# Service difficulty reports: Aircraft Builders Assoc DC10

A list on [Aircraft Builders Assoc DC10](https://openairdocs.org/model/aircraft-builders-assoc-dc10.md).

Newest first. General aviation reporting is voluntary.

- [SDR WRLA2008072](https://openairdocs.org/sdr/WRLA2008072.md): Bolt · sheared · Aug 26, 2008 · N139WA · Doug DC10 · Fuselage Miscellaneous Structure
  > DURING C-CHECK INSPECTION FOUND 1 BOLT SHEARED AND RUSTED, AND 1 BOLT RUSTED AT RT WING ROOT FUSELAGE ANGLE. FUSELAGE STA 1371. REAMED HOLES, EDDY CURRENT INSPECTION ACCOMPLISHED, MFG AND INSTALLED TAPERED WASHERS, TREAT, PRIME, SEAL AND PAINT IAW ENGINEERIN
- [SDR 232587](https://openairdocs.org/sdr/232587.md): Housing · cracked · Mar 20, 2008 · Doug DC10 · Hydraulic System, Main
  > HOUSING IS CRACKED NEAR PRESSURE PORTS.
- [SDR CNMA20070006](https://openairdocs.org/sdr/CNMA20070006.md): Channel · corroded · Mar 18, 2007 · N270AX · Doug DC10 · Fuselage Miscellaneous Structure
  > BS 2007, RBL 20-23, CORROSION ON CHANNEL SUPPORT UNDERNEATH GALLEY. CORRODED PORTION REMOVED NEW FABRICATED M/F S2920883-12000 AND INSTALLED WITH EXISTING FASTNERS IAW SRM VOL 2 51-31-01 AND CHERRY-MAX MS 2885/6-4/08.
- [SDR 05FDEA02632](https://openairdocs.org/sdr/05FDEA02632.md): Skin · corroded · Aug 24, 2005 · N360FE · Doug DC10* · Fuselage Main, Plate/Skin
  > BARE METAL AT CIRCUMFERENTIAL STRAP BETW. L40L & L41L FS 1871. REMOVED CORROSION,FABRICATED AND INSTALLED SHIM,DOUBLER,TRIPLER AND FINGER DOUBLERS IAW DC10-10/MD10-10 SRM 51-21-01 VOL I & II,53-20-00 VOL I PG.73 FIG. 6 SHT. 3,53- 20-00 VOL.I PG. 74 FIG.
- [SDR 05FDEA01868](https://openairdocs.org/sdr/05FDEA01868.md): Bracket · cracked · Jul 9, 2005 · N313 · Doug DC10 · Wing, Center Box
  > CTR WING LOWER STRUCTURE; RT BARREL STA 1277 INTERCOSTAL PRIMARY ATTACH BRACKET CRACKED. AS MARKED. ACCESS THRU CLG OR CAC. REMOVED AND REPLACED CRACKED BRACKET P/N AYB7035-12 AS PER S.R.M. 51/00/01, 51/33/01. REF.N/R N00612
- [SDR 05FDEA01867](https://openairdocs.org/sdr/05FDEA01867.md): Bracket · cracked · Jul 9, 2005 · N313 · Doug DC10 · Wing, Center Box
  > CTR WING LOWER STRUCTURE; RT BARREL STRUCTURE STA 1237 INTERCOSTAL PRIMARY ATTACH BRACKET CRACKED THRU AS MARKED IN RED. ACCESS THRU CLG WHEEL WELL OR CAC0. REMOVED AND REPLACED CRACKED BRACKET P/N AYB7033-10 AS PER S.R.M. 51/00/01, 51/33/01, REF N/R N006
- [SDR 05FDEA00708](https://openairdocs.org/sdr/05FDEA00708.md): Hinge · corroded · Mar 30, 2005 · N10060 · Doug DC10* · Trailing Edge Flaps
  > LEFT WING INBOARD FLAP, OUTBOARD SUPPORT, PIVOT ATTACH POINT OUTBOARD BORE CORRODED. REMOVED CORROSION FROM BORE IAW DAC CMM 57-52-01. ALODINED AND PRIMED BORE IAW DC10-10 SRM 51-21-01 VOL 2, FABRICATED AND INSTALLED FINAL HONED NEW OVERSIZED BUSHING TO 0.99
