N15841, cancelled Jul 16, 2008

Service difficulty reports · 95

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 = 'N15841' AND deregistration_id = 'N15841-2008-07-16'
  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 CALA0400410Web · crackedWEB CRACKED AT FWD LWR SIDE OF BAG BIN DOOR AT STA 636, LONG 27 LEFT. REMOVED AND REPLACED WEB PER ECRA 5310-04416.Apr 23, 2004 · N15841 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0400404Shear Tie · corrodedA/B/B SHEAR TIE CORRODED AT LONGERON 30 AND 28 RIGHT AT STATION 1193. FABRICATED AND INSTALLED SHEAR TIE REPAIR SPLICE BETWEEN LONG 30 AND 29 RIGHT PER SRM 53-03 FIG 3.Apr 20, 2004 · N15841 · Doug DC982 · Fuselage Main, Longeron/StringerSDR CALA0300053Longeron · crackedINSPECTION FOUND LONGERON 2L CRACKED AT STA 1418. REPAIRED IAW ECRA 5311-01132.Feb 17, 2003 · N15841 · Doug DC982 · Fuselage Main, Longeron/StringerSDR CALA0300048Longeron · crackedINSPECTION FOUND A 2" CRACK IN LONGERON 2R AT STA 1418. A SECTION OF LONGERON WAS SPLICED IN IAW ECRA 5311-01132.Feb 15, 2003 · N15841 · Doug DC982 · Fuselage Main, Longeron/StringerSDR CALA0001412Skin · crackedINSPECTION FOUND LT WING LEADING EDGE SKIN CRACKED AT APPROXIMATELY STA XIS 60. REPAIR DOUBLERS, SHIMS, ANGLES, AND NUT PLATE STRIPS WERE INSTALLED IAW EA 9-5721-2-AD760 AND ECRA 5721-01057.Sep 12, 2000 · N15841 · Doug DC982 · Wing, Plate/SkinSDR CALA0001411Frame · corrodedINSPECTION FOUND AFT CARGO FRAME AFT SIDE CORRODED UNDER PAINT AT FS 1309, L24R-24L. THE CORRODED SECTION WAS CUT OUT AND A FRAME REPAIR SPLICE WAS INSTALLED IAW SRM 53-03, FIGURE 2A.Sep 12, 2000 · N15841 · Doug DC982 · Fuselage Main, FrameSDR CALA0001410Cargo Track · corrodedINSPECTION FOUND MID CARGO RT CARGO TIE DOWN TRACK CORRODED AT FS 532 - 625 AND FS 693 - 807. THE TIE DOWN TRACK SECTIONS WERE REMOVED AND NEW TRACK SECTIONS WERE INSTALLED IAW SRM 53-05, FIGURE 4.Sep 11, 2000 · N15841 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0001409Skin · crackedAN INTERIM REPAIR WAS REMOVED AND A PERMANENT REPAIR WAS INSTALLED WHERE A 1 INCH CRACK EXISTED ON L/E LOWER SURFACE OF LT WING SKIN AT NR 2 SLAT CENTER TRACK CUTOUT, XFS 206. THE INTERIM REPAIR WAS REMOVED IAW SRM 51-10-4. EXTERNAL AND INTERNAL DOUBLERS ANDSep 11, 2000 · N15841 · Doug DC982 · Wing, Plate/SkinSDR CALA0001408Fairing · crackedINSPECTION FOUND A 1 INCH CRACK IN RT WING FLAP HINGE FAIRING NR 3 AFT. THE CRACK WAS STOP DRILLED AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 57-01, FIGURE 3, SHEET 2, 51-10-4, AND 51-10-3.Sep 11, 2000 · N15841 · Doug DC982 · Wing Miscellaneous StructureSDR CALA0001403Floor Support · corrodedINSPECTION FOUND MID CARGO RT TRACK FLOOR SUPPORT CORRODED AT FS 598 - 636. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-01, 51-10-04, 51-30-02, AND 51-30-01.Sep 8, 2000 · N15841 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001402Seat Track · corrodedINSPECTION FOUND LEFT I/B CABIN SEAT TRACK CORRODED AT FS 1117 - 1309. THE CORROSION WAS REMOVED IAW SRM 53-05, FIGURE 4. CORROSION REMOVAL WAS WITHIN LIMITS FROM FS 1212 - 1309. THE SEAT TRACK SECTION FROM FS 1117 - 1212 WAS REPLACED IAW SRM 51-30-1, 53-05Sep 7, 2000 · N15841 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0001400Skin · dentedINSPECTION FOUND NR 2 LEFT T/E FLAP DENTED ON LOWER SIDE. THE DENTED AREA WAS TRIMMED OUT AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 