# Douglas C-118A - Type: Aircraft model (FAA registry) - Registry code: 3021710 - Manufacturer (registry): DOUGLAS - Model: C-118A - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 4 · Reciprocating - Seats: 96 - Weight class: 20,000 lb and over - Cruise speed: 216 mph - Certification: Type certificated - Data sheet: [TCDS A19NM](https://openairdocs.org/tcds/A19NM) (OpenAirDocs) - Holder: Hawkins & Powers Aviation Inc. - Registered aircraft: 5 - Page: https://openairdocs.org/model/douglas-c-118a Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker. ## ADs that may apply (OpenAirDocs) Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. None matched. ## Registered aircraft (5) - [N100CE](https://openairdocs.org/aircraft/N100CE): [Tatonduk Outfitters Ltd](https://openairdocs.org/faa-owner/TATONDUK%20OUTFITTERS%20LTD), [Fairbanks, AK](https://openairdocs.org/faa-place/AK/Fairbanks), built 1953, S/N 44662 - [N251CE](https://openairdocs.org/aircraft/N251CE): [Everts Air Fuel](https://openairdocs.org/faa-owner/EVERTS%20AIR%20FUEL), [Fairbanks, AK](https://openairdocs.org/faa-place/AK/Fairbanks), built 1953, S/N 44612 - [N351CE](https://openairdocs.org/aircraft/N351CE): [Everts Air Fuel Inc](https://openairdocs.org/faa-owner/EVERTS%20AIR%20FUEL%20INC), [Fairbanks, AK](https://openairdocs.org/faa-place/AK/Fairbanks), built 1954, S/N 44599 - [N747CE](https://openairdocs.org/aircraft/N747CE): [Tatonduk Outfitters Ltd](https://openairdocs.org/faa-owner/TATONDUK%20OUTFITTERS%20LTD), [Fairbanks, AK](https://openairdocs.org/faa-place/AK/Fairbanks), built 1955, S/N 44661 - [N951CE](https://openairdocs.org/aircraft/N951CE): [Everts Air Fuel Inc](https://openairdocs.org/faa-owner/EVERTS%20AIR%20FUEL%20INC), [Fairbanks, AK](https://openairdocs.org/faa-place/AK/Fairbanks), built 1952, S/N 43696 ## NTSB investigations (5) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB ANC19LA045](https://openairdocs.org/ntsb/ANC19LA045), Aug 1, 2019: Douglas C 118A (N451CE), Buckland, AK, substantial damage. Probable cause: The pilot's failure to maintain an adequate glidepath during the approach, which resulted in the airplane impacting rocks and dirt at the runway threshold, a separation of the right main landing… - [NTSB ENG14IA016](https://openairdocs.org/ntsb/ENG14IA016), Feb 25, 2014: Douglas C 118A (N351CE), Emmonak, AK, incident, minor damage. Probable cause: The fatigue failure of the lower wing skin due to aging mechanisms. Contributing to the failure were lower wing skin inspection procedures insufficient to identify the crack. - [NTSB ANC14CA012](https://openairdocs.org/ntsb/ANC14CA012), Nov 25, 2013: Douglas DC-6 (N100CE), Nuiqsut, AK, substantial damage. Probable cause: A load shift during takeoff, which resulted in substantial damage to the aft bulkhead and associated structures. - [NTSB MIA87LA156](https://openairdocs.org/ntsb/MIA87LA156), May 3, 1987: Douglas DC-6A (N43867), Ft.Lauderdale, FL, substantial damage - [NTSB ANC84LA086](https://openairdocs.org/ntsb/ANC84LA086), Jun 9, 1984: Douglas C-118A (N4206L), Deadhorse, AK, substantial damage ## FAA accident and incident reports (14) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Accident 20190801013109A](https://openairdocs.org/incident/20190801013109A), Aug 1, 2019: Douglas C-118A (N451CE), Candle, AK, Destroyed. With the PIC at the controls, after overflying RW20 at AK75, the aircraft remained in a normal traffic pattern to land RW20 at 1500' AGL. The aircraft began… - [Incident 20140224003089I](https://openairdocs.org/incident/20140224003089I), Feb 24, 2014: Douglas C-118A (N351CE), Emmonak, AK, Substantial damage. Ptrs number: AL07201401642. After fxga, flt 99, arrived at Emmonak, AK. The crew discovered a