Douglas DC-8-62F

Service difficulty reports · 1,163

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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 = 'DC862F'
  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.

SDR IXXA09SMN006SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING UPPER SKIN CRACKED AT STATION XCW 69.500. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK AND NO CORROSION NOTED. FABRICATED NEW SKIN, FILLER PLUG.Jan 20, 2009 · N799AL · Doug DC862F · Wing, Plate/SkinSDR IXXA09SMN002SSkin · misrepairedDURING ROUTINE C-CHECK INSPECTION, FOUND IMPROPER REPAIR AT RIGHT AFT FUSELAGE SKIN AT LONGERON 28 REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK OR NO CORROSION FOUND. FABRJan 20, 2009 · N799AL · Doug DC862F · Fuselage Main, Plate/SkinSDR IXXA09SMN001SDoor Frame · crackedDURING ROUTINE C CHECK INSPECTION, FOUND "A" CARGO DOOR FORWARD LOWER JAMB CORNER CRACKED. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION. FABRICATED DOUBLERS, FILLER. CLEANED, TREATEJan 16, 2009 · N799AL · Doug DC862F · Fuselage Main, StructureSDR IXXA080039OFan · burned outON TOP OF DESCENT FLIGHT ATTENDANT'S DETECTED SMOKE IN CABIN. AFTER TURNING OFF THE RT RECIRCULATION FAN THE ODOR DISSIPATED. THE CREW LANDED IN PHIK WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND LT RECIRCULATION FAN EMMITTING BURNING ODOR. MAINTEDec 29, 2008 · N71CX · Doug DC862F · Air Distribution FanSDR IXXA080037OElbow · brokenDURING CLIMB FROM KMCC, THE CREW NOTICED A LOSS OF HYDRAULIC QUANTITY TO THE FIVE GALLON LEVEL. THE CREW RETURNED TO KMCC AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE HYDRAULIC SYSTEM AND FOUND THE RIGHT MAIN LANDING GEAR ACTUATING CYLINDER, UPPER Dec 14, 2008 · N799AL · Doug DC862F · Hydraulic System, MainSDR IXXA080034OVideo Monitor · burned outAPPROXIMATELY 15 MINUTES AFTER TAKEOFF FROM KSUU, THE CREW DETECTED AN ELECTRICAL ODOR IN THE CABIN. THE CREW RETURNED TO KSUU AND LANDED WITHOUT INCIDENT. MAINTENANCE VERIFIED ELECTRICAL ODOR WAS COMING FROM THE FORWARD VIDEO MONITOR. THE FORWARD VIDEO MONNov 23, 2008 · N799AL · Doug DC862F · Audio/Video MonitoringSDR IXXA080032OOil System · leakingDURING CRUISE, NR 4 ENGINE OIL PRESSURE WAS FLUCTUATING & OIL PRESSURE LIGHT FLICKERING, OIL QUANTITY READ 0. CREW RAN ABNORMAL OIL PRESSURE CHECKLIST FOLLOWED BY EMERGENCY SHUTDOWN CHECKLIST. WINDMILL OIL PRESSURE 14 PSI. RESTORED FUEL TO FUEL CONTROL EVERNov 5, 2008 · N799AL · Doug DC862F · Turbine Engine Oil SystemSDR IXXA08SMN220SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT SPLICE FITTING CRACKED AT STATION 902.000 LONGERON 1. REMOVED CRACKED SPLICE FITTING. CLEANED, TREATED, AND PRIMED AREA. INSTALLED NEW SPLICE FITTING IAW DC8 SRM 51-1-20D AND SRM 51-3-1 TABLE IOct 28, 2008 · N71CX · Doug DC862F · Fuselage Miscellaneous StructureSDR IXXA08SMN219SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING INBOARD CENTER LEADING EDGE LOWER SKIN CRACKED AT STATION XS 520.