Douglas DC-8-62

Service difficulty reports · 2,778

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 = 'DC862'
  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 IXXA06SMN349SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT OUTBOARD AILERON LOWER SKIN HAS IMPROPER FASTENERS FROM STATION XA620.000 TO STATION XA722.000. REMOVED IMPROPER FASTENERS AND DAMAGED SKIN. FABRICATED NEW SKIN AND BONDED DOUBLER. BONDED BOTH PARTS WITH HYSOL. Nov 4, 2006 · N799AL · Doug DC862 · AileronsSDR IXXA06SMN348SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND FITTING CRACKED AT STATION 742.000, LONGERON 13 LEFT. REMOVED CRACK FITTING. CLEANED TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, DC8 SRM 51-3-1, AND DC8 SRM 51-1-8B.Nov 4, 2006 · N799AL · Doug DC862 · Fuselage Main, Attach FittingsSDR IXXA06SMN345SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND CRACKED FITTING AT STATION 680.000, LONGERON 11 LEFT. REMOVED CRACKED FITTING. CLEANED TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D DC8 SRM 51-3-1, AND DC8 SRM 51-1-8B.Nov 4, 2006 · N799AL · Doug DC862 · Fuselage Main, Attach FittingsSDR IXXA06SMN344SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND FITTING CRACKED AT STATION 879.000, LONGERON 13 RIGHT. REMOVED CRACKED FITTING. FABRICATED NEW FITTING. PERFORMED NDT INSPECTION, NO CRACKS OR CORROSION FOUND. CLEANED, TREATED AND PRIMED FITTING. INSTALLED FITTINGNov 4, 2006 · N799AL · Doug DC862 · Fuselage Main, Attach FittingsSDR IXXA06SMN343SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND FITTING CRACKED AT STATION 717.000 , LONGERON 13 LEFT. REMOVED DAMAGED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC-8 SRM 51-3-0, DC-8 SRM 51-3-1 AND DC-8 SRM 51-1-8B.Nov 4, 2006 · N799AL · Doug DC862 · Fuselage Main, Attach FittingsSDR IXXA06SMN341SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING SKIN CRACKED AT STATION XW74.000, STRINGER 11. REMOVED FASTENERS AS NEEDED. REMOVED DAMAGED AREA PERFORMED NDT INSPECTION, NO CRACKS OR CORROSION FOUND AFTER DAMAGE REMOVED. FABRICATED REPAIR DOUBLER AND FINov 4, 2006 · N799AL · Doug DC862 · Wing, Plate/SkinSDR IXXA06SMN340SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING SKIN CORRODED FROM STATION XF422.520 TO STATION XOLDI6.225 UPPER SIDE. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION, NO CRACKS OR CORROSION FOUND AFTER DAMAGE REMOVNov 4, 2006 · N799AL · Doug DC862 · Wing, Plate/SkinSDR IXXA06SMN338SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND EXISTING REPAIR AT STATION FS 1460, LONGERON 21 LEFT, DO NOT MEET CURRENT AD, SB, AND SRM REQUIREMENTS. REMOVED NON STANDARD REPAIR EXISTING. