Douglas DC-8F-54

Service difficulty reports · 194

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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 = 'DC8F54'
  ORDER BY difficulty_date DESC"

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SDR 96ZZZM1112Skin · corrosionDURING D-CHECK INSPECTION, LEFT WING UPPER SKIN CORROSION WAS FOUND IN VARIOUS PLACES BETWEEN WING STATION 554 AND 659. REMOVED ALL CORROSION DAMAGE AND BLENDED THE AREA OUT TO A 63 MICRO INCH FINISH. INSTALLED 35 INCH BY 63.5 INCH .100 7075-T6 DOUBLER IAW ENov 24, 1995 · N54FA · Doug DC8F54 · Wing, Plate/SkinSDR 96ZZZM1111Skin · corrosionDURING D-CHECK INSPECTION, RIGHT WING LOWER SKIN OF INBOARD AILERON HAD CORROSION AT OUTBOARD END OF AILERON SKIN. CUT AND REMOVED CORRODED SKIN PANEL AND INSTALLED NEW IDENTICAL REPLACEMENT PANEL OF .050 2024-T3 MATERIAL WITH A .063 2024-T3 SPLICE PLATE IAW Nov 24, 1995 · N54FA · Doug DC8F54 · AileronsSDR 96ZZZM1110Skin · corrosionDURING D-CHECK INSPECTION, RIGHT WING LOWER SKIN OF OUTBOARD AILERON HAD CORROSION AT LOWER OUTBOARD SKIN PANEL. CUT AND REMOVED CORRODED SKIN PANEL AND INSTALLED NEW IDENTICAL REPLACEMENT PANEL OF .050 2024-T3 MATERIAL IAW EO 9507251. 8110-3 ISSUED BY DER SNov 24, 1995 · N54FA · Doug DC8F54 · AileronsSDR 96ZZZM1109Plating · corrosionDURING D-CHECK INSPECTION, FOUND CORROSION ON THE UPPER PLATING OF THE RIGHT WING UPPER SURFACE AT STATION XRS 600. CUT AND REMOVED CORRODED PLATING AND INSTALLED A 2 INCH BY 80 INCH .100 7075-T3 FILLER WITH 47 BY 84 INCH .100 7075-T6 DOUBLER IAW EO 9510181. Nov 24, 1995 · N54FA · Doug DC8F54 · Wing, Plate/SkinSDR 96ZZZM1108Skin · corrosionDURING D-CHECK INSPECTION, RT WING AT THE OUTBOARD END OF THE UPPER AND LOWER SKIN OF THE OUTBOARD FLAP CORROSION DAMAGE WAS FOUND. CUT AND REMOVED THE AREA OF CORRODED SKIN AND INSTALLED A .050 2924-T3 MATERIAL DOUBLER WITH A .063 2024-T3 SPLICE PLATE IAW EONov 24, 1995 · N54FA · Doug DC8F54 · Trailing Edge FlapsSDR 96ZZZM1107Frame · corrodedDURING D-CHECK INSPECTION, FUSELAGE FRAME AT FS 500 IN THE CABIN BETWEEN LONGERONS 9 AND 10 RIGHT FOUND CRACK. CUT OUT THE DAMAGED MATERIAL. INSTALLED A 2.25 FILLER FROM AN IDENTICAL FRAME SECTION AND INSTALLED TWO 11.0 INCH .050 AISI 301 1/2H REPAIR DOUBLERNov 24, 1995 · N54FA · Doug DC8F54 · Fuselage Main, FrameSDR 96ZZZM1106Frame · corrosionDURING D-CHECK INSPECTION, FUSELAGE FRAME AT FUSELAGE STATION 540, 560 AND 580 WERE FOUND WITH CORROSION DAMAGE ALONG THE LOWER SEVERAL INCHES WHERE THEY JOIN THE FLOOR ATTACH