Douglas DC-10-40F

Service difficulty reports · 52

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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 = 'DC1040F'
  ORDER BY difficulty_date DESC"

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SDR 22AA20090203Indicator · inoperativeTAKEOFF ABORTED FROM MHLM AT 110 KTS. ON TAKEOFF ROLL ENGINE NR 2 EPR GAUGE FAILED AT 1.20 EPR. POINTER AND ANALOG DIGITS FAILED IN PLACED WITH NO FLAG IN VIEW. TRANSFERRED TO DMI 22467, PLACARD INSTALLED, PER MEL 77-3-2, PAGE 77-2. REMOVED AND REPLACED NRFeb 22, 2009 · N141WE · Doug DC1040F · Engine Pressure Ratio (EPR)SDR 22AA20081003Mechanism · lack of lubeUPON RETRACTING FLAPS 2 1/2 UNITS OF AILERON TRIM TO THE RT MUST BE USED TO KEEP WINGS LEVEL. PERFORMED AILERONS SYSTEM TEST IN ACCORDANCE WITH M/M 27-10-00. FOUND NORMAL, FLAP SYSTEM TEST IN ACCORDANCE WITH M/M 27-50-00. FOUND NORMAL SPOILER SYSTEM OPERATIOct 19, 2008 · N140WE · Doug DC1040F · Aileron Control SystemSDR ARWA20080801Warning System · malfunctionedATC REPORT FOR DOOR OPEN ON ACFT. RETURN TO RAMP. INSPECTED ACFT. FOUND NO DOOR OPEN, NORMAL CONDITION IAW WITH MM 52-00-00. ALL CLOSED AND LIGHT OFF. (S)Aug 5, 2008 · N140WE · Doug DC1040F · Door Warning SystemSDR ARWA20080702O-Ring · leakingHYDRAULIC SYSTEM QTY STARTED TO DROP AT OP OF DESCENT. PERFORMED THE HYD QTY LOSS ALTERATIVE. OPS CHECKLIST. FLUID LOSS CONTINUED. PERFORMED SINGLE HYD SYS FAILURE ABNORMAL CHECKLIST, PERFORMED AT 50 FLAP NORMAL CONFIGURATION, FLT LANDED UNEVENTFUL AFTER LJul 18, 2008 · N140WE · Doug DC1040F · Hydraulic System, MainSDR ARQA20080703Line · leakingEVIDENCE OF HYDRAULIC LEAK LT HAND WHEEL WB 11. REPAIRED SECTION OF HYDRAULIC LINE DAMAGED, USING TYPE 3 REPAIRED IN ACCORDANCE WITH DC10-MM 20-10-01. LEAK CHECK FOUND NORMAL. (A)Jul 18, 2008 · N140WE · Doug DC1040F · Hydraulic System, MainSDR ARWA20080603Throttle · obstructedUPON INITIATION OF TAKEOFF ROLL NR 3 POWER LEVER WOULD NOT ADVANCE BEYOND 128 EPR. RETURNED TO RAMP. OPENED ENGINE FOUND HYD TEMP C/P WIRE AROUND THROTTLE BELL CRANK BEHIND HYD FILTER MODULE. SECURED WIRE IAW M/M 20-30-07. OPS CHECK THROTTLE IAW MM 76-11-0Jun 22, 2008 · N140WE · Doug DC1040F · Power LeverSDR ARWA20080503Thermocouple · shortedIN FLIGHT NR 2 ENGINE EGT INDICATOR FLUCTUATING 20 TO 30 DEGREES BOTH POINTER AND COUNTER, ALL OTHER PARAMETERS NORMAL. TROUBLE SHOT IN ACCORDANCE WITH TAFY MANUAL 77-21-00, FOUND THERMO COUPLE SHORTED