR CALA9800460](https://openairdocs.org/sdr/CALA9800460.md): Support · corroded · Mar 15, 1998 · N14063 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION 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. - [SDR CALA9800459](https://openairdocs.org/sdr/CALA9800459.md): Angle · cracked · Mar 15, 1998 · N14063 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION 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. - [SDR CALA9800458](https://openairdocs.org/sdr/CALA9800458.md): Angle · cracked · Mar 15, 1998 · N14063 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION 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. - [SDR CALA9800457](https://openairdocs.org/sdr/CALA9800457.md): Support · corroded · Mar 15, 1998 · N14063 · Doug DC1030 · Fuselage Miscellaneous Structure > INTERIOR 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. - [SDR CALA9800456](https://openairdocs.org/sdr/CALA9800456.md): Floor Track · corroded · Mar 15, 1998 · N14063 · Doug DC1030 · Fuselage, Seat/Cargo Attach Fittings > INTERIOR 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. Next page: https://openairdocs.org/deregistered/N14063-2013-06-11/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 = 'N14063' AND deregistration_id = 'N14063-2013-06-11' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N14063-2013-06-11/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.