# Service difficulty reports: Douglas C-118A

A list on [Douglas C-118A](https://openairdocs.org/model/douglas-c-118a.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 3 · 120 reports

- [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 FXGA202108202130](https://openairdocs.org/sdr/FXGA202108202130.md): Skin · corroded · Aug 20, 2021 · N747CE · Doug C118A · Cargo/Baggage Doors
  > FWD CARGO DOOR CORRODED STRUCTURE. TO REPAIR A CORRODED SKIN ON THE MAIN CABIN FORWARD CARGO DOOR AROUND THE DOOR LATCH ASSEMBLY (F/STA 122 APPROXIMATELY). PERFORM REPAIR PER STS EA 80-2021-124.
- [SDR FXGA 202108202128](https://openairdocs.org/sdr/FXGA%20202108202128.md): Skin · corroded · Aug 20, 2021 · N747CE · Doug C118A · Cargo/Baggage Doors
  > AFT CARGO DOOR SKIN REPAIR. TO REPAIR A CORRODED SKIN SEAM AT THE AFT EDGE OF THE MAIN CARGO DOOR AT F/STA 798. PERFORM REPAIRS AT AFT EDGE OF MAIN CARGO DOOR PER DC-6 A&B OVERHAUL MANUAL FIGURE 12-22.
- [SDR FXGA2021090202129](https://openairdocs.org/sdr/FXGA2021090202129.md): Skin · corroded · Aug 20, 2021 · N747CE · Doug C118A · Fuselage Main, Plate/Skin
  > UPPER FUSELAGE SKIN CORROSION @ F/STA 157. TO REPAIR CORRODED FUSELAGE SKIN AROUND THE GPS ANTENNA AT F/STA 82 BETWEEN STRINGER 1R & 2R. PERFORM REPAIR PER DC-6 A&B OHM FIGURE 12-22.
- [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 FXGA202102132112](https://openairdocs.org/sdr/FXGA202102132112.md): Skin · corroded · Feb 13, 2021 · N747CE · Doug C118A · Wing, Plate/Skin
  > UPPER WING SKIN REMOVAL AND REPLACEMENT, BETWEEN CENTER AND AFT SPARS, BETWEEN W/STA 167R AND 193R. TO REMOVE AND REPLACE A CORRODED SKIN BETWEEN W/STA 167R AND 193R. REMOVE CORRODED SKIN BETWEEN EXISTING SPLICES AT W/STA 167R AND 193R. USING EXISTING SKIN AS
- [SDR FXGA202102012107](https://openairdocs.org/sdr/FXGA202102012107.md): Stringer · cracked · Feb 1, 2021 · N747CE · Doug C118A · Wing, Longeron/Stringer
  > CRACKED WING STRINGER AT W/STA 242L, STRINGER 19. TO REPAIR A CRACKED WING STRINGER AT W/STA 242L, STRINGER 19. RREPAIR CRACKED STRINGER PER STS INSTRUCTIONS IN EA 69-2021-019.
- [SDR FXGA202102012108](https://openairdocs.org/sdr/FXGA202102012108.md): Skin · cracked · Feb 1, 2021 · N747CE · Doug C118A · Wing, Plate/Skin
  > CRACKED WING SKIN AT W/STA 207L, STRINGER 20. TO REPAIR A CRACKED WING SKIN AT 4 FASTENER LOCATIONS AT W/STA 207L, STRINGER 20. CUT OUT DAMAGE AND REPAIR WING SKIN PER STS ENGINEERING AUTHORIZATION EA 74-2021-007.
- [SDR FXGA202010082017](https://openairdocs.org/sdr/FXGA202010082017.md): Skin · damaged · Oct 8, 2020 · N747CE · Doug C118A · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DAMAGE AT F/STA 736 TO 743 BETWEEN STRINGERS 24 AND 25. TO REPAIR FUSELAGE SKIN DAMAGE CAUSED BY A FORKLIFT. CUT OUT DAMAGE AND PERFORM REPAIR, PER DC-6 A&B SRM FIGURE 12-21 FUSELAGE PLATING REPAIR.
