# Service difficulty reports: N16813, cancelled Nov 13, 2002 A list on [N16813, cancelled Nov 13, 2002](https://openairdocs.org/deregistered/N16813-2002-11-13.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 · 98 reports - [SDR CALA0200443](https://openairdocs.org/sdr/CALA0200443.md): Skin · corroded · Aug 27, 2002 · N16813 · Doug DC982 · Fuselage Main, Plate/Skin > INSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 275 LONGERON 30 AFT OF LOWER ADF ANTENNA. THE SKIN SECTION WAS REMOVED AND REPLACED IAW SRM 51-30-02. - [SDR CALA0100712](https://openairdocs.org/sdr/CALA0100712.md): Floor Panel · corroded · Jul 29, 2001 · N16813 · Doug DC982 · Fuselage Floor Panel > INSPECTION FOUND FORWARD ENTRY FLOOR PANEL AT R-1 DOOR JAMB CORRODED, FS 160-200, RBL 48. THE FLOOR PANEL AND SUPPORT WERE REMOVED AND A NEW FLOOR PANEL AND SUPPORT WERE INSTALLED IAW SRM 51-10-4, 53-30-1, AND 51-30-1. - [SDR CALA0100693](https://openairdocs.org/sdr/CALA0100693.md): Floor Panel · delaminated · Jul 25, 2001 · N16813 · Doug DC982 · Fuselage Floor Panel > INSPECTION FOUND MAIN CABIN R/H I/B FLOOR PANEL DELAMINATED AT FS 1003-1079. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265. - [SDR CALA0100657](https://openairdocs.org/sdr/CALA0100657.md): Floor Panel · delaminated · Jul 16, 2001 · N16813 · Doug DC982 · Fuselage Floor Panel > INSPECTION FOUND CAPTAIN'S R/H SIDE AFT FLOORBOARD DELAMINATED. THE FLOOR PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 51-30-01. - [SDR CALA0100653](https://openairdocs.org/sdr/CALA0100653.md): Door Frame · dented · Jul 12, 2001 · N16813 · Doug DC982 · Fuselage Main, Structure > INSPECTION FOUND R-1 DOOR JAMB DENTED AT AFT LATCHING MECHANISM. THE BAYONET ROLLER ATTACH ARM WAS REMOVED IAW SRM 51-30-01. A REPAIR DOUBLER AND SHIM WERE INSTALLED IAW SRM 51-30-2. A NEW DOOR STOP WAS INSTALLED IAW SRM 51-30-5. THE BAYONET ROLLER ATTACH - [SDR CALA0100638](https://openairdocs.org/sdr/CALA0100638.md): Skin · dented · Jul 7, 2001 · N16813 · Doug DC982 · Fuselage Main, Plate/Skin > INSPECTION FOUND L/H FORWARD FUSELAGE EXTERNAL SKIN DENTED AT FS 120, LONGERON 18L. THE DENT WAS COLD WORKED AND A REPAIR DOUBLER WAS INSTALLED IAW EA 9-5331-2-A0902 AND ECRA 5331-01095. - [SDR CALA0100636](https://openairdocs.org/sdr/CALA0100636.md): Slat · dented · Jul 6, 2001 · N16813 · Doug DC982 · Leading Edge Devices > INSPECTION FOUND R/H WING #2 SLAT DENTED AT LEADING EDGE. THE DENT WAS FILLED IAW SRM 57-03, FIGURE 20A & B. - [SDR CALA0100635](https://openairdocs.org/sdr/CALA0100635.md): Angle · corroded · Jul 6, 2001 · N16813 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND LT CUSP ANGLE CORRODED ON UPPER SURFACE AT AFT END OF L-1 DOOR ENTRANCE, STA 186. THE AREA WAS REPAIRED IAW EA 9-5310-2-A0895 AND ECRA 5310-04156. - [SDR CALA0100632](https://openairdocs.org/sdr/CALA0100632.md): Floor Support · corroded · Jul 3, 2001 · N16813 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND MID CARGO RT BULKHEAD FLOOR SUPPORT CORRODED AT FS 541. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-10-4, AND 51-10-3. - [SDR CALA0100631](https://openairdocs.org/sdr/CALA0100631.md): Door Frame · cracked · Jul 3, 2001 · N16813 · Doug DC982 · Fuselage Main, Structure > INSPECTION FOUND A 5 INCH CRACK IN DOOR JAMB SKIN TANG AT AFT END OF L-1 DOOR, FS 207, LONGERON 11L. A 1 INCH CRACK WAS FOUND IN THE DOOR JAMB SKIN TANG AT FS 207, LONGERON 15L. THE CRACKED AREA WERE TRIMMED OUT IAW ECRA 5310-04155. FILLER AND DOUBLER WERE - [SDR CALA0100629](https://openairdocs.org/sdr/CALA0100629.md): Skin · dented · Jul 2, 2001 · N16813 · Doug DC982 · Cargo/Baggage Doors > INSPECTION FOUND AFT CARGO DOOR EXTERIOR SKIN DENTED. THE SKIN WAS REPAIRED IAW SRM 52-05, PAGE 2. - [SDR CALA0100628](https://openairdocs.org/sdr/CALA0100628.md): Doubler · cracked · Jul 1, 2001 · N16813 · Doug DC982 · Cargo/Baggage Doors > INSPECTION FOUND A 3" CRACK IN EXISTING DOUBLER REPAIR AT LOWER FORWARD CARGO DOOR. THE EXISTING DOUBLER WAS REMOVED AND THE CRACK WAS STOP DRILLED IAW SRM 51-10-4. A NEW DOUBLER WAS INSTALLED IAW SRM 52-33, FIGURE 1, 51-10-3, 51-10-4, AND 51-30-4. - [SDR CALA0100627](https://openairdocs.org/sdr/CALA0100627.md): Web · corroded · Jul 1, 2001 · N16813 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND FORWARD PIT(TORQUE BOX) FWD CLOSEOUT AT LIGHTENING HOLE(SLANT PANEL) CORRODED AT AND AROUND FASTENER HOLES AT FS 336. REMOVED FITTING, WEB, AND ANGLE IAW SRM 51-30-1 AND 51-30-2. A NEW WEB AND ANGLE WERE INSTALLED IAW SRM 51-10-4, 51-10-3, AND - [SDR CALA0100623](https://openairdocs.org/sdr/CALA0100623.md): Pan · corroded · Jun 30, 2001 · N16813 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND FORWARD PIT DOOR PAN BETWEEN TWO LOWER STOPS AT DRAIN HOLE CORRODED. THE CORRODED AREA WAS CUT OUT IAW SRM 53-05, FIGURE 44. A NEW LOWER PAN AND REPAIR ANGLES WERE INSTALLED IAW SRM 51-10-4, 53-05, FIGURE 44, 51-30-1, 51-30-2, 51-30-5, AND 51- - [SDR CALA0100622](https://openairdocs.org/sdr/CALA0100622.md): Angle · corroded · Jun 30, 2001 · N16813 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND JACK SUPPORT ANGLE CORRODED IN CHANNEL AREA AT BOTTOM OF APB, FS 1338, LONGERON 30. THE JACK SUPPORT ANGLE AND VERTICAL CHANNEL STRINGER TIE FITTINGS WERE REMOVED IAW SRM 51-30-2 AND 51-30-5. A NEW ANGLE WAS INSTALLED WITH TIE FITTINGS IAW SRM - [SDR CALA0100621](https://openairdocs.org/sdr/CALA0100621.md): Skin · gouged · Jun 30, 2001 · N16813 · Doug DC982 · Wing, Plate/Skin > INSPECTION FOUND LOWER SURFACE OF SKIN PANEL #1613 GOUGED AT R/H I/B FLAP T/E AREA. THE PANEL SKIN WAS REMOVED AND NEW SKIN WAS INSTALLED IAW SRM 51-30-2, 57-50-9, AND 51-10-3. - [SDR CALA0100619](https://openairdocs.org/sdr/CALA0100619.md): Web · corroded · Jun 29, 2001 · N16813 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND CUSP WEB CORRODED AT LOWER CORNER FORWARD END OF R-1 DOOR JAMB, FS 160 - 238. THE LOWER DOOR PAN, TWO TORQUE BOX WEB PANELS, STRAPS, AND COMPOSITE CHANNEL WERE REMOVED TO GAIN ACCESS. THE CUSP WEB WAS REPLACED IAW SRM 53-05, FIGURE 55. REIN - [SDR CALA0100618](https://openairdocs.org/sdr/CALA0100618.md): Floor Panel · punctured · Jun 29, 2001 · N16813 · Doug DC982 · Fuselage Floor Panel > INSPECTION FOUND R/H CABIN FLOOR PANEL PUNCTURED AT STA 256-313 SIDEWALL SUPPORT STRUCTURE. THE FLOOR PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 51-30-1, 51-10-4, AND ECRA 5320-01265. - [SDR CALA0100617](https://openairdocs.org/sdr/CALA0100617.md): Web · corroded · Jun 29, 2001 · N16813 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND MAIN CABIN CUSP WEB CORRODED AT FS 202-218, RBL 54. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-30-02, 51-10-4, AND 51-10-3. - [SDR CALA0100615](https://openairdocs.org/sdr/CALA0100615.md): Floor Support · corroded · Jun 26, 2001 · N16813 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 160 - 196, LBL 44. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AND 51-30-2. - [SDR CALA0100614](https://openairdocs.org/sdr/CALA0100614.md): Floor Support · cracked · Jun 26, 2001 · N16813 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND A 6 INCH CRACK IN COCKPIT CENTER FLOORBOARD CENTER FLOOR SUPPORT AT FS 140, BL 0. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-10-4, AND 51-10-3. - [SDR CALA0100613](https://openairdocs.org/sdr/CALA0100613.md): Floor Support · corroded · Jun 26, 2001 · N16813 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 160 - 195, LBL 56. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-10-4 AND 51-30-2. - [SDR CALA0100612](https://openairdocs.org/sdr/CALA0100612.md): Floor Support · corroded · Jun 26, 2001 · N16813 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 157 - 200, RBL 6. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-4, 51-10-1, AND 51-10-3. - [SDR CALA0100611](https://openairdocs.org/sdr/CALA0100611.md): Floor Support · corroded · Jun 26, 2001 · N16813 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 157 - 198, RBL 45. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AND 51-30-2. - [SDR CALA0100610](https://openairdocs.org/sdr/CALA0100610.md): Cargo Track · corroded · Jun 26, 2001 · N16813 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND FORWARD PIT RT SIDE CARGO TIE DOWN TRACK CORRODED AT LOWER SIDE OF FASTENER HOLES FROM FS 218 TO FORWARD DOOR FRAME. THE TIE DOWN TRACK AND ATTACHING ANGLE WERE REMOVED AND A NEW TRACK AND ATTACH ANGLE WERE INSTALLED IAW SRM 51-30-2 AND 51-30 - [SDR CALA0100609](https://openairdocs.org/sdr/CALA0100609.md): Web · corroded · Jun 26, 2001 · N16813 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND LT FLOOR CUSP WEB BEHIND LAV AREA CORRODED AT FS 218 - 228, LBL 45 - 56. THE CUSP WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-30-2, 51-30-5, 51-30-8, 51-10-3, AND 51-10-4. - [SDR CALA0100608](https://openairdocs.org/sdr/CALA0100608.md): Floor Support · corroded · Jun 26, 2001 · N16813 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND FLOOR SUPPORT IN CENTER CARGO PIT CORRODED ON UPPER SURFACE AT FS 636 FROM LONGERON 29R-28L. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2. - [SDR CALA0100607](https://openairdocs.org/sdr/CALA0100607.md): Web · corroded · Jun 26, 2001 · N16813 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND FORWARD ENTRY SUBFLOOR CORRODED AT FS 160 - 200, RBL 56. THE FLOOR SUPPORTS AND WEB SUPPORTS WERE REMOVED TO GAIN ACCESS TO SUBFLOOR. THE SUBFLOOR WAS REMOVED AND A NEW SUBFLOOR WAS INSTALLED WITH WEB AND FLOOR SUPPORTS IAW SRM 53-14-1, 51-3 - [SDR CALA0100606](https://openairdocs.org/sdr/CALA0100606.md): Web · cracked · Jun 26, 2001 · N16813 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND CUSP WEB CRACKED IN TWO PLACES AT FS 218 - 238, RBL 54. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-30-2 AND 51-30-4. - [SDR CALA0100605](https://openairdocs.org/sdr/CALA0100605.md): Skin · dented · Jun 25, 2001 · N16813 · Doug DC982 · Fuselage Main, Plate/Skin > INSPECTION FOUND L/H FUSELAGE EXTERNAL SKIN CREASED AND DENTED AT FS 389, LONGERON 22L. THE DAMAGED AREA WAS REFORMED AND A DOUBLER WAS INSTALLED IAW SRM 51-10-2, 51-10-4, AND 51-10-3. - [SDR CALA0100604](https://openairdocs.org/sdr/CALA0100604.md): Angle · corroded · Jun 25, 2001 · N16813 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND MAIN CABIN WEB ATTACH ANGLE CORRODED AT FS 200-214, LBL 54. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-3 AND 51-30-5. - [SDR CALA0100603](https://openairdocs.org/sdr/CALA0100603.md): Shear Tie · cracked · Jun 25, 2001 · N16813 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND A 1" CRACK IN FORWARD CARGO SHEAR TIE AT FS 370, LONGERON 22-23L. THE CRACKED AREA WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 7, 53-03, FIGURE 7, AND 51-10-3. - [SDR CALA0100600](https://openairdocs.org/sdr/CALA0100600.md): Floor Panel · corroded · Jun 25, 2001 · N16813 · Doug DC982 · Fuselage Floor Panel > INSPECTION FOUND CABIN FLOOR PANEL "F" CORRODED AROUND FASTENER HOLES. THE PANEL WAS REPLACED IAW SRM 53-21-0 AND 51-10-3. - [SDR CALA0100599](https://openairdocs.org/sdr/CALA0100599.md): Floor Panel · cracked · Jun 25, 2001 · N16813 · Doug DC982 · Fuselage Floor Panel > INSPECTION FOUND L/H O/B FLOOR PANEL CRACKED AROUND SCREW HOLES AT BOTH ENDS, STA 826-927. A DOUBLER WAS INSTALLED AT EACH END IAW SRM 53-01, FIGURE 4 AND 51-10-3. - [SDR CALA0100598](https://openairdocs.org/sdr/CALA0100598.md): Skin · dented · Jun 25, 2001 · N16813 · Doug DC982 · Fuselage Main, Plate/Skin > INSPECTION FOUND R/H FUSELAGE EXTERNAL SKIN DENTED AT FS 579 BETWEEN LONGERONS 20R AND 21R. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38. - [SDR CALA0100597](https://openairdocs.org/sdr/CALA0100597.md): Skin · dented · Jun 24, 2001 · N16813 · Doug DC982 · Fuselage Main, Plate/Skin > INSPECTION FOUND R/H FUSELAGE EXTERNAL SKIN DENTED AT FS 541 BETWEEN LONGERONS 20R AND 21R. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38. - [SDR CALA0100596](https://openairdocs.org/sdr/CALA0100596.md): Skin · dented · Jun 24, 2001 · N16813 · Doug DC982 · Fuselage Main, Plate/Skin > INSPECTION FOUND R/H EXTERNAL FUSELAGE SKIN DENTED AT FS 370 JUST BELOW LONGERON 20R. THE DENTED AREA WAS COLD WORKED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38. - [SDR CALA0100595](https://openairdocs.org/sdr/CALA0100595.md): Seat Track · corroded · Jun 24, 2001 · N16813 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND MAIN CABIN SEAT TRACK CORRODED AT FS 1070-1203, LBL 25. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 53-05, FIGURE 4, 51-10-4, AND 51-10-3. - [SDR CALA0100594](https://openairdocs.org/sdr/CALA0100594.md): Web · corroded · Jun 24, 2001 · N16813 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND LT FLOOR CUSP WEB CORRODED ON LOWER SURFACE AT FS 1117. THE CORRODED AREA WAS REMOVED AND A NEW CUSP WEB WAS INSTALLED IAW SRM 51-30-2, 51-10-4, 51-10-3, AND 51-30-1. - [SDR CALA0100593](https://openairdocs.org/sdr/CALA0100593.md): Fitting · corroded · Jun 24, 2001 · N16813 · Doug DC982 · Fuselage Main, Attach Fittings > INSPECTION FOUND ATTACH FITTING(FORWARD OF L-2 DOOR) CORRODED AT FS 1136, LBL 56. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-30-1, 51-30-4, AND 51-10-3. - [SDR CALA0100592](https://openairdocs.org/sdr/CALA0100592.md): Web · corroded · Jun 24, 2001 · N16813 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND MAIN CABIN CUSP WEB CORRODED AT FS 1174 - 1193, LBL 54. THE CORRODED AREA WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-30-2, 51-10-4, AND 51-10-3. - [SDR CALA0100589](https://openairdocs.org/sdr/CALA0100589.md): Seat Track · corroded · Jun 23, 2001 · N16813 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND SEAT TRACK CORRODED AT FS 1097-1215, LBL 45. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-2, 51-10-4, AND 51-10-3. - [SDR CALA0100588](https://openairdocs.org/sdr/CALA0100588.md): Angle · corroded · Jun 23, 2001 · N16813 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND L/H MAIN CABIN T-ANGLE CORRODED AT FS 1140. THE T-ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-3, 51-10-4, 51-10-5, AND 51-30-2. - [SDR CALA0100587](https://openairdocs.org/sdr/CALA0100587.md): Angle · corroded · Jun 23, 2001 · N16813 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND AFT ENTRY DOOR Z-ANGLE COMMON TO CUSP MEMBRANE CORRODED AT FS 1136-1174, LBL 48.5. THE Z-ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2 AND 51-10-4. - [SDR CALA0100586](https://openairdocs.org/sdr/CALA0100586.md): Channel · corroded · Jun 23, 2001 · N16813 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND AFT ENTRY DOOR SEAL AREA AFT HAT CHANNEL FOR THRESHOLD CORRODED. THE HAT CHANNEL WAS REMOVED AND A NEW CHANNEL WAS INSTALLED IAW SRM 51-30-2 AND 51-10-4. - [SDR CALA0100585](https://openairdocs.org/sdr/CALA0100585.md): Skin · dented · Jun 22, 2001 · N16813 · Doug DC982 · Wing, Plate/Skin > INSPECTION FOUND R/H WING SKIN I/B LOWER SURFACE NICKED AND DENTED. NEW SKIN WAS FABRICATED AND INSTALLED IAW SRM 51-60-4 AND 51-30-2. - [SDR CALA0100584](https://openairdocs.org/sdr/CALA0100584.md): Fitting · corroded · Jun 22, 2001 · N16813 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND CABIN FRAME TO WEB FITTING CORRODED AT FS 160, RBL 56. THE FRAME FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-01, 51-30-05, AND 51-10-4. - [SDR CALA0100583](https://openairdocs.org/sdr/CALA0100583.md): Skin · dented · Jun 22, 2001 · N16813 · Doug DC982 · Fuselage Main, Plate/Skin > INSPECTION FOUND L/H FUSELAGE EXTERNAL SKIN DENTED AT FS 474 JUST ABOVE LONGERON 21L. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 3B. - [SDR CALA0100579](https://openairdocs.org/sdr/CALA0100579.md): Floor Panel · delaminated · Jun 22, 2001 · N16813 · Doug DC982 · Fuselage Floor Panel > INSPECTION FOUND CABIN FLOOR PANEL DELAMINATED AT STA 1041-1117. THE FLOOR PANEL WAS REPLACED IAW ECRA 5320-01265. - [SDR CALA0100578](https://openairdocs.org/sdr/CALA0100578.md): Floor Panel · delaminated · Jun 22, 2001 · N16813 · Doug DC982 · Fuselage Floor Panel > INSPECTION FOUND CABIN FLOOR PANELS I & J AT LT FORWARD ENTRY DELAMINATED. THE FLOOR PANELS WERE REPLACED IAW ECRA 5320-01265. Next page: https://openairdocs.org/deregistered/N16813-2002-11-13/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 = 'N16813' AND deregistration_id = 'N16813-2002-11-13' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N16813-2002-11-13/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.