N14810, cancelled May 20, 2015

Service difficulty reports · 79

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 = 'N14810' AND deregistration_id = 'N14810-2015-05-20'
  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 CALA0100854Web · crackedINSPECTION 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.Sep 9, 2001 · N14810 · Doug DC982 · Landing Gear DoorsSDR CALA0100853Shear Tie · crackedINSPECTION 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.Sep 9, 2001 · N14810 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0100852Seat Track · corrodedINSPECTION 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.Sep 9, 2001 · N14810 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0100851Web · crackedINSPECTION 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.Sep 9, 2001 · N14810 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0100850Skin · gougedINSPECTION 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.Sep 9, 2001 · N14810 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0100843Skin · corrodedINSPECTION 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.Sep 8, 2001 · N14810 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0100841Floor Support · corrodedINSPECTION 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.Sep 7, 2001 · N14810 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0100839Angle · corrodedINSPECTION 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.Sep 7, 2001 · N14810 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0100825Pan · corrodedINSPECTION 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.Aug 31, 2001 · N14810 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0100813Floor Panel · delaminatedINSPECTION FOUND CABIN FLOOR PANEL DELAMINATED AT FS 927-1003. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265.Aug 27, 2001 · N14810 · Doug DC982 · Fuselage Floor PanelSDR CALA0100812Seat Track · corrodedINSPECTION 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.Aug 27, 2001 · N14810 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0100809Web · crackedINSPECTION 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.Aug 27, 2001 · N14810 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0100800Floor Panel · corrodedINSPECTION FOUND FORWARD ENTRY FLOOR PANELS WITH BROKEN AND CORRODED INSERTS AT FS 160-200, LBL 8 TO RBL 6 AND AT FS 200-256.Aug 24, 2001 · N14810 · Doug DC982 · Fuselage Floor PanelSDR CALA0100795Web · corrodedINSPECTION 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.Aug 24, 2001 · N14810 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0100794Floor Panel · delaminatedINSPECTION FOUND CABIN FORWARD ENTRY FLOOR PANEL DELAMINATED. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265.Aug 24, 2001 · N14810 · Doug DC982 · Fuselage Floor PanelSDR CALA0100793Floor Panel · delaminatedINSPECTION 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.Aug 24, 2001 · N14810 · Doug DC982 · Fuselage Floor PanelSDR CALA0100792Floor Panel · delaminatedINSPECTION FOUND CABIN CENTER FLOOR PANEL DELAMINATED AT FS 1003-1079. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265.Aug 24, 2001 · N14810 · Doug DC982 · Fuselage Floor PanelSDR CALA0100791Floor Panel · delaminatedINSPECTION 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.Aug 24, 2001 · N14810 · Doug DC982 · Fuselage Floor PanelSDR CALA0100790Floor Panel · damagedINSPECTION FOUND RT CABIN FLOOR PANEL CREASED AT FS 466-542. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265.Aug 24, 2001 · N14810 · Doug DC982 · Fuselage Floor PanelSDR CALA0100789Floor Panel · delaminatedINSPECTION FOUND CABIN R/H FLOOR PANELS DELAMINATED AT FS 1193-1250 AND FS 1250-1309. NEW FLOOR PANELS WERE INSTALLED IAW ECRA 5320-01265.Aug 24, 2001 · N14810 · Doug DC982 · Fuselage Floor PanelSDR CALA0100788Floor Panel · delaminatedINSPECTION 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.Aug 24, 2001 · N14810 · Doug DC982 · Fuselage Floor PanelSDR CALA0100787Floor Panel · delaminatedINSPECTION 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.Aug 24, 2001 · N14810 · Doug DC982 · Fuselage Floor PanelSDR CALA0100786Skin · dentedINSPECTION 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.Aug 24, 2001 · N14810 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0100783Floor Panel · puncturedINSPECTION FOUND CABIN L/H AND R/H FLOOR PANELS PUNCTURED AT FS 1003-1079. NEW FLOOR PANELS WERE INSTALLED IAW ECRA 5320-01265.Aug 23, 2001 · N14810 · Doug DC982 · Fuselage Floor PanelSDR CALA0100782Floor Panel · delaminatedINSPECTION FOUND CABIN R/H FLOOR PANEL DELAMINATED AT FS 693-765. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265.Aug 23, 2001 · N14810 · Doug DC982 · Fuselage Floor PanelSDR CALA0100781Floor Panel · puncturedINSPECTION FOUND CABIN L/H FLOOR PANEL PUNCTURED AT FS 927-1003. