Douglas C-118A
Service difficulty reports · 120
Newest first. General aviation reporting is voluntary.
Query with SQL
duckdb -csv -c "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"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR FXGA20220802221None · noneFUSELAGE 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 FXGA202208022221Stringer · crackedFUSELAGE 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 FXGA202108202130Skin · corrodedFWD 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 202108202128Skin · corrodedAFT 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 FXGA2021090202129Skin · corrodedUPPER 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 FXGA202105182121Skin · corrodedCORROSION 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 OUSDR FXGA202102132112Skin · corrodedUPPER 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 FXGA202102012107Stringer · crackedCRACKED 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 FXGA202102012108Skin · crackedCRACKED 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 FXGA202010082017Skin · damagedFUSELAGE 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 FXGA2020091412013Stringer · crackedCRACKED 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 FXGA2020091402012Skin · corrodedCORRODED 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 FXGA202009012010Doubler · crackedLANDING 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 FXGA20200826001Spring · brokenHYDRAULIC BYPASS STUCK IN UP POSITION, UPON INSPECTIN FOUND HYDRAULIC BYPASS RETURN SPRING BROKEN.SDR FXGA201912271981Skin · crackedCRACKED 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 FXGA201909171973Skin · corrodedCORRODED 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 ISDR FXGA201909171972Skin · corrodedCORRODED 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 FXGA2019082861968Trunnion · crackedR/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 FITTINSDR FXGA201908081965Floorbeam · corrodedCORROSION 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 ANGSDR FXGA2019081061962Doubler · corrodedREMOVAL 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 MANUFACTURESDR FXGA201908051960Stringer · chafedFUSELAGE 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 FXGA201908051959Skin · crackedUPPER 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 FXGA201903141927Frame · crackedFUSELAGE 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 FXGA201812240001Propeller · shearedEXCESSIVE VIBRATION ON #4 ENGINE NO OTHER INDICATION PRECAUTIONARY SHUTDOWN #4 ENGINE/ TWO BLADES WENT TO FEATHER THIRD BLADE STAYED IN LOW PITCH CONDITIONSDR FXGA201811281827Skin · crackedCRACKED 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 FXGA201811021824Plate · corrodedCORRODED 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 66SDR FXGA201804121809Skin · corrodedFUSELAGE SKIN CORRODED AT BS 974, STRINGER 1R. REPAIRED IAW DRAWING 1809-01.SDR FXGA201801101801Tab · crackedRIGHT INBOARD AILERON TRIM TAB SKIN HAD TWO CRACKS. REMOVED THE TAB, STOP DRILLED THE CRACKS.SDR FXGA20171208001Carburetor · leakingCOMING OUT OF REVERSE #1 ENGINE STARTED ON FIRE, UNABLE TO RESTART BLEW RIGHT SIDE CO2 BANKSDR FXGA201703091705Fitting · crackedCRACKED 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 FXGA201702081703Skin · corrodedUPPER 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 FXGA201610141636Frame · crackedCRACKED 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 FXGA201609151628Skin · corrodedCORRODED 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 FXGA201609151627Skin · corrodedCORRODED 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 FXGA201606231615Skin · wornLOOSE 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 LSDR FXGA201606231607Stringer · crackedCRACKED 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 SSDR FXGA201606160001Stringer · crackedCRACKED 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 9115SDR FXGA201508141509Cap · crackedWING 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 FXGA201508071533Skin · corrodedCORRODED SKIN AT FS 200, BETWEEN STRINGER 4L & 8L. REPAIRED CORRODED SKIN, PERFORMED SKIN SPLICE IAW EAC EO 05 21 & 0301.SDR FXGA201508071532Skin · corrodedTO REPAIR A CORRODED SKIN LAP JOINT AT FS 200, STRINGER 4L, PERFORMED SKIN LAP REPAIR IAW THE INSTRUCTIONS GIVEN IN EAC EO 0502.SDR FXGA201508061513Cap · crackedWING 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 FXGA201508061505Cap · crackedWING 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 FXGA201508061506Cap · crackedNUMBER 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 FXGA201508061508Cap · crackedWING 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 FXGA201508061531Skin · corrodedTO 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 FXGA201508051530Repair · crackedREPAIR CRACKED WEB ON THE FUSELAGE BULKHEAD AT FS 600. PERFORM REPAIR IAW DC-6 A & B OVERHAUL MANUAL FIGURE 12-6.SDR FXGA201507311529Skin · corrodedREPAIR 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 FXGA201507141528Web · crackedTO REPAIR CRACKED WEB AT FS 600 BULKHEAD. PERFORM REPAIR IAW A & B OVERHAUL MANUAL FIGURE 12-6.SDR FXGA20150626001Bearing · galledDEPARTING 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 FXGA201506091522Doubler · crackedREPLACEMENT 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
Back to Douglas C-118A