- [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 FXGA20200826001](https://openairdocs.org/sdr/FXGA20200826001.md): Spring · broken · Aug 25, 2020 · N747CE · Doug C118A · Hydraulic System, Main
  > HYDRAULIC BYPASS STUCK IN UP POSITION, UPON INSPECTIN FOUND HYDRAULIC BYPASS RETURN SPRING BROKEN.
- [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 FXGA201908081965](https://openairdocs.org/sdr/FXGA201908081965.md): Floorbeam · corroded · Aug 8, 2019 · N747CE · Doug C118A · Fuselage Main, Floor Beam
  > CORROSION ON RBL 11.5 FLOOR BEAM AT F/STA 240. TO REINFORCE THE LOWER FLANGE OF THE RBL 11.5 FLOOR BEAM AT F/STA 240, AFTER CORROSION REMOVAL. THE CORROSION IS LOCATED ON THE BOTTOM SIDE OF THE LOWER FLANGE. CLEAN CORROSION AND INSTALL LOWER REINFORCING ANG
- [SDR FXGA2019081061962](https://openairdocs.org/sdr/FXGA2019081061962.md): Doubler · corroded · Aug 6, 2019 · N747CE · Doug C118A · Nacelle/Pylon, Plate/Skin
  > REMOVAL AND REPLACEMENT OF CORROSION DOUBLER OUTBOARD OF #3 NACELLE BETWEE CENTER AND AFT SPAR. TO REMOVE AND REPLACE A PREVIOUSLY INSTALLED "CORROSION DOUBLER" BETWEEN W/STA 176R AND 206R BETWEEN CENTER AND REAR SPAR. REMOVE EXISTING DOUBLER AND MANUFACTURE
- [SDR FXGA201908051960](https://openairdocs.org/sdr/FXGA201908051960.md): Stringer · chafed · Aug 5, 2019 · N747CE · Doug C118A · Fuselage Main, Longeron/Stringer
  > FUSELAGE STRINGER #14L REPAIR AT F/STA -36. TO REPAIR A CHAFFED HOLE IN STRINGER 14L. TRIM CHAFFED AREA AND REPAIR STRINGER PER DC-6 A&B OVERHAUL MANUAL FIGURE 12-2A.
- [SDR FXGA201908051959](https://openairdocs.org/sdr/FXGA201908051959.md): Skin · cracked · Aug 5, 2019 · N747CE · Doug C118A · Wing, Plate/Skin
  > UPPER WING SKIN CRACKED AT W/STA 96R, STRINGER #3. TO REPAIR A SMALL CRACK AROUND A FUEL QUANTITY PROBE ACCESS HOLE AT W/STA 96R, STRINER 3. TRIM OUT CRACK AND REPAIR SKIN PER DC-6 A&B OVERHAUL MANUAL FIGURE 13-30.
- [SDR FXGA201903141927](https://openairdocs.org/sdr/FXGA201903141927.md): Frame · cracked · Mar 14, 2019 · N451CE · Doug C118A · Fuselage Main, Frame
  > FUSELAGE FRAME REPAIR REPLACEMENT AT F/STA -29 LT SIDE. TO REPAIR CRACK ON FRAME REPAIR AT F/STA -29 ABOVE FWD DOOR HINGE. REMOVE AND REPLACE EXISTING REPAIR PER OVERHAUL MANUAL 11-4-8 AND 11-4-9.
- [SDR FXGA201812240001](https://openairdocs.org/sdr/FXGA201812240001.md): Propeller · sheared · Dec 21, 2018 · N451CE · Doug C118A · Propeller Feathering/Reversing
  > EXCESSIVE VIBRATION ON #4 ENGINE NO OTHER INDICATION PRECAUTIONARY SHUTDOWN #4 ENGINE/ TWO BLADES WENT TO FEATHER THIRD BLADE STAYED IN LOW PITCH CONDITION
- [SDR FXGA201811281827](https://openairdocs.org/sdr/FXGA201811281827.md): Skin · cracked · Nov 28, 2018 · N451CE · Doug C118A · Fuselage Main, Plate/Skin
  > CRACKED FUSELAGE SKIN UNDER COMM ANTENNA AT F/STA 348 BETWEEN STRINGER 1L AND 1R. CRACKED FUSELAGE SKIN UNDER NR 2 COMM ANTENNA AT F/STA 348 BETWEEN STRINGER 1L AND 1R. PERFORM SKIN REPAIR PER DC-6 A&B OHM FIGURE 12-22.
