# Service difficulty reports: Douglas DC-10-40F

A list on [Douglas DC-10-40F](https://openairdocs.org/model/douglas-dc-10-40f.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 52 reports

- [SDR 22AA20090203](https://openairdocs.org/sdr/22AA20090203.md): Indicator · inoperative · Feb 22, 2009 · N141WE · Doug DC1040F · Engine Pressure Ratio (EPR)
  > TAKEOFF 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 NR
- [SDR 22AA20081003](https://openairdocs.org/sdr/22AA20081003.md): Mechanism · lack of lube · Oct 19, 2008 · N140WE · Doug DC1040F · Aileron Control System
  > UPON 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 OPERATI
- [SDR ARWA20080801](https://openairdocs.org/sdr/ARWA20080801.md): Warning System · malfunctioned · Aug 5, 2008 · N140WE · Doug DC1040F · Door Warning System
  > ATC 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)
- [SDR ARWA20080702](https://openairdocs.org/sdr/ARWA20080702.md): O-Ring · leaking · Jul 18, 2008 · N140WE · Doug DC1040F · Hydraulic System, Main
  > HYDRAULIC 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 L
- [SDR ARQA20080703](https://openairdocs.org/sdr/ARQA20080703.md): Line · leaking · Jul 18, 2008 · N140WE · Doug DC1040F · Hydraulic System, Main
  > EVIDENCE 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)
- [SDR ARWA20080603](https://openairdocs.org/sdr/ARWA20080603.md): Throttle · obstructed · Jun 22, 2008 · N140WE · Doug DC1040F · Power Lever
  > UPON 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 76-11-0
- [SDR ARWA20080503](https://openairdocs.org/sdr/ARWA20080503.md): Thermocouple · shorted · May 17, 2008 · N140WE · Doug DC1040F · Engine EGT/TIT Indicating System
  > IN 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, REMOVED
- [SDR ARWA20080502](https://openairdocs.org/sdr/ARWA20080502.md): Indicator · faulty · May 17, 2008 · N140WE · Doug DC1040F · Engine EGT/TIT Indicating System
  > IN 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.
- [SDR ARWA20070801](https://openairdocs.org/sdr/ARWA20070801.md): Door · damaged · Aug 3, 2007 · N140WE · Doug DC1040F · Landing Gear Doors
  > AFTER 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;
- [SDR ARWA20070603](https://openairdocs.org/sdr/ARWA20070603.md): Valve · unknown · Jun 6, 2007 · N140WE · Doug DC1040F · Engine Oil Indicating System
  > 3 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.
- [SDR ARWA20070307](https://openairdocs.org/sdr/ARWA20070307.md): Connector · loose · Mar 23, 2007 · N140WE · Doug DC1040F · Engine Exhaust System Wiring
  > ON 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 SYSTEM
- [SDR ARWA20070305](https://openairdocs.org/sdr/ARWA20070305.md): Cable · broken · Mar 22, 2007 · N140WE · Doug DC1040F · Engine Thrust Reverser
  > ON 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 NORM
- [SDR ARWA20061002](https://openairdocs.org/sdr/ARWA20061002.md): Line · damaged · Oct 12, 2006 · N140WE · Doug DC1040F · Engine Indicating System
  > IN 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 77-1
- [SDR CLC2005F00003](https://openairdocs.org/sdr/CLC2005F00003.md): Control Cable · corroded · Jul 21, 2005 · N140WE · Doug DC1040F · Rudder Control System
  > DURING 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
- [SDR CLC2005F00007](https://openairdocs.org/sdr/CLC2005F00007.md): Ring · damaged · Jul 11, 2005 · N140WE · Doug DC1040F · Engine Air Intake System
  > DURING 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 SEA
- [SDR CLC2005F00006](https://openairdocs.org/sdr/CLC2005F00006.md): Inlet · damaged · Jul 11, 2005 · N140WE · Doug DC1040F · Engine Air Intake System
  > DURING 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
