# Service difficulty reports: N14810, cancelled May 20, 2015 A list on [N14810, cancelled May 20, 2015](https://openairdocs.org/deregistered/N14810-2015-05-20.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 · 79 reports - [SDR CALA0100854](https://openairdocs.org/sdr/CALA0100854.md): Web · cracked · Sep 9, 2001 · N14810 · Doug DC982 · Landing Gear Doors > INSPECTION FOUND A 1" CRACK IN R/H MLG WHEEL WELL DOOR LOWER WEB. A REPAIR WAS INSTALLED IAW EA 9-5281-2-A0920 AND ECRA 5281-01017. - [SDR CALA0100853](https://openairdocs.org/sdr/CALA0100853.md): Shear Tie · cracked · Sep 9, 2001 · N14810 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND A 1" CRACK IN SHEAR TIE AT STA 1418 BETWEEN LONGERON 1R AND 2R. THE SHEAR TIE WAS REMOVED AND A NEW SHEAR TIE WAS INSTALLED IAW SRM 53-03, 51-30-02, 51-10-3, AND 51-30-5. - [SDR CALA0100852](https://openairdocs.org/sdr/CALA0100852.md): Seat Track · corroded · Sep 9, 2001 · N14810 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND SEAT TRACK CORRODED AT FS 200-218, LBL 45. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK, SPLICE, AND TAB WERE INSTALLED IAW SRM 53-03, FIGURE 4B, 51-30-2, 51-10-4, 51-10-3, AND 53-05-4. - [SDR CALA0100851](https://openairdocs.org/sdr/CALA0100851.md): Web · cracked · Sep 9, 2001 · N14810 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND A 4" CRACK IN FRAME TO LONGERON ATTACH WEB IN AFT ACCESSORY AREA AT FS 1430, R/H SIDE. THE CRACK WAS STOP DRILLED IAW SRM 53-01, FIGURE 2. A DOUBLER WAS INSTALLED IAW SRM 53-14-4, 51-10-4, 51-10-3, AND 51-30-2. - [SDR CALA0100850](https://openairdocs.org/sdr/CALA0100850.md): Skin · gouged · Sep 9, 2001 · N14810 · Doug DC982 · Fuselage Main, Plate/Skin > INSPECTION FOUND L/H FUSELAGE SKIN GOUGED AFT OF L-1 DOOR AT STA 218. THE GOUGED SKIN SECTION WAS REMOVED AND A NEW SECTION OF SKIN WAS INSTALLED IAW SRM 51-30-2, 51-10-3, AND ECRA 5330-02445. - [SDR CALA0100843](https://openairdocs.org/sdr/CALA0100843.md): Skin · corroded · Sep 8, 2001 · N14810 · Doug DC982 · Fuselage Main, Plate/Skin > INSPECTION FOUND EXTERNAL FUSELAGE SKIN HAD TWO SHEARED FASTENERS AT FS 1183 WITH CORROSION ON INSIDE. THE DOUBLER WAS REMOVED AND REPLACED IAW SRM 51-10-4, 51-30-5, 51-30-2, ECRA 5330-03100, AND EA 9-5332-2-A924. - [SDR CALA0100841](https://openairdocs.org/sdr/CALA0100841.md): Floor Support · corroded · Sep 7, 2001 · N14810 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND AFT LT LAV FLOOR SUPPORT CORRODED AT STA 1309-1338, L18L. THE CORROSION WAS REMOVED IAW SRM 51-10-3 AND THE SUPPORT WAS REPAIRED IAW EA 9-5314-2-A0919 AND ECRA 5310-04182. - [SDR CALA0100839](https://openairdocs.org/sdr/CALA0100839.md): Angle · corroded · Sep 7, 2001 · N14810 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND CUSP ANGLE CORRODED AT FS 207, LBL 54. THE CUSP ANGLE WAS REMOVED AND A NEW CUSP ANGLE WAS INSTALLED IAW SRM 51-30-1 AND EA 9-5310-2-A0917. - [SDR CALA0100825](https://openairdocs.org/sdr/CALA0100825.md): Pan · corroded · Aug 31, 2001 · N14810 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND FORWARD CARGO DOOR FRAME PAN CORRODED AROUND 10 EACH NUTS. THE PAN AND SPLICES WERE REMOVED IAW SRM 53-05, FIGURE 44. A NEW PAN AND SPLICE WERE INSTALLED IAW SRM 53-05, FIGURE 44. - [SDR CALA0100813](https://openairdocs.org/sdr/CALA0100813.md): Floor Panel · delaminated · Aug 27, 2001 · N14810 · Doug DC982 · Fuselage Floor Panel > INSPECTION FOUND CABIN FLOOR PANEL DELAMINATED AT FS 927-1003. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265. - [SDR CALA0100812](https://openairdocs.org/sdr/CALA0100812.md): Seat Track · corroded · Aug 27, 2001 · N14810 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND MAIN DECK R/H SEAT TRACK CORRODED AT FS 250-788. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-5 AND 53-05, FIGURE 4F. - [SDR CALA0100809](https://openairdocs.org/sdr/CALA0100809.md): Web · cracked · Aug 27, 2001 · N14810 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND WEB CRACKED IN FOUR PLACES AT CANTED FRAME STA 1463, I/B OF LONGERON 7L. THE WEB AND STIFFENERS WERE REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-30-2, 51-30-1, AND 51-10-4. - [SDR CALA0100800](https://openairdocs.org/sdr/CALA0100800.md): Floor Panel · corroded · Aug 24, 2001 · N14810 · Doug DC982 · Fuselage Floor Panel > INSPECTION FOUND FORWARD ENTRY FLOOR PANELS WITH BROKEN AND CORRODED INSERTS AT FS 160-200, LBL 8 TO RBL 6 AND AT FS 200-256. - [SDR CALA0100795](https://openairdocs.org/sdr/CALA0100795.md): Web · corroded · Aug 24, 2001 · N14810 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND CUSP WEB CRACKED AND CORRODED AT FS 218-239, LBL 44 TO LBL 55. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-30-2, 51-10-3, AND 51-30-5. - [SDR CALA0100794](https://openairdocs.org/sdr/CALA0100794.md): Floor Panel · delaminated · Aug 24, 2001 · N14810 · Doug DC982 · Fuselage Floor Panel > INSPECTION FOUND CABIN FORWARD ENTRY FLOOR PANEL DELAMINATED. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265. - [SDR CALA0100793](https://openairdocs.org/sdr/CALA0100793.md): Floor Panel · delaminated · Aug 24, 2001 · N14810 · Doug DC982 · Fuselage Floor Panel > INSPECTION FOUND CABIN R/H FLOOR PANEL DELAMINATED AT FS 245-313 AND A CREASE IN FLOOR PANEL AT FS 313-390. NEW FLOOR PANELS WERE INSTALLED IAW ECRA 5320-01265. - [SDR CALA0100792](https://openairdocs.org/sdr/CALA0100792.md): Floor Panel · delaminated · Aug 24, 2001 · N14810 · Doug DC982 · Fuselage Floor Panel > INSPECTION FOUND CABIN CENTER FLOOR PANEL DELAMINATED AT FS 1003-1079. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265. - [SDR CALA0100791](https://openairdocs.org/sdr/CALA0100791.md): Floor Panel · delaminated · Aug 24, 2001 · N14810 · Doug DC982 · Fuselage Floor Panel > INSPECTION FOUND CABIN CENTER AND L/H FLOOR PANELS DELAMINATED AT FS 769-807 AND FS 769-826. A R/H FLOOR PANEL AT FS 769-807 WAS FOUND TORN AT EDGES. NEW FLOOR PANELS WERE INSTALLED IAW ECRA 5320-01265. - [SDR CALA0100790](https://openairdocs.org/sdr/CALA0100790.md): Floor Panel · damaged · Aug 24, 2001 · N14810 · Doug DC982 · Fuselage Floor Panel > INSPECTION FOUND RT CABIN FLOOR PANEL CREASED AT FS 466-542. