# Service difficulty reports: N100CE

A list on [N100CE](https://openairdocs.org/aircraft/N100CE.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR FXGA20220802221](https://openairdocs.org/sdr/FXGA20220802221.md): None · none · Aug 2, 2022 · N100CE · Doug C118A · Fuselage Structure (General)
  > FUSELAGE STRINGER REPAIR AT F/STA -38, STRINGER 14R. TO REPAIR A CRACKED STRINGER BEHIND #4 FIRE BOTTLE, STRINGER 14R, F/STA -38. PERFORM STRINGER REPAIR PER DC-6A&B OVERHAUL MANUAL FIGURE 12-2.
- [SDR FXGA202208022221](https://openairdocs.org/sdr/FXGA202208022221.md): Stringer · cracked · Aug 2, 2022 · N100CE · Doug C118A · Fuselage Main, Longeron/Stringer
  > FUSELAGE STRINGER REPAIR AT F/STA -38, STRINGER 14R. TO REPAIR A CRACKER STRINGER BEHIND #4 FIRE BOTTLE. STRINGER 14R, F/STA -38. PERFORM STRINGER REPAIR PER DC-6A&B OVERHAUL MANUAL FIGURE 12-2.
- [SDR FXGA202105182121](https://openairdocs.org/sdr/FXGA202105182121.md): Skin · corroded · May 18, 2021 · N100CE · Doug C118A · Wing, Plate/Skin
  > CORROSION IN RIGHT HAND LOWER WING SKIN AT STATION 422, STRINGER 16. CORROSION IN RIGHT HAND LOWER WING SKIN AT STATION 422, STRINGER 16. CORROSION OF RH LOWER WING SKIN AT STA 422, STRINGER 16 WITH SMALL CRACK AROUND A FASTERNER REQUIRING A !" BY 0.5" TRIM OU
- [SDR FXGA2020091412013](https://openairdocs.org/sdr/FXGA2020091412013.md): Stringer · cracked · Sep 11, 2020 · N100CE · Doug C118A · Wing, Longeron/Stringer
  > CRACKED WING STRINGER 22 AT W/STA 243R TO REPAIR A CRACKED WING STRINGER 22 AT W/STA 243R. REPAIR CRACKED STRINGER, PER DC-6 A&B OVERHAUL MANUAL FIGURE 13-10 WING STRINGER REPAIRS.
- [SDR FXGA2020091402012](https://openairdocs.org/sdr/FXGA2020091402012.md): Skin · corroded · Sep 10, 2020 · N100CE · Doug C118A · Fuselage Main, Plate/Skin
  > CORRODED SKIN LAP AT F/STA 66, STRINGER 11L. TO REPAIR A CORRODED SKIN LAP AT F/STA 66, STRINGER 11L. CUT OUT DAMAGE AND REPAIR, PER EAC EO 0502, GENERIC REPAIR TO SKIN SAP SEAMS.
- [SDR FXGA202009012010](https://openairdocs.org/sdr/FXGA202009012010.md): Doubler · cracked · Sep 1, 2020 · N100CE · Doug C118A · Wing Main, Frame Structure
  > LANDING DOUBLER REPLACEMENT BETWEEN W/STA 167R AND 242R PER SB 799. TO REPLACE A CRACKED LANDING DOUBLER PER SB 799. REMOVE AND REPLACE CRACKED LANDING DOUBLER PER INSTRUCTIONS IN DOUGLAS SB 799.
- [SDR FXGA201912271981](https://openairdocs.org/sdr/FXGA201912271981.md): Skin · cracked · Dec 27, 2019 · N100CE · Doug C118A · Wing, Plate/Skin
  > CRACKED WING SKIN AND STRINGER AT W/STA 240L STRINGER #22. TO REPAIR A CRACK SKIN AND STRINGER #22 AT W/STA 240L. PERFORM WING STRINGER REPAIR PER OHM FIGURE 13-10, AND PERFORM WING SKIN REPAIR PER OHM FIGURE 13-30.