- [SDR 05FDEA00706](https://openairdocs.org/sdr/05FDEA00706.md): Skin · damaged · Mar 30, 2005 · Doug DC10* · Trailing Edge Flaps
  > RIGHT WING INBOARD FLAP, INCORRECT REPAIR ON UPPER SKIN, INBOARD WEDGE. REMOVED DOUBLER, FABRICATED NEW SKIN, FINGER DOUBLERS AND DOUBLER AND BONDED IAW FEDEX EA 8- 5710-84001 AND TPS 1001 REV E AND DC10 SRM 51-21-01 VOL 2 AND DC10 SRM 51-31-01 VOL 2. REFE
- [SDR 2005FA0000383](https://openairdocs.org/sdr/2005FA0000383.md): Nose Cowl · corroded · Mar 22, 2005 · Doug DC10* · Powerplant System
  > NOSE COWL SENT TO US FOR REPAIR. DURING EVALUATION SEVERE INTERGRANULAR CORROSION WAS DISCOVERED ON THE OUTER SKIN OF THE ACOUSTIC BARREL. SUSPECT IMPROPER HEAT TREATMENT AT MFG. PART IS CONSIDERED BEYOND ECONOMICAL REPAIR AND WILL BE SCRAPPED AT THIS LOCAT
- [SDR 05FDEA00140](https://openairdocs.org/sdr/05FDEA00140.md): Frame · dented · Jan 21, 2005 · N395FE · Doug DC10 · Fuselage Main, Frame
  > STATION 322 ON LEFT SIDE OF NOSE FUSELAGE JUST BELOW COCKPIT FLOOR FRAME IS DENTED. REFERENCE NON-ROUTINE N01203. COMPLIED WITH FEDEX EA 8-5310-83962,
- [SDR 05FDEA00141](https://openairdocs.org/sdr/05FDEA00141.md): Skin · dented · Jan 21, 2005 · N395FE · Doug DC10 · Fuselage Main, Plate/Skin
  > FIRST OFFICERS PRIMARY STATIC PORT HAS EXTERNAL DOUBLER REPAIR WITHIN REDUCED VERTICAL SEPARATIONS. MINIMUN CONTROLLED AREA AT THE 9 TO 10 O'CLOCK POSITION PREVENTING REDUCED VERTICAL SEPARATION OPERATION UNDER FEDEX DC10-10 SRM 53-00-00. REPAIR WAS ACCOMPLI
- [SDR 05FDEA00139](https://openairdocs.org/sdr/05FDEA00139.md): Hinge · corroded · Jan 21, 2005 · N395FE · Doug DC10 · Trailing Edge Flaps
  > RIGHT WING INBOARD FLAP HINGE INBOARD PIVOT BUSHING GALLED AND PITTED. MEASURED BORE DIAMATER, FOUND TO BE OUT OF LIMITS IAW DAC CMM 57-52-01. ALODINE AND PRIMED BORE IAW DC10-10 SRM 51-21-01 VOL 2, FABRICATED, INSTALLED AND HONED BUSHING TO A FINAL INSIDE D
- [SDR 05FDEA00138](https://openairdocs.org/sdr/05FDEA00138.md): Hinge · corroded · Jan 21, 2005 · N395FE · Doug DC10 · Leading Edge Devices
  > LEFT WING INBOARD FLAP HINGE INBOARD PIVOT BUSHING GALLED AND PITTED. MEASURED BORE DIAMETER, FOUND TO BE OUT OF LIMITS IAW DAC CMM 57-52-01, ALODINE AND PRIMED BORE IAW DC10-10 SRM 51-21-01 VOL 2, FABRICATED, INSTALLED AND HONED BUSHING TO A FINAL INSIDE DIA
- [SDR 05FDEA00137](https://openairdocs.org/sdr/05FDEA00137.md): Balance Weight · corroded · Jan 21, 2005 · N395FE · Doug DC10 · Ailerons