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. PERFORMED STOP HOLE. PERFORMED NDT INSPECTION. NO CRACK AND NO CORROSION FOUND. FABRICAOct 28, 2008 · N71CX · Doug DC862F · Wing, Plate/SkinSDR IXXA08SMN218SFrame · damagedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT RIGHT FLANGE FRAME HAS MISDRILLED HOLE AT STATION 1080.000 LONGERON 19-20 RIGHT. BLENDED OUT MISDRILLED AREA. PERFORMED NDT INSPECTION. NO CRACK AND NO CORROSION FOUND. FABRICATED ANGLE DOUBLEOct 28, 2008 · N71CX · Doug DC862F · Fuselage Main, FrameSDR IXXA08SMN217SFrame · damagedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT RIGHT FLANGE FRAME HAS MISDRILLED HOLE AT STATION 1040.000 LONGERON 19-20 RIGHT. BLENDED OUT MISDRILLED AREA. PERFORMED NDT INSPECTION. NO CRACK AND NO CORROSION FOUND. FABRICATED ANGLE DOUBLEOct 28, 2008 · N71CX · Doug DC862F · Fuselage Main, FrameSDR IXXA08SMN216SFrame · damagedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT RIGHT FLANGE FRAME HAS MISDRILLED HOLE AT STATION 420.000 LONGERON 17-18 RIGHT. BLENDED OUT MISDRILLED AREA. PERFORMED NDT INSPECTION. NO CRACK AND NO CORROSION FOUND. FABRICATED ANGLE DOUBLEROct 28, 2008 · N71CX · Doug DC862F · Fuselage Main, FrameSDR IXXA08SMN215SFrame · damagedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT RIGHT FLANGE FRAME HAS MISDRILLED HOLE AT STATION 420.000 LONGERON 19 RIGHT. BLENDED OUT MISDRILLED AREA. PERFORMED NDT INSPECTION. NO CRACK AND NO CORROSION FOUND. FABRICATED ANGLE DOUBLER. Oct 28, 2008 · N71CX · Doug DC862F · Fuselage Main, FrameSDR IXXA08SMN214SFrame · damagedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT RIGHT FLANGE FRAME HAS MISDRILLED HOLE AT STATION 280.000 LONGERON 19-20 RIGHT. BLENDED OUT MISDRILLED AREA. PERFORMED NDT INSPECTION. NO CRACK AND NO CORROSION FOUND. FABRICATED ANGLE DOUBLEROct 28, 2008 · N71CX · Doug DC862F · Fuselage Main, FrameSDR IXXA08SMN213SFrame · damagedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT RIGHT FLANGE FRAME HAS MISDRILLED HOLE AT STATION 1320.000 LONGERON 16 RIGHT. BLENDED OUT MISDRILLED AREA. PERFORMED NDT INSPECTION. NO CRACK AND NO CORROSION FOUND. FABRICATED ANGLE DOUBLER. Oct 28, 2008 · N71CX · Doug DC862F · Fuselage Main, FrameSDR IXXA08SMN212SFrame · damagedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT RIGHT FLANGE FRAME SHOWS MISDRILLED HOLE AT STATION 1400.000 LONGERON 16 RIGHT. BLENDED OUT MISDRILLED AREA. PERFORMED NDT INSPECTION. NO CRACK AND NO CORROSION FOUND. FABRICATED INTERNAL DOUBOct 28, 2008 · N71CX · Doug DC862F · Fuselage Main, FrameSDR IXXA08SMN211SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STATION 834.000 LONGERON 22 RIGHT. REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, SRM 51-3-1, AND DC8 SRM 51-1-8B.Oct 28, 2008 · N71CX · Doug DC862F · Fuselage Miscellaneous StructureSDR IXXA08SMN210SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND FORWARD CARGO COMPARTMENT SPLICE FITTING CRACKED AT STATION 600.000-620.000 LONGERON 31 LEFT. REMOVED CRACKED SPLICE FITTING. CLEANED, TREATED, AND PRIMED AREA. INSTALLED NEW SPLICE FITTING IAW DC8 SRM 51-1-20D, SRM Oct 28, 2008 · N71CX · Doug DC862F · Fuselage Miscellaneous StructureSDR IXXA08SMN209SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND FORWARD CARGO COMPARTMENT SPLICE FITTING CRACKED AT STATION 600.000 - 620.000 LONGERON 31 RIGHT. REMOVED CRACKED FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, AND SRM 51-3-1.Oct 28, 2008 · N71CX · Doug DC862F · Fuselage Miscellaneous StructureSDR IXXA08SMN208SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT MAIN LANDING GEAR WHEEL WELL FITTING CRACKED AT STATION 940.000 LONGERON 24 RIGHT. REMOVED DAMAGED FITTING FRAME. FABRICATED SPLICES, DOUBLER, AND FILLERS. PERFORMED HEAT TREATMENT. INSTALL NEW FITTING AND REPOct 28, 2008 · N71CX · Doug DC862F · Main Landing GearSDR IXXA08SMN207SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND EMPENNAGE RUDDER RIGHT SKIN CRACKED AT STATION ZR 253.00. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND BONDED DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED, PRIMED AREA AND REPAIR PART. PERFORMED BAOct 28, 2008 · N71CX · Doug DC862F · Rudder, Plate/SkinSDR IXXA08SMN206SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND AFT ACCESSORY COMPARTMENT FITTING CRACKED AT STATION 1530.000 LONGERON 36. REMOVED DAMAGED FITTING. CLEANED, TREATED, AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-21, DC8 SRM 51-1-8B, SRM 51-1-20D, AND SRMOct 25, 2008 · N71CX · Doug DC862F · Fuselage Miscellaneous StructureSDR IXXA08SMN205SFloorbeam · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LT FUSELAGE CENTER SECTION FLOORBEAM LOWER HORIZONTAL FLANGES AND FLOOR PRESS PANEL CORRODED AT STATION 902.000 LBL 51. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED EXISTING DAMAGED SPLICE ANGLE. REMOVED DAMAGED Oct 25, 2008 · N71CX · Doug DC862F · Fuselage Main, Floor BeamSDR IXXA08SMN204SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT INBOARD FLAP LEADING EDGE CORRODED AT STATION XW 2.000-91.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK AOct 25, 2008 · N71CX · Doug DC862F · Trailing Edge FlapsSDR IXXA08SMN203SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING NUMBER 4 STUB WING INNER FITTING CRACKED AT STATION XS 526.000. REMOVED CRACKED FITTING. FABRICATED NEW FITTING. CLEANED, TREATED, AND PRIMED AREA AND FITTING. INSTALLED FITTING IAW DC8 SRM 51-1-20D, ATI Oct 25, 2008 · N71CX · Doug DC862F · Wing Miscellaneous StructureSDR IXXA08SMN202SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING UPPER SKIN CRACKED AT STATION XRS 74.869 STRINGER 9. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN, AND FILLER PLUG. PERFORMED NDT INSPECTION. NO CRACK AND NO COct 24, 2008 · N71CX · Doug DC862F · Wing, Plate/SkinSDR IXXA08SMN201SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT OUTBOARD AILERON LOWER HAS IMPROPER REPAIR AT STATION XW 698.000. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, AND DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED, PRIMED AREA AND REPAIR PART. POct 24, 2008 · N71CX · Doug DC862F · AileronsSDR IXXA08SMN200SSpar Cap · crackedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING UPPER REAR SPAR CAP VERTICAL FLANGE CRACKED AT STATION XRS 554.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. PERFORMED STOP HOLE. PERFORMED NDT INSPECTION. NO CRACK AND NO CORROSION FOUND AFTER DRILOct 24, 2008 · N71CX · Doug DC862F · Wing SparSDR IXXA08SMN199SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT ELEVATOR TRAILING EDGE LOWER SKIN CORRODED AT STATION XE 147.188A - XE 156.168. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED SKIN. FABRICATED NEW SKIN, FINGER DOUBLER. BONDED PARTS AS NEEDED WITH Oct 24, 2008 · N71CX · Doug DC862F · Elevator, Plate/SkinSDR IXXA08SMN198SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER TRAILING EDGE LOWER SKIN CORRODED AT STATION XE 52.825-75.672. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED SKIN. FABRICATED NEW SKIN, STIFFENER. CLEANED, TREATED, PRIMED AREOct 24, 2008 · N71CX · Doug DC862F · Horizontal Stabilizer, Plate/SkinSDR IXXA08SMN197SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER TRAILING EDGE LOWER SKIN CORRODED AT STA XE 29.812 - 52.825. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED SKIN. FABRICATED NEW SKIN, AND STIFFENER. CLEANED, TREATED, PRIMED AOct 24, 2008 · N71CX · Doug DC862F · Horizontal Stabilizer, Plate/SkinSDR IXXA08SMN196SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER TRAILING EDGE UPPER SKIN CORRODED AT STATION XE 29.812. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED SKIN. CLEANED, TREATED, PRIMED AREA. INSTALLED NEW SKIN IAW SRM 55-3-1 FIGOct 24, 2008 · N71CX · Doug DC862F · Horizontal Stabilizer, Plate/SkinSDR IXXA08SMN195SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT ELEVATOR TRAILING EDGE LOWER SKIN CORRODED AT STATION XE 74.469. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, FINGER DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANOct 24, 2008 · N71CX · Doug DC862F · Elevator, Plate/SkinSDR IXXA08SMN194SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT ELEVATOR TRAILING EDGE LOWER SKIN CORRODED AT STATION XE 89.719. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED EXISTING REPAIR. FABRICATED NEW SKIN, FINGER DOUBLER. BONDED PARTS AS NEEDED. CLEANEDOct 24, 2008 · N71CX · Doug DC862F · Elevator, Plate/SkinSDR IXXA08SMN193SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT ELEVATOR TRAILING EDGE LOWER SKIN CORRODED AT STATION XE 55.062. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, FINGER DOUBLER. BONDED PARTS AS NEEDED. CLEANED, TREATEDOct 24, 2008 · N71CX · Doug DC862F · Elevator, Plate/SkinSDR IXXA08SMN192SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER TRAILING EDGE LOWER SKIN CORRODED AT STATION XE 77.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, AND STIFFENER. CLEANED, TREATED, PRIMED AREAOct 24, 2008 · N71CX · Doug DC862F · Horizontal Stabilizer, Plate/SkinSDR IXXA08SMN191SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND DOUBLER BELOW MAIN CARGO DOOR OPENING HAS IMPROPER REPAIR AT STATION FS 400 LONGERON 25 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. Oct 21, 2008 · N71CX · Doug DC862F · Fuselage Main, Plate/SkinSDR IXXA08SMN190SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, FOUND LT WING INBOARD OUTER L/E UPPER EXTERNAL SKIN CORRODED AT STATION XFS 560.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. Oct 21, 2008 · N71CX · Doug DC862F · Wing, Plate/SkinSDR IXXA08SMN189SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LT WING LOWER CENTER OUTER LEADING EDGE SKIN CORRODED AT STATION XFS 280.250.REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NOOct 21, 2008 · N71CX · Doug DC862F · Wing, Plate/SkinSDR IXXA08SMN188SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING OUTBOARD OUTER LEADING EDGE UPPER EXTERNAL SKIN CORRODED AT STATION XW 762.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK AOct 21, 2008 · N71CX · Doug DC862F · Wing, Plate/SkinSDR IXXA08SMN187SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND FUSELAGE EXTERNAL SKIN CORRODED AT STATION 1530.000 LONGERON 35 RIGHT. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN SEGMENT, SPLICE, INTERNAL DOUBLERS, Oct 21, 2008 · N71CX · Doug DC862F · Fuselage Main, Plate/SkinSDR IXX2008F00093Line · looseDURING TAKEOFF ROLL, NR (1) ENGINE WOULD NOT ACCELERATE PAST 78 PERCENT. NR 2 WITH CORRESPONDING LOW N1, FUEL FLOW AND EGT. THE CREW REJECTED TAKEOFF AND RETURNED TO BLOCKS. MAINT INSPECTED AND FOUND LOOSE PT2 LINE ON PRBC VALVE. MAINT RECONNECTED LINE. OPERSep 7, 2008 · N71CX · Doug DC862F · Engine (Turbine/Turboprop)SDR IXX2008F00007Engine · oil consumptionDURING CRUISE, THE CREW SHUTDOWN NR 3 ENGINE DUE TO OIL QUANTITY DROPPING TO LESS THAN ONE GALLON, OIL PRESSURE GAUGE FLUCTUATING, OIL TEMP WAS ABOVE 115C, OIL PRESSURE LIGHT INTERMITTENT, THE CREW LANDED WITHOUT FURTHER INCIDENT. AC WAS AUTHORIZED FERRY FLIGJul 6, 2008 · N71CX · Doug DC862F · Engine (Turbine/Turboprop)SDR IXXA080025OCompass · defectiveDURING CRUISE FROM KBWI, THE CREW PERFORMED COMPASS RATING CHECK, BOTH COMPASS SYSTEM HAD EXCESSIVE DRIFT (20 DEGREE IN 30 MIN). THE CREW LANDED IN CYYR WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REMOVED AND REPLACED FOG GYRO COMPASS SYSTEM. OPERATIONAL CHMay 29, 2008 · N71CX · Doug DC862F · Magnetic CompassSDR IXXA080017OPressure Switch · leakingDURING CRUISE FROM HIK, THE CREW SHUTDOWN NR 1 ENGINE AT 2102Z DUE TO FLUCTUATING OIL PRESSURE AND FLICKERING OIL PRESSURE LIGHT. WIND MILLING OIL PRESSURE FLUCTUATION BETWEEN 18PSI TO 25PSI AT CRUISE ALTITUDE, OIL QUANTITY INDICATED 2.5 GALLONS AND OIL TEMP May 1, 2008 · N799AL · Doug DC862F · Engine Oil Indicating SystemSDR IXXA080010OSpeaker · odorDURING CRUISE FROM PKWA, THE CREW NOTICE A ELECTRICAL ODOR COMING FROM THE RIGHT RECIRC FAN. THE CREW TURNED OFF THE RIGHT RECIRC FAN AND LANDED WITHOUT INCIDENT IN PHIK. MAINTENANCE INSPECTED AND FOUND THAT THE ELECTRICAL ODOR WAS COMING FROM THE FIRST OFFMar 6, 2008 · N71CX · Doug DC862F · Communications SystemSDR IXXA08SMN033SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND CORROSION AND DENTS ON LEFT ELEVATOR LOWER SKIN AT STATION XE 28.800 TO STATION XE 127.900. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED. FABRICATED NEW SKIJan 22, 2008 · N41CX · Doug DC862F · Elevator, Plate/SkinSDR IXXA08SMN032SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT ELEVATOR CORRODED ON LOWER SKIN AT STATION XE 104.310 TO STATION XE 108.843. REMOVED CORROSION FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN, INTJan 22, 2008 · N41CX · Doug DC862F · Elevator, Plate/SkinSDR IXXA08SMN031SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND CORROSION ON LEFT WING ON LEADING EDGE OUTER UPPER PART AT STATION XFS 822.500. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGE AREA. PERFORMED NDT INSPECTION. Jan 22, 2008 · N41CX · Doug DC862F · Wing, Plate/SkinSDR IXXA08SMN030SBeam · crackedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO LOWER FLANGE BEAM CRACKED AND CORROSION AT STATION 902.000 LEFT BOTTOM LINE 51". REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT IJan 22, 2008 · N41CX · Doug DC862F · Fuselage Main, Structure
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