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FONov 4, 2006 · N799AL · Doug DC862 · Fuselage Main, Plate/SkinSDR IXXA06SMN337SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, EXISTING REPAIR AT STA FS 1500, LONGERON 16 RIGHT HAS AN INTERIM REPAIR. REMOVED EXISTING REPAIR DC8 REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION, NO CRACKS OR CORROSION FOUND DAMAGE REMOVED. FABRICATED NEW REPAIR DOUBLENov 4, 2006 · N799AL · Doug DC862 · Standard Practices/StructuresSDR IXXA06SMN336SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND EXISTING REPAIR FROM STATION 1240 TO 1280 LONGERON 32 RIGHT TO LONGERON 35 RIGHT IS NOT IN COMPLIANCE WITH AD.2005-18-07 OR SB DC8-53-078. REMOVED EXISTING REPAIR. MANUFACTURED REPAIR PARTS. CLEANED, TREATED AND PRIMNov 4, 2006 · N799AL · Doug DC862 · Fuselage Main, Plate/SkinSDR IXXA06SMN335SSkin · misrepairedDURING ROUTINE C CHECK, FOUND FREON EXHAUST AFT UPPER CORNER HAS INTERMEDIATE REPAIR AT STATION, FS 255.000 LONGERON 28.5 LEFT. REMOVE EXISTING REPAIR DOUBLER. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTSNov 4, 2006 · N799AL · Doug DC862 · Fuselage Main, Plate/SkinSDR IXXA06SMN334SSkin · misrepairedDURING ROUTINE C CHECK, FOUND FREON EXHAUST FORWARD UPPER CORNER HAS INTERMEDIATE REPAIR AT STATION, FS 238.000 LONGERON 28.5 LEFT. REMOVE EXISTING REPAIR DOUBLER. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PNov 4, 2006 · N799AL · Doug DC862 · Fuselage Main, Plate/SkinSDR IXXA06SMN333SSkin · misrepairedDURING ROUTINE C CHECK, FOUND FREON EXHAUST FORWARD LOWER CORNER HAS INTERMEDIATE REPAIR AT STATION, FS 238.000 LONGERON 29.5 LEFT. REMOVE EXISTING REPAIR DOUBLER. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PANov 4, 2006 · N799AL · Doug DC862 · Fuselage Main, Plate/SkinSDR IXXA06SMN332SSkin · misrepairedDURING ROUTINE C CHECK, FOUND FREON EXHAUST AFT LOWER CORNER HAS INTERMEDIATE REPAIR AT STATION, FS 255, LONGERON 29.5 LEFT. REMOVE EXISTING REPAIR DOUBLER. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. Nov 4, 2006 · N799AL · Doug DC862 · Fuselage Main, Plate/SkinSDR IXXA060453OEngine · leakingAPPROXIMATELY FIVE HOURS AFTER TAKEOFF FROM TAPA THE NR 2 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED AND OIL PRESSURE DROPPED TO 20 PSI. THE ENGINE WAS SHUTDOWN AND CHECKLIST WAS COMPLIED WITH THE CREW RETURNED TO TAPA AND LANDED. MAINTENANCE FOUND THE OIL EJun 21, 2006 · N799AL · Doug DC862 · Turbine Engine Oil SystemSDR IXXA060182OFitting · looseAFTER TAKEOFF FROM LPLA, CREW EXPERIENCED LOSS OF HYDRAULIC FLUID. WHILE RUNNING CHECKLIST GOT A DOOR UNSAFE LIGHT ON THEN GEAR UNSAFE LIGHT. GEAR UPLATCH CHECK AFTER TAKEOFF WAS GOOD. FLUID LOST TO ALMOST TOP OF STANDPIPE. CREW RETURNED AIRCRAFT TO LPLA AMay 14, 2006 · N799AL · Doug DC862 · Fuselage Main, Attach FittingsSDR IXXA060181OTransmitter · looseDURING CRUISE FROM KBWI TO BGTL THE NR 1 ENGINE FUEL PRESSURE WAS INTERMITTENT AND THERE WAS A FUEL ODOR IN THE COCKPIT WITH THE NR 3 HIGH STAGE BLEED IN HIGH. MAINTENANCE FOUND A LOOSE CONNECTION TO THE TRANSMITTER. REPAIRED PER ALL APPLICABLE MANUALS AND FMay 11, 2006 · N799AL · Doug DC862 · Fuel Flow IndicatingSDR IXXA0500117OValve · leakingDURING