Douglas DC-8-62

Service difficulty reports · 2,778

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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 IXXA0200069SDoor · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED AT FUSELAGE STATION 15OO, AFT PASSENGER DOOR FRAME AT THE LOWER AFT CORNER. REPAIR ACCOMPLISHED REMOVAL OF THE DAMAGE AREA, FABRICATION AND INSTALLATION OF A NEW INTERNAL REPAIR ANGLE AND FRAME IN ACCOMay 21, 2002 · N728PL · Doug DC862 · Passenger/Crew DoorsSDR IXXA0200020OFan · defectiveENROUTE FROM BWI TO WRI, THE FLIGHT CREW SENSED AN ODOR IN THE COCKPIT WHEN THE RIGHT RECIRCULATION FAN WAS OPERATING. THE FLIGHT CREW SECURED THE FAN AND THE ODOR SUBSIDED. THE FLIGHT CONTINUED FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT WHIMay 19, 2002 · N21CX · Doug DC862 · Air Distribution FanSDR IXXA0200067SDoor · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED UNDER A TEMPORARY REPAIR OF THE FORWARD ENTRANCE DOOR CUT OUT FORWARD UPPER CORNER. REPAIR ACCOMPLISHED, REMOVAL OF THE TEMPORARY REPAIR AND DAMAGED AREA, FABRICATION AND INSTALLATIN OF A REPAIR FILLER, May 17, 2002 · N728PL · Doug DC862 · DoorsSDR IXXA0200066SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE LEFT HAND SIDE FUSELAGE SKIN BELOW THE AFT PASSENGER DOOR SKIN CUT OUT AT STATION 1480 TO 1510. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGED SKIN, FABRICATION AND INSTALLATION OF FILLER REPAIR DOULBEMay 16, 2002 · N728PL · Doug DC862 · Fuselage Main, Plate/SkinSDR IXXA0200065SSkin · crackedDURING ROUTINE C-CHECK, A CRACK WAS DETECTED IN THE AFT PASSENGER DOOR FORWARD LOWER SKIN CORNER AT SKIN CUTOUT. REPAIR ACCOMPLISHED, REMOVAL OF THE DAMAGED AREA, FABRICATION AND INSTALLATION OF A REPAIR FILLER, DOUBLER AND TRIPLER IN ACCORDANCE WITH THE DOUGMay 15, 2002 · N728PL · Doug DC862 · Fuselage Main, Plate/SkinSDR IXXA0200064SSpar · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON TOP OF THE LEFT WING INTERSPAR SKIN BETWEEN XRS 190 INBOARD TO WING WALK AREA TO INCLUDE THE MAIN SKIN EXTENSION OVER GEAR TRUNNION AREA. REPAIR ACCOMPLISHED CORROSION REMOVAL. FABRICATION AND INSTAMay 15, 2002 · N728PL · Doug DC862 · Wing SparSDR IXXA0200063SSpar · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE UPPER WING EXTERNAL PLATING BETWEEN WING STATION XFS 172 AND XFS 255. REPAIR ACCOMPLISHED, CORROSION REMOVAL OF THE DAMAGE ARE, FABRICATION AND INSTALLATION OF A REPAIR DOUBLER IN ACCORDANCE WITHMay 15, 2002 · N728PL · Doug DC862 · Wing SparSDR IXXA0200062SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, LIGHT CORROSION WAS DETECTED ON THE TOP OF THE LEFT WING INTERSPAR SKIN BETWEEN STATION XW 408 XRS 590 TO STATION XRS 590. REPAIR ACCOMPLISHED CORROSION REMOVAL OF THE AFFECTED AREA IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL RMay 15, 2002 · N728PL · Doug DC862 · Wing, Plate/SkinSDR IXXA0200061SSkin · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACKED WAS DETECTED ON THE RIGHT WING OUTBOARD LEADING EDGE PANEL AT THE INBOARD AREA AT STATION XRS 634. REPAIR ACCOMPLISHED REMOVAL OF THE DAMAGED AREA, FABRICATION AND INSTALLATION OF A FILLER AND REPAIR DOUBLER IN ACCMay 14, 2002 · N728PL · Doug DC862 · Leading Edge DevicesSDR IXXA0200060SSkin · crackedDURING ROUTINE C-CHECK INSPECTION, CORROSION AND A CRACK WAS DETECTED ON THE RIGHT WING LEADING EDGE AT WING STATION XES710, UPPER CHORD MOUNTS. REPAIR ACCOMPLISHED REMOVAL OF THE DAMAGED AREA, FABRICATION AND INSTALLATION OF A REPAIR FILLER AND EXTERNAL DOUBMay 14, 2002 · N728PL · Doug DC862 · Leading Edge DevicesSDR IXXA0200059SSkin · crackedDURING ROUTINE C-CHECK INSPECTION, CORROSION AND A CRACK WAS DETECTED ON THE LEFT WING OUTBOARD LOWER LEADING EDGE AT STATION XFS 566. REPAIR ACCOMPLISHED REMOVAL OF THE DAMAGED AREA, FABRICATION AND INSTALLATION OF A REPAIR FILLER AND EXTERNAL DOUBLER IN ACCOMay 11, 2002 · N728PL · Doug DC862 · Leading Edge DevicesSDR IXXA0200058SStructure · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE LT WING OUTBOARD UPPER LEADING EDGE AT STATION XFS 705. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF A REPAIR DOUBLER AND FILLER IN ACCORDANCE WITH THE DOUGLAS SMay 11, 2002 · N728PL · Doug DC862 · Leading Edge DevicesSDR IXXA0200057SStructure · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE RT WING OUTBOARD LEADING EDGE AT STATION XFS 705. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF AN EXTERNAL REPAIR DOUBLER AND INTERNAL FILLER IN ACCORDANCE WITH May 11, 2002 · N728PL · Doug DC862 · Leading Edge DevicesSDR IXXA0200056SStructure · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED IN THE LEFT WING LEADING EDGE TOP SIDE AT STATION XFS 825. REMOVAL ACCOMPLISHED, REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF REPAIR DOUBLER IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIRMay 11, 2002 · N728PL · Doug DC862 · Wing Main, Frame StructureSDR IXXA0200055SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED AROUND THE SCREW HEADS ON THE TOP LEFT WING LEADING EDGE XFS 885. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF FILLER AND REPAIR DOUBLER IN ACCORDANCE WITH THE DOUGLAS May 11, 2002 · N728PL · Doug DC862 · Wing, Plate/SkinSDR IXXA0200054SStructure · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE FUSELAGE AT STATION 1440 AT LONGERON 22RT. REPAIR ACCOMPLISHED REMOVAL OF THE DAMAGED AREA, FABRICATION AND INSTALLATION OF A REPAIR DOUBLER AND INTERNAL FILLER IN ACCORDANCE WITH THE DOUGLAS STMay 10, 2002 · N728PL · Doug DC862 · Fuselage Main, StructureSDR