- [SDR FXGA201811021824](https://openairdocs.org/sdr/FXGA201811021824.md): Plate · corroded · Nov 2, 2018 · N747CE · Doug C118A · Fuselage Miscellaneous Structure
  > CORRODED FLOOR PLATING IN FRONT OF THE MAIN CARGO DOOR BETWEEN F/STA 667 AND 794. TO REPAIR THE CORRODED CABIN FLOOR PLATING JUST INBOARD OF THE MAIN CARGO DOOR. CUT CORRODED SECTION OF FLOOR, 24" WIDE STARTING AT THE LT EDGE OF FLOOR PLATING BETWEEN F/STA 66
- [SDR FXGA201804121809](https://openairdocs.org/sdr/FXGA201804121809.md): Skin · corroded · Apr 13, 2018 · N747CE · Doug C118A · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CORRODED AT BS 974, STRINGER 1R. REPAIRED IAW DRAWING 1809-01.
- [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 FXGA20171208001](https://openairdocs.org/sdr/FXGA20171208001.md): Carburetor · leaking · Dec 7, 2017 · N451CE · Doug C118A · Fuel Control/Reciprocating Engines
  > COMING OUT OF REVERSE #1 ENGINE STARTED ON FIRE, UNABLE TO RESTART BLEW RIGHT SIDE CO2 BANK
- [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 FXGA201610141636](https://openairdocs.org/sdr/FXGA201610141636.md): Frame · cracked · Oct 14, 2016 · N747CE · Doug C118A · Fuselage Main, Frame
  > CRACKED FUSELAGE FRAME AT FS 1071 STRINGER 14R. REPAIR A 1/4" CRACK IN A FUSELAGE FRAME. THE CRACK GOES FROM STRINGER 14R RELIEF RADIUS TO A RIVET HOLE. INSTALL REPAIR DOUBLER ON CRACKER FRAME AT FS 1071 PER DRAWING 1636-01 AND OVERHAUL MANUAL FIGURE 12-3A.
- [SDR FXGA201609151628](https://openairdocs.org/sdr/FXGA201609151628.md): Skin · corroded · Sep 12, 2016 · N451CE · Doug C118A · Fuselage Main, Plate/Skin
  > CORRODED SKIN LAP JOINT AT BS 380 BETWEEN STRINGER 20R AND 21R. CORRODED SKIN LAP JOINT. CUT-OUT DAMAGE AND INSTALL REPAIR DOUBLER PER THE INSTRUCTIONS CONTAINED IN EAC EO 0502.
- [SDR FXGA201609151627](https://openairdocs.org/sdr/FXGA201609151627.md): Skin · corroded · Sep 9, 2016 · N451 · Doug C118A · Fuselage Main, Plate/Skin
  > CORRODED FUSELAGE SKIN AFT OF CABIN HEATER EXHAUST SHIELD. REMOVE CORRODED SKIN AND INSTALL REPAIR DOUBLER PER DC-6 A&B OVERHAUL MANUAL FIGURE 12-22.