AT 6 O'CLOCK POSITION AND HARNESS ISOLATION HIGH, REMOVEDMay 17, 2008 · N140WE · Doug DC1040F · Engine EGT/TIT Indicating SystemSDR ARWA20080502Indicator · faultyIN FLIGHT NR 2 ENGINE EGT INDICATOR FLUCTUATING 20 TO 30 DEGREES BOTH POINTER AND COUNTER ALL OTHER PARAMETERS NORMAL. REMOVED AND REPLACED NR 2 EGT INDICATOR CHECK GOOD IN ACCORDANCE WITH M/M 77-21-00 AND M/M 71-00-00.May 17, 2008 · N140WE · Doug DC1040F · Engine EGT/TIT Indicating SystemSDR ARWA20070801Door · damagedAFTER GEAR RETRACTION RED LEFT LGD GEAR LIGHT ON FWD AND F/E PANELS REMAINED ON. PERFORMED THE APPROPRIATE CHECK-LIST AND RETURN TO LANDING AFTER DUMPING FUEL TO MAX LANDING WEIGHT. REMOVED AND REPLACED MAIN LANDING GEAR DOOR IN ACCORDANCE WITH M/M 32-14-01;Aug 3, 2007 · N140WE · Doug DC1040F · Landing Gear DoorsSDR ARWA20070603Valve · unknown3 IDLE OIL PRESSURE 23 PSI. REMOVED AND REPLACED NR 3 ENGINE OIL PRESSURE FILTER ADJUSTED OIL PRESSURE RELIEF VALVE IN ACCORDANCE WITH DC-10 M/M 71-00-01. PERFORMED ENGINE RUN OPERATIONAL NORMAL IN ACCORDANCE WITH 71-00-00.Jun 6, 2007 · N140WE · Doug DC1040F · Engine Oil Indicating SystemSDR ARWA20070307Connector · looseON ROTATION, NR 1 ENGINE REVERSER UNLOCK LIGHT CAME ON AND REMAINED ON; SHUT ENGINE DOWN AND RETURNED TO MIAMI. PERFORMED ELECTRICAL SYSTEM CHECK AND FOUND LOOSE CONNECTOR AT PRESSURE REG. S/O VALVE FROM PDM. TIGHTENED AND SECURED AS REQUIRED. NEEDS SYSTEMMar 23, 2007 · N140WE · Doug DC1040F · Engine Exhaust System WiringSDR ARWA20070305Cable · brokenON TAKEOFF ROLL, NR 2 ENGINE REVERSER UNLOCK LIGHT CAME ON. ABORTED TAKEOFF AS SOON AS THROTTLES WERE ADVANCED. DEACTIVATED NR 2 ENGINE THRUST REVERSER AS PER MEL 78-1 (DDG) AFTER DEACTIVATION COMPLETED; CHECKED AT BLAST FENCE, VERIFIED SYSTEM AND FOUND NORMMar 22, 2007 · N140WE · Doug DC1040F · Engine Thrust ReverserSDR ARWA20061002Line · damagedIN CRUISE FLIGHT TO MAINTAIN NR 1 ENGINE N1 ALIGNMENT WITH ALL OTHER ENGINES N1 NR 1 EPR INDICATING 1.15 NR 2 EPR 1.32 AND NR 3 EPR 1.32 ALL N2 ALIGNED. PERFORMED NR 1 CHECK AND CHECKED PT7, 4 SENSE AIR, FOUND LINE DAMAGE; REMOVED AND REPLACED LINE IAW MM 77-1Oct 12, 2006 · N140WE · Doug DC1040F · Engine Indicating SystemSDR CLC2005F00003Control Cable · corrodedDURING PREFLIGHT, FOUND RUDDER NOSE RIGHT CABLE 2D BROKEN. FOUND RT RUDDER CONTROL CABLE 2D CORRODED AND BROKEN. REMOVED AND REPLACED RUDDER CONTROL CABLE NOSE RT 2D IAW AMM. ACCOMPLISHED RUDDER CONTROL SYSTEM OPERATIONAL, CHECK