# Service difficulty reports: N16815, cancelled Sep 17, 2002

A list on [N16815, cancelled Sep 17, 2002](https://openairdocs.org/deregistered/N16815-2002-09-17.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 · 86 reports

- [SDR CALA0200001](https://openairdocs.org/sdr/CALA0200001.md): Fuse · blown · Jan 2, 2002 · N16815 · Doug DC982 · Emergency Lighting
  > INSPECTION FOUND SEAT MOUNTED EMERGENCY LIGHTS AT ROW 5-12 INOPERATIVE. MAINTENANCE FOUND FUSE BLOWN IN BATTERY CHARGER AND WIRING AT ROW 5 SHORTED TO THE SEAT TRACK. REPAIRED WIRING IAW STANDARD WIRING PRACTICES. REPLACED FUSE IAW MM 33-51-00.
- [SDR CALA0100764](https://openairdocs.org/sdr/CALA0100764.md): Floor Panel · delaminated · Aug 19, 2001 · N16815 · Doug DC982 · Fuselage Floor Panel
  > INSPECTION FOUND MAIN CABIN CENTER FLOOR PANEL DELAMINATED AT FS 1117-1174. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265.
- [SDR CALA0100761](https://openairdocs.org/sdr/CALA0100761.md): Floor Panel · punctured · Aug 15, 2001 · N16815 · Doug DC982 · Fuselage Floor Panel
  > INSPECTION FOUND CABIN FLOOR PANEL PUNCTURED AT FS 256-313. THE FLOOR PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 51-30-1 AND ECRA 5320-01265.
- [SDR CALA0100746](https://openairdocs.org/sdr/CALA0100746.md): Intercostal · cracked · Aug 8, 2001 · N16815 · Doug DC982 · Service Doors
  > INSPECTION FOUND A 7" CRACK IN R-1 DOOR INNER INTERCOSTA UNDER HINGE ATTACH POINT. THE R-1 DOOR WAS REMOVED IAW MM 52-41-00. THE CRACK WAS STOP DRILLED AND A REPAIR CAP AND FITTING WERE INSTALLED IAW SRM 52-05, FIGURE 5. REINSTALLED R-1 DOOR IAW MM 52-41-00.
- [SDR CALA0100745](https://openairdocs.org/sdr/CALA0100745.md): Pan · gouged · Aug 7, 2001 · N16815 · Doug DC982 · Service Doors
  > INSPECTION FOUND R-1 DOOR LOWER PAN GOUGED AT RIVNUTS. THE PAN SUPPORT WAS REMOVED FOR ACCESS IAW SRM 51-30-02. A REPAIR ANGLE AND DOUBLER WAS INSTALLED IAW ECRA 5240-01386. THE SUPPORT PAN WAS REINSTALLED IAW SRM 51-30-2.
- [SDR CALA0100744](https://openairdocs.org/sdr/CALA0100744.md): Skin · dented · Aug 7, 2001 · N16815 · Doug DC982 · Trailing Edge Flaps
  > INSPECTION FOUND RT WING O/B FLAP O/B TRAILING EDGE SKIN LOWER SURFACE DENTED. THE SKIN WAS REMOVED IAW SRM 51-30-2 AND THE SUPPORT RIBS WERE FOUND DAMAGED. NEW RIBS AND A REPAIR DOUBLER WERE INSTALLED AND THE SKIN WAS REINSTALLED IAW SRM 51-10-4, 51-10-3, 5
- [SDR CALA0100742](https://openairdocs.org/sdr/CALA0100742.md): Mount · corroded · Aug 5, 2001 · N16815 · Doug DC982 · Trailing Edge Flaps
  > INSPECTION FOUND R/H WING I/B FLAP HINGE #2 CORRODED IN BOTTOM MOUNT HOLE. THE HOLE WAS REAMED AND TWO BUSHINGS WERE INSTALLED IAW EA 9-2750-2-A0914 AND ECRA 2750-01333.
- [SDR CALA0100741](https://openairdocs.org/sdr/CALA0100741.md): Frame · corroded · Aug 4, 2001 · N16815 · Doug DC982 · Fuselage Main, Frame
  > INSPECTION FOUND FRAME CORRODED AT FS 1271 FROM LONGERON 27L TO 27R. THE CORRODED AREA OF FRAME WAS CUT OUT IAW SRM 53-03, FIGURE 2A. A REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 2A, 53-10-3, AND 53-03, FIGURE 2A.