fuel leak in the post flight walk around inspection. The leak was… - [Accident 20131125025379A](https://openairdocs.org/incident/20131125025379A), Nov 25, 2013: Douglas C-118A (N100CE), Deadhorse, AK, Substantial damage. During an all cargo flight from Alpine strip, Alaska to Deadhorse Alaska on 11/25/2013 the aircraft experienced a cargo load shift resulting in damage to the… - [Incident 20110614012919I](https://openairdocs.org/incident/20110614012919I), Jun 14, 2011: Douglas C-118A (N351CE), Anchorage, AK, No damage. Ptrs 201104308DURING reversing on landing rollout in Anchorage, the number 1 engine backfired and exhaust pipe caught fire. The exhaust fire extinguished… - [Incident 20090118024979I](https://openairdocs.org/incident/20090118024979I), Jan 18, 2009: Douglas DC-6-C118A (N888DG), Atqasuk, AK, Minor damage. Pilot reported having runway 24 in sight approximately 1.2-1.5 miles out with flat light, blowing snow, and a 30 knot crosswind from 230. Pilot stated that he… - [Incident 19990421014739I](https://openairdocs.org/incident/19990421014739I), Apr 21, 1999: Doug DC6B (N874TA), Miami, FL. Flight 100 from mjbq to mdsd experienced a complete hydraulic failure prior to landing in mdsd. Hydraulic failure procedures were followed and a no flap… - [Incident 19980320007969I](https://openairdocs.org/incident/19980320007969I), Mar 20, 1998: Doug C118A (N351CE), Anchorage, AK. Narrative: departed Anchorage International Airport. Aprox. 15 min into flight, #3 engine indicated an intermittent oil quantity decrease. #3 propeller was… - [Incident 19911018051009I](https://openairdocs.org/incident/19911018051009I), Oct 18, 1991: Doug C118A (N9045P), St Louis, MO. Hydraulic failure. No brakes or steering. Ran off end of runway. Found hydraulic manifold mfp 5105521 had cracked. - [Incident 19900213005969I](https://openairdocs.org/incident/19900213005969I), Feb 13, 1990: Doug C118A (N90444), St Louis, MO. Lost hydraulic pressure and quantity on approach. Found surge accumulator had a loose b nut on pressure line. - [Incident 19890405016469I](https://openairdocs.org/incident/19890405016469I), Apr 5, 1989: Doug C118A (N90444), San Antonio, TX. Left outboard gear tire damaged on touchdown. Punctured by unknown object on runway. - [Accident 19870503033829A](https://openairdocs.org/incident/19870503033829A), May 3, 1987: Doug C118A (N43867), Ft Lauderdale, FL, Substantial damage. Severe nosewheel shimmy encountred during rollout. Horizontal stabilizer damaged. - [Incident 19860712042779I](https://openairdocs.org/incident/19860712042779I), Jul 12, 1986: Doug C118A (N1377K), Anchorage, AK, Minor damage. Shortly after liftoff, ring cowl departed NR1 engine. Returned. Maintenance had ring off before takeoff. - [Incident 19860227016269I](https://openairdocs.org/incident/19860227016269I), Feb 27, 1986: Doug C118A (N888DG), Talkeetna, AK, Substantial damage. Engine shut down after sparkplugs shorted on a cylinder. Fire in right accessory section. Safe emergency landing. - [Accident 19840608031639A](https://openairdocs.org/incident/19840608031639A), Jun 8, 1984: Doug C118A (N4206L), Kuparak, AK, Substantial damage. Struck an NDB antenna tower on IFR approach near end of runway. Decision height not maintained. Tower not lighted. ## Service difficulty reports (120, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR FXGA20220802221](https://openairdocs.org/sdr/FXGA20220802221), Aug 2, 2022: NONE. NONE. 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 - [SDR FXGA202208022221](https://openairdocs.org/sdr/FXGA202208022221), Aug 2, 2022: STRINGER. CRACKED. 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 - [SDR FXGA202108202130](https://openairdocs.org/sdr/FXGA202108202130), Aug 20, 2021: SKIN. CORRODED. 