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265. - [SDR CALA0100789](https://openairdocs.org/sdr/CALA0100789.md): Floor Panel · delaminated · Aug 24, 2001 · N14810 · Doug DC982 · Fuselage Floor Panel > INSPECTION FOUND CABIN R/H FLOOR PANELS DELAMINATED AT FS 1193-1250 AND FS 1250-1309. NEW FLOOR PANELS WERE INSTALLED IAW ECRA 5320-01265. - [SDR CALA0100788](https://openairdocs.org/sdr/CALA0100788.md): Floor Panel · delaminated · Aug 24, 2001 · N14810 · Doug DC982 · Fuselage Floor Panel > INSPECTION FOUND R/H CABIN FLOOR PANEL DELAMINATED AT FS 826-864 AND R/H CABIN FLOOR PANEL CRACKED AT FS 889-927. NEW FLOOR PANELS WERE INSTALLED IAW ECRA 5320-01265. - [SDR CALA0100787](https://openairdocs.org/sdr/CALA0100787.md): Floor Panel · delaminated · Aug 24, 2001 · N14810 · Doug DC982 · Fuselage Floor Panel > INSPECTION FOUND CABIN CENTER AND R/H FLOOR PANELS DELAMINATED AT FS 1079-1117 AND R/H FLOOR PANEL DELAMINATED AT FS 1117-1174. NEW FLOOR PANELS WERE INSTALLED IAW ECRA 5320-01265. - [SDR CALA0100786](https://openairdocs.org/sdr/CALA0100786.md): Skin · dented · Aug 24, 2001 · N14810 · Doug DC982 · Fuselage Main, Plate/Skin > INSPECTION FOUND L/H FORWARD FUSELAGE EXTERIOR SKIN DENTED BELOW #2 CABIN WINDOW AT FS 264-285, LONGERON 16-18L. THE DENTED SECTION OF SKIN WAS REMOVED AND NEW SKIN WAS INSTALLED IAW ECRA 5330-02445 AND SRM 51-30-2. - [SDR CALA0100783](https://openairdocs.org/sdr/CALA0100783.md): Floor Panel · punctured · Aug 23, 2001 · N14810 · Doug DC982 · Fuselage Floor Panel > INSPECTION FOUND CABIN L/H AND R/H FLOOR PANELS PUNCTURED AT FS 1003-1079. NEW FLOOR PANELS WERE INSTALLED IAW ECRA 5320-01265. - [SDR CALA0100782](https://openairdocs.org/sdr/CALA0100782.md): Floor Panel · delaminated · Aug 23, 2001 · N14810 · Doug DC982 · Fuselage Floor Panel > INSPECTION FOUND CABIN R/H FLOOR PANEL DELAMINATED AT FS 693-765. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265. - [SDR CALA0100781](https://openairdocs.org/sdr/CALA0100781.md): Floor Panel · punctured · Aug 23, 2001 · N14810 · Doug DC982 · Fuselage Floor Panel > INSPECTION FOUND CABIN L/H FLOOR PANEL PUNCTURED AT FS 927-1003. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265. - [SDR CALA0100779](https://openairdocs.org/sdr/CALA0100779.md): Floor Panel · torn · Aug 23, 2001 · N14810 · Doug DC982 · Fuselage Floor Panel > INSPECTION FOUND CABIN CENTER FLOOR PANEL TORN BY INSERT HOLE AT FS 945-1003. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265. - [SDR CALA0100778](https://openairdocs.org/sdr/CALA0100778.md): Floor Panel · delaminated · Aug 23, 2001 · N14810 · Doug DC982 · Fuselage Floor Panel > INSPECTION FOUND CABIN L/H FLOOR PANEL DELAMINATED AT FS 1250-1309. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265. - [SDR CALA0100777](https://openairdocs.org/sdr/CALA0100777.md): Floor Panel · delaminated · Aug 23, 2001 · N14810 · Doug DC982 · Fuselage Floor Panel > INSPECTION FOUND CABIN CENTER FLOOR PANEL DELAMINATED AT FS 254-313. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265. - [SDR CALA0100776](https://openairdocs.org/sdr/CALA0100776.md): Floor Panel · delaminated · Aug 23, 2001 · N14810 · Doug DC982 · Fuselage Floor Panel > INSPECTION FOUND COCKPIT CENTER FLOOR PANEL DELAMINATED AT FS 120-160. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265. - [SDR CALA0100775](https://openairdocs.org/sdr/CALA0100775.md): Floor Panel · delaminated · Aug 23, 2001 · N14810 · Doug DC982 · Fuselage Floor Panel > INSPECTION FOUND CABIN CENTER FLOOR PANELS DELAMINATED AT FS 1250-1309 AND FS 1309-1347. NEW FLOOR PANELS WERE INSTALLED IAW ECRA 5320-01265. - [SDR CALA0100774](https://openairdocs.org/sdr/CALA0100774.md): Floor Panel · delaminated · Aug 23, 2001 · N14810 · Doug DC982 · Fuselage Floor Panel > INSPECTION FOUND CABIN FORWARD ENTRY FLOOR PANEL C & J DELAMINATED. NEW FLOOR PANELS WERE INSTALLED IAW ECRA 5320-01265. - [SDR CALA0100773](https://openairdocs.org/sdr/CALA0100773.md): Floor Panel · corroded · Aug 23, 2001 · N14810 · Doug DC982 · Fuselage Floor Panel > INSPECTION FOUND FORWARD ENTRY FLOOR PANEL CORRODED AT FS 160-200, LBL 8-44. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265. - [SDR CALA0100772](https://openairdocs.org/sdr/CALA0100772.md): Floor Panel · delaminated · Aug 23, 2001 · N14810 · Doug DC982 · Fuselage Floor Panel > INSPECTION FOUND CABIN CENTER FLOOR PANEL DELAMINATED AT FS 826-886. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265. - [SDR CALA0100771](https://openairdocs.org/sdr/CALA0100771.md): Floor Panel · delaminated · Aug 23, 2001 · N14810 · Doug DC982 · Fuselage Floor Panel > INSPECTION FOUND CENTER CABIN FLOOR PANELS AT FS 1117-1174 AND FS 1174-1250 DELAMINATED. LEFT HAND CABIN FLOOR PANELS WERE FOUND DELAMINATED AT FS 1079-1155 AND FS 1155-1250. NEW FLOOR PANELS WERE INSTALLED IAW ECRA 5320-01265. - [SDR CALA0100770](https://openairdocs.org/sdr/CALA0100770.md): Floor Panel · delaminated · Aug 23, 2001 · N14810 · Doug DC982 · Fuselage Floor Panel > INSPECTION FOUND COCKPIT FLOOR PANEL DELAMINATED AT FS 150-160, LBL 8-12. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265. - [SDR CALA0100769](https://openairdocs.org/sdr/CALA0100769.md): Floor Panel · delaminated · Aug 23, 2001 · N14810 · Doug DC982 · Fuselage Floor Panel > INSPECTION FOUND CABIN L/H FLOOR PANEL DELAMINATED AROUND INSERT HOLES AT FS 673-763. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265. - [SDR CALA0100763](https://openairdocs.org/sdr/CALA0100763.md): Intercostal · corroded · Aug 16, 2001 · N14810 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND INTERCOSTAL CORRODED AT FS 1308-1322, LONGERONS 27L-28L. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-30-2. - [SDR CALA0001965](https://openairdocs.org/sdr/CALA0001965.md): Strut · discharged · Dec 19, 2000 · N14810 · Doug DC982 · Nose/Tail Landing Gear Strut/Axle > THE NLG WOULD NOT RETRACT AFTER TAKEOFF FROM IND. THE AIRCRAFT WAS RETURNED TO IND WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE STRUT PRESSURE LOW. THE STRUT WAS SERVICED WITH NITROGEN AND THE NOSE GEAR WAS LUBRICATED. A DIP WAS ISSUED FOR FULL - [SDR CALA9901295](https://openairdocs.org/sdr/CALA9901295.md): Seat Track · corroded · Sep 24, 1999 · N14810 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND RT SEAT TRACK CORRODED AT FS 1007-1320, RBL 24. THE SEAT TRACK WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 51-30-2 AND 51-30-1. - [SDR CALA9901294](https://openairdocs.org/sdr/CALA9901294.md): Panel · cracked · Sep 24, 1999 · N14810 · Doug DC982 · Vertical Stabilizer, Plate/Skin > INSPECTION