- [SDR CALA0100739](https://openairdocs.org/sdr/CALA0100739.md): Skin · gouged · Aug 3, 2001 · N16815 · Doug DC982 · Elevator, Plate/Skin
  > INSPECTION FOUND R/H ELEVATOR LOWER SKIN SURFACE O/B OF TRIM TAB PUSH ROD FAIRING GOUGED. THE SKIN WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-70-2 AND 55-03.
- [SDR CALA0100738](https://openairdocs.org/sdr/CALA0100738.md): Bracket · cracked · Aug 3, 2001 · N16815 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND A 1" CRACK IN T-BRACKET OF FORWARD CARGO DOOR UPPER INTERNAL PAN FORWARD OF AFT HINGES. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-30-5.
- [SDR CALA0100737](https://openairdocs.org/sdr/CALA0100737.md): Web · corroded · Aug 3, 2001 · N16815 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FORWARD CARGO TORQUE BOX WEB CORRODED AROUND FASTENER HOLES AT STA 370. THE TORQUE BOX WEB AND SUPPORT ANGLE WERE REMOVED IAW SRM 51-10-4 AND 51-30-2. A REPAIR WEB AND SUPPORT ANGLE WERE INSTALLED IAW SRM51-30-2.
- [SDR CALA0100736](https://openairdocs.org/sdr/CALA0100736.md): Web · cracked · Aug 3, 2001 · N16815 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1 INCH CRACK IN L-1 DOOR TORQUE BOX WEB TANG. THE CRACKED AREA OF WEB TANG WAS TRIMMED OUT AND A DOUBLER AND FILLER WERE INSTALLED IAW EA 9-5314-2-A0905 AND ECRA 5310-04170.
- [SDR CALA0100734](https://openairdocs.org/sdr/CALA0100734.md): Angle · cracked · Aug 3, 2001 · N16815 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND A 1" CRACK IN T-ANGLE AT FORWARD CARGO DOOR UPPER INTERNAL PAN AFT OF FORWARD HINGE. THE T-ANGLE WAS REMOVED AND A NEW T-ANGLE WAS INSTALLED IAW SRM 51-30-5.
- [SDR CALA0100733](https://openairdocs.org/sdr/CALA0100733.md): Channel · cracked · Aug 3, 2001 · N16815 · Doug DC982 · Landing Gear Doors
  > INSPECTION FOUND A 1" CRACK IN L/H MLG DOOR CHANNEL AT FORWARD END OF DOOR JUST ABOVE DOOR SEAL. A REPAIR DOUBLER WAS INSTALLED IAW EA 9-5281-2-A0904 AND ECRA 5280-01267.
- [SDR CALA0100731](https://openairdocs.org/sdr/CALA0100731.md): Splice · corroded · Jul 31, 2001 · N16815 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND LONGERON 29L SPLICE CORRODED IN FORWARD CARGO AREA AT FS 225. THE LONGERON SPLICE WAS REMOVED AND A NEW SPLICE WAS INSTALLED IAW SRM 53-01, FIGURE 1, 51-30-2, 51-10-4, AND 51-30-5.
- [SDR CALA0100730](https://openairdocs.org/sdr/CALA0100730.md): Frame · corroded · Jul 31, 2001 · N16815 · Doug DC982 · Fuselage Main, Frame
  > INSPECTION FOUND MID CARGO FRAME CORRODED AT FS 522 BETWEEN LONGERONS 28L AND 28R. THE CORRODED AREA OF FRAME WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-03 AND 51-30-5.
- [SDR CALA0100728](https://openairdocs.org/sdr/CALA0100728.md): Skin · gouged · Jul 31, 2001 · N16815 · Doug DC982 · Elevator, Plate/Skin
  > INSPECTION FOUND R/H ELEVATOR SKIN LOWER SURFACE JUST OUTBOARD OF #2 HINGE MOUNTING PAD GOUGED. THE SKIN PANEL WAS REMOVED AND A NEW SKIN PANEL WAS INSTALLED IAW SRM 51-30-2.
- [SDR CALA0100725](https://openairdocs.org/sdr/CALA0100725.md): Skin · dented · Jul 30, 2001 · N16815 · Doug DC982 · Rudder, Tab Structure
  > INSPECTION FOUND RUDDER CONTROL TAB SKIN DENTED IN THE LOWER LEFT SIDE. THE RUDDER TAB WAS REMOVED IAW MM 27-20-02. THE TAB WAS REPAIRED, WEIGHED, AND BALANCED IAW SRM 55-40-1. THE TAB WAS INSTALLED AND THROW CHECKS WERE COMPLETED IAW MM 27-20-02.