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265.Aug 23, 2001 · N14810 · Doug DC982 · Fuselage Floor PanelSDR CALA0100779Floor Panel · tornINSPECTION FOUND CABIN CENTER FLOOR PANEL TORN BY INSERT HOLE AT FS 945-1003. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265.Aug 23, 2001 · N14810 · Doug DC982 · Fuselage Floor PanelSDR CALA0100778Floor Panel · delaminatedINSPECTION FOUND CABIN L/H FLOOR PANEL DELAMINATED AT FS 1250-1309. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265.Aug 23, 2001 · N14810 · Doug DC982 · Fuselage Floor PanelSDR CALA0100777Floor Panel · delaminatedINSPECTION FOUND CABIN CENTER FLOOR PANEL DELAMINATED AT FS 254-313. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265.Aug 23, 2001 · N14810 · Doug DC982 · Fuselage Floor PanelSDR CALA0100776Floor Panel · delaminatedINSPECTION FOUND COCKPIT CENTER FLOOR PANEL DELAMINATED AT FS 120-160. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265.Aug 23, 2001 · N14810 · Doug DC982 · Fuselage Floor PanelSDR CALA0100775Floor Panel · delaminatedINSPECTION FOUND CABIN CENTER FLOOR PANELS DELAMINATED AT FS 1250-1309 AND FS 1309-1347. NEW FLOOR PANELS WERE INSTALLED IAW ECRA 5320-01265.Aug 23, 2001 · N14810 · Doug DC982 · Fuselage Floor PanelSDR CALA0100774Floor Panel · delaminatedINSPECTION FOUND CABIN FORWARD ENTRY FLOOR PANEL C & J DELAMINATED. NEW FLOOR PANELS WERE INSTALLED IAW ECRA 5320-01265.Aug 23, 2001 · N14810 · Doug DC982 · Fuselage Floor PanelSDR CALA0100773Floor Panel · corrodedINSPECTION FOUND FORWARD ENTRY FLOOR PANEL CORRODED AT FS 160-200, LBL 8-44. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265.Aug 23, 2001 · N14810 · Doug DC982 · Fuselage Floor PanelSDR CALA0100772Floor Panel · delaminatedINSPECTION FOUND CABIN CENTER FLOOR PANEL DELAMINATED AT FS 826-886. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265.Aug 23, 2001 · N14810 · Doug DC982 · Fuselage Floor PanelSDR CALA0100771Floor Panel · delaminatedINSPECTION 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.Aug 23, 2001 · N14810 · Doug DC982 · Fuselage Floor PanelSDR CALA0100770Floor Panel · delaminatedINSPECTION FOUND COCKPIT FLOOR PANEL DELAMINATED AT FS 150-160, LBL 8-12. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265.Aug 23, 2001 · N14810 · Doug DC982 · Fuselage Floor PanelSDR CALA0100769Floor Panel · delaminatedINSPECTION FOUND CABIN L/H FLOOR PANEL DELAMINATED AROUND INSERT HOLES AT FS 673-763. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265.Aug 23, 2001 · N14810 · Doug DC982 · Fuselage Floor PanelSDR CALA0100763Intercostal · corrodedINSPECTION 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.Aug 16, 2001 · N14810 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001965Strut · dischargedTHE 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 FULLDec 19, 2000 · N14810 · Doug DC982 · Nose/Tail Landing Gear Strut/AxleSDR CALA9901295Seat Track · corrodedINSPECTION 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.Sep 24, 1999 · N14810 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA9901294Panel · crackedINSPECTION 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.Sep 24, 1999 · N14810 · Doug DC982 · Vertical Stabilizer, Plate/SkinSDR CALA9901277Skin · dentedINSPECTION 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.Sep 22, 1999 · N14810 · Doug DC982 · Leading Edge DevicesSDR CALA9901266Fairing · crackedINSPECTION 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.Sep 19, 1999 · N14810 · Doug DC982 · Aerodynamic FairingsSDR CALA9901265Doubler · corrodedINSPECTION 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.Sep 19, 1999 · N14810 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA9901264Vane · gougedINSPECTION 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.Sep 19, 1999 · N14810 · Doug DC982 · Wing Miscellaneous StructureSDR CALA9901263Skin · delaminatedINSPECTION FOUND RT GROUND SPOILER DELAMINATED. THE SPOILER WAS REMOVED, REPAIRED, AND REINSTALLED IAW MM 27-62-01.Sep 19, 1999 · N14810 · Doug DC982 · SpoilersSDR CALA9901262Vane · puncturedINSPECTION FOUND LT WING I/B FIXED VANE PUNCTURED ON TOP CENTER. THE VANE WAS REMOVED, REPAIRED, AND REINSTALLED IAW MM 27-51-03.Sep 19, 1999 · N14810 · Doug DC982 · Wing Miscellaneous StructureSDR CALA9901261Pan · corrodedINSPECTION 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.Sep 19, 1999 · N14810 · Doug DC982 · Cargo/Baggage DoorsSDR CALA9901260Support · crackedINSPECTION 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.Sep 19, 1999 · N14810 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA9901259Fitting · corrodedINSPECTION 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.Sep 18, 1999 · N14810 · Doug DC982 · Fuselage Miscellaneous Structure
Back to N14810, cancelled May 20, 2015