  > RIGHT WING OUTBOARD AILERON 1 EACH BALANCE WEIGHT HAS CORROSION OUTBOARD SIDE OF ACTUATOR. REMOVED AND REPLACED RIGHT WING OUTBOARD AILERON BALANCE WEIGHT, BALANCE WITHIN LIMITS IAW FEDEX EA 8-5751-83957, WINGS REPLACEMENT OF CORRODED RIGHT HAND OUTBOARD AILE
- [SDR 05FDEA00136](https://openairdocs.org/sdr/05FDEA00136.md): Hinge · corroded · Jan 21, 2005 · N395FE · Doug DC10 · Trailing Edge Flaps
  > RIGHT WING INBOARD FLAP HINGE OUTBOARD PIVOT BUSHING GALLED AND PITTED. MEASURED BORE DIAMETER, FOUND TO BE OUT OF LIMITS IAW CMM 57-52-01, ALODINE AND PRIMED BORE IAW DC10-10 SRM 51-21-01. FABRICATED, INSTALLED AND HONED BUSHING TO A FINAL INSIDE DIAMETER O
- [SDR 04FDEA03413](https://openairdocs.org/sdr/04FDEA03413.md): Fitting · cracked · Dec 14, 2004 · N395FE · Doug DC10 · Fuselage Miscellaneous Structure
  > CENTER ACCESSORY COMPARTMENT AT FUSELAGE STATION 1156 LT WING BOX FITTING IS CRACKED. REMOVED INNER ATTACHED ANGLE IAW DC10 SRM 51-33-01 VIL 2, FABRICATED REPAIR PARTS AND INSTALLED REPAIR PARTS IAW DC10 SRM 51-21-01 VOL 2 AND 53-30-00 VOL 1. REINSTALLED INNE
- [SDR 04FDEA02879](https://openairdocs.org/sdr/04FDEA02879.md): Hinge · corroded · Oct 5, 2004 · N392FE · Doug DC10 · Trailing Edge Flaps
  > LT WING OB FLAP IB HINGE, LOCATION NR 6, OB BORE IS CORRODED. REMOVED CORROSION, BEGINNING BORE DIAMETER 1.240, FINAL 1.266, MATERIAL LOSS 0.026 IAW DAC CMM 57-44-08, ETCH INSPECTED IAW DAC CMM 57-44-08 AND 20-11-02. PEENED IAW DAC CMM 57-44-08 AND 20-11-01.
- [SDR 04FDEA02802](https://openairdocs.org/sdr/04FDEA02802.md): Skin · damaged · Sep 22, 2004 · N321FE · Doug DC10 · Nacelle/Pylon, Plate/Skin
  > NR 1 ENGINE IB COE COWL IS DAMAGED AT LEADING EDGE. REMOVED CORE COWL, CUT OUT DAMAGE, REMOVED FRAME AND RUBSTRIP, FABRICATED DOUBLER AND FILLER, DRILLED AND FITTED NEW FRAME AND RUBSTRIP, INSTALLED DOUBLER AND FILLER, FRAME AND RUBSTRIP IAW DC10 SRM 54-0
- [SDR 04FDEA02647](https://openairdocs.org/sdr/04FDEA02647.md): Panel · debonded · Sep 4, 2004 · Doug DC10 · Wing, Plate/Skin
  > FINGER DOUBLERS DISBONDED INSIDE LEFT WING TRAILING EDGE FAIRING BETWEEN XW 373 AND XORS 486, ACCESS THROUGH 641 MB. REMOVED ARC0584-1 SKIN FOR REPLACEMENT IAW DC10 SRM 51-35-01, 51-33-01 VOL II. FABRICATED NEW ARC0584-1 SKIN ASSEMBLY IAW DAC DWG 0584. INST
- [SDR 04FDEA02644](https://openairdocs.org/sdr/04FDEA02644.md): Pan · gouged · Sep 4, 2004 · N68058 · Doug DC10 · Nacelle/Pylon Miscellaneous Structure
  > NR 2 ENGINE RT FAN COWL INTERIOR HAS RUBBING APPROXIMATELY 8 INCHES ABOVE CENTER U-BOLT. REMOVED CENTER U-BOLT FITTING TO FOM. REMOVED DAMAGED SECTION OF PAN IAW SRM 51-35-01, VOL II. WELD REPAIRD IAW EA 8-5410-81450. INSTALLED PAN IAW SRM 51-31-01 VOL II.