AND FOUND NORMAL. AIRCRAFT Jul 21, 2005 · N140WE · Doug DC1040F · Rudder Control SystemSDR CLC2005F00007Ring · damagedDURING PREFLIGHT CHECK, DAMAGE WAS FOUND TO NR 2 ENGINE INTAKE AND FAN BLADES. ENGINE INTAKE HAS DAMAGE TO UPPER AND LOWER BELL MOUTH ADAPTOR RINGS, INTAKE INLET LIP HAD SKIN BLOWN OUT, NUMEROUS CRACKS FOUND ALONG CIRCUMFERENCE AT ATTACH FASTENERS. INLET SEAJul 11, 2005 · N140WE · Doug DC1040F · Engine Air Intake SystemSDR CLC2005F00006Inlet · damagedDURING PREFLIGHT CHECK, DAMAGE WAS FOUND NR 2 ENGINE INTAKE AND FAN BLADES. ENG INTAKE HAS DAMAGE TO UPPER AND LWR BELL MOUTH ADAPTOR RINGS, INTAKE INLET LIP HAD SECTION OF SKIN BLOWN OUT, NUMEROUS CRACKS FOUND ALONG CIRCUMFERENCE AT ATTACH FASTENERS. INLET Jul 11, 2005 · N140WE · Doug DC1040F · Engine Air Intake SystemSDR CLC2005F00005Seal · damagedDURING PREFLIGHT CHECK, DAMAGE WAS FOUND TO NR 2 ENGINE INTAKE AND FAN BLADES. ENGINE INTAKE HAS DAMAGE TO UPPER AND LWR BELLMOUTH ADAPTOR RINGS, INTAKE INLET LIP HAD SECTION OF SKIN BLOWN OUT, NUMEROUS CRACKS FOUND ALONG CIRCUMFERENCE AT ATTACH FASTENERS. IJul 11, 2005 · N140WE · Doug DC1040F · Engine Air Intake SystemSDR CLC2005F00004Adapter Ring · damagedDURING PREFLIGHT CHECK, DAMAGE WAS FOUND TO NR 2 ENGINE INTAKE AND FAN BLADES. ENGINE INTAKE HAS DAMAGE TO UPPER AND LOWER BELL MOUTH ADAPTOR RINGS, INTAKE INLET LIP HAD SKIN BLOWN OUT, NUMEROUS CRACKS FOUND ALONG CIRCUMFERENCE AT ATTACH FASTENERS. INLET SEAJul 11, 2005 · N140WE · Doug DC1040F · Engine Air Intake SystemSDR CLC2006F00006Window Frame · out of adjustR1 DOOR WILL NOT DISARM, WHILE TROUBLESHOOTING THE DOOR THE SLIDE DEPLOYED. FOUND VIEW WINDOW FRAME FOR THE ARMED LEVER BINDING. REPOSITIONED VIEW WINDOW FRAME, REPLACED SLIDE, FUNCTIONAL CHECKED NORMAL. AIRCRAFT RETURNED TO REVENUE SERVICE. (K)Jul 28, 2004 · N140WE · Doug DC1040F · Escape SlideSDR 2004F00201Pin · shearedHORIZONTAL STABILIZER JAMMED AT APPROXIMATELY 1.5 ANU DURING CRUISE. ABNORMAL PROCEDURES COMPLIED WITH FOR LANDING. LANDING AT DESTINATION UNEVENTFL. FOUND SHEAR PIN SHEARED ON HORIZ STAB DRIVE UNIT. REPLACED HORIZ STAB CHAIN DRIVE UNIT, OPERATIONAL CHECKSApr 29, 2004 · N140WE · Doug DC1040F · Stabilizer Control SystemSDR 2003F00115Cowling · delaminatedDURING SCHEDULED MAINTENANCE, NR 1 FAN COWL PREVIOUS REPAIR WAS FOUND DELAMINATED ON THE INBOARD LOWER CORNER. REPAIRED IAW AS11 DRAWING AS11476, DOUBLER REPAIR. AIRCRAFT RETURNED TO SERVICE. (M)Dec 4, 2002 · N141WE · Doug DC1040F · Engine Cowling SystemSDR 2003F00088Wedge · damagedDURING ROUTINE MAINTENANCE, THE LEFT WING OUTBOARD FLAP INBOARD TRAILING EDGE WEDGE WAS FOUND DAMAGED. ACCOMPLISHED REPAIR IAW AS11 DRAWING AS11467, AND 8110-3 WAS ISSUED. RETURNED AIRCRAFT TO REVENUE SERVICE. (M)Nov 8, 2002 · N140WE · Doug DC1040F · Trailing Edge FlapsSDR 2003F00089Thrust Reverser · debondedDURING ROUTINE MAINTENANCE, THE NR 2 ENGINE THRUST REVERSER INNER SURFACE WAS FOUND DEBONDED. REMOVED DEBONDED AREA, FABRICATED DOUBLER REPAIR AND REPAIRED AREA IAW AS11 DRAWING AS11465, AND AN 8110-3 WAS ISSUED. RETURNED AIRCRAFT TO REVENUE SERVICE. (M)Nov 3, 2002 · N141WE · Doug DC1040F · Engine Thrust ReverserSDR 2002F00629Hydraulic System · malfunctionedFLT 558 - MSLP-KMIA - DURING CLIMB-OUT, LOST HYDRAULIC SYSTEMS ONE AND TWO. RETURNED TO MSLP AND A NORMAL LANDING WITHOUT INCIDENT WAS MADE. NR 1 TIRE MISSING A LARGE SECTION OF TREAD, NR 5 TIRE DAMAGED BY GROUND DEBRIS. BOTH NR 1 AND 5 WHEELS WERE INTACT. Apr 27, 2002 · N141WE · Doug DC1040F · Hydraulic System, MainSDR 2002F00334Thrust Reverser · damagedDURING C-CHECK, THE NR 2 ENGINE THRUST REVERSER LEFT COWL SKIN WAS FOUND DAMAGED ON LEADING EDGE. A DOUBLER WAS INSTALLED IAW REO-G08284. THE AIRCRAFT WAS RETURNED TO REVENUE SERVICE. (M)Dec 1, 2001 · N141WE · Doug DC1040F · Engine Collector/Tailpipe/NozzleSDR 2002F00333Structure · corrodedDURING C-CHECK, THE FORWARD LT AIR CONDITIONING BAY CAP ANGLE AT STATION 595 BETWEEN LONGERON 47L AND 48L WAS CORRODED PAST SRM LIMITS. A REPAIR DOUBLER WAS INSTALLED ON THE EXTERIOR OF THE SKIN TO REINFORCE THE BLEND AREA. THE AIRCRAFT WAS RETURNED TO REVENDec 1, 2001 · N141WE · Doug DC1040F · Fuselage Main, StructureSDR 2002F00332Longeron · crackedDURING C-CHECK, LONGERON 13L WAS FOUND CRACKED BETWEEN FASTENER HOLES AT CANTED STATION Y2153. LONGERON 13L WAS REPAIRED. THE AIRCRAFT WAS RETURNED TO REVENUE SERVICE. (M)Dec 1, 2001 · N141WE · Doug DC1040F · Fuselage Main, Longeron/StringerSDR 2002F00331Structure · corrodedDURING C-CHECK, THE LEFT NOSE WHEEL WELL CHORD VERTICAL LEG WAS FOUND CORRODED AND BLENDED JUST PAST SRM REPAIRABLE LIMITS. A REPAIR ANGLE WAS INSTALLED IAW TIMCO REO-G08344 REV IR AND REO G8336 REV IR. THE AIRCRAFT WAS RETURNED TO REVENUE SERVICE. (M)Dec 1, 2001 · N141WE · Doug DC1040F · Fuselage Main, StructureSDR 2002F00330Thrust Reverser · damagedDURING C-CHECK, THE NR 2 ENGINE THRUST REVERSER LEFT COWL SKIN