FITTING. CUT EACH OF THE 3 FRAMES AT A LOCATION 19 INCHES ABOVE THE FLOOR LEVEL ANDNov 24, 1995 · N54FA · Doug DC8F54 · Fuselage Main, FrameSDR 96ZZZM1105Skin · corrosionDURING D-CHECK INSPECTION, FOUND CORROSION DAMAGE ON THE LOWER EDGE OF THE FUSELAGE SKIN PANEL JUST FORWARD OF LONGERON 24 CLEVIS AND RUNNING FORWARD FOR ABOUT 32 INCHES AT STATION 850. CORROSION WAS CUT OUT AND INSTALLED TWO 40 BY 8.5 INCHES .100 AISI 3011/2Nov 24, 1995 · N54FA · Doug DC8F54 · Fuselage Main, Plate/SkinSDR 96ZZZM1104Skin · corrosionDURING D-CHECK INSPECTION, FOUND CORROSION ON SEVERAL AREAS OF FUSELAGE SKIN FROM FS 1140 TO 1340 FROM L31 LEFT TO L31 RIGHT. REMOVED AND REPLACED LOWER FUSELAGE SKIN IAW SRM 51-21-1. ALSO, TREATED AND PRIMED ALL AREAS IAW SRM 51-1-8. (M)Nov 24, 1995 · N54FA · Doug DC8F54 · Fuselage Main, Plate/SkinSDR 96ZZZM1103Skin · corrosionDURING D-CHECK INSPECTION, CORROSION AND DENTS WERE FOUND BELOW THE AFT PASSENGER DOOR FUSELAGE SKIN. CUT OUT ALL CORROSION AND DENTS ON DAMAGED SKIN. INSTALLED A 36.5 BY 6.5 INCH .090 7075-T6 FILLER WITH A 66 INCH BY 24.5 INCH .100 7075-T6 QQ-A-250/13 REPAINov 24, 1995 · N54FA · Doug DC8F54 · Fuselage Main, Plate/SkinSDR 96ZZZM1102Skin · corrosionDURING D-CHECK INSPECTION, CORROSION WAS FOUND ON SEVERAL AREAS OF FUSELAGE SKIN FROM FS 610 TO 670 AND FROM L31 RT TO L31 LT. REMOVED AND REPLACED LOWER FUSELAGE SKIN IAW SRM 51-1-21. ALSO, TREATED AND PRIMED ALL AREAS IAW SRM 51-1-8. (M)Nov 24, 1995 · N54FA · Doug DC8F54 · Fuselage Main, Plate/SkinSDR 96ZZZM1101Skin · corrosionDURING D-CHECK INSPECTION, CORROSION WAS FOUND ON THE UPPER AND LOWER SKIN CENTER PANELS OF THE LEFT ELEVATOR FROM STATION XE 133 TO STATION XE 246. REMOVED THE DAMAGED SKIN PANELS FROM THE ELEVATOR AND INSTALLED A NEW IDENTICAL SKINS PANEL OF .040 2024-T3 IANov 24, 1995 · N54FA · Doug DC8F54 · Elevator, Plate/SkinSDR 96ZZZM1100Skin · corrosionDURING D-CHECK INSPECTION, CORROSION WAS FOUND ON THE UPPER AND LOWER INBOARD SKIN PANELS OF THE LEFT ELEVATOR FROM STATION XE 32 TO STATION XE 133. REMOVED EACH DAMAGED SKIN PANEL FROM THE ELEVATOR AND INSTALLED A NEW IDENTICAL SKIN PANEL OF .040 2024-T3 IAWNov 24, 1995 · N54FA · Doug DC8F54 · Elevator, Plate/SkinSDR 96ZZZM1099Skin · corrosionDURING D-CHECK INSPECTION, CORROSION WAS FOUND ON SEVERAL AREAS OF FUSELAGE SKIN FROM FS 430 TO 610 AND FROM LONGERON 31 RIGHT TO LONGERON 31 LEFT. REMOVED AND REPLACED LOWER FUSELAGE SKIN FROM FS 430 TO 610 AND FROM L31 RIGHT TO L31 LEFT IAW SRM 51-1-21. ALNov 24, 1995 · N54FA · Doug DC8F54 · Fuselage Main, Plate/SkinSDR 96ZZZM1098Floor Beam · corrosionDURING D-CHECK INSPECTION, CORROSION FOUND ON THE WEB OF THE FLOOR BEAM AT FS 920 UNDER OUTBOARD TRACK. DAMAGED AREA WAS CUT OUT AND INSTALLED 14 BY 7 INCHES .063 301 1/2H MIL-S-5059 DOUBLER WITH A 2 INCH .188 7075-T6 FILLER IAW EO 9508221, 8110-3 ISSUED BY DNov 24, 1995 · N54FA · Doug DC8F54 · Fuselage Main, Floor BeamSDR BUFA9526Hyd Pump · inoperativeDSD-MIA - LOST HYD FLUID DOWN TO AUX SYS IN CRUISE. DECLARED AN EMERGENCY INTO MIA. SERVICED AND OPS GOOD ON GROUND IAW MM 29-01 PG 601. R/R SPOILER PUMP ASSY SERV SYS, OPS CK NORMAL, LEAK CK GOOD IAW MM 27-34-6. R/R NR 3 EDHP CASE DRAIN FILTER ELEMENT IAWNov 16, 1995 · N925BV · Doug DC8F54 · Hydraulic Pump (Electric/Engine), MainSDR 96ZZZM11Hyd Pump · inoperativeDSD-MIA - LOST HYD FLUID DOWN TO AUX SYS IN CRUISE. DECLARED AN EMERGENCY INTO MIA. SERVICED AND OPS GOOD ON GROUND IAW MM 29-01 PG 601. R/R SPOILER PUMP ASSY SERV SYS, OPS CK NORMAL, LEAK CK GOOD IAW MM 27-34-6. R/R NR 3 EDHP CASE DRAIN FILTER ELEMENT IAWNov 16, 1995 · N925BV · Doug DC8F54 · Hydraulic Pump (Electric/Engine), MainSDR CKSA95139Link Assy · failedKCVG - FLT 68278 - UPON GEAR RETRACTION DURING CLIMB, NOSE GEAR DOOR DID NOT FULLY CLOSE. THIS CAUSED A VIBRATION IN NOSE GEAR DOOR WELL. FLEW ACFT AT 230KIAS/M.65. (UPLATCH FAIL CHECK SPEED). WITH GEAR DOWN, NO VIBRATION NOTED. ALL OTHER GEAR INDICATIONSOct 26, 1995 · N806CK · Doug DC8F54 · Landing Gear Door Retract SectionSDR 95ZZZM603Seat Track · corrodedOSC - NR 5 SEAT TRACK CORRODED AT STATION 1269.5 TO STATION 1380. REPLACED NR 5 SEAT TRACK FROM STATION 1269.5 TO STATION 1380 IAW DC-8 SRM 53-2-3 AND FUSELAGE CENTER SECTION FLOOR PLANK. REPAIR IAW COTNEY DESIGNATION NR SO-782, SKETCH AIA/E/2112. (M)Oct 15, 1995 · N802CK · Doug DC8F54 · Fuselage, Seat/Cargo Attach FittingsSDR 95ZZZM657Arm Assy · shearedFLT NR 517 - KPDX-KPIA - ON GEAR RETRACTION OUT OF KPDX, GEAR UNSAFE LIGHT AND RT ALTERNATE GEAR WARNING LIGHT CAME ON. ACCOMPLISHED QRH AND RETURNED TO KPDX. FOUND BOGIE UNLOCK SWIVEL ARM SHEARED. S/D - MAINTENANCE REMOVED AND REPLACED THE BOGIE PIVOT ARM Oct 13, 1995 · N992CF · Doug DC8F54 · Landing Gear Retraction/Extension SystemSDR 95ZZZM604Skin · corrodedOSC - LEFT TOP SURFACE OF CENTER WING TANK CORROSION AT PANEL NR 516. INSTALLED REPAIR ACCORDING TO COTNEY DESIGNATION NR SO-782, SKETCH AIA/E/2107 AS IT REQUIRED AND IAW DC-8 SRM 51-1-20B AND 51-1-12. (M)Oct 13, 1995 · N802CK · Doug DC8F54 · Wing, Plate/SkinSDR 