- [SDR FXGA201909171973](https://openairdocs.org/sdr/FXGA201909171973.md): Skin · corroded · Sep 17, 2019 · N100CE · Doug C118A · Cargo/Baggage Doors
  > CORRODED SKIN AROUND EXTERNAL HANDLE OF FWD MAIN CARGO DOOR. TO REPAIR CORRODED SKINS AT THE FWD MAIN CARGO DOOR DIRECTLY BELOW THE EXTERNAL HANDLE AT THE SEAM, AROUND F/STA 120. PERFORM 2 SKIN REPAIRS PER DC-6 A&B OVERHAUL MANUAL FIGURE 12-22. ONE REPAIR I
- [SDR FXGA201909171972](https://openairdocs.org/sdr/FXGA201909171972.md): Skin · corroded · Sep 17, 2019 · N100CE · Doug C118A · Cargo/Baggage Doors
  > CORRODED SKIN ON MAIN AFT CARGO DOOR LOWER EDGE. TO REPAIR A CORRODED SKIN ON THE LOWER EDGE OF THE MAIN CARGO DOOR AT F/STA 762 AND AT F/STA 798. PERFORM REPAIRS AT LOWER EDGE OF AFT CARGO DOOR PER DC-6 A&B OVERHAUL MANUAL FIGURE 12-22.
- [SDR FXGA2019082861968](https://openairdocs.org/sdr/FXGA2019082861968.md): Trunnion · cracked · Aug 26, 2019 · N100CE · Doug C118A · Wing, Landing Gear Attach Fittings
  > R/H MLG OUTBOARD TRUNNION FITTING REPLACEMENT. TO REPLACE THE CRACKED RIGHT HAND MLG OUTBOARD TRUNNION FITTING. PERFORM CUT-OUTS IN THE UPPER WING SKIN AND RIB AT W/STA 167R TO PERMIT THE REMOVAL AND REPLACEMENT OF THE RIGHT HAND MLG OUTBOARD TRUNNION FITTIN
- [SDR FXGA201801101801](https://openairdocs.org/sdr/FXGA201801101801.md): Tab · cracked · Jan 10, 2018 · N100CE · Doug C118A · Aileron Tabs
  > RIGHT INBOARD AILERON TRIM TAB SKIN HAD TWO CRACKS. REMOVED THE TAB, STOP DRILLED THE CRACKS.
- [SDR FXGA201703091705](https://openairdocs.org/sdr/FXGA201703091705.md): Fitting · cracked · Mar 9, 2017 · N100CE · Doug C118A · Nacelle/Pylon Miscellaneous Structure
  > CRACKED FITTING ON NR 2 NACELLE (TEMPORARY REPAIR). TO PERFORM A STOP DRILL ON A CRACKED FITTING. A CRACK WAS FOUND ON THE LOWER INBOARD AFT FITTING OF THE NR 2 NACELLE (P/N 3320980). THE CRACK WILL BE STOP DRILLED AND A STACK UP OF TWO 2024-T3 0.050" AND ONE
- [SDR FXGA201702081703](https://openairdocs.org/sdr/FXGA201702081703.md): Skin · corroded · Feb 17, 2017 · N100CE · Doug C118A · Wing, Plate/Skin
  > UPPER WING SKIN SPLICE AT W/STA 212L BETWEEN CENTER AND AFT SPARS. TO REPLACE A SECTION OF CORRODED SKIN. PERFORM WING SKIN SPLICE PER SRM TO 1C-118A-3-1 FIGURE 2-59, AND CENTER SPAR CORROSION CLEAN UP PER SRM TO 1C-118A-3-1 FIGURE C-2.
- [SDR FXGA201501141502](https://openairdocs.org/sdr/FXGA201501141502.md): Stringer · cracked · Jan 14, 2015 · N100CE · Doug C118A · Wing, Longeron/Stringer
  > CRACKED WING STRINGER 15 AT WS 368L. CUT CRACKED STRINGER AT WS 368L. R & R INBD SECTION ENDING AT WS 353 5L. MANUFACTURE & INSTALL REPAIR DOUBLER IAW DC-6 A & B OVERHAUL MANUAL FIGURE 13-9. DUE TO MINIMUM EDGE DISTANCE BETWEEN THE 2 ROWS ON THE STRINGER C
- [SDR FXGA20131125001](https://openairdocs.org/sdr/FXGA20131125001.md): Stringer · corroded · Oct 31, 2013 · N100CE · Doug C118A · Wing, Longeron/Stringer
  > CORROSION WAS FOUND ON THE INBD END OF WING STRINGER 18L AT WS 287L. REMOVED CORRODED STRINGER SECTION BETWEEN WS 281L & 336L & INSTALLED A NEW SECTION MANUFACTURED FROM EXTRUSION PN S1245691.
