Douglas DC-8-62F

Service difficulty reports · 1,163

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 = '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 IXXA10SMN065SAngle · corrodedDURING ROUTINE C-CHECK INSP, FOUND EMPENNAGE VERTICAL STABILIZER TO FUSELAGE LT JOINT ANGLE CORRODED AT STA 1640.382. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED ANGLE, FILLER AND TAPERED SHIMS. PERFORMED HEAT TREATMENT. CLEANED,Jun 17, 2010 · N71CX · Doug DC862F · Fuselage Miscellaneous StructureSDR IXXA10SMN063SSkin · corrodedDURING ROUTINE C-CHECK INSP, FOUND RT WING INBD L/E OUTER SECTION UPPER PART CORRODED AT STA XW 257.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED NEW SKIN, REPAIR DOUBLER, AND FILLERS. Jun 17, 2010 · N71CX · Doug DC862F · Wing, Plate/SkinSDR IXXA10SMN062SSkin · corrodedDURING ROUTINE C, CHECK INSP FOUND EXTERNAL FUSELAGE LOWER SKIN PANEL BUTT SPLICE CORRODED AT STA 1460.000, LONGERON 11LT. REMOVED FASTENERS AS NEED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DIJun 17, 2010 · N71CX · Doug DC862F · Fuselage Main, Plate/SkinSDR IXXA10SMN061SSkin · corrodedDURING ROUTINE C-CHECK INSP FOUND LT WING UPPER PANEL EXTERNAL SKIN CORRODED AT STA XRS 204.000 STR 14. REMOVED CORROSION. FOUND OUT OF LIMITS. PERFORMED NDT INSP. NO DISCREPANCY FOUND. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. FABRICATED NEW SKIN AND Jun 16, 2010 · N71CX · Doug DC862F · Wing, Plate/SkinSDR IXXA10SMN064SFitting · corrodedDURING ROUTINE C-CHECK, INSP FOUND LT MLG WHEEL WELL FRAME FITTING CORRODED AT FS 879.000 LONGERON 24. REMOVED CORRODED FITTING. FABRICATED NEW FITTING, SPLICES AND DOUBLERS. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FITTING AND REPAIR PARJun 16, 2010 · N71CX · Doug DC862F · Fuselage Main, Attach FittingsSDR IXXA10SMN060SHook · crackedDURING ROUTINE C-CHECK INSP, FOUND AFT PAX DOOR HOLD OPEN HOOKS CRACKED AT STA FS 1440.000 LONGERON 14 LT LONGERON 15 LT. REMOVED FASTENERS AS NEED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED REPAIR DOUBLER, FILLER, FINGER DOUBLERS. PERFORMED NDT INJun 15, 2010 · N71CX · Doug DC862F · Passenger/Crew DoorsSDR IXXA10SMN059SSkin · misrepairedDURING ROUTINE C-CHECK INSP, FOUND IMPROPER REPAIR ON THE VERTICAL STABILIZER L/E AT STA ZFS 292. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN AND REPAIR SPLICE. PERFORMED NDT INSP. NO DIJun 10, 2010 · N71CX · Doug DC862F · Vertical Stabilizer, Plate/SkinSDR IXXA100036OController · defectiveDURING CRUISE, CABIN RATE OF CLIMB RAISED QUICKLY TO 10,000 FT, FLIGHT ENGINEER RAN PNEUMATIC TO HIGH AND OPERATED THE PRESSURE CONTROL VALVE. THE CREW WAS PERMITTED PARTIAL CONTROL OF CABIN PRESSURE UNTIL ACFT DESCENDED BLOW FL200. THEY RETURNED TO DEPARTURE Jun 4, 2010 · N71CX · Doug DC862F · Cabin Pressure ControllerSDR IXXA100034OFan · failedDURING CRUISE THE LT RECIRCULATION FAN STOPPED WORKING