FOUND A 3 CRACK IN VERTICAL STABILIZER PANEL ON LT SIDE. A REPAIR DOUBLER WAS INSTALLED IAW SRM 55-01, FIGURE 2, SHEET 2, 51-60-0, PAGE 5, 51-30-5, AND 51-30-2. - [SDR CALA9901277](https://openairdocs.org/sdr/CALA9901277.md): Skin · dented · Sep 22, 1999 · N14810 · Doug DC982 · Leading Edge Devices > INSPECTION FOUND LT SLAT 0 DENTED. THE DENTED AREA WAS CUT OUT IAW SRM 57-6, FIGURE 1. A REPAIR WAS INSTALLED IAW ECRA 5720-01170. - [SDR CALA9901266](https://openairdocs.org/sdr/CALA9901266.md): Fairing · cracked · Sep 19, 1999 · N14810 · Doug DC982 · Aerodynamic Fairings > INSPECTION FOUND A 3 INCH CRACK IN RT HORIZONTAL STABILIZER FAIRING. THE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-30-2. - [SDR CALA9901265](https://openairdocs.org/sdr/CALA9901265.md): Doubler · corroded · Sep 19, 1999 · N14810 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND DOUBLER AT SILL OF DOOR JAMB CORRODED AT FS 1174-1183, LONGERON 27R (AFT PIT). THE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-30-5, 51-30-1, 53-14-3, AND 51-10-4. - [SDR CALA9901264](https://openairdocs.org/sdr/CALA9901264.md): Vane · gouged · Sep 19, 1999 · N14810 · Doug DC982 · Wing Miscellaneous Structure > INSPECTION FOUND RT WING O/B NR 2 FIXED VANE GOUGED. THE FIXED VANE WAS REMOVED AND REPAIRED IAW DRAWING NR SR09570025. THE VANE WAS REINSTALLED IAW MM 27-51-03. - [SDR CALA9901263](https://openairdocs.org/sdr/CALA9901263.md): Skin · delaminated · Sep 19, 1999 · N14810 · Doug DC982 · Spoilers > INSPECTION FOUND RT GROUND SPOILER DELAMINATED. THE SPOILER WAS REMOVED, REPAIRED, AND REINSTALLED IAW MM 27-62-01. - [SDR CALA9901262](https://openairdocs.org/sdr/CALA9901262.md): Vane · punctured · Sep 19, 1999 · N14810 · Doug DC982 · Wing Miscellaneous Structure > INSPECTION FOUND LT WING I/B FIXED VANE PUNCTURED ON TOP CENTER. THE VANE WAS REMOVED, REPAIRED, AND REINSTALLED IAW MM 27-51-03. - [SDR CALA9901261](https://openairdocs.org/sdr/CALA9901261.md): Pan · corroded · Sep 19, 1999 · N14810 · Doug DC982 · Cargo/Baggage Doors > INSPECTION FOUND FORWARD CARGO DOOR PAN LOWER SIDE CORRODED AROUND RIB NUTS. THE PAN WAS REMOVED AND A NEW PAN WAS INSTALLED IAW SRM 51-30-2, 51-30-5, 51-30-1, 51-30-7, AND 51-20-0. - [SDR CALA9901260](https://openairdocs.org/sdr/CALA9901260.md): Support · cracked · Sep 19, 1999 · N14810 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND A 2 INCH CRACK IN MID CARGO PIT LEFT CEILING SUPPORT AT STA 731, LBL 24. THE CRACK WAS STOP DRILLED IAW SRM 53-01, FIGURE 2. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 2, 51-10-3, AND 53-10, FIGURE 2. - [SDR CALA9901259](https://openairdocs.org/sdr/CALA9901259.md): Fitting · corroded · Sep 18, 1999 · N14810 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND RT GALLEY SUPPORT FITTING CORRODED AT FS 200, RBL 48. THE GALLEY SUPPORT FITTING WAS REMOVED AND A NEW ONE WAS INSTALLED IAW SRM 51-30-2. Next page: https://openairdocs.org/deregistered/N14810-2015-05-20/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 = 'N14810' AND deregistration_id = 'N14810-2015-05-20' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N14810-2015-05-20/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.