- [SDR 04FDEA02348](https://openairdocs.org/sdr/04FDEA02348.md): Fitting · corroded · Aug 2, 2004 · N68058 · Doug DC10* · Fuselage Main, Attach Fittings
  > LOWER SFT WING TO CENTER BOX ATTACH SKI FITTING IS EXFOILATED. RIGHT WHEEL WELL STATION 1341 TO 1360 AT XCW 118. REMOVED ATTACHED STRUCTURE IAW DC10 SRM 51-33-01, 51-35-01 VOL II, REMOVED FITTING P/N ANB7015-2. INSTALLED NEW P/N ANB7015-2 IAW DAC DWG ANB70
- [SDR 04FDEA02345](https://openairdocs.org/sdr/04FDEA02345.md): Skin · corroded · Aug 2, 2004 · N68058 · Doug DC10* · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE UNDER WING BARREL SKIN IS CORRODED FROM STATION 1368 TO 1288 FROM LONGERON 47R TO 52R. REMOVED CORROSION IAW DC10 SRM 51-21-01 VOL II. ORIGINAL THICKNESS IS.090 IAW DWG AYB7030. AFTER BLENDOUT MATERIAL IS AT.080, WITHIN LIMITS IAW DC10 SRM
- [SDR 04FDEA001102](https://openairdocs.org/sdr/04FDEA001102.md): Control Unit · failed · Apr 24, 2004 · N365FE · Doug DC10 · Landing Gear Retraction/Extension System
  > ANTISKID FAILS (MULTIPLE REPEATS) REMOVED HUBCAPS, PERFORMED RINGOUT OF ALL WHEEL SPEED TRANSDUCERS, VALVES AND CONTROL WIRING, FOUND SHORT AT RECEPTACLE R5-264, REPLACED R5-264, PERFORMED OPS CHECK, FOUND ANTISKID CONTROL UNIT FAULTY, REPLACED CONTROL UNIT,
- [SDR 04FDEA001101](https://openairdocs.org/sdr/04FDEA001101.md): Skin · eroded · Apr 24, 2004 · N365FE · Doug DC10 · Ailerons
  > RT OUTBOARD AILERON TRAILING EDGE, INBOARD END IS ERRODED. CUTOUT AND REPLACED DAMAGED SECTION, FABRICATED ZEE FOR REPAIR IAW DC-10 SRM 57-20-00 FIGURE 10 VOLUME 1.
- [SDR 04FDEA001100](https://openairdocs.org/sdr/04FDEA001100.md): Altimeter · malfunctioned · Apr 24, 2004 · N365FE · Doug DC10 · Altimeter, Barometric/Encoder
  > FIRST OFFICERS RADIO ALTIMETER FLAG IN VIEW. AIRCRAFT CONTINUES TO DEVELOPE HISTORY OF RADIO ALTIMETER FAULTS. CLEANED RADIO ALTIMETER COOLING FANS AND R/T IAW DC10 MM 20-10-10. REMOVED AND REPLACED COOLING FAN IAW DC-10 MM 21-85-05. REMOVED AND REPLACED FIRS
- [SDR 04FDEA001099](https://openairdocs.org/sdr/04FDEA001099.md): Skin · cracked · Apr 24, 2004 · N365FE · Doug DC10 · Ailerons
  > RT OUTBOARD AILERON INBOARD SUDE HAS SKIN SEPERATING AND CRACKED. FABRICATED NEW SKIN SECTION AND REPAIR DOUBLERS IAW DC-10 SRM 57-10-00 FIGURE 6 VOLUME 1. INSTALLED REPAIR PARTS IAW DC-10 SRM 57-10-00 FIGURE 6 VOLUME 1. COMPLIED WITH WEIGHT AND BALANCE, AILE
- [SDR 04FDEA001098](https://openairdocs.org/sdr/04FDEA001098.md): Drum · wrong part · Apr 24, 2004 · N365FE · Doug DC10 · Leading Edge Slat Control System
  > LT SLAT DRIVE MECHANISM FOLLOWUP CABLW DRUM IS THE WRONG PART NUMBER. REMOVED AND REPLACE DRUM FOR LEFT HAND SLAT DRIVE MECHANISM IAW DAC CMM 27-83-11 PAGE 505 ITEM 9.