AFTER 40 MIN AND EMITTED A SMOKE ODOR. THE CREW PULLED CURCUIT BRAKERS AND LANDED IN PHIK WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT RECIRCULATION FAN. OPERATIONAL CHECK GOOD IAW MM 21-21-1 ANMay 21, 2010 · N71CX · Doug DC862F · Air Distribution FanSDR IXXA100033OFuel Filter · cloggedAFTER LEVEL OFF, WITH ANTI-ICE OFF NR 3 ENG N1 ROLLED BACK TO 80 PERCENT, N2 89 PERCENT, OIL PRESSURE 50PSI, FUEL FLOW FLUCTATING 2000-2800 AND PPH EPR 1.4-1.6. TURNED ON ANTI-ICE, NO HELP OIL TEMP BEGAN TO RISE FROM 90 TO 120. THE CREW SHUTDOWN NR 3 ENG. THEMay 19, 2010 · N799AL · Doug DC862F · Aircraft Fuel Filter/StrainerSDR IXXA100032OFan · burnedDURING CRUISE, THE LT RECIRCULATION FAN EMITTED A BURNED ELECTRICAL ODOR. THE CREW SHUTOFF LT RECIRCULATION FAN, ODOR WENT AWAY. THEY LANDED IN WITHOUT FURTHER INCIDENT. MX REPLACED LT RECIRCULATION FAN. OPS CHECK GOOD IAW MM 21-21-1. ACFT WAS RETURNED TO SERVMay 11, 2010 · N71CX · Doug DC862F · Air Distribution FanSDR IXXA100030OPulley · frozenDURING CLIMB OUT, AFTER GEAR RETRACTION GEAR DOOR LIGHT ILLUMINATED. THE CREW CYCLED GEAR AND LIGHT REMAINED ON. THE ALTERNATE LIGHT TESTED GOOD WHEN FWD RED GEAR DOOR LIGHT WAS ON. THEY LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED AND FOUND EXCESSIVE AMOUMay 3, 2010 · N799AL · Doug DC862F · Landing Gear Retraction/Extension SystemSDR IXXA100029SSkin · crackedDURING PREFLIGHT, FOUND VERTICAL STABILIZER L/E CRACKED AT STA ZFS 292 CTR LINE. REPLACED CRACKED L/E WITH INTERIM REPAIR IAW FVCI DWG NR 55-10165-1.May 1, 2010 · N71CX · Doug DC862F · Vertical Stabilizer, Plate/SkinSDR IXXA100024OFan · odorAFTER 10 MINUTES OF RUNNING THE RT RECIRCULATION FAN , THE CREW SENSED AN ELECTRICAL/ OZONE SMELL. THE RT RECIRCULATION FAN WAS TURNED OFF, CIRCUIT BREAKER WAS PULLED AND SMELL WENT AWAY. MX REPLACED THE RT RECIRCULATION FAN. OPS CHECK GOOD IAW MM 21-21-1 ANMar 27, 2010 · N71CX · Doug DC862F · Air Distribution FanSDR IXXA1000240Fan · odorAFTER 10 MINUTES OF RUNNING THE RT RECIRCULATION FAN, CREW SENSED AN ELECTRICAL/OZONE SMELL. THE RT RECIRCULATION FAN WAS SWITCHED OFF, CIRCUIT BREAKER WAS PULLED AND SMELL DISSIPATED. OPENMar 25, 2010 · N71CX · Doug DC862F · Air Distribution FanSDR IXXA100019OStriker · out of adjustDURING CLIMBOUT, AFTER GEAR RETRACTION THE DOOR NOT LATCH LIGHT REMAINED ON. THE CREW CYCLED THE GEAR AND LIGHT REMAINED ON. THEY LANDED WITHOUT FURTHER INCIDENT. MX FOUND THE LT GEAR DOOR STRIKER OUT OF ADJUSTMENT. THEY ADJUSTED THE DOOR STRIKER. OPS CHECK GOMar 3, 2010 · N799AL · Doug DC862F · Landing Gear Position and WarningSDR IXXA100018OAnti-Ice Valve · defectiveDURING CLIMB OUT WITH ANTI-ICE ON NR 4 ENG COMPRESSOR STALLED. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX REPLACED NR 4 INBD ANTI-ICE CONTROL VALVE REGULATOR. OPS CHECK GOOD IAW MM 75-10-1. ACFT WAS RETURNED TO SERVICE.Feb 28, 2010 · N799AL · Doug DC862F · Engine Anti-Icing SystemSDR IXXA100017OStriker · out of adjustDURING CLIMBOUT, THE DOOR NOT LATCH LIGHT REMAINED ON AFTER GEAR RETRACTION, CREW CYCLED THE GEAR AND LIGHT REMAINED ON. THEY LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED MLG AND FOUND THE LT MLG DOOR STRIKER OUT OF ADJUSTMENT. THEY ADJUSTED THE DOOR STRIKEFeb 19, 2010 · N799AL · Doug DC862F · Landing Gear Position and WarningSDR IXXA100012OOil System · low pressureDURING CRUISE FROM NR 2 ENGINE LOW OIL PRESSURE LIGHT CAME ON. THE CREW SHUTDOWN NR 2 ENG AND LANDED WITHOUT FURTHER INCIDENT. MX REPLACED MAIN OIL FILTER, LOW OIL PRESSURE SWITCH AND OIL PRESSURE DIFFERENTIAL SWITCH. OPS CHECK GOOD IAW MM 79-20-7, ERH 01.03.1Jan 31, 2010 · N799AL · Doug DC862F · Engine Oil PressureSDR IXXA100011OPressure Switch · malfunctionedDURING CRUISE, NR 2 ENG LOW PRESSURE LIGHT CAME ON. THE CREW SHUTDOWN NR 2 ENG AND LANDED WITHOUT FURTHER INCIDENT. MX REPLACED LOW OIL PRESSURE SWITCH AND OIL DIFFERENTIAL SWITCH. OPS CHECK GOOD IAW MM 79-33-1 AND 79-32-2. ACFT WAS RETURNED TO SERVICE.Jan 30, 2010 · N799AL · Doug DC862F · Engine Oil PressureSDR IXXA100008OControl Box · defectiveDURING CLIMB OUT, BOTH ATC TRANSPONDERS INOP. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX REPLACED TCAS/ATC CONTROL PANEL AND TIGHTENED CONNECTOR ON TRANSPONDER ANTENNA SWITCHING RELAY. OPS CHECK GOOD IAW MM 34-53-0. ACFT WAS RETURNED TO SERVJan 23, 2010 · N71CX · Doug DC862F · ATC Transponder SystemSDR IXXA100001OBleed Valve · stuckDURING TAKEOFF ROLL AT APPROX 90 PERCENT N2 RPM THE ENG COMPRESSOR STALLED, EPR, N2 AND EGT ROLLED BACK. THE CREW ABORTED THE TAKEOFF AND RETURNED TO PARKING. MX INSPECTED THE ENG AND FOUND THE PRESSURE RATIO BLEED CONTROL VALVE, (PRBC) STICKING. PRBC WAS LUJan 14, 2010 · N71CX · Doug DC862F · Compressor Bleed ValveSDR IXXA090077OO-Ring · damagedDURING CRUISE, ACFT LOST HYD FLUID TO THE STANDPIPE LEVEL. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MX INSPECTED THE HYD SYS AND FOUND THE O-RING ON THE NR 2 SYS HYD PUMP PRESSURE LINE LEAKING. THE O-RING WAS REPLACED, THE LEAK AND OPS CHECKS WERE GOOD ANDec 21, 2009 · N41CX · Doug DC862F · Hydraulic System, MainSDR IXXA090076OFan · smokeDURING CRUISE, THE LT RECIRCULATION FAN EMITTING BURNED ODOR. THE CREW TURNED OFF LT RECIRCULATION FAN AND LANDED WITHOUT FURTHER INCIDENT. IN WORK.Dec 18, 2009 · N799AL · Doug DC862F · Air Distribution FanSDR IXXA090073OWarning Light · false activationDURING TAKEOFF ROLL CABIN DOOR WARNING LIGHT BEGAN TO BLINK. THE CREW REJECTED TAKEOFF AND RETURNED TO BLOCKS WITHOUT FURTHER INCIDENT. MX INSPECTED ALL CABIN DOORS. OPS CHECK GOOD IAW MM 52-70-1. ACFT WAS RETURNED TO SERVICE.Dec 14, 2009 · N71CX · Doug DC862F · Door Warning SystemSDR IXXA090072OEngine · power lossDURING TAKEOFF FROM WSAP NR 4 ENG FAILED TO PRODUCE TAKEOFF PWR. THE CREW REJECTED