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). PERF - [SDR FXGA 202108202128](https://openairdocs.org/sdr/FXGA%20202108202128), Aug 20, 2021: SKIN. CORRODED. 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 P - [SDR FXGA2021090202129](https://openairdocs.org/sdr/FXGA2021090202129), Aug 20, 2021: SKIN. CORRODED. 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 - [SDR FXGA202105182121](https://openairdocs.org/sdr/FXGA202105182121), May 18, 2021: SKIN. CORRODED. 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 - [SDR FXGA202102132112](https://openairdocs.org/sdr/FXGA202102132112), Feb 13, 2021: SKIN. CORRODED. 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 - [SDR FXGA202102012107](https://openairdocs.org/sdr/FXGA202102012107), Feb 1, 2021: STRINGER. CRACKED. 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 - [SDR FXGA202102012108](https://openairdocs.org/sdr/FXGA202102012108), Feb 1, 2021: SKIN. CRACKED. 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 S - [SDR FXGA202010082017](https://openairdocs.org/sdr/FXGA202010082017), Oct 8, 2020: SKIN. DAMAGED. 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, PE - [SDR FXGA2020091412013](https://openairdocs.org/sdr/FXGA2020091412013), Sep 11, 2020: STRINGER. CRACKED. 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 WI - [SDR FXGA2020091402012](https://openairdocs.org/sdr/FXGA2020091402012), Sep 10, 2020: SKIN. CORRODED. 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 - [SDR FXGA202009012010](https://openairdocs.org/sdr/FXGA202009012010), Sep 1, 2020: DOUBLER. CRACKED. 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 - [SDR FXGA20200826001](https://openairdocs.org/sdr/FXGA20200826001), Aug 25, 2020: SPRING. BROKEN. HYDRAULIC BYPASS STUCK IN UP POSITION, UPON INSPECTIN FOUND HYDRAULIC BYPASS RETURN SPRING BROKEN. - [SDR FXGA201912271981](https://openairdocs.org/sdr/FXGA201912271981), Dec 27, 2019: SKIN. CRACKED. 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 - [SDR FXGA201909171973](https://openairdocs.org/sdr/FXGA201909171973), Sep 17, 2019: SKIN. CORRODED. 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, - [SDR FXGA201909171972](https://openairdocs.org/sdr/FXGA201909171972), Sep 17, 2019: SKIN. CORRODED. 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 REPAI - [SDR FXGA2019082861968](https://openairdocs.org/sdr/FXGA2019082861968), Aug 26, 2019: TRUNNION. CRACKED. 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 - [SDR FXGA201908081965](https://openairdocs.org/sdr/FXGA201908081965), Aug 8, 2019: FLOORBEAM. CORRODED. 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 - [SDR FXGA2019081061962](https://openairdocs.org/sdr/FXGA2019081061962), Aug 6, 2019: DOUBLER. CORRODED. REMOVAL AND REPLACEMENT OF CORROSION DOUBLER OUTBOARD OF #3 NACELLE BETWEE CENTER AND AFT SPAR. TO REMOVE AND REPLACE A PREVIOUSLY INSTALLED "CORROSION DOUBLER" - [SDR FXGA201908051960](https://openairdocs.org/sdr/FXGA201908051960), Aug 5, 2019: STRINGER. CHAFED. 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 - [SDR FXGA201908051959](https://openairdocs.org/sdr/FXGA201908051959), Aug 5, 2019: SKIN. CRACKED. 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 - [SDR FXGA201903141927](https://openairdocs.org/sdr/FXGA201903141927), Mar 14, 2019: FRAME. CRACKED. 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 PE - [SDR FXGA201812240001](https://openairdocs.org/sdr/FXGA201812240001), Dec 21, 2018: PROPELLER. SHEARED. 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), Nov 28, 2018: SKIN. CRACKED. 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 - [SDR FXGA201811021824](https://openairdocs.org/sdr/FXGA201811021824), Nov 2, 2018: PLATE. CORRODED. 