- [SDR CLC2005F00005](https://openairdocs.org/sdr/CLC2005F00005.md): Seal · damaged · Jul 11, 2005 · N140WE · Doug DC1040F · Engine Air Intake System
  > DURING 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. I
- [SDR CLC2005F00004](https://openairdocs.org/sdr/CLC2005F00004.md): Adapter Ring · damaged · Jul 11, 2005 · N140WE · Doug DC1040F · Engine Air Intake System
  > DURING 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 SEA
- [SDR CLC2006F00006](https://openairdocs.org/sdr/CLC2006F00006.md): Window Frame · out of adjust · Jul 28, 2004 · N140WE · Doug DC1040F · Escape Slide
  > R1 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)
- [SDR 2004F00201](https://openairdocs.org/sdr/2004F00201.md): Pin · sheared · Apr 29, 2004 · N140WE · Doug DC1040F · Stabilizer Control System
  > HORIZONTAL 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 CHECKS
- [SDR 2003F00115](https://openairdocs.org/sdr/2003F00115.md): Cowling · delaminated · Dec 4, 2002 · N141WE · Doug DC1040F · Engine Cowling System
  > DURING 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)
- [SDR 2003F00088](https://openairdocs.org/sdr/2003F00088.md): Wedge · damaged · Nov 8, 2002 · N140WE · Doug DC1040F · Trailing Edge Flaps
  > DURING 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)
- [SDR 2003F00089](https://openairdocs.org/sdr/2003F00089.md): Thrust Reverser · debonded · Nov 3, 2002 · N141WE · Doug DC1040F · Engine Thrust Reverser
  > DURING 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)
- [SDR 2002F00629](https://openairdocs.org/sdr/2002F00629.md): Hydraulic System · malfunctioned · Apr 27, 2002 · N141WE · Doug DC1040F · Hydraulic System, Main
  > FLT 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.
- [SDR 2002F00334](https://openairdocs.org/sdr/2002F00334.md): Thrust Reverser · damaged · Dec 1, 2001 · N141WE · Doug DC1040F · Engine Collector/Tailpipe/Nozzle
  > DURING 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)
- [SDR 2002F00333](https://openairdocs.org/sdr/2002F00333.md): Structure · corroded · Dec 1, 2001 · N141WE · Doug DC1040F · Fuselage Main, Structure
  > DURING 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 REVEN
- [SDR 2002F00332](https://openairdocs.org/sdr/2002F00332.md): Longeron · cracked · Dec 1, 2001 · N141WE · Doug DC1040F · Fuselage Main, Longeron/Stringer
  > DURING 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)
- [SDR 2002F00331](https://openairdocs.org/sdr/2002F00331.md): Structure · corroded · Dec 1, 2001 · N141WE · Doug DC1040F · Fuselage Main, Structure
  > DURING 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)
- [SDR 2002F00330](https://openairdocs.org/sdr/2002F00330.md): Thrust Reverser · damaged · Dec 1, 2001 · N141WE · Doug DC1040F · Engine Thrust Reverser
  > DURING 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 SERVI
- [SDR 2002F00318](https://openairdocs.org/sdr/2002F00318.md): Angle · corroded · Dec 1, 2001 · N141WE · Doug DC1040F · Fuselage Miscellaneous Structure
  > DURING 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 WAS
- [SDR 2002F00317](https://openairdocs.org/sdr/2002F00317.md): Longeron · cracked · Dec 1, 2001 · N141WE · Doug DC1040F · Fuselage Main, Longeron/Stringer
  > DURING 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 RETURN
- [SDR 2002F00316](https://openairdocs.org/sdr/2002F00316.md): Frame · corroded · Dec 1, 2001 · N141WE · Doug DC1040F · Fuselage Main, Frame
  > DURING 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
- [SDR 2002F00025](https://openairdocs.org/sdr/2002F00025.md): Frame · corroded · Dec 1, 2001 · N141WE · Doug DC1040F · Fuselage Main, Frame
  > DURING 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)
- [SDR 2002F00024](https://openairdocs.org/sdr/2002F00024.md): Longeron · cracked · Dec 1, 2001 · N141WE · Doug DC1040F · Fuselage Main, Longeron/Stringer