TAKEOFF AND RETURNED TO BLOCKS WITHOUT FURTHER INCIDENT. MX PERFORMED POWER RUN AND ACCELERATION CHECK. OPS CHECK GOOD IAW ERH 72.01.1. ACFT WAS RETURNED TO SERVICE.Dec 14, 2009 · N41CX · Doug DC862F · Engine (Turbine/Turboprop)SDR IXXA090068OPrbc · dryDURING CLIMB OUT, THE CREW HEARD A LOUD BANG, F/A REPORTED A FLASH ON LT SIDE. THEY RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX INSPECTED BOTH NR 1 AND NR 2 ENGINE'S, LUBED THE PRBC'S. OPS CHECK GOOD IAW MM 72-00, ERH 70.01, ERH 75.01, AND MM 12-80-0. Nov 29, 2009 · N41CX · Doug DC862F · Turbine Engine Compressor SectionSDR IXXA090065ORegulator · defectiveDURING CLIMB OUT FROM NR 2 ENG COMPRESSOR STALLED WITH GEAR UP, EPR 1.86 AND ANTI-ICE VALVE ON. THE CREW RETURNED TO WITHOUT FURTHER INCIDENT. MX REPLACED BOTH ANTI-ICE VALVE REGULATOR'S. OPS CHECK GOOD IAW MX MM 75-10-2. ACFT WAS RETURNED TO SERVICE.Nov 5, 2009 · N71CX · Doug DC862F · Compressor Bleed ValveSDR IXXA090064OWire · burnedDURING CLIMB OUT FROM TAPA NR 4 ENG EPR INOP, NR 4 GENERATOR CAUSED A MOMENTARY LOSS OF ALL POWER THEN LOCKED OUT-SHORTLY AFTER ZOLTS AND FREQUENCY WENT TO ZERO, AND NR 4 ENG BEGAN TO SPARK EVERY 25 SECONDS THE CREW SHUTDOWN NR 4 ENG. THEY RETURNED TO TAPA WIOct 26, 2009 · N799AL · Doug DC862F · Engine Indicating System WiringSDR IXXA090063OReservoir · lowDURING CLIMB OUT FROM RJTY THE CREW NOTICE HYDRAULIC FLUID DROPPED TO STANDPIPE WITH RESERVOIR LOW PRESSURE LIGHT ON, THE CREW RETURNED TO RJTY WITHOUT FURTHER INCIDENT. MAINTENANCE SERVICED HYDRAULIC RESERVOIR. OPERATIONAL CHECK GOOD IAW MM 12-30-1, ERH 70.01Oct 25, 2009 · N41CX · Doug DC862F · Hydraulic Reservoir, MainSDR IXXA090061OPower Supply · defectiveDURING CRUISE, ALL FOUR FUEL FLOW INDICATORS WENT TO ZERO AND NUMBER FOUR EPR FAILED. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED BOTH FUEL FLOW POWER SUPPLY. OPERATIONAL CHECK GOOD IAW ATI ERH 71.01 AND ERH 70.01. AIRCRAFT WAOct 19, 2009 · N799AL · Doug DC862F · Fuel Indicating SystemSDR IXXA090058OClamp · looseDURING APPROACH INTO KBWI NUMBER FOUR ENGINE FIRE WARNING CAME ON INTERMITTENTLY. THE CREW SHUTDOWN NUMBER FOUR ENGINE AS A PRECAUTION, THEY LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND TIGHTENED LOOSE CLAMP ON HIGH STAGE BLEED VALVE. OPERATIONALOct 18, 2009 · N799AL · Doug DC862F · Engine Bleed Air SystemSDR IXXA090055OFan · defectiveDURING C CHECK TEST FLIGHT FROM SPLP THE LEFT HAND RECIRCULATION FAN EMITTED ELECTRICAL ODOR. THE CREW TURNED OFF LEFT RECIRCULATION FAN. THEY RETURNED TO SPLP WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT HAND RECIRCULATION FAN. OPERATIONAL CHECK Sep 30, 2009 · N41CX · Doug DC862F · Air Distribution FanSDR IXXA090048ODoor · lack of lubeDURING CLIMB OUT, CREW HEARD A VIBRATION SOUND COMING FROM THE NLG AREA. THEY CYCLED THE NLG AND THE NOISE CONTINUED. CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX INSPECTED AND FOUND RT NOSE GEAR DOOR WAS DOWN. MX LUBED DOOR LOCK MECHANISM. OPSSep 3, 2009 · N799AL · Doug DC862F · Landing Gear Door Retract SectionSDR IXXA090047OAmplifier · defectiveDURING CLIMB OUT, NR 2 COMPASS SYS PRECESSED EXCESSIVELY. CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX REPLACED NR 2 INSTRUMENT AMP RACK. OPS CHECK GOOD IAW MM 34-20-2. ACFT WAS RETURNED TO SERVICE.Sep 3, 2009 · N799AL · Doug DC862F · Magnetic CompassSDR IXXA090044OIndicator · defectiveDURING TAKEOFF FROM NR 1 EPR GUAGE WOULD NOT ACCELERATE. THE CREW RETURNED TO BLOCKS WITHOUT FURTHER INCIDENT. MX REPLACED NR 1 EPR TRANSMITTER. OPS CHECK GOOD IAW MM 77-11-1, AND ERH 70.01.1. ACFT WAS RETURNED TO SERVICE.Aug 30, 2009 · N799AL · Doug DC862F · Engine Pressure Ratio (EPR)SDR IXXA090043OAnti-Skid Sys · defectiveDURING TAKEOFF, ANTI-SKID INOP LIGHT ILLUMINATED ON SKID CONTROL MONITOR. THE CREW RETURNED TO BLOCK WITHOUT FURTHER INCIDENT. MX REPLACED ANTI-SKID CONTROL VALVE AND ANTI-SKID TRANSDUCER. OPS CHECK GOOD IAW MM 32-43-0, 32-43-3. ACFT WAS RETURNED TO SERVICEAug 29, 2009 · N799AL · Doug DC862F · Brake Anti-Skid SectionSDR IXXA09SMN094SSkin · corrodedDURING ROUTINE C-CHECK INSP, FOUND FUSELAGE EXTERNAL SKIN CORRODED AT STA 960.000 LONGERON 18-19 RT. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASETNERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR DOUBLER. PERFORMED NDT INSP. NO CRACK OR COAug 21, 2009 · N41CX · Doug DC862F · Fuselage Main, Plate/SkinSDR IXXA09SMN093SSkin · dentedDURING ROUTINE C CHECK INSPECTION FOUND LEFT WING INBOARD AILERON UPPER SKIN DENTED AT STATION XA 515.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED SKIN. FABRICATED NEW SKIN AND BONDED DOUBLERS. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED,Aug 13, 2009 · N41CX · Doug DC862F · AileronsSDR IXXA09SMN092SSkin · crackedDURING ROUTINE C CHECK INSPECTION FOUND LT WING INBOARD AILERON UPPER SKIN CRACKED AT STATION XW 563.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED SKIN. FABRICATED NEW SKIN AND BONDED DOUBLERS. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, Aug 13, 2009 · N41CX · Doug DC862F · AileronsSDR IXXA09SMN091SSkin · corrodedDURING ROUTINE C CHECK INSPECTION FOUND RUDDER LT SKIN CORRODED AT STATION ZR 238.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED EXISTING SKIN. FABRICATED NEW SKIN AND BONDED DOUBLERS. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED, AND PRIMED AREA Aug 13, 2009 · N41CX · Doug DC862F · Rudder, Plate/SkinSDR IXXA09SMN090SFitting · crackedDURING ROUTINE C CHECK INSPECTION FOUND MAIN CARGO COMPARTMENT SUB FLOOR FITTING CRACKED AT STATION 798.000 LBL 24". REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AREA AND FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, SRM 51-3-0, DC8 SRM 51-1-8BAug 13, 2009 · N41CX · Doug DC862F · Fuselage Main, Attach FittingsSDR IXXA09SMN089SSkin · corrodedDURING ROUTINE C-CHECK INSP FOUND RT WING L/E LWR SKIN CORRODED AT STA XFS 566.250. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO CRACK OR CORROSION. FABRICATED DOUBLER, AND FILLER. CLEANED, TREATED, AND PRIMED AREA ANAug 11, 2009 · N41CX · Doug DC862F · Wing, Plate/SkinSDR IXXA09SMN087SSpar Cap · corrodedDURING ROUTINE C-CHECK INSP, FOUND RUDDER RT SIDE FRONT SPAR CAP CORRODED AT STA ZR 323.000. REMOVED CORROSION, FOUND OUT OF LIMITS. REMOVED DAMAGED SPAR CAP. FABRICATED NEW SPAR CAP. CLEANED, TREATED, AND PRIMED AREA AND NEW SPAR CAP. INSTALLED NEW SPAR CAP Aug 11, 2009 · N41CX · Doug DC862F · Wing SparSDR IXXA09SMN088SLongeron · corrodedDURING ROUTINE C CHECK INSPECTION FOUND MAIN CARGO COMPARTMENT CORROSION ON LONGERON 22 RT AT STATION 1530.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED LONGERON. CLEANED, TREATED, AND PRIMED AREA AND LONGERON. INSTALLED NEW LONGERON IAW SRM CHAAug 11, 2009 · N41CX · Doug DC862F · Fuselage Main, Longeron/StringerSDR IXXA09SMN086SAngle · corrodedDURING ROUTINE C CHECK INSPECTION FOUND MAIN CARGO COMPARTMENT AFT RING ANGLE CORRODED AT STATION 1530.000 LONGERON 26-28 LT. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED EXISTING REPAIR ANGLE. FABRICATED REPAIR ANGLE SPLICE. CLEANED, TREATED, AND PRIMED ARAug 11, 2009 · N41CX · Doug DC862F · Fuselage Miscellaneous StructureSDR IXXA09SMN085SFitting · corrodedDURING ROUTINE C CHECK INSPECTION FOUND MAIN CARGO COMPARTMENT RIGHT HAND AFT BATHTUB FITTING CORRODED AT STATION 1530.000 LONGERON 30RIGHT. REMOVED CORRODED FITTING. CLEANED, TREATED, AND PRIMED AREA AND FITTING. INSTALLED NEW FITTING IAW SRM 51-1-21, SRM 51-Aug 11, 2009 · N41CX · Doug DC862F · Fuselage Main, Attach FittingsSDR IXXA09085SFitting · corrodedDURING ROUTINE C CHECK INSPECTION FOUND MAIN CARGO COMPARTMENT RIGHT HAND AFT BATHTUB FITTING CORRODED AT STATION 1530.000 LONGERON 30RIGHT. REMOVED CORRODED FITTING. CLEANED, TREATED, AND PRIMED AREA AND FITTING. INSTALLED NEW FITTING IAW SRM 51-1-21, SRM 51-Aug 11, 2009 · N41CX · Doug DC862F · Fuselage Main, Attach FittingsSDR IXXA09SMN084SFloorbeam · crackedDURING ROUTINE C-CHECK INSP FOUND FUSELAGE TAIL SEC FLOORBEAM UPPER FLANGE CRACKED AT STA 1540.000 LT BOTTOM LINE 39. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED EXTRUSION REPAIR CHANNEL, FILLERS, AND SPACERS. CLEANED, TAug 10, 2009 · N41CX · Doug DC862F · Fuselage Main, Floor BeamSDR IXXA09SMN083SCargo Track · corrodedDURING ROUTINE C-CHECK INSP, FOUND MAIN CARGO COMPARTMENT RT SIDE NR 7 TRACK CORRODED AT STA 1050.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED EXISTING SPLICE FWD SIDE AND DAMAGED TRACK SEGMENT. FABRICATED SPLICES. PERFORMED HEAT TREATMENT. CLEANEAug 8, 2009 · N41CX · Doug DC862F · Fuselage, Seat/Cargo Attach Fittings
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