57-01, FIGURE 5 AND FIGURE 3.Sep 5, 2000 · N15841 · Doug DC982 · Trailing Edge FlapsSDR CALA0001399Angle · crackedINSPECTION FOUND FOUR VERTICAL STABILIZER DOGHOUSE ANGLES CRACKED. LOCATIONS WERE RT AND LT FWD LOWER AND RT AND LT AFT LOWER AREA. THE CRACKS WERE .5 INCH LONG. THE ANGLES WERE REPAIRED IAW SRM 55-01, FIGURE 2, 55-10-4, 51-10-3, AND 51-30-2.Sep 5, 2000 · N15841 · Doug DC982 · Vertical StabilizerSDR CALA0001398Door Frame · corrodedINSPECTION FOUND AFT CARGO DOOR CUTOUT LOWER JAMB CORRODED. A DOUBLER AND STRAP WERE INSTALLED IAW SRM 51-10-4 AND ECRA 5310-03027.Sep 5, 2000 · N15841 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001397Doubler · corrodedINSPECTION FOUND ANTENNA DOUBLER CORRODED ON MOUNTING FLANGE AT FS 700, LONGERON 30. THE ANTENNA DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-30-2 AND 51-30-5.Sep 5, 2000 · N15841 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0001389Pan · crackedINSPECTION FOUND A 1.9 INCH CRACK AT CAM LATCH OF FWD CARGO DOOR FWD EDGE OF INNER PAN. THE CRACKED SECTION WAS REMOVED IAW EA 9-5231-2-A0749. A REPAIR ANGLE AND FILLER WERE INSTALLED IAW SRM 52-05, FIGURE 26A, 51-10-3, 51-30-2, AND 51-30-5.Sep 3, 2000 · N15841 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0001388Angle · corrodedINSPECTION FOUND UPPER AND LOWER SURFACE OF DOOR Z-ANGLE CORRODED AT RT SIDE OF AFT PIT. THE Z-ANGLE WAS REMOVED AND A NEW Z-ANGLE WAS INSTALLED IAW SRM 51-30-1, 51-10-3, AND 51-30-2.Sep 3, 2000 · N15841 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0001387Bracket · corrodedINSPECTION FOUND L-2 DOOR THRESHOLD SUPPORT BRACKETS CORRODED. THE BRACKETS WERE REMOVED AND NEW BRACKETS WERE INSTALLED IAW SRM 51-30-5.Sep 3, 2000 · N15841 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001386Cargo Track · corrodedINSPECTION FOUND RT TIEDOWN TRACK CORRODED FROM STA 1211 - 1309 AND LT TIEDOWN TRACK CORRODED FROM STA 1007 - 1309 IN AFT PIT. THE TRACKS WERE REMOVED AND NEW TRACKS WERE INSTALLED IAW SRM 53-05, FIGURE 5, 51-10-3, 51-10-4, AND 51-30-5.Sep 3, 2000 · N15841 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0001385Seat Track · corrodedINSPECTION FOUND LEFT I/B SEAT TRACK CORRODED AT FS 936 - 1212. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-1 AND 53-05, FIGURE 1.Sep 3, 2000 · N15841 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0001383Fairing · crackedINSPECTION FOUND A 1 INCH CRACK IN RT UPPER HORIZONTAL STABILIZER BANANA FAIRING ON FORWARD END. A REPAIR DOUBLER WAS INSTALLED IAW SRM 55-01, FIGURE 2, 55-10-0, FIGURE 7, AND 51-30-02.Sep 3, 2000 · N15841 · Doug DC982 · Horizontal Stabilizer StructureSDR CALA0001382Frame · crackedINSPECTION FOUND A 3 INCH CRACK IN LT MLG WHEEL WELL DOOR FRAME AT O/B FORWARD CORNER. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-30-2, 51-30-1, AND 51-30-8.Sep 3, 2000 · N15841 · Doug DC982 · Landing Gear DoorsSDR CALA0001381Cargo Track · corrodedINSPECTION FOUND LT CARGO TIE DOWN TRACK CORRODED IN MID CARGO COMPARTMENT AT FS 522. THE TIE DOWN TRACK WAS REMOVED AND A REPLACEMENT TRACK WAS INSTALLED IAW SRM 53-05, FIGURE 4G.Sep 3, 2000 · N15841 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0001380Seat Track · corrodedINSPECTION FOUND LT CENTER SEAT TRACK CORRODED AT STA 1126 - 1240. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1, 51-30-2, AND 53-05, FIGURE 4.Sep 3, 2000 · N15841 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0001379Skin · dentedINSPECTION FOUND LOWER FUSELAGE SKIN DENTED AT STA 294, LONGERON 22L. THE SKIN WAS REPAIRED IAW SRM 53-04, FIGURE 38G.Sep 3, 2000 · N15841 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0001378Structure · corrodedINSPECTION FOUND CABIN AREA SUPPORT CORRODED AT STA 200, LBL 10. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2, 53-14-1, 51-10-4, 51-10-3, AND 51-30-5.Sep 3, 2000 · N15841 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001377Doubler · gougedINSPECTION FOUND FORWARD CARGO DOOR FORWARD LOWER OUTER SKIN DOUBLER LOWER EDGE GOUGED. THE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-30-2.Sep 3, 2000 · N15841 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0001376Web · bentINSPECTION FOUND CABIN SUBFLOOR LIGHTENING HOLE DOUBLER BENT AND TORN AT STA 160, LBL 12. THE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-30-2, 51-10-4, AND 51-10-3.Sep 3, 2000 · N15841 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001375Structure · crackedINSPECTION FOUND A 1 INCH CRACK IN RT WING LEADING EDGE I/B SUPPORT. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-10-4, AND 51-10-3.Sep 3, 2000 · N15841 · Doug DC982 · Wing Miscellaneous StructureSDR CALA0001373Floor Panel · corrodedINSPECTION FOUND COCKPIT RT METAL FLOOR PANEL CORRODED AND DENTED. THE FLOOR PANEL WAS REMOVED AND REPLACED IAW SRM 51-30-1 AND 53-24-0.Sep 3, 2000 · N15841 · Doug DC982 · Fuselage Floor PanelSDR CALA0001367Floor Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 160, BL 0. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW 51-30-02, 51-10-04, AND 51-30-05.Sep 2, 2000 · N15841 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001366Floor Support · corrodedINSPECTION FOUND CABIN FLOOR SUPPORTS CORRODED AT STA 160, RBL 45 AND AT STA 200, RBL 51. THE FLOOR SUPPORTS WERE REMOVED AND NEW SUPPORTS WERE INSTALLED IAW SRM 51-30-05, 51-10-04, 51-10-2, AND 51-30-1.Sep 2, 2000 · N15841 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001365Bracket · crackedINSPECTION FOUND A 1 INCH CRACK IN TWO AFT CARGO PIT L BRACKETS AT FORWARD AND AFT END OF OVERHEAD CARGO DOOR LATCH SUPPORT. THE BRACKETS WERE REMOVED AND REPLACED IAW SRM 51-10-2, 51-10-3, AND 51-30-2.Sep 2, 2000 · N15841 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001364Bracket · crackedINSPECTION FOUND TWO L BRACKETS CRACKED IN FORWARD CARGO PIT AT FORWARD AND AFT END OF CARGO DOOR LATCH SUPPORT. THE CRACKS WERE .25 INCH LONG. THE BRACKETS WERE REMOVED AND NEW BRACKETS WERE INSTALLED IAW SRM 51-30-2 AND 51-10-4.Sep 2, 2000 · N15841 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001363Panel · crackedINSPECTION FOUND A 1 INCH CRACK IN AFT CARGO CENTER FLOOR TRANSITION PANEL AT STA 1212 - 1231. THE CRACKED AREA WAS TRIMMED OUT IAW SRM 53-01, FIGURE 4, SHEET 3. DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-01, 51-10-4, 51-10-3, AND 51-30-2.Sep 2, 2000 · N15841 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001361Floor Support · corrodedINSPECTION FOUND CABIN AREA FLOOR SUPPORTS CORRODED AT STA 200, BL 0 AND AT STA 140 - 200, RBL 7. THE FLOOR SUPPORTS WERE REMOVED AND NEW SUPPORTS WERE INSTALLED IAW SRM 51-30-02, 51-10-03, 51-10-04, AND 51-30-1.Sep 2, 2000 · N15841 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001360Angle · crackedINSPECTION FOUND A 1 INCH CRACK IN LT MLG FORWARD KEELBEAM ANGLE. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-4, 51-10-03, 51-30-05, AND 51-30-01.Sep 2, 2000 · N15841 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001359Skin · dentedINSPECTION FOUND L-1 DOOR UPPER AFT I/B EDGE DENTED. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38.Sep 2, 2000 · N15841 · Doug DC982 · Passenger/Crew DoorsSDR CALA0001354Skin · dentedINSPECTION FOUND LOWER FUSELAGE SKIN DENTED AT STA 294, LONGERON 21L. THE SKIN WAS REPAIRED IAW SRM 53-04, FIGURE 38, VIEW G.Aug 31, 2000 · N15841 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0001353Seat Track · corrodedINSPECTION FOUND LEFT O/B SEAT TRACK AFT OF L-2 DOOR CORRODED AT FS 1174. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-1, 51-10-4, AND 51-10-3.Aug 31, 2000 · N15841 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0001352Floor Support · crackedINSPECTION FOUND A 1 INCH CRACK IN LOWER FLOOR PANEL SUPPORT IN FORWARD CARGO AREA AT FS 522. THE FLOOR PANEL SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-02 AND 51-10-03.Aug 31, 2000 · N15841 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001351Web · corrodedINSPECTION FOUND LOWER SURFACE OF CABIN SUBFLOOR CORRODED AT FS 200 BETWEEN BL 0 AND RT SIDE OF AIRCRAFT. THE SUBFLOOR WAS REMOVED AND REPLACED IAW SRM 53-14-01, FIGURE 11, 51-10-3, AND ECRA 5100-01844.Aug 31, 2000 · N15841 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001348Skin · dentedINSPECTION FOUND LOWER FUSELAGE SKIN DENTED AT FS 465, LONGERON 23R - 24R. THE SKIN WAS REPAIRED IAW SRM 53-04, FIGURE 38, VIEW G.Aug 29, 2000 · N15841 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0001347Floor Support · corrodedINSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT FS 168, RBL 28. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-2.Aug 29, 2000 · N15841 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001346Floor Support · corrodedINSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT FS 200, RBL 29. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2, 53-14-1, AND 51-10-4.Aug 29, 2000 · N15841 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001345Skin · dentedINSPECTION FOUND AFT CARGO DOOR EXTERIOR SKIN DENTED. REPAIRED SKIN IAW SRM 52-05, FIGURE 1 AND 51-10-3.Aug 29, 2000 · N15841 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0001344Fitting · corrodedINSPECTION FOUND FORWARD AIRSTAIRS DOOR MOUNT BASE FITTING CORRODED AT STA 180. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AND 51-30-1.Aug 29, 2000 · N15841 · Doug DC982 · Entrance StairsSDR CALA0001340Web · crackedINSPECTION FOUND TWO 1 INCH CRACKS IN RT CUSP WEB AT FS 218 - 237. THE CUSP WEB WAS REMOVED AND A NEW PART WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AND 51-30-2.Aug 28, 2000 · N15841 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001339Floor Support · corrodedINSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT STA 160, LBL 52. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-5, 51-10-4, AND 51-30-2.Aug 28, 2000 · N15841 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001338Cover · corrodedINSPECTION FOUND CABIN FLOOR SUPPORT COVER PLATE CORRODED AT FS 160 - 200, RBL 54. THE COVER PLATE WAS REMOVED AND A NEW COVER PLATE WAS INSTALLED IAW SRM 51-30-1.Aug 28, 2000 · N15841 · Doug DC982 · Fuselage Miscellaneous Structure
Back to N15841, cancelled Jul 16, 2008