WAS FOUND DAMAGED ON LEADING EDGE. A DOUBLER WAS INSTALLED IAW REO-G08284 AND A 8110-3 WAS ISSUED, DER DERT-511032-CE FAR 145 REPAIR AGENCY NR TIPR833K. THE AIRCRAFT WAS RETURNED TO REVENUE SERVIDec 1, 2001 · N141WE · Doug DC1040F · Engine Thrust ReverserSDR 2002F00318Angle · corrodedDURING C-CHECK, THE FORWARD LEFT AIRCONDITIONING BAY CAP ANGLE AT STATION 595 BETWEEN LONGERON 47L AND 48L WAS CORRODED PAST SRM LIMITS. A REPAIR DOUBLER WAS INSTALLED ON THE EXTERIOR OF THE SKIN TO REINFORCE THE BLEND AREA IAW TIMCO REO-GO8333. A 8110-3 WASDec 1, 2001 · N141WE · Doug DC1040F · Fuselage Miscellaneous StructureSDR 2002F00317Longeron · crackedDURING C-CHECK, LONGERON 13L WAS FOUND CRACKED BETWEEN FASTENER HOLES AT CANTED STATION Y2153. LONGERON 13L WAS REPAIRED IAW TIMCO REO-GO8321 REV IR AND FAA FORM 8110-3 WAS ISSUED DER DERY 510314-CE FAR 145 REPAIR AGENCY NR TIPR833K. THE AIRCRAFT WAS RETURNDec 1, 2001 · N141WE · Doug DC1040F · Fuselage Main, Longeron/StringerSDR 2002F00316Frame · corrodedDURING C-CHECK, THE LT NOSE WHEEL WELL CHORD VERTICAL LEG WAS FOUND CORRODED AND BLENDED JUST PAST SRM REPAIRABLE LIMITS. A REPAIR ANGLE WAS INSTALLED IAW TIMCO REO-GO8344 REV IR AND REO G8336 REV IR A 8110-3 WAS ISSUED BY DER, DERY 510314-CE FAR 145 REPAIR Dec 1, 2001 · N141WE · Doug DC1040F · Fuselage Main, FrameSDR 2002F00025Frame · corrodedDURING C-CHECK, THE LEFT NOSE WHEEL WELL CHORD VERTICAL LEG WAS FOUND CORRODED AND BLENDED JUST PAST SRM REPAIRABLE LIMITS. A REPAIR ANGLE WAS INSTALLED IAW TIMCO REO-G08344 REV IR AND REO G8336 REV IR. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Dec 1, 2001 · N141WE · Doug DC1040F · Fuselage Main, FrameSDR 2002F00024Longeron · crackedDURING C-CHECK, LONGERON 13L WAS FOUND CRACKED BETWEEN FASTENER HOLES AT CANTED STATION Y2153. LONGERON 13L WAS REPAIRED IAW TIMCO REO-GO8321 REV IR AND FAA FORM 8110-3. THE AIRCRAFT WAS RETURNED TO REVENUE SERVICE. (M)Dec 1, 2001 · N141WE · Doug DC1040F · Fuselage Main, Longeron/StringerSDR 2002F00023Angle · corrodedDURING C-CHECK, THE FORWARD LEFT AIR CONDITIONING BAY CAP ANGLE AT STATION 595 BETWEEN LONGERON 47L AND 48L WAS CORRODED PAST SRM LIMITS. A REPAIR DOUBLER WAS INSTALLED ON THE EXTERIOR OF THE SKIN TO REINFORCE THE BLEND AREA IAW TIMCO REO-G08333. THE AIRCRAFDec 1, 2001 · N141WE · Doug DC1040F · Fuselage Miscellaneous StructureSDR 2002F00022Thrust Reverser · damagedDURING C-CHECK, THE NR 2 ENGINE THRUST REVERSER LEFT COWL