- [SDR FXGA201606231615](https://openairdocs.org/sdr/FXGA201606231615.md): Skin · worn · Jun 23, 2016 · N251CE · Doug C118A · Wing, Plate/Skin
  > LOOSE RIVETS AT FORWARD SPAR UPPER CAP BETWEEN ENGINE NR 3 AND NR 4. REPAIR OF WORN WING SKIN COUNTERSINKS CAUSED BY LOOSE RIVETS BETWEEN WING STA 201 AND 280. PERFORM SKIN CUTOUT AT FRONT SPAR AFT TANG BETWEEN WING STA 201R AND 280R. PERFORM NEW FASTENER L
- [SDR FXGA201606231607](https://openairdocs.org/sdr/FXGA201606231607.md): Stringer · cracked · Jun 23, 2016 · N251CE · Doug C118A · Wing, Longeron/Stringer
  > CRACKED WING STR 21R AT WING STA 203R, TO REPAIR WING STRINGER 21R CRACKED AT WING STA 203R. REMOVE EXISTING SKIN DOUBLER INSTALLED IAW T/O 1C-118A-3-1, FIGURE 2-61, REPAIR CRACKED STR IAW EAC EO 9915 AND EXTENDED EXTERNAL REPAIR DOUBLER TO INCLUDE EXISTING S
- [SDR FXGA201606160001](https://openairdocs.org/sdr/FXGA201606160001.md): Stringer · cracked · Jun 16, 2016 · N251CE · Doug C118A · Wing, Longeron/Stringer
  > CRACKED WING STR 18R AT WING STA 242R. TO REPAIR WING STR 18R CRACKED AT WING STA 242R, CUT CRACKED STR CAP AT WING STA 223.5 AND 255.25. STOP DRILL CRACKS IN STR 18L BETWEEN WING STA 239 AND STA 244. MANUFACTURE AND INSTALL STR REPAIR PARTS IAW EAC EO 9115
- [SDR FXGA201508141509](https://openairdocs.org/sdr/FXGA201508141509.md): Cap · cracked · Aug 14, 2015 · N451CE · Doug C118A · Wing, Longeron/Stringer
  > WING STRINGER CAP 21, CRACKED AT STATION 238R. REMOVE STRINGER CAP FROM STATION 230.5 TO 252.0. MANUFACTURE & INSTALL CAP STRINGER SPLICES IAW REPAIR SKETCH 891212002.
- [SDR FXGA201508071533](https://openairdocs.org/sdr/FXGA201508071533.md): Skin · corroded · Aug 7, 2015 · N351CE · Doug C118A · Fuselage Main, Plate/Skin
  > CORRODED SKIN AT FS 200, BETWEEN STRINGER 4L & 8L. REPAIRED CORRODED SKIN, PERFORMED SKIN SPLICE IAW EAC EO 05 21 & 0301.
- [SDR FXGA201508071532](https://openairdocs.org/sdr/FXGA201508071532.md): Skin · corroded · Aug 7, 2015 · N351CE · Doug C118A · Fuselage Main, Plate/Skin
  > TO REPAIR A CORRODED SKIN LAP JOINT AT FS 200, STRINGER 4L, PERFORMED SKIN LAP REPAIR IAW THE INSTRUCTIONS GIVEN IN EAC EO 0502.
- [SDR FXGA201508061513](https://openairdocs.org/sdr/FXGA201508061513.md): Cap · cracked · Aug 6, 2015 · N451CE · Doug C118A · Wing, Longeron/Stringer
  > WING STRINGER CAP 21, CRACKED AT STATION 242L. REMOVE STRINGER CAP FROM STATION 230.0 TO 250.0. MANUFACTURE & INSTALL CAP STRINGER SPLICES IAW REPAIR SKETCH 891212002.
- [SDR FXGA201508061505](https://openairdocs.org/sdr/FXGA201508061505.md): Cap · cracked · Aug 6, 2015 · N451CE · Doug C118A · Wing, Longeron/Stringer
  > WING STRINGER CAP 18, CRACKED AT STATION 238L. REMOVED STRINGER CAP FROM STATION 232L TO 250L. MANUFACTURE & INSTALL STRINGER CAP & SPLICES IAW REPAIR SKETCH 891212002.
- [SDR FXGA201508061506](https://openairdocs.org/sdr/FXGA201508061506.md): Cap · cracked · Aug 6, 2015 · N451CE · Doug C118A · Wing, Longeron/Stringer
  > NUMBER 2 MAIN TANK, OTBD LANDING DOUBLER CRACKED. REMOVE STRINGER CAP FROM STATION 230.0 TO 250.0. MANUFACTURE & INSTALL CAP STRINGER SPLICES IAW REPAIR SKETCH 891212002.