95ZZZM602Press Deck · corrodedOSC - SEVERAL AREAS OF CORROSION STATION 159.5 TO STATION 2480 COCKPIT PRESSURE DECK JUST BELOW LONG 21R. INSTALLED REPAIR AS IT REQUIRED ACCORDING TO COTNEY DESIGNATION NR SO-782, SKETCH AIA/E/2109 AND IAW DC-8 SRM 53-2-0, 51-1-2, 51-1-11. (ALSO BMS FORM 60Oct 13, 1995 · N802CK · Doug DC8F54 · Fuselage Miscellaneous StructureSDR 95ZZZM605Rib · crackedOSC - FLAP WELL SUPPORT RIB CRACKED JUST OUTBOARD OF STATION 219 FLAP ACTUATOR. INSTALLED REPAIR ACCORDING TO SKETCH AIA/E/2108 AS IT REQUIRED.Oct 11, 1995 · N802CK · Doug DC8F54 · Wing, Rib/BulkheadSDR 95ZZZM607Blkhd Angle · corrodedOSC - FOUND CORROSION C-PIT STATION 980 TO 36R AND 34R, BODY TO BULKHEAD ANGLE. CUT OUT DAMAGED AREA, INSTALLED REPAIR AS IT REQUIRED ACCORDING TO SKETCH AIA/E/2104 AND DOUGLAS SRMS 51-1-8 AND 51-1-20D. ENGINEERING DESIGNATION NR SO-782, SKETCH AIA/E/2104.Oct 10, 1995 · N802CK · Doug DC8F54 · Fuselage Main, BulkheadSDR 95ZZZM502Skin · crackedDURING C-CHECK, MAINTENANCE FOUND A 1.25 INCH CRACK ON OUTER SKIN OF RIGHT AFT SERVICE DOOR AT FUSELAGE TOP AFT CORNER. CUT OUT CRACKED OUTER SKIN, INSTALLED A REPAIR DOUBLER AND TRIPLER IAW DOUGLAS DRAWING NR SRO 8530021. (M)Aug 25, 1995 · N427FB · Doug DC8F54 · Fuselage Main, Plate/SkinSDR 95ZZZM501Skin · corrosionDURING C-CHECK, MAINTENANCE FOUND CORROSION ON THE FUSELAGE EXTERIOR SKIN RIGHT SIDE AT STATION 980, AROUND THE CABIN WINDOW IN THE LINE OF WINDOW ATTACHMENT FASTENERS. REMOVED ALL CORROSION AND BLENDED TO A 63 MICRO-INCH FINISH AND INSTALLED A .160 7075-T6 RAug 25, 1995 · N427FB · Doug DC8F54 · Fuselage Main, Plate/SkinSDR 95ZZZM405Skin · crackedDURING B-CHECK, MAINTENANCE FOUND A .5 INCH CRACK ON LEFT WING UPPER SURFACE SKIN AT STATION 90.0. CUT OUT CRACK SECTION, INSTALLED 1.5 INCH FILLER AND 10 INCH BY 8 INCH EXTERNAL DOUBLER IAW SRM 57-2-1, FIG 20.Aug 10, 1995 · N57FB · Doug DC8F54 · Wing, Plate/SkinSDR 95ZZZM404Skin · crackedDURING B-CHECK, MAINTENANCE FOUND A 1.5 INCH CRACK ON RIGHT WING UPPER SURFACE SKIN AT STATION 75.312. CUT OUT CRACK SECTION, INSTALLED TWO .75 INCH FILLER AND 2 FOOT BY 1 FOOT EXTERNAL DOUBLER IAW SRM 57-2-1, FIG 39.Aug 10, 1995 · N57FB · Doug DC8F54 · Wing, Plate/SkinSDR 95ZZZM291Fire Wire · looseUPON ROTATION NR 1 ENGINE FIRE WARNING WENT OFF. COMPLETED APPROPRIATE CHECKLIST. DUE TO BEING ON 3 ENGINE FERRY, WAS NOW ON 2 ENGINES. DECLARED EMERGENCY, RETURNED TO HUF. TROUBLESHOT, FOUND NO FIRE BUT INDICATION ONLY. FOUND WIRE PULLED FROM AFT OUTBOARDJul 18, 1995 · N802CK · Doug DC8F54 · Fire DetectionSDR CKSA95064Floor Beam · corrosionKOSC - DURING C-CHECK INSPECTION, FOUND CORROSION ON FLOOR BEAM WEB AT LIGHTING HOLE AT RIGHT END STATION 440 'A' PIT. REMOVED CORROSION IAW SRM 51-1-6 FABRICATED AND INSTALLED PART IAW ENGINEERING SKA95118-1. COMPLIED WITH AIA EA95-176. (M)Jul 11, 1995 · N806CK · Doug DC8F54 · Fuselage Main, Floor BeamSDR CKSA95063Angle · corrosionKOSC - DURING C-CHECK INSPECTION, FOUND INBOARD LOWER AFT ANGLE IN WHEELWELL DOGHOUSE AREA SURFACE CORRODED. REMOVED ANGLE, REMOVED CORROSION IN CENTER WING UPPER SKIN PANEL. CORROSION REMOVAL OUT OF SRM LIMITS. REPAIRED SKIN PER ENGINEERING SKETCH SKA95118Jul 11, 1995 · N806CK · Doug DC8F54 · Fuselage Miscellaneous StructureSDR 95ZZZX3379Engine · fireKDAY/KBWI - FLT 114 - DURING DESCENT INTO KBWI, SHUT DOWN NR 1 ENGINE FOR FIRE WARNING. MAINTENANCE INSPECTED NR 1 ENGINE AND FOUND VARIOUS DAMAGE FROM POSSIBLE FIRE. THE AIRCRAFT WAS FERRIED TO GTC FOR REPAIRS AND ENGINE CHANGE. CURRENTLY UNDER INVESTIGATIJun 14, 1995 · N992CF · Doug DC8F54 · Engine (Turbine/Turboprop)SDR 95ZZZM94Sensor · detachedON DEPARTURE MIAMI EXPERIENCED FIRE WARNING ON NR 2 ENGINE. SHUTDOWN ENGINE AND RETURNED AND LANDED WITHOUT INCIDENT. INSPECTION REVEALED DETACHED FIRE WARNING SENSOR ON AFT COWL. PERFORMED OVERWEIGHT LANDING INSPECTION AND REPLACED FIRE WARNING SENSOR. AIRJun 6, 1995 · N57FB · Doug DC8F54 · Fire DetectionSDR 95ZZZZ266Engine · failedMIA - IN CLIMB, THE NR 1 ENGINE EGT INCREASED AND EXPERIENCED ENGINE VIBRATION. SHUTDOWN NR 1 ENGINE AND RETURNED AND LANDED AT MIA WITHOUT INCIDENT. INSPECTION REVEALED METAL IN THE TAIL PIPE. REPLACED NR 1 ENGINE.May 23, 1995 · N427FB · Doug DC8F54 · Engine (Turbine/Turboprop)SDR 95ZZZZ234Rod Assy · unlockedAFTER TAKEOFF MIAMI FELT SEVERE VIBRATION. RETURNED TO MIAMI AND LANDED WITHOUT INCIDENT. INSPECTION REVEALED RT NOSE LANDING GEAR DOOR OPEN. CLEANED, LUBED AND RESET RT FWD DOOR ROD AND OPS CHECKED OK. PERFORMED OVERWEIGHT LANDING INSPECTION. RETURNED ACMay 4, 1995 · N426FB · Doug DC8F54 · Landing Gear Door Retract SectionSDR 95ZZZX2311Cap Assy · leakingMIAMI - AFTER TAKEOFF, NOTED FUEL LOSS FROM NR 1 ALT FUEL TANK. RETURNED TO MIAMI. LANDED WITHOUT INCIDENT. INSPECTION REVEALED LEAKING FUEL TANK CAP AT NR 1 ALT TANK. REPLACED FUEL TANK CAP. AIRCRAFT RETURNED TO SERVICE. TOTAL CYCLES 20,256.Apr 29, 1995 · N426FB · Doug DC8F54 · Fuel StorageSDR BUFA9510Uplatch · lack of lubeGEAR UPLATCH CHECK WARNING LIGHT ON. CYCLE GEAR LIGHT OUT. CLEANED AND LUBED MLG UP-LATCH