CRUISE, LT MANIFOLD INFLIGHT DECAY CHECK FAILED 30-20 PSI IN ONLY 1.5 SECONDS. CREW RETURNED A/C AND LANDED W/O INCIDENT. ON THE GROUND, DECAY CHECK WAS 5 SECONDS. RT MANIFOLD GROUND DECAY FAILED 30-20-PSI IN ONLY 5 SECONDS. UPON INSPECTION MX FOUND Nov 18, 2005 · N799AL · Doug DC862 · Airfoil Anti/De-ice SystemSDR IXXA0500077OWire · burnedDURING CRUISE AT APPROX 1 HOUR AND 20 MINUTES INTO FLIGHT FROM KSUU, F/A CALLED AND REPORTED A BURNING ODOR IN THE LEFT LAV. THE POWER SOURCE WAS ISOLATED AND ODOR WAS STILL PRESENT. CREW DIVERTED AIRCRAFT TO KSFO AND LANDED WITHOUT INCIDENT. MAINTENANCE TRMay 22, 2005 · N799AL · Doug DC862 · Water/Waste System WiringSDR IXXA0500015OEngine · failedDURING CLIMBOUT FROM KBWI, NR 4 ENGINE OIL PRESSURE LIGHT CAME ON. OIL PRESSURE/QUANTITY NORMAL. OIL TEMP WAS SLIGHTLY HIGHER THEN OTHERS AT 105C. COMPLETED CHECKLIST AND LIGHT WOULD NOT GO OUT. CREW SHUT DOWN ENGINE INFLIGHT THEN DIVERTED AIRCRAFT TO KWRIFeb 5, 2005 · N799AL · Doug DC862 · Engine (Turbine/Turboprop)SDR RRXA05141Frame · damagedDURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLES IN THE UPPER CARGO COMPT FS 1220 AND L21R TO L21L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED DISCREPANT HOLES, FABRICATED DOUBLERS FROM 70Jan 26, 2005 · N994CF · Doug DC862 · Fuselage Main, FrameSDR ARWA20041002Clamp · out of positionDURING TAKEOFF ROLL, NR 2 ENGINE EGT REACHED 580 DEGREES CELSIUS, PULLED POWER BACK OIL PRESS LIGHT ILLUMINATED, N1 AND EPR INDICATION ERRATIC. SHUTDOWN ENGINE NR 2; 200 PERCENT N1 5 PERCENT. OIL PRESSURE 10 PSI. FOUND ANTI-ICE DUCT CLAMP OUT OF POSITION, SOct 12, 2004 · N8969U · Doug DC862 · Engine Anti-Icing SystemSDR IXXA0400111OFiber Optic Gyro · faultyAFTER TAKEOFF FROM KCOF, CAPTAINS ADI GYRO "OFF FLAG" AND NR 1 COMPASS "OFF FLAG" APPEARED. CREW RETURNED AIRCRAFT TO KCOF AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED FOG GYRO PER ALL APPLICABLE MANUALS AND AIRCRAFT WAS RETURNED TO SERVICE.Oct 4, 2004 · N31CX · Doug DC862 · Directional Gyro and Indicating SystemSDR IXXA0400107OComputer · failedAFTER TAKEOFF FROM WSAP, YAW DAMPER ENGAGED, RUDDER KICKED TO THE LEFT. DISENGAGED YAW DAMPER. CREW TRIED TO RE-ENGAGE YAW DAMPER AND RUDDER KICKED LEFT AGAIN, TURNED OFF YAW DAMPER. CREW RETURNED AIRCRAFT TO WSAP AND LANDED WITHOUT INCIDENT. AN INVESTIGATSep 21, 2004 · N799AL · Doug DC862 · Autopilot SystemSDR IXXA0400106O9Yaw Damper · malfunctionedAFTER TAKEOFF FROM WSAP, YAW DAMPER ENGAGED, RUDDER KICKED TO THE LEFT. DISENGAGED YAW DAMPER. CREW TRIED TO RE-ENGAGE YAW DAMPER AND RUDDER KICKED LEFT AGAIN, TURNED OFF YAW DAMPER. CREW RETURNED AIRCRAFT TO WSAP AND LANDED WITHOUT INCIDENT. AN INVESTIGATSep 21, 2004 · N799AL · Doug DC862 · Autopilot SystemSDR IXXA060419SPanel · delaminatedDURING ROUTINE C CHECK, FOUND LEFT WING TRAILING EDGE DIHEDRAL PANEL DELAMINATED. REPLACED PANEL PER ALL APPLICABLE DATA.Sep 16, 2004 · N41CX · Doug