- [SDR CALA0100718](https://openairdocs.org/sdr/CALA0100718.md): Skin · dented · Jul 30, 2001 · N16815 · Doug DC982 · Leading Edge Devices
  > INSPECTION FOUND L/H "0" SLAT EXTERNAL SKIN DENTED. THE SKIN AND ATTACHING PARTS WERE REMOVED IAW SRM 51-30-6 AND 51-30-1. A DOUBLER WAS INSTALLED IAW SRM 57-09, FIGURE 10A. THE SKIN AND ATTACHING PARTS WERE REINSTALLED IAW SRM 51-30-6 AND 51-30-1.
- [SDR CALA0100717](https://openairdocs.org/sdr/CALA0100717.md): Web · corroded · Jul 30, 2001 · N16815 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CUSP WEB CORRODED AT FS 160 - 200, RBL 35 TO RBL 50. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-30-2 AND 53-10-1.
- [SDR CALA0100716](https://openairdocs.org/sdr/CALA0100716.md): Spacer · corroded · Jul 29, 2001 · N16815 · Doug DC982 · Fuselage Main, Structure
  > INSPECTION FOUND MID CARGO DOOR LOWER JAMB BEAM SPACER CORRODED AROUND RIVNUTS. THE SPACER WAS REMOVED AND A NEW SPACER WAS INSTALLED IAW SRM 51-30-4 AND 51-10-4.
- [SDR CALA0100715](https://openairdocs.org/sdr/CALA0100715.md): Seat Track · corroded · Jul 29, 2001 · N16815 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND R/H I/B SEAT TRACK CORRODED AT FS 845-1032. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED WITH SPLICES IAW SRM 53-05, FIGURE 4F AND 51-10-3.
- [SDR CALA0100714](https://openairdocs.org/sdr/CALA0100714.md): Skin · dented · Jul 29, 2001 · N16815 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND L/H EXTERIOR FUSELAGE SKIN DENTED AT FS 522 ABOVE L25 AND AT FS 494 ABOVE L25. THE DENTS WERE COLD WORKED IAW SRM 53-04, FIGURE 38. A DOUBLER WAS INSTALLED AT EACH LOCATION IAW SRM 53-04, FIGURE 38, 51-10-4, AND 51-30-2.
- [SDR CALA0100713](https://openairdocs.org/sdr/CALA0100713.md): Seat Track · corroded · Jul 29, 2001 · N16815 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND CABIN L/H CENTER SEAT TRACK CORRODED AT FS 1032-1309. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-1, 51-30-2, 51-30-5, 51-10-4, 51-10-3, AND 53-05, FIGURE 4F.
- [SDR CALA0100711](https://openairdocs.org/sdr/CALA0100711.md): Floor Panel · broken · Jul 29, 2001 · N16815 · Doug DC982 · Fuselage Floor Panel
  > INSPECTION FOUND CABIN L/H O/B FLOOR PANELS BROKEN OFF AT FASTENER HOLES AT FS 1079-1155 AND FS 1155-1250. THE PANELS WERE REPAIRED IAW SRM 51-70-1.
- [SDR CALA0100710](https://openairdocs.org/sdr/CALA0100710.md): Seat Track · corroded · Jul 29, 2001 · N16815 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND L/H O/B SEAT TRACK CORRODED AT FS 1174-1309. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-1 AND 51-10-3.
- [SDR CALA0100709](https://openairdocs.org/sdr/CALA0100709.md): Floor Panel · punctured · Jul 29, 2001 · N16815 · Doug DC982 · Fuselage Floor Panel
  > INSPECTION FOUND CABIN R/H I/B FLOOR PANEL PUNCTURED AT FS 389-408. A NEW PANEL WAS INSTALLED IAW ECRA 5320-01265 AND SRM 51-30-1.
- [SDR CALA0100708](https://openairdocs.org/sdr/CALA0100708.md): Floor Panel · delaminated · Jul 28, 2001 · N16815 · Doug DC982 · Fuselage Floor Panel
  > INSPECTION FOUND COPILOT'S I/B FLOOR PANEL DELAMINATED. THE FLOOR PANEL WAS REMOVED AND A NEW FLOOR PANEL WAS INSTALLED IAW SRM 53-30-01, 53-21-0, SHEET 23, 51-30-1, AND 51-30-2.
- [SDR CALA0100705](https://openairdocs.org/sdr/CALA0100705.md): Web · corroded · Jul 27, 2001 · N16815 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CUSP WEB CORRODED AT FS 200-237, RBL 44 TO RBL 56. THE CORRODED SECTION OF CUSP WEB WAS REMOVED AND A NEW CUSP WEB WAS INSTALLED IAW SRM 51-30-02.