  > DURING 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)
- [SDR 2002F00023](https://openairdocs.org/sdr/2002F00023.md): Angle · corroded · Dec 1, 2001 · N141WE · Doug DC1040F · Fuselage Miscellaneous Structure
  > DURING 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 AIRCRAF
- [SDR 2002F00022](https://openairdocs.org/sdr/2002F00022.md): Thrust Reverser · damaged · Dec 1, 2001 · N141WE · Doug DC1040F · Engine Thrust Reverser
  > DURING 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)
- [SDR 2002F00021](https://openairdocs.org/sdr/2002F00021.md): Frame · corroded · Dec 1, 2001 · N141WE · Doug DC1040F · Fuselage Main, Frame
  > DURING 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)
- [SDR 2002F00020](https://openairdocs.org/sdr/2002F00020.md): Longeron · cracked · Dec 1, 2001 · N141WE · Doug DC1040F · Fuselage Main, Longeron/Stringer
  > DURING 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)
- [SDR 2002F00019](https://openairdocs.org/sdr/2002F00019.md): Skin · corroded · Dec 1, 2001 · N141WE · Doug DC1040F · Fuselage Main, Plate/Skin
  > DURING 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 AIRCRAF
- [SDR 2002F00018](https://openairdocs.org/sdr/2002F00018.md): Thrust Reverser · damaged · Dec 1, 2001 · N141WE · Doug DC1040F · Engine Thrust Reverser
  > DURING 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)
- [SDR 2001F00421](https://openairdocs.org/sdr/2001F00421.md): Skin · chafed · Jun 11, 2001 · N140WE · Doug DC1040F · Trailing Edge Flaps
  > DURING 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)
- [SDR 2001F00420](https://openairdocs.org/sdr/2001F00420.md): Panel · corroded · Jun 11, 2001 · N140WE · Doug DC1040F · Engine Thrust Reverser
  > DURING 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)
- [SDR 2001F00419](https://openairdocs.org/sdr/2001F00419.md): Door Frame · corroded · Jun 11, 2001 · N140WE · Doug DC1040F · Fuselage Main, Structure
  > DURING 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)
- [SDR 2001F00418](https://openairdocs.org/sdr/2001F00418.md): Flap · corroded · Jun 11, 2001 · N140WE · Doug DC1040F · Trailing Edge Flaps
  > DURING 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 AND
- [SDR 2001F00417](https://openairdocs.org/sdr/2001F00417.md): Spar Cap · corroded · Jun 11, 2001 · N140WE · Doug DC1040F · Wing Spar
  > DURING 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)
- [SDR 2001F00416](https://openairdocs.org/sdr/2001F00416.md): Rib · corroded · Jun 11, 2001 · N140WE · Doug DC1040F · Trailing Edge Flaps
  > DURING 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
- [SDR 2001F00415](https://openairdocs.org/sdr/2001F00415.md): Rib · cracked · Jun 11, 2001 · N140WE · Doug DC1040F · Leading Edge Devices
  > DURING 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)
- [SDR 20010126SG001](https://openairdocs.org/sdr/20010126SG001.md): Pin · sheared · Dec 28, 2000 · N140WE · Doug DC1040F · Stabilizer Control System
  > FLT 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)
- [SDR 20000630AP001](https://openairdocs.org/sdr/20000630AP001.md): Flange · corroded · Mar 25, 2000 · N140WE · Doug DC1040F · Wing Miscellaneous Structure
  > DURING 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 ISS
- [SDR 2000ZZZX214](https://openairdocs.org/sdr/2000ZZZX214.md): Oil Cap · missing · Sep 30, 1999 · N140WE · Doug DC1040F · Engine Oil Storage (Airframe Furnished)
  > KMIA/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. FOUND

Next page: https://openairdocs.org/model/douglas-dc-10-40f/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/model/douglas-dc-10-40f/reports

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