SKIN WAS FOUND DAMAGED ON LEADING EDGE. A DOUBLER WAS INSTALLED IAW REO-G08284 AND A 8110-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Dec 1, 2001 · N141WE · Doug DC1040F · Engine Thrust ReverserSDR 2002F00021Frame · corrodedDURING C-CHECK, THE LEFT NOSE WHEEL WELL CHORD VERTICAL LEG WAS FOUND CORRODED AND BLENDED JUST PAST SRM REPAIRABLE LIMITS. A REPAIR ANGLE WAS INSTALLED IAW TIMCO REO-G08344 REV IR AND REO G8336 REV IR. THE AIRCRAFT WAS RETURNED TO REVENUE SERVICE. (M)Dec 1, 2001 · N141WE · Doug DC1040F · Fuselage Main, FrameSDR 2002F00020Longeron · crackedDURING C-CHECK, FOUND LONGERON 13L WAS FOUND CRACKED BETWEEN FASTENER HOLES AT CANTED STATION Y2153. LONGERON 13L WAS REPAIRED IAW TIMCO REO-G08321 REV IR AND FAA FORM 8110-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Dec 1, 2001 · N141WE · Doug DC1040F · Fuselage Main, Longeron/StringerSDR 2002F00019Skin · corrodedDURING C-CHECK, THE FORWARD LEFT AIR CONDITIONING BAY CAP ANGLE AT STATION 595 BETWEEN LONGERON 47L AND 47L WAS CORRODED PAST SRM LIMITS. A REPAIR DOUBLER WAS INSTALLED ON THE EXTERIOR OF THE SKIN TO REINFORCE THE BLEND AREA IAW TIMCO REO-G08333. THE AIRCRAFDec 1, 2001 · N141WE · Doug DC1040F · Fuselage Main, Plate/SkinSDR 2002F00018Thrust Reverser · damagedDURING C-CHECK, THE NR 2 ENGINE THRUST REVERSER LEFT COWL SKIN AS FOUND DAMAGED ON LEADING EDGE. A DOUBLER WAS INSTALLED IAW REO-GO8284 AND A 8110-3 WAS ISSUED. THE AIRCRAFT WAS RETURNED TO REVENUE SERVICE. (M)Dec 1, 2001 · N141WE · Doug DC1040F · Engine Thrust ReverserSDR 2001F00421Skin · chafedDURING C-CHECK, FOUND RIGHT OUTBOARD FLAP UPPER SKIN WAS FOUND CHAFED NEAR STATION XOF 759. REPAIRED CHAFED SKIN ON RIGHT OUTBOARD FLAP UPPER SKIN NEAR STATION XOF 759 IAW EA NR 10-5753-24-A0859. AIRCRAFT WAS RETURNED TO SERVICE. (M)Jun 11, 2001 · N140WE · Doug DC1040F · Trailing Edge FlapsSDR 2001F00420Panel · corrodedDURING C-CHECK, FOUND CORROSION ON THE NR 3 ENGINE OUTBOARD THRUST REVERSER INTERNAL SKIN ACOUSTICAL PANEL. CORROSION WAS REMOVED AND THE PANEL WAS REPAIRED IAW AIRBORNE NACELLE ENGINEERING REPAIR ORDER ANS-DC10-R0010. AIRCRAFT WAS RETURNED TO SERVICE. (M)Jun 11, 2001 · N140WE · Doug DC1040F · Engine Thrust ReverserSDR 2001F00419Door Frame · corrodedDURING C-CHECK, FOUND CORROSION ON THE LOWER FORWARD END OF THE FORWARD CARGO DOOR JAMB FRAME AT STATION 886. CORROSION WAS REMOVED AND REPAIRED IAW EA NR 10-5316-24-A0861. AIRCRAFT WAS RETURNED TO SERVICE. (M)Jun 