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 - [SDR FXGA201804121809](https://openairdocs.org/sdr/FXGA201804121809), Apr 13, 2018: SKIN. CORRODED. FUSELAGE SKIN CORRODED AT BS 974, STRINGER 1R. REPAIRED IAW DRAWING 1809-01. - [SDR FXGA201801101801](https://openairdocs.org/sdr/FXGA201801101801), Jan 10, 2018: TAB. CRACKED. RIGHT INBOARD AILERON TRIM TAB SKIN HAD TWO CRACKS. REMOVED THE TAB, STOP DRILLED THE CRACKS. - [SDR FXGA20171208001](https://openairdocs.org/sdr/FXGA20171208001), Dec 7, 2017: CARBURETOR. LEAKING. COMING OUT OF REVERSE #1 ENGINE STARTED ON FIRE, UNABLE TO RESTART BLEW RIGHT SIDE CO2 BANK - [SDR FXGA201703091705](https://openairdocs.org/sdr/FXGA201703091705), Mar 9, 2017: FITTING. CRACKED. 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 - [SDR FXGA201702081703](https://openairdocs.org/sdr/FXGA201702081703), Feb 17, 2017: SKIN. CORRODED. 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 - [SDR FXGA201610141636](https://openairdocs.org/sdr/FXGA201610141636), Oct 14, 2016: FRAME. CRACKED. 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 - [SDR FXGA201609151628](https://openairdocs.org/sdr/FXGA201609151628), Sep 12, 2016: SKIN. CORRODED. 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 CONTAINE - [SDR FXGA201609151627](https://openairdocs.org/sdr/FXGA201609151627), Sep 9, 2016: SKIN. CORRODED. 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), Jun 23, 2016: SKIN. WORN. 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. - [SDR FXGA201606231607](https://openairdocs.org/sdr/FXGA201606231607), Jun 23, 2016: STRINGER. CRACKED. 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 - [SDR FXGA201606160001](https://openairdocs.org/sdr/FXGA201606160001), Jun 16, 2016: STRINGER. CRACKED. 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 S - [SDR FXGA201508141509](https://openairdocs.org/sdr/FXGA201508141509), Aug 14, 2015: CAP. CRACKED. 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 891 - [SDR FXGA201508071533](https://openairdocs.org/sdr/FXGA201508071533), Aug 7, 2015: SKIN. CORRODED. 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), Aug 7, 2015: SKIN. CORRODED. 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), Aug 6, 2015: CAP. CRACKED. 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 891 - [SDR FXGA201508061505](https://openairdocs.org/sdr/FXGA201508061505), Aug 6, 2015: CAP. CRACKED. WING STRINGER CAP 18, CRACKED AT STATION 238L. REMOVED STRINGER CAP FROM STATION 232L TO 250L. MANUFACTURE & INSTALL STRINGER CAP & SPLICES IAW REPAIR SKETCH 89 - [SDR FXGA201508061506](https://openairdocs.org/sdr/FXGA201508061506), Aug 6, 2015: CAP. CRACKED. 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 - [SDR FXGA201508061508](https://openairdocs.org/sdr/FXGA201508061508), Aug 6, 2015: CAP. CRACKED. 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 SKE - [SDR FXGA201508061531](https://openairdocs.org/sdr/FXGA201508061531), Aug 6, 2015: SKIN. CORRODED. 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), Aug 5, 2015: REPAIR. CRACKED. 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), Jul 28, 2015: SKIN. CORRODED. 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 - [SDR FXGA201507141528](https://openairdocs.org/sdr/FXGA201507141528), Jul 14, 2015: WEB. CRACKED. 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), Jun 25, 2015: BEARING. GALLED. 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 STO - [SDR FXGA201506091522](https://openairdocs.org/sdr/FXGA201506091522), Jun 9, 2015: DOUBLER. CRACKED. 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 All 120: https://openairdocs.org/model/douglas-c-118a/reports.md --- 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.