- [SDR WRLA200401](https://openairdocs.org/sdr/WRLA200401.md): Aspirator · separated · Jan 3, 2004 · N541SA · Doug DC10 · Escape Slide
  > DURING MAINTENANCE CHECK, AT GSO, THE REQUIRED TEST DEPLOYMENT OF THE R1 DOOR EVACUATION SLIDE WAS ACCOMPLISHED. DURING TEST THE AFT ASPIRATOR OF THE SLIDE CAME APART. FOUND THE RETAINING RING THAT HOLDS THE ASPIRATOR IN PLACE ON THE SLIDE CAME OUT WHEN THE
- [SDR WRLA200315](https://openairdocs.org/sdr/WRLA200315.md): Slide · malfunctioned · Jun 16, 2003 · N541SA · Doug DC10 · Escape Slide
  > DURING A FUNCTIONAL CHECK OF RT FORWARD DOOR SLIDE ASSY (R1) DOOR FAILED TO OPEN TO ITS FULL TRAVEL. DOOR PNEUMATIC ACCUMULATOR BOTTLE NOTED TO HAVE BEEN AT LOW SIDE OF ITS GREEN SERVICING INDICATION BAND. THE DOOR WAS CLOSED AND THE DOOR PNEUMATIC ACCUMULAT
- [SDR WRLA200312](https://openairdocs.org/sdr/WRLA200312.md): Control Panel · inoperative · Jun 3, 2003 · N541SA · Doug DC10 · Autopilot System
  > AUTOPILOTS 1 AND 2 FAILED TO ENGATE RETURNED TO LAX, THE AIRCRAFT RETURNED TO THE DEPARTING STATION LAX FOR REPAIR. ALIGNED INU'S PRESSURIZED HYDRAULICS, YAW UPPER AND LOWER YAW ON, FD'S ON FLAGS IN VIEW PERFORMED TEST TO SYSTEM. OPERATIONAL CHECKED OK REPLAC
- [SDR WRLA200302](https://openairdocs.org/sdr/WRLA200302.md): Pressure Switch · inoperative · Feb 18, 2003 · N541SA · Doug DC10* · Turbine Engine Oil System
  > NR 3 ENGINE OIL STRAINER CLOG CAME ON AFTER TAKEOFF LIGHT-SHUT DOWN ENGINE. IAW FLIGHT MANUAL PROCEDURES, RETURNED TO DEPARTURE STATION. REMOVED AND REPLACED NR 3 OIL STRAINER PRESSURE SWITCH. PERFORMED ENGINE RUN UP PRESSURE AND TEMPERATURE NORMAL SYSTEM OP
- [SDR F9B2002F00000](https://openairdocs.org/sdr/F9B2002F00000.md): Duct · damaged · Nov 20, 2002 · Doug DC10 · Engine Air Intake System
  > INLET DUCT ASSEMBLY DAMAGED.
- [SDR 02FDEA00285](https://openairdocs.org/sdr/02FDEA00285.md): Bolt · corroded · Apr 24, 2002 · N311FE · Doug DC10* · Fasteners
  > RIGHT I/B FLAP O/B HINGE FWD BRACKET O/B H-11 BOLT CORRODED. R&R BOLTS PER EA 8-5750-60625.
- [SDR WRLA2002206](https://openairdocs.org/sdr/WRLA2002206.md): Gcu · failed · Mar 13, 2002 · N107WA · Doug DC10 · AC Regulator
  > DURING TAXI OUT, NR 3 GENERATOR OFF LIGHT ILLUMINATED NR 3 GENERATOR WAS RESET PER FCOM. DURING CLIMB APPROXIMATELY 15,000 FEET NR 3 GENERATOR VOLTS AND FREQUENCIES WENT TO ZERO. ATTEMPTED RESET NR 3 GENERATOR MAINTAINED VOLTS AND FREQUENCIES, LOAD FOR SECON
- [SDR 20010129CW020](https://openairdocs.org/sdr/20010129CW020.md): Slide Raft · misinstalled · Jan 2, 2001 · Doug DC10 · Escape Slide
  > FOUND 8 FT LONG BY 2 INCHES WIDE, RED WEBBING STRAP TIED AROUND THE FOLDED INFLATABLE SLIDE/RAFT. IF THE UNIT WERE TO BE USED IN AN EMERGENCY, THE SLIDE WOULD NOT HAVE DEPLOYED PROPERLY.