- [SDR CALA0100704](https://openairdocs.org/sdr/CALA0100704.md): Angle · corroded · Jul 27, 2001 · N16815 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND R-1 DOOR CUSP ANGLE CORRODED AT FS 203. THE CORRODED SECTION OF CUSP ANGLE WAS CUT OUT IAW SRM 51-30-1. A CUSP ANGLE AND SPLICE WERE INSTALLED IAW SRM 53-05, FIGURE 55, SHEET 2.
- [SDR CALA0100702](https://openairdocs.org/sdr/CALA0100702.md): Seat Track · corroded · Jul 27, 2001 · N16815 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND L/H SEAT TRACK CORRODED AT STA 1108-1309. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK AND SPLICE WERE INSTALLED IAW SRM 51-30-1.
- [SDR CALA0100701](https://openairdocs.org/sdr/CALA0100701.md): Pan · cracked · Jul 27, 2001 · N16815 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND DOOR PAN CRACKED AROUND BOTTOM STOP AT AFT CARGO DOOR AFT SIDE. A DOUBLER AND FILLER WERE INSTALLED IAW SRM 52-05, FIGURE 1 & 4 AND ECRA 5230-01540.
- [SDR CALA0100700](https://openairdocs.org/sdr/CALA0100700.md): Web · cracked · Jul 27, 2001 · N16815 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CUSP WEB CRACKED AFT OF L-2 DOOR AT STA 1174, LBL 60. THE CUSP WEB WAS REMOVED AND A NEW CUSP WEB WAS INSTALLED IAW SRM 51-30-2 AND 51-30-1.
- [SDR CALA0100699](https://openairdocs.org/sdr/CALA0100699.md): Seat Track · corroded · Jul 26, 2001 · N16815 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND CABIN SEAT TRACK CORRODED AT STA 798-1108. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-1.
- [SDR CALA0100698](https://openairdocs.org/sdr/CALA0100698.md): Skin · dented · Jul 26, 2001 · N16815 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE EXTERNAL SKIN DENTED AT STA 218, LONGERON 16L AND 18L. THE DENTS WERE COLD WORKED IAW SRM 53-04, FIGURE 38. DOUBLERS WERE INSTALLED IAW SRM 53-10, FIGURE 38 AND 51-10-4.
- [SDR CALA0100697](https://openairdocs.org/sdr/CALA0100697.md): Skin · gouged · Jul 26, 2001 · N16815 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND RT FUSELAGE EXTERNAL SKIN DENTED AND GOUGED BELOW NR 2 ENGINE APRON AT STA 1309. THE DAMAGED AREA WAS REMOVED IAW SRM 53-04, FIGURE 38. A REPAIR DOUBLER AND SKIN PLUG WAS INSTALLED IAW SRM 53-04, FIGURE 38 AND 51-30-2.
- [SDR CALA0100696](https://openairdocs.org/sdr/CALA0100696.md): Skin · gouged · Jul 26, 2001 · N16815 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND FORWARD CARGO DOOR EXTERNAL SKIN GOUGED BELOW HANDLES. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 1 AND 52-05.
- [SDR CALA0100692](https://openairdocs.org/sdr/CALA0100692.md): Seat Track · corroded · Jul 25, 2001 · N16815 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND R/H CENTER SEAT TRACK CORRODED AT FS 798-874. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-2, 51-30-5, AND 51-30-3.
- [SDR CALA0100690](https://openairdocs.org/sdr/CALA0100690.md): Floor Panel · delaminated · Jul 25, 2001 · N16815 · Doug DC982 · Fuselage Floor Panel
  > INSPECTION FOUND CABIN FLOOR PANELS M-P DELAMINATED. NEW FLOOR PANELS WERE INSTALLED IAW ECRA 5320-01265.
- [SDR CALA0100689](https://openairdocs.org/sdr/CALA0100689.md): Floor Panel · delaminated · Jul 25, 2001 · N16815 · Doug DC982 · Fuselage Floor Panel
  > INSPECTION FOUND CABIN FLOOR PANELS B-K DELAMINATED. NEW FLOOR PANELS WERE INSTALLED IAW ECRA 5320-01265.
- [SDR CALA0100688](https://openairdocs.org/sdr/CALA0100688.md): Floor Panel · delaminated · Jul 25, 2001 · N16815 · Doug DC982 · Fuselage Floor Panel
  > INSPECTION FOUND CABIN L/H I/B FLOOR PANEL DELAMINATED AT FS 1079-1155 AND R/H I/B FLOOR PANEL WAS DELAMINATED AT FS 927-1003. NEW FLOOR PANELS WERE INSTALLED IAW ECRA 5320-01265.