IXXA0200053SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE AFT LOWER FUSELAGE FORWARD OF ACCESS PANEL NUMBER 60, STATION 1557 TO 1574, LONGERON 35 RT. REPAIR ACCOMPLISHED, REMOVAL OF THE DAMAGED AREA, FABRICATION AND INSTALLATION OF A INTERNAL FILLER ANMay 10, 2002 · N728PL · Doug DC862 · Fuselage Main, Plate/SkinSDR IXXA0200052SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE AFT LOWER FUSELAGE STATION 1520 BETWEEN LONGERONS 30LT TO 30RT. REPAIR ACCOMPLISHED, DAMAGED AREA CUT OUT, FABRICATION AND INSTALLATION OF FILLER AND REPAIR DOUBLER IN ACCORDANCE WITH THE DOUGLAMay 10, 2002 · N728PL · Doug DC862 · Fuselage Main, Plate/SkinSDR ARWA20020504Actuator · failedAFTER TAKEOFF PTC BECAME INOP. DURING CLIMB FLAP POSITION INDICATOR FAIL, HYD OIL TEMP LIGHT ON TEMP 69 DEGREES & CLIMBING. AT 31.0 FL HEAVY SMOKE OUT OF PEDESTAL AFT OF THROTTLE QUADRANT. DURING DESCENT NR 2 & 4 MANIFOLD OVERTEMP LIGHT ON. FOUND PTC ACTUAMay 10, 2002 · N8968U · Doug DC862 · Elevator Control SystemSDR ARWA20020503Garlock Seal · leakingNR 4 ENGINE OIL QUANTITY 3/4 OF A GALLON. PERFORMED INFLIGHT SHUT DOWN ABNORMAL. OIL PRESS WINDMILLING 20 PSI. SERVICED ENGINE OIL IAW DC-8 MM 12-20-1 AND PERFORMED ENGINE RUN-UP; FOUND OIL LEAK AT MAIN FUEL PUMP DRAIN. REMOVED AND REPLACED MAIN FUEL PUMP May 8, 2002 · N810BN · Doug DC862 · Turbine Engine Oil SystemSDR ARWA20020507Spar · crackedDURING C-CHECK, NR 4 PYLON INTERIOR, STA YN 165, RM UPPER CHORD WITH 4 INCH CRACK. REPAIRED UPPER SPAR CAP OF NR 4 PYLON IAW AS ELEVEN INC DRAWING AS 11403, SHEET 1 TO 6. ISSUED FAA FORM 8110-3 APPROVING THIS REPAIR.May 7, 2002 · N1804 · Doug DC862 · Nacelle/Pylon, Frame/Spar/RibSDR ARWA20020502Splice · crackedDURING C-CHECK, FORWARD LOWER CARGO COMPARTMENT FUSELAGE FS 340, FS 360, FS 380, FS 400, FS 420, FS 440 & FS 460; LBL 62.5 FLOORBEAM SPLICE WITH 2.750 INCH CRACK. REMOVED AND REPLACED FLOORBEAM SPLICE PLATE IAW AS ELEVEN INC DRAWING AS 11077, SHEET 1 OF 9, DAMay 6, 2002 · N1804 · Doug DC862 · Fuselage Miscellaneous StructureSDR ARWA20020501Longeron · crackedDURING C-CHECK, FORWARD CARGO COMPARTMENT LONGERON L-21L AT FUSELAGE FS 280 WITH 2 INCH CRACK. FABRICATED SHIM & REPAIR ANGLE IAW AS ELEVEN, INC DRAWING AS 11410, SHEET 1 & 2. INSTALLED PARTS IAW AS ELEVEN, INC DRAWING AS 11410, SHEET 1 & 2. ISSUED FAA FORMMay 6, 2002 · N1804 · Doug DC862 · Fuselage Main, Longeron/StringerSDR IXXA0200012OMechanism · stiffAFTER TAKE OFF FROM HIK, THE LANDING GEAR NOT LATCHED LIGHT ILLUMINATED FOLLOWING LANDING GEAR RETRACTION. THE FLIGHT CREW CYCLED THE GEAR BUT THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT RETURNED TO HIK FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTEDApr 1, 2002 · N41CX · Doug DC862 · Landing Gear Position and WarningSDR IXXA0200011OTerminal · looseAFTER TAKEOFF FROM HIK, THE GEAR DOOR NOT LATCHED AND THE GEAR NOT LATCHED LIGHT ILLUMINATED AFTER GEAR RETRACTION. THE FLIGHT CREW CYCLED THE LANDING GEAR BUT THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT RETURNED TO HIK FOR AN UNEVENTFUL LANDING. MAINApr 1, 2002 · N41CX · Doug DC862 · Landing Gear Position and WarningSDR IXXA0200037SDoor · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED UNDER A TEMPORARY REPAIR OF THE FORWARD ENTRANCE DOOR CUTOUT FORWARD UPPER CORNER. REPAIR ACCOMPLSISHED REMOVAL OF THE TEMPORART REPAIR AND DAMAGED AREA. FABRICATED AND INSTALLED REPAIR FILLER AND EXTERMar 25, 2002 · N799AL · Doug DC862 · DoorsSDR ARWA20020311Line · leakingDURING CLIMBOUT NR 1 ENGINE FAILED TO PRODUCE APPROPRIATE POWER ALL OTHER ENGINE PARAMETERS NORMAL, PROCEEDED WITH ABNORMAL CHECKLIST AND LANDED WITH NO FURTHER INCIDENTS. PREFORMED EPR CHECK IAW MM 77-11-0, FOUND PT-2 LINE OBSTRUCTED AT INLET GUIDE VANE CASMar 24, 2002 · N8969U · Doug DC862 · Engine Pressure Ratio (EPR)SDR IXXA0200036SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE RIGHT HAND WING LEADING EDGE AT STATION XFS 566. REPAIR ACCOMPLISHED REMOVAL DAMAGED AREA, FABRICATION AND INSTALLATION OF FILLERS AND EXTENDED DOUBLER IN ACCORDANCE WITH DOUGLAS MAINTENANCE MANMar 18, 2002 · N799AL · Doug DC862 · Wing, Plate/SkinSDR IXXA0200035SDoor Frame · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION AND CRACKS WERE DETECTED ALONG THE LOWER EDGE OF THE FUSELAGE AFT SERVICE DOOR AND DOOR FRAME BETWEEN LONGERONS 16 AND 17 AT AXXPRXIMATE FS1500. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLAMar 16, 2002 · N799AL · Doug DC862 · Service DoorsSDR ARWA20020306Transformer · malfunctionedSMOKE EMANATED MOMENTARILY FROM RT CORNER OF F/O GLARESHIELD (10 SEC), SMOKE STOPPED AS EMERGENCY CHECKLIST WAS INITIATED. REMOVED AND REPLACED BALLAST TRANSFORMER AND REPLACED LAMPS IAW MM 33-12-0.Mar 8, 2002 · N8969U · Doug DC862 · Flight Compartment LightingSDR IXXA0200034SLongeron · dentedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE EXTERNAL PLATING AT FUSELAGE STATION 480 AT STRINGER 21L. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF AN INTERNAL FILLER AND EXTERNAL REPAIR DOUBLER IN ACCORDANCE Mar 7, 2002 · N799AL · Doug DC862 · Fuselage Main, Longeron/StringerSDR IXXA0200033SAileron · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE RIGHT WING OUTBOARD AILERON INBOARD SIDE LOWER PLATING. REPAIR ACCOMPLISHED, DAMAGED AREA CUT OUT, FABRICATED AND INSTALLED FILLER AND DOUBLER REPAIR IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MAMar 6, 2002 · N799AL · Doug DC862 · AileronsSDR IXXA0200032SThreshold · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE C-1 DOOR UNDER THE THRESHOLD PLATE. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF REPAIR FILLER AND DOUBLER IN ACCORDANCE WITH DOUGLAS STRUCTURAL MAINTENANCE MANUAMar 6, 2002 · N799AL · Doug DC862 · Service DoorsSDR ARWA20020301Vhf Comm · malfunctionedRETURNED TO SVMI DUE TO TOTAL LOSS OF RADIO COMMUNICATION (VHF). AIRCRAFT LANDED UNEVENTFUL. CHECKED FOR SECURITY OF RADIO AND RECEIVER PANELS, OPS CHECK OF VHF OK IAW MM 23-20-00.Mar 3, 2002 · N8968U · Doug DC862 · VHF Communications SystemSDR ARWA20020208Transformer · faultyAFTER LANDING ROLL IN MGGT, HEAVY SMOKE WAS SEEN COMING OUT FROM BEHIND F/O'S INSTRUMENT PANEL. AREA WAS INSPECTED, FOUND THE GLARESHIELD LIGHT BALLAST (B6) AT FAULT. REMOVED AND REPLACED BALLAST TRANSFORMER IAW MM 33-12-0, PERFORMED OPERATIONAL CHECK IAW MMFeb 27, 2002 · N810BN · Doug DC862 · Flight Compartment LightingSDR IXXA0200031SWing · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED AROUND SCREW HEADS ON THE LEFT WING OUTBOARD LEADING EDGE XFS892 TO XFS930. REPAIR ACCOMPLISHED REMOVAL OF THE CORROSION, FABRICATION AND INSTALLATION OF AN EXTERNAL REPAIR DOUBLER IN ACCORDANCE WITH TFeb 26, 2002 · N799AL · Doug DC862 · Wing StructureSDR ARWA20020207Compressor · stalledUPON COMMENCING T/O ROLL NR 2 ENGINE COMPRESSOR STALLED SPEED NIL WIND CALM. AIRCRAFT RETURNED TO THE RAMP. PERFORMED VISUAL INSPECTION OF NR 2 ENGINE IN ACCORDANCE WITH 71-00, OPS CHECKED FOUND NORMAL ON GROUND RUN UP.Feb 26, 2002 · N1808E · Doug DC862 · Turbine Engine Compressor SectionSDR IXXA0200030SWing · corrodedDURING ROUTINE C-CHECK INSPECTION CORROSION WAS DETECTED AROUND THREE SCREW HOLES ON THE LEFT WING OUTBOARD LEADING EDGE AT STATION XFS 885. REPAIR ACCOMPLISHED, REMOVAL OF THE CORROSION, FACRICATION AND INSTALLATION OF AN EXTERNAL REPAIR DOUBLER IN ACCORDANCFeb 25, 2002 · N799AL · Doug DC862 · Wing StructureSDR IXXA0200029SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED AROUND THE HI-LOK HEAD ON THE LEFT WING UPPER LEADING EDGE APPROXIMATELY 21 INCHES OUTBOARD OF THE NR 2 PYLON. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF REPAIR DOUBLFeb 24, 2002 · N799AL · Doug DC862 · Wing, Plate/SkinSDR ARWA20020203Fitting · crackedDURING C-CHECK, RIGHT WING NR 4 ALTERNATE FUEL TANK INTERIOR S-58 END FITTING WITH 1 INCH CRACK AT STA XRS 408.00.Feb 4, 2002 · N802BN · Doug DC862 · Wing Miscellaneous StructureSDR ARWA20020202Fitting · crackedDURING C-CHECK, LT WING NR 1 ALTERNATE FUEL TANK INTERIOR S-57 END FITTING WITH 1 INCH CRACK STA XRS 408.00. REMOVED AND REPLACED STRINGER END FITTINGS IAW DC-8 SRM 51-1-20D.Feb 4, 2002 · N802BN · Doug DC862 · Wing Miscellaneous StructureSDR ARWA20020111Proximity Switch · malfunctionedWITH LANDING GEAR HANDLE IN DOWN POSITION ALL THREE GREEN LANDING GEAR LIGHTS CAME ON AND DOOR RED LIGHT STAYED ON AND LANDING GEAR UNSAFE