- [SDR 00FDEA00885](https://openairdocs.org/sdr/00FDEA00885.md): Transmitter · failed · Dec 16, 2000 · N366FE · Doug DC10* · Engine Oil Indicating System
  > 00-364 NR 3 ENGINE OIL TEMP GAGE MAXED OUT AT 200 DEG. SHUT DOWN NR 3 ENG IAW RED TAB PROC. RESECURED LOOSE CONNECTOR PLUG AND FAN COWLS.
- [SDR 20000712SH037](https://openairdocs.org/sdr/20000712SH037.md): Seal · damaged · Jul 12, 2000 · Doug DC10 · Turbine Engine Compressor Section
  > ON TAKEOFF FROM ORD, ENGINE SUSTAINED SEVERE LPT DAMAGE RESULTING IN ATB. THE ENGINE HAD COMPLETED 833 HRS AND 341 CYCLES SINCE OVERHAUL. SUBSEQUENT STRIP INVESTIGATION HRS REVEALED THE HPT DAMPER SLEEVE WAS NOT FITTED AT THE LAST SHOP VISIT. INVESTIGATIONS
- [SDR 00FDEA00418](https://openairdocs.org/sdr/00FDEA00418.md): Skin · corroded · Jul 1, 2000 · N377FE · Doug DC10* · Ailerons
  > SKIN BULGING AROUND FASTENERS ON LWR SURFACE OF RT O/B AILERON. FOUND CORROSION BETWEEN SKIN AND FINGER DOUBLER. *S/D* REMOVED AND REPLACED LWR SURFACE SKIN OF RT O/B AILERON REF SRM 51-00-01.
- [SDR 20000426SH007](https://openairdocs.org/sdr/20000426SH007.md): Retainer · damaged · Apr 3, 2000 · N3240 · Doug DC10 · Main Landing Gear
  > VISUAL INSPECTION SHOWED RING RETAINER AREA DAMAGED BEYOND LIMITS AND HEAVY CORROSION AT BOLT HOLE AREAS. (X)
- [SDR 99FDEA00312](https://openairdocs.org/sdr/99FDEA00312.md): Spar · gouge · Aug 4, 1999 · N377FE · Doug DC10* · Wing Spar
  > RIGHT WING AFT SPAR AFT TANG HAS A GOUGE ACROSS THE FLANGE AT XROS 414. COMPLIED WITH EA 8-5710-42395 RT REAR SPAR DEVIATION FROM EO 8-5710-7-30041.
- [SDR 98UAL900384](https://openairdocs.org/sdr/98UAL900384.md): Tube · failed · Aug 5, 1998 · Doug DC10* · Life Raft
  > SLIDE/RAFT HAD A SEAM FAILURE ON THE LOWER TUBE AFTER FLAT FIRE TEST DURING UNIT OVERHAUL. SCRAPPED UNIT.
- [SDR 98ZZZX844](https://openairdocs.org/sdr/98ZZZX844.md): Valve Body · cracked · Feb 11, 1998 · Doug DC10* · Leading Edge Slat Control System
  > HAD SEVERAL INSTANCES WHERE FLIGHT CONTROL VALVE BODY WAS CRACKED. CRACK IS LOCATED IN THREAD RELIEF AREA.
- [SDR 98ZZZX843](https://openairdocs.org/sdr/98ZZZX843.md): Valve Body · cracked · Feb 11, 1998 · Doug DC10* · Leading Edge Slat Control System
  > FLIGHT CONTROL BYPASS VALVE HAS HAD SEVERAL INSTANCES WHERE THE VALVE BODY HAS BEEN CRACKED. VALVE CRACKED IN RADIUS BETWEEN INSIDE DIAMETER AND BOTTOM OF BODY.