- [SDR FXGA201508061508](https://openairdocs.org/sdr/FXGA201508061508.md): Cap · cracked · Aug 6, 2015 · N451CE · Doug C118A · Wing, Longeron/Stringer
  > WING STRINGER CAP 19, CRACKED AT STATION 238R & 244R. REMOVE STRINGER CAP FROM STATION 230.5 TO 252.0. MANUFACTURE & INSTALL CAP STRINGER SPLICES IAW REPAIR SKETCH 891212002.
- [SDR FXGA201508061531](https://openairdocs.org/sdr/FXGA201508061531.md): Skin · corroded · Aug 6, 2015 · N351CE · Doug C118A · Fuselage Main, Plate/Skin
  > TO REPAIR CORROSION DAMAGE ABOVE THE AFT EDGE OF THE FWD CARGO DOOR, AT WS 217, PERFORMED SKIN LAP REPAIR IAW THE INSTRUCTIONS GIVEN IN EAC EO 0502.
- [SDR FXGA201508051530](https://openairdocs.org/sdr/FXGA201508051530.md): Repair · cracked · Aug 5, 2015 · N351CE · Doug C118A · Fuselage Main, Bulkhead
  > REPAIR CRACKED WEB ON THE FUSELAGE BULKHEAD AT FS 600. PERFORM REPAIR IAW DC-6 A & B OVERHAUL MANUAL FIGURE 12-6.
- [SDR FXGA201507311529](https://openairdocs.org/sdr/FXGA201507311529.md): Skin · corroded · Jul 28, 2015 · N351CE · Doug C118A · Cargo/Baggage Doors
  > REPAIR A CORRODED SKIN ON THE UPPER AFT CORNER OF THE FWD CARGO DOOR. PERFORM CUT OUT OF CORRODED SKIN AT FS 200. REMOVE AFT SECTION OF SKIN AT EXISTING LAP AT SAME LEVEL OF FUSELAGE STRINGER 12L. LAYOUT NEW SEAM AT FS 200 IAW DWG 1529-01 & MANUFACTURE NEW
- [SDR FXGA201507141528](https://openairdocs.org/sdr/FXGA201507141528.md): Web · cracked · Jul 14, 2015 · N251CE · Doug C118A · Fuselage Miscellaneous Structure
  > TO REPAIR CRACKED WEB AT FS 600 BULKHEAD. PERFORM REPAIR IAW A & B OVERHAUL MANUAL FIGURE 12-6.
- [SDR FXGA20150626001](https://openairdocs.org/sdr/FXGA20150626001.md): Bearing · galled · Jun 25, 2015 · N747CE · Doug C118A · Wheel/Ski/Float
  > DEPARTING AIRPORT, ACFT LOST NR 4 MLG WHEEL & TIRE ASSEMBLY. ACFT DIVERTED, DECLARED AN EMER HELD OVER TO BURN FUEL OFF FOR LANDING WEIGHT. LANDING WAS FULL STOP & UNEVENTFUL.
- [SDR FXGA201506091522](https://openairdocs.org/sdr/FXGA201506091522.md): Doubler · cracked · Jun 9, 2015 · N747CE · Doug C118A · Wing Miscellaneous Structure
  > REPLACEMENT OF LANDING DOUBLER IAW SB 799. TWO CRACKS WERE FOUND AT LT WS 214 LOWER ON THE INBD LANDING DOUBLER REQUIRE THE REMOVAL & REPLACEMENT OF THE DOUBLER. NOTE SERVICE BULLETIN 799 ATTACHED TO THIS EO FOR SCOPE OF WORK & REPAIR DATA. NOTE REPLACEMENT

Next page: https://openairdocs.org/model/douglas-c-118a/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 aircraft_model_key = 'C118A'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/douglas-c-118a/reports

---
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