MECHANISM IAW MM 32-6-2, CYCLED GEAR 6 TIMES AND OPS CHECKED IAW MM 32-3-0. RII INSPECTED. OPS CHECK OKAY. (X)Apr 13, 1995 · N925BV · Doug DC8F54 · Landing Gear Retraction/Extension SystemSDR 95ZZZW654Engine · failedFLT 114 - KDAY-KBWI - DURING CRUISE NR 4 ENGINE FAILED. N-1 DROPPED OFF THEN N-2 FROZE. LOUD BANG FROM ENGINE WHEN FAILED. RETURNED TO KDAY. MAINTENANCE INSPECTED NR 4 ENGINE AND FOUND METAL IN TAIL PIPE. AIRCRAFT BEING SET UP TO FERRY FOR ENGINE CHANGE.Apr 11, 1995 · N992CF · Doug DC8F54 · Engine (Turbine/Turboprop)SDR 95ZZZX1945Line · looseMPTO/MPTO - FLT APW 615 - RETURNED TO PANAMA DUE TO LOSS OF OIL, NR 3 ENGINE. FOUND FEED OIL LINE LOOSE, TIGHTENED B-NUT -- OKAY.Apr 9, 1995 · N43UA · Doug DC8F54 · Turbine Engine Oil SystemSDR CKSA95015Hyd Line · leakingYIP/SFO - FLT 63060 - EN ROUTE AT 1315Z, LOST ALL MAIN SYSTEM HYDRAULIC PRESSURE, LOST QUANTITY, BUT STILL IN NORMAL RANGE. DECLARED EMERGENCY WITH ATC AND PROCEEDED TO DESTINATION. REPLACED LEAKING HYDRAULIC LINE, PN R124-01-2, AT LEFT AILERON POWER PACK SEApr 6, 1995 · N803CK · Doug DC8F54 · Hydraulic System, MainSDR 95ZZZX1933Actuator · motor inopMIA - AFTER TAKEOFF, COULD NOT PRESSURIZE AIRCRAFT. RETURNED TO MIAMI AND MADE LANDING WITHOUT INCIDENT. PERFORMED OVERWEIGHT INSPECTION. GROUND INSPECTION REVEALED DEFECTIVE OUTFLOW VALVE ACTUATOR. REPLACED ACTUATOR AND GROUND CHECKED OKAY. RETURNED AIRCMar 27, 1995 · N426FB · Doug DC8F54 · Pressure Regulator/Outflow ValveSDR BUFA9502Line · looseMIA - ON CLIMB, THE HYDRAULIC FLUID LOSS TO STANDPIPE. RETURNED TO MIA, NO EMERGENCY DECLARED, AND HAD UNEVENTFUL LANDING. FOUND LOOSE LINE AT CASE DRAIN. TIGHTENED 'B' NUT, RAN ENGINE AND PERFORMED OPERATION AND LEAK CHECK. CHECK OK PER MM. (W)Feb 5, 1995 · N7046G · Doug DC8F54 · Hydraulic System, MainSDR 95ZZZZ53Clamp · looseFALSE FIRE WARNING NR 3 ENGINE DURING CLIMB WARNING CEASED WHEN ENGINE BLEED AIR TURNED OFF ALL OTHER PARAMETERS NORMAL. RETORQUED CLAMPS ON REGULATOR VALVE DUCTING. CHECKS GOOD ON ENGINE RUN UP. FIRE WARNING SYSTEM INTEGRITY OK.Jan 18, 1995 · N802CK · Doug DC8F54 · Pneumatic Distribution SystemSDR 95ZZZZ35Voltage Reg · overheatedFLT 228 - KDAY-KMCO - DURING CRUISE NR 2 GENERATOR UNPARALLELED LIGHT CAME ON. FREQS NORMAL, VOLTS ERRATIC. TURNED GENERATOR OFF. DISCONNECTED GENERATOR AFTER ELECTRICAL SMOKE FILLED COCKPIT. MAINTENANCE FOUND VOLTAGE REGULATOR BAD. SMOKE CAUSED BY OVERHEJan 10, 1995 · N991CF · Doug DC8F54 · AC Regulator
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