- [SDR 97ZZZX4715](https://openairdocs.org/sdr/97ZZZX4715.md): Pump · damaged · Oct 27, 1997 · Doug DC10* · Engine Fuel Pump
  > PUMP RETURNED FOR OVERHAUL AND SB COMPLIANCE. FOUND BEYOND REPAIR AND FOD BOLT WAS WEDGED BETWEEN VANES OF IMPELLER SECTION ALONG WITH WASHER FRAGMENTS. INTERNAL DAMAGE TO IMPELLER VANES AND GOUGED HOUSING. UNIT COULD HAVE SEIZED AND SHEARED SHAFT.
- [SDR 97ZZZX3907](https://openairdocs.org/sdr/97ZZZX3907.md): Resistor · failed · Aug 27, 1997 · Doug DC10* · DC Regulator
  > RESISTORS FAILED CAUSING CSD LOAD CONTROLLER TO FAIL AND MAINTAIN PROPER CYCLES. THIS IS THE SECOND TYPE OF THIS FAILURE. ORIGINAL PARTS CAME FROM MANUFACTURER.
- [SDR 97ZZZX3906](https://openairdocs.org/sdr/97ZZZX3906.md): Resistor · failed · Aug 27, 1997 · Doug DC10* · DC Regulator
  > RESISTORS FAILED CAUSING CSD LOAD CONTROLLER TO FAIL AND MAINTAIN PROPER CYCLES. THIS IS THE SECOND TYPE OF THIS FAILURE. ORIGINAL PARTS CAME FROM MANUFACTURER.
- [SDR 97ZZZX3757](https://openairdocs.org/sdr/97ZZZX3757.md): Stator Housing · oversized · Aug 13, 1997 · Doug DC10* · AC Generator-Alternator
  > DURING DISASSEMBLY OF BEARING LINER FROM THE HOUSING, A SHIM WAS FOUND AROUND THE HOUSING INSIDE DIAMETER WHERE THE BEARING LINER SITS. THE HOUSING I.D. WHERE BEARING LINER SITS IS OVERSIZED AND SHIM WAS INSTALLED BY UNKNOWN SHOP TO ACCOMMODATE THE NEW BEARIN
- [SDR 96ZZZX4137](https://openairdocs.org/sdr/96ZZZX4137.md): Duct · flange broken · Jul 16, 1996 · Doug DC10* · Pneumatic Distribution System
  > THE DUCT WAS RECEIVED WITH ONE FLANGE RUPTURED AT A PREVIOUS WELD REPAIR LOCATION. ALL OTHER HIDDEN DAMAGE INSPECTION TO THE DUCT ASSEMBLY DID NOT REVEAL ANY SUBSEQUENT DAMAGE AS A RESULT OF THE DUCT FAILURE. WELD WAS AT A RADIUS OF THE FLANGE IN AN AREA NOT
- [SDR 96ZZZX2370](https://openairdocs.org/sdr/96ZZZX2370.md): Fitting · corroded · Apr 11, 1996 · Doug DC10* · Trailing Edge Flaps
  > HANGAR MOUNT FITTINGS THAT ARE RIVETED TO TWO RIBS AND THEN THE RIB AND FITTING ASSYS ARE BONDED TO THE CORE AND SKIN. THIS IS WHAT ATTACHES THE VANE TO THE FLAP. UPON COMPLETION OF DISASSEMBLING THE VANE, THE FITTINGS WERE FOUND TO HAVE EXCESSIVE DISSIMILAR
- [SDR 96ZZZX2369](https://openairdocs.org/sdr/96ZZZX2369.md): Fitting · corroded · Apr 11, 1996 · Doug DC10* · Trailing Edge Flaps
  > HANGAR MOUNT FITTINGS THAT ARE RIVETED TO TWO RIBS AND THEN THE RIB AND FITTING ASSYS ARE BONDED TO THE CORE AND SKIN. THIS IS WHAT ATTACHES THE VANE TO THE FLAP. UPON COMPLETION OF DISASSEMBLING THE VANE, THE FITTINGS WERE FOUND TO HAVE EXCESSIVE DISSIMILAR

## 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 = 'DC10'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/aircraft-builders-assoc-dc10/reports

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