# Service difficulty reports: N83873, cancelled Dec 21, 2004 A list on [N83873, cancelled Dec 21, 2004](https://openairdocs.org/deregistered/N83873-2004-12-21.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 · 91 reports - [SDR CALA0200432](https://openairdocs.org/sdr/CALA0200432.md): Intercostal · corroded · Jul 29, 2002 · N83873 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND INTERCOSTAL CORRODED AT FS 1117-1136, L21L. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-30-5. - [SDR CALA0200429](https://openairdocs.org/sdr/CALA0200429.md): Angle · corroded · Jul 24, 2002 · N83873 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND L-2 DOOR JAMB ANGLE AT FORWARD LOWER CORNER CORRODED AT LOWER END, STA 1136. THE CORRODED SECTION OF ANGLE WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW ECRA 5311-01130. - [SDR CALA0200428](https://openairdocs.org/sdr/CALA0200428.md): Web · corroded · Jul 24, 2002 · N83873 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND CUSP WEB CORRODED AT FS 1174-1250, LBL 44-58. THE CUSP WEB WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-1. - [SDR CALA0200427](https://openairdocs.org/sdr/CALA0200427.md): Seat Track · corroded · Jul 24, 2002 · N83873 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND L/H CENTER SEAT TRACK CORRODED AT STA 1070. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1 AND 51-30-2. - [SDR CALA0200424](https://openairdocs.org/sdr/CALA0200424.md): Web · corroded · Jul 20, 2002 · N83873 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND CUSP WEB CORRODED AT FS 1155-1212, LBL 48-58. REPAIRED IAW ECRA 5310-04269. - [SDR CALA0200423](https://openairdocs.org/sdr/CALA0200423.md): Fitting · corroded · Jul 20, 2002 · N83873 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND FLOORBEAM TO FRAME END FITTING CORRODED AT FS 1174. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-5. - [SDR CALA0200422](https://openairdocs.org/sdr/CALA0200422.md): Longeron · corroded · Jul 20, 2002 · N83873 · Doug DC982 · Fuselage Main, Longeron/Stringer > INSPECTION FOUND LONGERON 20L CORRODED AT FS 1174. REPAIRED IAW ECRA 5310-04264. - [SDR CALA0200418](https://openairdocs.org/sdr/CALA0200418.md): Longeron · corroded · Jul 18, 2002 · N83873 · Doug DC982 · Fuselage Main, Longeron/Stringer > INSPECTION FOUND LONGERON 26L CORRODED ON O/B SURFACE AT FS 1200. THE LONGERON WAS REMOVED AND REPLACED IAW ECRA 5310-04268. - [SDR CALA0200417](https://openairdocs.org/sdr/CALA0200417.md): Seat Track · corroded · Jul 18, 2002 · N83873 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND L/H O/B SEAT TRACK CORRODED AT G-3 GALLEY ATTACH POINT. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1. - [SDR CALA0200416](https://openairdocs.org/sdr/CALA0200416.md): Angle · corroded · Jul 18, 2002 · N83873 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND L2 DOOR JAMB CUSP ANGLE CORRODED AT STA 1089-1221, LBL 54. THE CORROSION WAS REMOVED IAW SRM 53-01, FIGURE 1. REPAIR WAS INSTALLED IAW SRM 51-10-4 AND 51-30-05. - [SDR CALA0200415](https://openairdocs.org/sdr/CALA0200415.md): Seat Track · corroded · Jul 18, 2002 · N83873 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND O/B SEAT TRACK CORRODED AT #4 GALLEY ATTACH POINT, FS 1180, LBL 54. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-10-4. - [SDR CALA0200414](https://openairdocs.org/sdr/CALA0200414.md): Longeron · corroded · Jul 18, 2002 · N83873 · Doug DC982 · Fuselage Main, Longeron/Stringer > INSPECTION FOUND LONGERON 19L CORRODED AT FS 1174. THE CORRODED SECTION OF LONGERON WAS REMOVED AND REPLACED IAW EA 9-5312-2-A0961. - [SDR CALA0200413](https://openairdocs.org/sdr/CALA0200413.md): Doubler · corroded · Jul 18, 2002 · N83873 · Doug DC982 · Fuselage Main, Plate/Skin > INSPECTION FOUND L-2 DOOR FAIL SAFE DOUBLER CORRODED AT FS 1128, LONGERON 19L. THE FAIL SAFE DOUBLER WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5. - [SDR CALA0200412](https://openairdocs.org/sdr/CALA0200412.md): Intercostal · corroded · Jul 18, 2002 · N83873 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND INTERCOSTAL CORRODED AT FS 1155-1174, LONGERON 21L. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-4. - [SDR CALA0200411](https://openairdocs.org/sdr/CALA0200411.md): Intercostal · corroded · Jul 18, 2002 · N83873 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND AFT CARGO COMPARTMENT DOOR CUTOUT TORQUE BOX VERTICAL SUPPORTS FOR SKIN CORRODED AT LOWER ATTACH ANGLES, FS 1100-1200. REMOVED SCUFF PLATE FOR ACCESS IAW SRM 51-30-1. REPLACED TWO EACH INTERCOSTALS IAW SRM 51-30-2 AND 51-30-5. - [SDR CALA0200410](https://openairdocs.org/sdr/CALA0200410.md): Support · corroded · Jul 18, 2002 · N83873 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND FORWARD AND AFT GIRT BAR SUPPORT FITTINGS CORRODED AT L-2 DOOR JAMB. REMOVED AND REPLACED TWO EACH GIRT BAR SUPPORTS IAW SRM 51-30-2. - [SDR CALA0200409](https://openairdocs.org/sdr/CALA0200409.md): Shear Tie · corroded · Jul 18, 2002 · N83873 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND SHEAR TIE CORRODED AT FS 1291 JUST ABOVE LONGERON 24L. THE SHEAR TIE WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5. - [SDR CALA0200408](https://openairdocs.org/sdr/CALA0200408.md): Skin · corroded · Jul 18, 2002 · N83873 · Doug DC982 · Fuselage Main, Plate/Skin > INSPECTION FOUND AFT CARGO COMPARTMENT SKIN CORRODED AROUND LONGERON 26R AT FS 1220-1231. THE CORRODED AREA WAS REMOVED AND A SPLICE, TIE ROD, FINGER DOUBLER, AND NEW LONGERON SECTION WERE INSTALLED IAW SRM 51-10-4, 51-30-2, 51-30-5, AND ECRA 5310-04263. - [SDR CALA0200407](https://openairdocs.org/sdr/CALA0200407.md): Frame · corroded · Jul 18, 2002 · N83873 · Doug DC982 · Fuselage Main, Frame > INSPECTION FOUND FRAME CORRODED AT FRAME TO LONGERON ATTACH POINTS, STA 1174, LONGERON 20L-25L. THE CORRODED SECTION OF FRAME WAS REMOVED AND REPLACED IAW SRM 51-10-04. - [SDR CALA0200402](https://openairdocs.org/sdr/CALA0200402.md): Web · corroded · Jul 15, 2002 · N83873 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND CUSP WEB CORRODED AT FS 1040-1060, LBL 44-58. A NEW WEB AND FITTINGS WERE INSTALLED IAW SRM 51-30-2, 51-30-1, AND 51-30-5. - [SDR CALA0200400](https://openairdocs.org/sdr/CALA0200400.md): Web · punctured · Jul 15, 2002 · N83873 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND AFT CARGO COMPARTMENT DOOR CUTOUT LOWER TORQUE BOX WEB PUNCTURED AT FS 1136 WITH A 1" CRACK AT FS 1212. THE TORQUE BOX WEB WAS REMOVED AND REPLACED IAW SRM 51-30-2, 51-30-1, AND 51-30-5. - [SDR CALA0200399](https://openairdocs.org/sdr/CALA0200399.md): Longeron · corroded · Jul 15, 2002 · N83873 · Doug DC982 · Fuselage Main, Longeron/Stringer > INSPECTION FOUND LONGERON 21L CORRODED ON OUTBOARD SURFACE AT FS 1117. THE CORRODED SECTION OF LONGERON WAS REMOVED AND REPLACED IAW ECRA 5310-04264. - [SDR CALA0200398](https://openairdocs.org/sdr/CALA0200398.md): Web · corroded · Jul 15, 2002 · N83873 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND L/H CUSP WEB CORRODED FROM FS 1250-1309. A NEW WEB AND FITTING WERE INSTALLED IAW SRM 51-30-2, 51-30-1, AND 51-30-5. - [SDR CALA0200392](https://openairdocs.org/sdr/CALA0200392.md): Seat Track · corroded · Jul 4, 2002 · N83873 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND R/H CENTER SEAT TRACK CORRODED FROM FS 200-300. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-04, FIGURE 4. - [SDR CALA0200390](https://openairdocs.org/sdr/CALA0200390.md): Skin · corroded · Jul 3, 2002 · N83873 · Doug DC982 · Fuselage Main, Plate/Skin > INSPECTION FOUND MID CARGO COMPARTMENT DOOR CUTOUT AREA SKIN CORRODED ON INNER SURFACE LOWER AFT CORNER AT FS 665. REPAIRED IAW EA 9-5312-2-A0957 AND ECRA 5330-03142. - [SDR CALA0200388](https://openairdocs.org/sdr/CALA0200388.md): Floor Support · corroded · Jul 2, 2002 · N83873 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND FORWARD ENTRY FLOOR SUPPORT CORRODED AT STA 200, LBL 10 TO LBL 14. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-2. - [SDR CALA0200387](https://openairdocs.org/sdr/CALA0200387.md): Seat Track · corroded · Jul 2, 2002 · N83873 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND SEAT TRACK CORRODED AT FS 200-236, LBL 44. A NEW SEAT TRACK AND SPLICE WERE INSTALLED IAW SRM 51-30-5. - [SDR CALA0200386](https://openairdocs.org/sdr/CALA0200386.md): Stiffener · cracked · Jul 2, 2002 · N83873 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND FORWARD ENTRY SUBFLOOR STIFFENER BENT AND CRACKED AT STA 200-218, RBL 30. REMOVED AND REPLACED STIFFENER IAW SRM 51-30-2. - [SDR CALA0200385](https://openairdocs.org/sdr/CALA0200385.md): Floor Support · corroded · Jul 2, 2002 · N83873 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND FORWARD ENTRY FLOOR SUPPORT CORRODED AT STA 196, LBL 15 TO LBL 44. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-2. - [SDR CALA0200384](https://openairdocs.org/sdr/CALA0200384.md): Longeron · corroded · Jul 2, 2002 · N83873 · Doug DC982 · Fuselage Main, Longeron/Stringer > INSPECTION FOUND LONGERON SPLICES CORRODED AT FS 1200, L20L AND L21L. REMOVED AND REPLACED LONGERON SPLICES IAW SRM 53-01, FIGURE 1, 51-10-4, AND 51-30-5. - [SDR CALA0200381](https://openairdocs.org/sdr/CALA0200381.md): Web · corroded · Jul 1, 2002 · N83873 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND SUBFLOOR UNDER G1 GALLEY DRAIN PAN CORRODED. THE CORRODED AREA WAS REMOVED AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-11-1, FIGURE 13 AND 53-01, FIGURE 1. - [SDR CALA0200380](https://openairdocs.org/sdr/CALA0200380.md): Web · corroded · Jul 1, 2002 · N83873 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND SUBFLOOR CORRODED AT FS 218, RBL 30. THE CORRODED AREA WAS REMOVED AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 51-30-2 AND 53-14-1, FIGURE 11. - [SDR CALA0200379](https://openairdocs.org/sdr/CALA0200379.md): Seat Track · corroded · Jul 1, 2002 · N83873 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND SEAT TRACK CORRODED AT STA 200-220, RBL 24. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-10-4 AND 53-05, FIGURE 4. - [SDR CALA0200378](https://openairdocs.org/sdr/CALA0200378.md): Web · cracked · Jul 1, 2002 · N83873 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND SUBFLOOR WEB CRACKED AT FS 200 LBL 10 AND FS 200 RBL 10. THE CRACKS WERE 1 INCH LONG. THE CRACKS WERE STOP DRILLED AND A DOUBLER REPAIR WAS INSTALLED AT EACH LOCATION IAW SRM 53-01, FIGURE 2, 51-30-2, AND 53-01, FIGURE 4. - [SDR CALA0200377](https://openairdocs.org/sdr/CALA0200377.md): Web · corroded · Jul 1, 2002 · N83873 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND FLOOR WEB CORRODED NEAR FORWARD ENTRY AREA AT FS 186-194. THE DAMAGED AREA WAS CUT OUT AND DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-01, FIGURE 4 AND 51-30-2. - [SDR CALA0200374](https://openairdocs.org/sdr/CALA0200374.md): Seat Track · corroded · Jun 28, 2002 · N83873 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND SEAT TRACK CORRODED AT STA 225, LBL 24. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-5 AND 51-30-1. - [SDR CALA0200373](https://openairdocs.org/sdr/CALA0200373.md): Web · cracked · Jun 28, 2002 · N83873 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND A CRACK AT FASTENER HOLE OF FORWARD ENTRY SUB FLOOR AT FS 218, LBL 20. THE CRACK WAS LESS THAN 1/8 INCH LONG. A DOUBLER WAS INSTALLED IAW SRM 51-30-2. - [SDR CALA0200372](https://openairdocs.org/sdr/CALA0200372.md): Web · punctured · Jun 28, 2002 · N83873 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND SUB FLOOR PUNCTURED AT FS 196, LBL 26. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-01, FIGURE 4 AND 51-30-2. - [SDR CALA0200371](https://openairdocs.org/sdr/CALA0200371.md): Frame · punctured · Jun 28, 2002 · N83873 · Doug DC982 · Fuselage Main, Frame > INSPECTION FOUND A PUNCTURE IN THE FRAME WEB OF AFT ACCESSORY COMPARTMENT AT RT SIDE, BS 1463, S17R. THE DAMAGE WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 51-10-4 AND 51-70-4, FIGURE 2, SHEET 2. - [SDR CALA0200370](https://openairdocs.org/sdr/CALA0200370.md): Web · cracked · Jun 28, 2002 · N83873 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND AFT R/H LAV SUBFLOOR AREA(WEB) BETWEEN INTERCOSTAL 23.875 AND 16.438 CRACKED AT THE O/B UPPER CORNER, STA 1338. THE INTERCOSTAL WEB WAS REMOVED AND REPLACED IAW SRM 51-30-5. - [SDR CALA0200365](https://openairdocs.org/sdr/CALA0200365.md): Intercostal · corroded · Jun 25, 2002 · N83873 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND FORWARD CARGO COMPARTMENT INTERCOSTAL CORRODED BETWEEN FS 428 AND 440 AT S29R. A REPAIR WAS INSTALLED IAW SRM 51-30-2 AND 51-30-5. - [SDR CALA0200356](https://openairdocs.org/sdr/CALA0200356.md): Floorbeam · corroded · Jun 19, 2002 · N83873 · Doug DC982 · Fuselage Main, Floor Beam > INSPECTION FOUND FLOORBEAM CORRODED UNDER NUTPLATES AT FS 1338, RBL 58 TO LBL 58. THE UPPER FLOORBEAM CAP WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5. - [SDR CALA0200355](https://openairdocs.org/sdr/CALA0200355.md): Seat Track · corroded · Jun 19, 2002 · N83873 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND L/H I/B SEAT TRACK CORRODED AT FS 1041-1250. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 4F. - [SDR CALA0200354](https://openairdocs.org/sdr/CALA0200354.md): Longeron · corroded · Jun 19, 2002 · N83873 · Doug DC982 · Fuselage Main, Longeron/Stringer > INSPECTION FOUND LONGERON 29R CORRODED AT FS 1271-1287. A LONGERON SPLICE REPAIR AND FITTING WERE INSTALLED IAW SRM 51-30-2 AND 53-02, FIGURE 18. - [SDR CALA0200353](https://openairdocs.org/sdr/CALA0200353.md): Web · cracked · Jun 19, 2002 · N83873 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND A 1.5" CRACK IN TANG OF L-1 DOOR TORQUE BOX WEB AT STA 208, LONGERON 15L. A DOUBLER AND FILLER WERE INSTALLED IAW ECRA 5314-01010. - [SDR CALA0200336](https://openairdocs.org/sdr/CALA0200336.md): Fitting · corroded · Jun 10, 2002 · N83873 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION MID CARGO COMPARTMENT DOOR CUTOUT FORWARD AND AFT LOWER CORNER FITTINGS CORRODED AT STA 636 AND 693 RESPECTIVELY. THE FITTINGS WERE REMOVED AND REPLACED IAW SRM 51-30-5. - [SDR CALA0100824](https://openairdocs.org/sdr/CALA0100824.md): Longeron · corroded · Aug 31, 2001 · N83873 · Doug DC982 · Fuselage Main, Longeron/Stringer > INSPECTION FOUND LONGERON 23R CORRODED IN AFT CARGO COMPARTMENT AT STA 1231. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIGURE 18. - [SDR CALA0100801](https://openairdocs.org/sdr/CALA0100801.md): Angle · cracked · Aug 25, 2001 · N83873 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND A.5 INCH CRACK IN TAIL COMPARTMENT LEFT VENT BOX FORWARD UPPER SUPPORT ANGLE. THE SUPPORT ANGLE WAS REMOVED AND A NEW SUPPORT ANGLE WAS INSTALLED IAW SRM 51-30-0. - [SDR CALA0100799](https://openairdocs.org/sdr/CALA0100799.md): Pan · corroded · Aug 25, 2001 · N83873 · Doug DC982 · Fuselage Main, Structure > INSPECTION FOUND FORWARD BAGGAGE BIN JAMB PAN CORRODED AT MID LOWER EDGE STA 344. A NEW PAN SECTION WAS INSTALLED IAW SRM 53-05, FIGURE 44. - [SDR CALA0100798](https://openairdocs.org/sdr/CALA0100798.md): Frame · cracked · Aug 25, 2001 · N83873 · Doug DC982 · Fuselage Main, Frame > INSPECTION FOUND A 2" CRACK IN TAIL COMPARTMENT CANTED FRAME AT STA 1446, L2L. THE FRAME WAS REMOVED AND REPLACED AT STA 1446 IAW SRM 51-30-2. Next page: https://openairdocs.org/deregistered/N83873-2004-12-21/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 = 'N83873' AND deregistration_id = 'N83873-2004-12-21' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N83873-2004-12-21/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.