DC862 · Wing, Plate/SkinSDR IXXA060420SDoubler · misinstalledDURING ROUTINE C CHECK, FOUND LEFT WING OUTBOARD AILERON REPAIR SHORT ONE RIVET FROM STATION XA661 TO XA671. REPLACED PER ALL APPLICABLE DATA.Sep 1, 2004 · N41CX · Doug DC862 · AileronsSDR IXXA060435SAngle · wornDURING ROUTINE C CHECK, FOUND RIGHT WING OUTBOARD FLAP HINGE FITTING ANGLE WORN AT STATION XF218. REPAIRED PER ALL APPLICABLE DATA.Aug 24, 2004 · N41CX · Doug DC862 · Trailing Edge FlapsSDR ARWA20040805Switch · failedON ENGINE START, NR 4 ENGINE WOULD NOT LIGHT UP WITH A & B AND BOTH IGNITERS. T/S DOWN TO FUEL SHUT-OFF LEVER SWITCH TRANSFERRED TO DMI 18678 IN ACCORDANCE WITH MEL 74-1 CATEGORY-C, PLACARD INSTALLED. REPLACED START LEVER SWITCH PER MM 74-00; OPERATIONAL NORAug 24, 2004 · N810BN · Doug DC862 · Ignition SystemSDR IXXA060418SFitting · crackedDURING ROUTINE C CHECK, FOUND LEFT WING IN BOARD FLAP FITTING CRACKED AT STATION XW97. REPLACED FITTING PER ALL APPLICABLE DATA.Aug 20, 2004 · N41CX · Doug DC862 · Trailing Edge FlapsSDR IXXA0400103OB-Nut · looseDURING TAKEOFF FROM PGUA, HYDRAULIC FLUID DROPPED TO STAND PIPE LEVEL. HYDRAULIC FLUID WAS LEAKING FROM NR 2 ENGINE. AIRCRAFT RETURNED TO PGUA AND LANDED WITH INCIDENT. AN INSPECTION IS ON GOING. INFORMATION WILL BE PROVIDED AS SOON AS IT IS AVAILABLE. MAAug 8, 2004 · N799AL · Doug DC862 · Hydraulic System, MainSDR IXXA060417SSkin · corrodedDURING ROUTINE C CHECK, FOUND LEFT WING LEADING EDGE SKIN CORRODED AT STATION XFS61. REPAIRED PER ALL APPLICABLE DATA.Jul 30, 2004 · N41CX · Doug DC862 · Wing, Plate/SkinSDR ARWA20040702Actuator · inoperativeFUEL DUMPED PER ABNORMAL CHECKLIST AT MAXIMUM LANDING WEIGHT SWITCH PUT IN DRAIN POSITION, BUT CONTINUED DUMPING MANUALLY PUT IN DRAIN POSITION FOR 5 MINUTES, REMAINDER OF ELECTRICAL CYCLE OK. TRANSFERRED TO DMI 18610 IN ACCORDANCE WITH MEL 28-9-1. MANUAL FUJul 14, 2004 · N810BN · Doug DC862 · Fuel Dump SystemSDR ARWA20040701Linkage · vibrationAFTER TAKEOFF HEAVY NOISE VIBRATION EXPERIENCE. CYCLE GEAR SEVERAL TIMES WITH NO CHANGE, RETURNED TO FIELD. FUEL DUMPED PER ABNORMAL CHECKLIST. CHECKED NOSE GEAR DOOR LINKAGE IN ACCORDANCE WITH MM 32-22-2; OPERATIONS AND TESTED IN ACCORDANCE WITH MM 32-21-1Jul 14, 2004 · N810BN · Doug DC862 · Landing Gear Door Retract SectionSDR IXXA060444SFitting · corrodedDURING ROUTINE C CHECK, FOUND RIGHT WING OUTBOARD FLAP HINGE FITTING CORRODED AT STATION XF219. REPAIRED PER ALL APPLICABLE DATA.Jul 5, 2004 · N41CX · Doug DC862 · Wing StructureSDR IXXA060443SFitting · corrodedDURING ROUTINE C CHECK, FOUND RIGHT WING FLAP HINGE FITTINGS CORRODED AT STATIONS XW219 AND XW97. REPAIRED PER ALL APPLICABLE DATA.Jul 2, 2004 · N41CX · Doug DC862 · Trailing Edge FlapsSDR IXXA060441SSkin · crackedDURING ROUTINE C CHECK, FOUND RIGHT WING OUTBOARD FLAP TRAILING EDGE SKIN CRACKED AT STATION XF300. REPAIRED PER ALL APPLICABLE DATA.Jul 2, 2004 · N41CX · Doug DC862 · Trailing Edge FlapsSDR