- [SDR FXGA20131125003](https://openairdocs.org/sdr/FXGA20131125003.md): Skin · corroded · Oct 17, 2013 · N100CE · Doug C118A · Fuselage Main, Plate/Skin
  > CORRODED FUSELAGE SKIN FOUND UNDER AN ADF ANTENNA AT FS 152 BETWEEN STRINGERS 33 LT & RT. CUT OUT DAMAGED SKIN & INSTALLED A 2024-T3 0.040 INCH DOUBLER IAW C-118 SRM T O 1C-118-3-A FIGURE 4-31.
- [SDR FXGA20131125004](https://openairdocs.org/sdr/FXGA20131125004.md): Skin · dented · Oct 14, 2013 · N100CE · Doug C118A · Wing, Plate/Skin
  > WING LE SKIN REQUIRED A DENT REPAIR AT WS 615.75R. THE AFFECTED AREA WAS CUTOUT & REPAIRED WITH A FLUSH PATCH IAW DC-6 OVERHAUL MANUAL FIGURE 13-33 & DRAWINGS 1359-01 & -02.
- [SDR FXGA20131125002](https://openairdocs.org/sdr/FXGA20131125002.md): Skin · cracked · Oct 9, 2013 · N100CE · Doug C118A · Wing, Plate/Skin
  > CRACKS WERE FOUND ON THE LOWER WING SKIN AT WS 281 LT & RT. INSTALLED DOUBLERS INBD OF THE NR 1 & NR 4 NACELLES IAW THE GENERAL SERVICE LETTER MIL235 DAC SB 661.
- [SDR FXGA201302121304](https://openairdocs.org/sdr/FXGA201302121304.md): Web · cracked · Feb 12, 2013 · N100CE · Doug C118A · Fuselage Miscellaneous Structure
  > CRACK IN A WEB ADJACENT TO THE VERTICAL STAB AT BS 1094. REPAIRED IAW EO 1304.
- [SDR FXGA201210011274](https://openairdocs.org/sdr/FXGA201210011274.md): Structure · corroded · Oct 1, 2012 · N100CE · Doug C118A · Wing Main, Frame Structure
  > CORRODED EXTRUSION WS 75R AT REAR INSPECTION DOOR 123 EO 1274.
- [SDR FXGA201209281276](https://openairdocs.org/sdr/FXGA201209281276.md): Spar · corroded · Sep 28, 2012 · N100CE · Doug C118A · Vertical Stabilizer, Spar/Rib
  > CORRODED VERTICAL STABILIZER FRONT SPAR ATTACH FITTINGS. R & R.
- [SDR FXGA201209271273](https://openairdocs.org/sdr/FXGA201209271273.md): Skin · cracked · Sep 27, 2012 · N100CE · Doug C118A · Nacelle/Pylon, Plate/Skin
  > NR 1 NACELLE SKIN CRACK AT FUEL DUMP OPENING EO 1273.
- [SDR FXGA201209261272](https://openairdocs.org/sdr/FXGA201209261272.md): Frame · corroded · Sep 26, 2012 · N100CE · Doug C118A · Fuselage Main, Frame
  > CORRODED TEE WEB ON A FUSELAGE FRAME AT BS 1049. REPAIRED IAW EO 1272.
- [SDR FXGA201209181271](https://openairdocs.org/sdr/FXGA201209181271.md): Skin · cracked · Sep 18, 2012 · N100CE · Doug C118A · Trailing Edge Flaps
  > RIGHT FLAP CRACKED AT W STA 149. REPAIRED IAW EO 1271.
- [SDR FXGA201204091226](https://openairdocs.org/sdr/FXGA201204091226.md): Frame · damaged · Apr 9, 2012 · N100CE · Doug C118A · Nacelle/Pylon, Frame/Spar/Rib
  > NR 1 ENG NACELLE ACCESS FRAME DAMAGED. REMOVED DAMAGE & INSERTED REPAIR. FABRICATE DOUBLERS & INSTALLED.
- [SDR FXGA201204051224](https://openairdocs.org/sdr/FXGA201204051224.md): Door · corroded · Apr 5, 2012 · N100CE · Doug C118A · Passenger/Crew Doors
  > FORWARD CABIN ENTRY DOOR HAS CORROSION. REMOVE CORROSION & INSTALL DOUBLER.
- [SDR FXGA2010114001](https://openairdocs.org/sdr/FXGA2010114001.md): Heater · cracked · Nov 4, 2010 · N100CE · Doug C118A · Heating System
  > CABIN HEATER EXHAUST ODOR IN COCKPIT DURING CRUISE FLIGHT. REPLACED CABIN HEATER IAW LMM 27-55-1 & 2, OPS CHECK GOOD.

## 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 = 'N100CE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N100CE/reports

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