11, 2001 · N140WE · Doug DC1040F · Fuselage Main, StructureSDR 2001F00418Flap · corrodedDURING C-CHECK, THE RIGHT OUTBOARD FLAP OUTBOARD HINGE ATTACH POINTS HAVE HEAVY EXFOLIATION AT LOWER MOUNT BULKHEAD FITTING (VIEWED INTERNALLY). RIGHT OUTBOARD FLAP WAS REMOVED AND SENT TO OVERHAUL AT HONEYCOMB COMPOSITE SYSTEMS, THE CORROSION WAS REMOVED ANDJun 11, 2001 · N140WE · Doug DC1040F · Trailing Edge FlapsSDR 2001F00417Spar Cap · corrodedDURING C-CHECK, FOUND CORROSION IN THE NR 3 ENGINE WING SPAR FITTING BULKHEAD UPPER CAP NR 3 ATTACH HOLE. THE CORROSION WAS REMOVED AND THE UPPER CAP WAS REPAIRED IAW EA 10-5720-24-A0865. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Jun 11, 2001 · N140WE · Doug DC1040F · Wing SparSDR 2001F00416Rib · corrodedDURING C-CHECK, THE LEFT OUTBOARD FLAP HAS CORROSION BETWEEN FRONT SPAR CAP STATION 538 THROUGH 554. SURFACE CORROSION ON RIBS AT STATION 538. LEFT OUTBOARD FLAP WAS REMOVED AND SENT TO OVERHAUL AT HONEYCOMB COMPOSITE SYSTEMS, WHERE THE CORROSION WAS REMOVED Jun 11, 2001 · N140WE · Doug DC1040F · Trailing Edge FlapsSDR 2001F00415Rib · crackedDURING C-CHECK, THE RIGHT WING NR 8 SLAT RIB AT STATION XOS1158 WAS FOUND CRACKED, 12 INCHES LONG. THE CRACK WAS REPAIRED IAW EA NR 10-5755-24-A0886. AIRCRAFT WAS RETURNED TO SERVICE. (M)Jun 11, 2001 · N140WE · Doug DC1040F · Leading Edge DevicesSDR 20010126SG001Pin · shearedFLT 95 - MIA-SVMI - STABILIZER JAM FULL NOSE UP POSITION. FOUND SHEAR PIN SHEARED ON HORIZONTAL STABILIZER DRIVE UNIT. REPLACED HORIZONTAL STAB CHAIN DRIVE UNIT PER AMM 27-44-05. AIRCRAFT RETURNED TO SERVICE. (M)Dec 28, 2000 · N140WE · Doug DC1040F · Stabilizer Control SystemSDR 20000630AP001Flange · corrodedDURING C-CHECK, FOUND CORROSION ON RIGHT WING REAR SPAR UPPER CAP AT STATION XORS 562.390, UNDER THE INBOARD FLAP HINGE OF THE OUTBOARD FLAP. CORROSION WAS REMOVED AND A MAJOR REPAIR WAS MADE IAW BOEING MESSAGE DAR-FCO-00-00001E, AND A FAA FORM 8110-3 WAS ISSMar 25, 2000 · N140WE · Doug DC1040F · Wing Miscellaneous StructureSDR 2000ZZZX214Oil Cap · missingKMIA/SEQU - FLT 85 AT 17:45 Z - DISCREPANCY AFTER TAKEOFF FROM MIA, EXPERIENCED LOSS OF OIL QUANTITY, ENGINE NR 1 FROM 11 GALLONS TO SIX GALLONS WHERE IT THEN STABILIZED. RETURNED TO MIA. NO FUEL DUMPED, LANDING AT 389,000 POUNDS, LANDING UNEVENTFUL. FOUNDSep 30, 1999 · N140WE · Doug DC1040F · Engine Oil Storage (Airframe Furnished)
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