IXXA060279SDoubler · corrodedDURING ROUTINE C CHECK, FOUND DOUBLER CORRODED FROM STATION 188 TO 208 AT Z=0 BETWEEN -X45 AND -X62. REPAIRED PER ALL APPLICABLE DATA.Jun 30, 2004 · N41CX · Doug DC862 · Fuselage Main, Plate/SkinSDR IXXA060440SSkin · corrodedDURING ROUTINE C CHECK, FOUND RIGHT WING SKIN CORRODED AT STATION XOLDI6.224. REPAIRED PER ALL APPLICABLE DATA.Jun 29, 2004 · N41CX · Doug DC862 · Wing, Plate/SkinSDR IXXA060278SFloorbeam · crackedDURING ROUTINE C CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED AT STATION Y1542, -X37 TO -X43. REPAIRED PER ALL APPLICABLE DATA.Jun 29, 2004 · N41CX · Doug DC862 · Fuselage Main, Floor BeamSDR IXXA060381SSkin · corrodedDURING ROUTINE C CHECK, FOUND LEFT ELEVATOR LOWER SKIN INTERNAL "TEE" AND SKIN CORRODED AT STATION XE40. REPAIRED PER ALL APPLICABLE DATA.Jun 18, 2004 · N41CX · Doug DC862 · Elevator, Plate/SkinSDR IXXA060379SSkin · bulgedDURING ROUTINE C CHECK, FOUND LEFT ELEVATOR LOWER SKIN TRAILING EDGE BULGED FROM STATION XE246 TO XE318. REPAIRED PER ALL APPLICABLE DATA.Jun 18, 2004 · N41CX · Doug DC862 · Elevator, Plate/SkinSDR IXXA060378SSkin · debondedDURING ROUTINE C CHECK, FOUND RIGHT ELEVATOR LOWER SKIN SURFACE CORRODED AND DEBONDED AT STATION XE205.687. REPAIRED PER ALL APPLICABLE DATA.Jun 18, 2004 · N41CX · Doug DC862 · Elevator, Plate/SkinSDR IXXA060439SStrap · corrodedDURING ROUTINE C CHECK, FOUND RIGHT WING OUTBOARD FLAP LEADING EDGE STRAP CORRODED AND WORN. REPAIRED PER ALL APPLICABLE DATA.Jun 17, 2004 · N41CX · Doug DC862 · Trailing Edge FlapsSDR IXXA060438SFitting · crackedDURING ROUTINE C CHECK, FOUND NUMBER 4 MAIN FUEL TANK FITTING CRACKED AT STATION 239.793 BETWEEN FRONT SPAR AND STRINGER 18. REPAIRED PER ALL APPLICABLE DATA.Jun 15, 2004 · N41CX · Doug DC862 · Wing, Attach FittingsSDR IXXA060437SSkin · dentedDURING ROUTINE C CHECK, FOUND RIGHT WING OUTBOARD FLAP LOWER SKIN DENTED AT STATION XF208. REPAIRED PER ALL APPLICABLE DATA.Jun 11, 2004 · N41CX · Doug DC862 · Trailing Edge FlapsSDR IXXA060434SPanel · delaminatedDURING ROUTINE C CHECK, FOUND RIGHT WING TRAILING EDGE FIXED PANEL DELAMINATED AND NICKED AT STATIONS XW10, XW40, AND XW75. REPAIRED PER ALL APPLICABLE DATA.Jun 11, 2004 · N41CX · Doug DC862 · Wing, Plate/SkinSDR IXXA060433SRib · crackedDURING ROUTINE C CHECK, FOUND RIGHT WING TRAILING EDGE RIB CRACKED AT STATION XW36. REPAIRED PER ALL APPLICABLE DATA.Jun 11, 2004 · N41CX · Doug DC862 · Wing, Rib/BulkheadSDR IXXA060342SFitting · corrodedDURING ROUTINE C CHECK, FOUND LONGERON 24 RIGHT FITTING CORRODED AT STATION Y910, -Z10. REPAIRED PER ALL APPLICABLE DATA.Jun 11, 2004 · N41CX · Doug DC862 · Fuselage Main, Attach FittingsSDR IXXA060432SSkin · corrodedDURING ROUTINE C CHECK, FOUND RIGHT WING OUTBOARD SLOT AREA UPPER SURFACE SKIN CORRODED. REPAIRED PER ALL APPLICABLE DATA.Jun 9, 2004 · N41CX · Doug DC862 · Wing, Plate/Skin
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