LIGHT STAYED ON. ALSO, WITH FLAPS AT 35 POSITION UNSAFE WARNING HORN CAME ON. REMOVED AND REPLACED LT DOOR PROXIMITY SWJan 18, 2002 · N8968U · Doug DC862 · Landing Gear Position and WarningSDR ARWA20020108Diffuser · damagedNR 4 ENGINE SHUT DOWN IN FLIGHT DUE TO FIRE WARNING, POST FLIGHT INSPECTION FOUND 4 INCH HOLE BURNED IN DIFFUSER CASE. AIRCRAFT FERRY FLIGHT TO SINGAPORE. REMOVED AND REPLACED NR 4 ENGINE. PERFORMED ENGINE RUN. ALL PARAMETERS NORMAL. AIRCRAFT RETURNED TO SERJan 6, 2002 · N8968U · Doug DC862 · Turbine Engine Compressor SectionSDR ARWA20020106Landing Gear · vibrationNOSE GEAR VIBRATION FELT AFTER LANDING.Jan 5, 2002 · N8968U · Doug DC862 · Nose/Tail Landing GearSDR ARWA20020105ValveLOG PAGE 108167. DISCREPANCY:ON ATART UP WHEN # 2 ENGINE THROTTLE IS ADVANCED ENGINE SURGES AND VIBRATES. WHEN REVERSE IS SELECTED TR TRANSLATES AND BUCKET DEPLOYS BUT ENGINE DOES NOT ACCELERATE IN REVERSE. CORRECTIVE ACTION: REMOVED AND REPLACED #2 ENGINE SURJan 5, 2002 · N1808E · Doug DC862 · Compressor Bleed ValveSDR ARWA20020104Switch · brokenWHILE STARTING ENGINE NR 4 STARTER SWITCH BROKE. REMOVED AND REPLACED NR 4 ENGINE STARTER SWITCH IAW MM 20-50-01. OPS CHECK ON ENGINE IDLE RUN UP IAW 71-00 FOUND NORMAL. AIRCRAFT RETURNED TO SERVICE.Jan 4, 2002 · N810BN · Doug DC862 · Engine CrankingSDR ARWA20020101Line · looseUNABLE TO PRESSURIZE AFTER TAKEOFF. GROUND CHECK OK. AIRCRAFT RETURNED TO DNA AND LANDED UNEVENTFUL. FOUND LOOSE LINE AT RT FLOW CONTROL VALVE, TIGHTENED IAW NASI SYSTEM STC ST466CH, OPS CHECKED FOUND NORMAL. AIRCRAFT RETURN TO SERVICE.Jan 1, 2002 · N8968U · Doug DC862 · Cabin Pressure Control SystemSDR ARWA20011213Hydraulic Line · leakingLOSS OF HYDRAULIC FLUID DURING LANDING ROLL IN SKBO. COMPLETED ABNORMAL EMERGENCY CHECKLIST, LEAK STOPPED. TAXIED UNEVENTFUL TO CARGO RAMP. T/S AND FOUND STANDBY RUDDER ACCUMULATOR PRESSURE HYDRAULIC HOSE TO PUMP LEAKING. REMOVED AND REPLACED HIGH PRESSURE Dec 27, 2001 · N810BN · Doug DC862 · Hydraulic System, MainSDR ARWA20011212Bleed Valve · lack of lubeNR 3 ENGINE COMPRESSOR STALL AT BRAKE RELEASE MAX POWER 1.89 EPR RETURN TO RAMP FOR CKV & FOR NOTE 13 DEGREE CELSIUS ENGINE ANTI ICE OFF AND NO WIND. LUBED SURGE BLEED VALVE IAW MM 75-30-3, SYSTEM OPS CKD NORMAL IAW MM 71-00 ENGINE RUN. AIRCRAFT RETURNED TO Dec 23, 2001 · N802BN · Doug DC862 · Compressor Bleed ValveSDR ARWA20011211Fitting · excess playDEPARTING KATL, GEAR NOT LATCHED LIGHT ILLUMINATED. ABNORMAL CHECKLIST COMPLETED AND LIGHT DID NOT EXTINGUISH, AFTER EACH UPLATCH CHECK (IN UPLATCH CHECK POSITION). CORRECTED PLAY AT RIGHT MLG UPLOCK ROLLER FITTING, ALSO LUBRICATED ALL GEARS. LANDING GEAR ODec 20, 2001 · N1804 · Doug DC862 · Landing Gear Position and Warning
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