- [SDR CALA0100687](https://openairdocs.org/sdr/CALA0100687.md): Floor Panel · delaminated · Jul 25, 2001 · N16815 · Doug DC982 · Fuselage Floor Panel
  > INSPECTION FOUND MAIN CABIN CENTER FLOOR PANELS DELAMINATED AT FS 1174-1250 AND FS 1309-1361. A R/H I/B FLOOR PANEL WAS DELAMINATED AT FS 1250-1309. A NEW FLOOR PANELS WERE INSTALLED IAW ECRA 5320-01265.
- [SDR CALA0100686](https://openairdocs.org/sdr/CALA0100686.md): Floor Panel · delaminated · Jul 25, 2001 · N16815 · Doug DC982 · Fuselage Floor Panel
  > INSPECTION FOUND CABIN R/H I/B AND CENTER FLOOR PANELS AT FS 1117-1174 DELAMINATED AND CENTER PANEL AT FS 1079-1117 DELAMINATED. NEW FLOOR PANELS WERE INSTALLED IAW ECRA 5320-01265.
- [SDR CALA0100685](https://openairdocs.org/sdr/CALA0100685.md): Floor Panel · delaminated · Jul 25, 2001 · N16815 · Doug DC982 · Fuselage Floor Panel
  > INSPECTION FOUND CABIN CENTER FLOOR PANELS DELAMINATED AT FS 826-886 AND AT FS 945-1003. NEW FLOOR PANELS WERE INSTALLED IAW ECRA 5320-01265.
- [SDR CALA0100684](https://openairdocs.org/sdr/CALA0100684.md): Floor Panel · delaminated · Jul 25, 2001 · N16815 · Doug DC982 · Fuselage Floor Panel
  > INSPECTION FOUND L/H I/B FLOOR PANEL PUNCTURED AT FS 769-826 AND L/H I/B FLOOR PANEL AT FS 864-886 WAS DELAMINATED. THE FLOOR PANELS WERE REPLACED IAW ECRA 5320-01265.
- [SDR CALA0100683](https://openairdocs.org/sdr/CALA0100683.md): Floor Panel · delaminated · Jul 25, 2001 · N16815 · Doug DC982 · Fuselage Floor Panel
  > INSPECTION FOUND R/H I/B FLOOR PANELS DELAMINATED AT FS 826-927. A CENTER PANEL AT FS 886-946 AND CENTER & RIGHT CENTER PANELS AT FS 807-826 WERE FOUND DELAMINATED. NEW PANELS WERE INSTALLED IAW ECRA 5320-01265.
- [SDR CALA0100682](https://openairdocs.org/sdr/CALA0100682.md): Floor Panel · delaminated · Jul 25, 2001 · N16815 · Doug DC982 · Fuselage Floor Panel
  > INSPECTION FOUND MAIN CABIN R/H CENTER AND L/H CENTER FLOOR PANELS DELAMINATED AT FS 693-769. NEW PANELS WERE INSTALLED IAW ECRA 5320-01265.
- [SDR CALA0100677](https://openairdocs.org/sdr/CALA0100677.md): Skin · dented · Jul 24, 2001 · N16815 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND L/H LOWER EXTERNAL FUSELAGE SKIN DENTED AT STA 389, LONGERON 29L. THE DENT WAS COLD FORMED AND A DOUBLER WAS INSTALLED IAW SRM 51-10-3 AND 53-05, FIGURE 38.
- [SDR CALA0100676](https://openairdocs.org/sdr/CALA0100676.md): Skin · dented · Jul 24, 2001 · N16815 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE EXTERNAL SKIN DENTED AT FS 275, LONGERON 17L. THE DENTED AREA OF SKIN WAS REMOVED IAW SRM 51-30-2. NEW SKIN WAS INSTALLED IAW SRM 51-30-2, 51-30-5, AND ECRA 5330-02445.
- [SDR CALA0100675](https://openairdocs.org/sdr/CALA0100675.md): Skin · damaged · Jul 24, 2001 · N16815 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN CREASED AT STA 180, LONGERON 23R. THE CREASED AREA WAS CUT OUT IAW SRM 53-04, FIGURE 12, PAGE 35. A REPAIR DOUBLER AND FINGER DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 12, PAGE 35, 51-10-4, 53-30-5, AND 51-30-2.

Next page: https://openairdocs.org/deregistered/N16815-2002-09-17/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 = 'N16815' AND deregistration_id = 'N16815-2002-09-17'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N16815-2002-09-17/reports

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