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

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

Newest first. General aviation reporting is voluntary.

Page 1 of 11 · 510 reports

- [SDR FDEA201606302206](https://openairdocs.org/sdr/FDEA201606302206.md): Light · inoperative · Jun 30, 2016 · N357FE · Doug DC1010F · Emergency Lighting
  > EMERGENCY LIGHTS ARE INOPERATIVE, TROUBLESHOT, 115VAC PRESENT AT PIN 6 & 5 OF P1-1756A, NO 28VDC AT PIN 8 OF P1-1756A, NO 28VDC AT TERMINAL D2 OF SWITCH S1-346. GOOD 28VDC COMING OFF C/B B1-907 EMERGENCY LIGHTS ARM UNABLE TO TROUBLESHOOT FURTHER TO FIND OPEN
- [SDR FDEA201606302204](https://openairdocs.org/sdr/FDEA201606302204.md): Seat Track · damaged · Jun 30, 2016 · N560FE · Doug DC1010F · Fuselage, Seat/Cargo Attach Fittings
  > LOCK S1388 BETWEEN POSITION 7L AND 8L FOUND LOOSE, UPON FURTHER INSPECTION FOUND SEAT TRACK IS DAMAGED. REPLACED DAMAGED SEAT TRACK SECTION IAW SRM 53-70-00.
- [SDR FDEA201004081102](https://openairdocs.org/sdr/FDEA201004081102.md): Rib · cracked · Apr 8, 2010 · N361FE · Doug DC1010F · Wing, Rib/Bulkhead
  > LEFT WING LEADING EDGE PANEL SUPPORT IS CRACKED. REMOVED DAMAGE BY CUT OUT IAW SRM 57-00-01, FIG 10, VOL I. FABRICATED REPAIR FILLER AND DOUBLER IAW SRM 57-00-01, FIG 10, VOL I. ALODINED AND PRIMED IAW SRM 51-1-01, VOL II. INSTALLED REPAIR FILLER AND DOUB
- [SDR FDEA201004061080](https://openairdocs.org/sdr/FDEA201004061080.md): Floorboard · delaminated · Apr 6, 2010 · N361FE · Doug DC1010F · Fuselage Floor Panel
  > AFT CARGO COMPARTMENT FLOORBOARD 187 FF IS DELAMINATED AND DENTED AT SEVERAL LOCATIONS. FABRICATED NEW AFT CARGO FLOOR PANEL 187 FF IAW DWG SRZ 25-005, REV "H" AND DWG SRZ 25-011, REV "C".
- [SDR FDEA201004061079](https://openairdocs.org/sdr/FDEA201004061079.md): Floorboard · delaminated · Apr 6, 2010 · N361FE · Doug DC1010F · Fuselage Floor Panel
  > AFT CARGO COMPARTMENT FLOORBOARD 187 FF IS DELAMINATED AND DENTED AT SEVERAL LOCATIONS. FABRICATED NEW AFT CARGO FLOOR PANEL 187 FF IAW DWG SRZ 25-005, REV "H" AND DWG SRZ 25-011, REV "C".
- [SDR FDEA200909123288](https://openairdocs.org/sdr/FDEA200909123288.md): Warning Light · illuminated · Sep 12, 2009 · N68053 · Doug DC1010F · Leading Edge Slat Position Indicating System
  > SLAT DISAGREE LIGHT LEVEL 2 ON SHORT FINAL, 36R MEM NO CONTROL ISSUES, ACFT STABLE AND HAD BEEN CONFIGURED FOR LONG TIME ALREADY. PERFORMED GO AROUND, RAN QRH, RECONFIGURED, NO MORE LITES. UNEVENTFULL LANDING. PSEU HAD NO FAULTS STORED AND RTS OK. FCC'S HA
- [SDR FDEA200905051536](https://openairdocs.org/sdr/FDEA200905051536.md): Skin · dented · May 5, 2009 · N68053 · Doug DC1010F · Fuselage Main, Plate/Skin
  > EXT FUSELAGE LWR SURFACE FOUND DENT ON SKIN 3 INCH BY 1.50 INCH. REPAIRED AREA IAW SRM 53-20-00, FIG 6, SHT 9 /10, VOL I.
- [SDR FDEA200904291463](https://openairdocs.org/sdr/FDEA200904291463.md): Skin · cracked · Apr 29, 2009 · N68053 · Doug DC1010F · Fuselage Main, Plate/Skin
  > EXT FUSELAGE UNDER WING TO FUSELAGE FAIRING FOUND CRACK ON REPAIR DOUBLER RT SIDE. REPAIRED AREA IAW DWG SR10530073 AND EA NR 8-5310-35912.
- [SDR FDEA200904221381](https://openairdocs.org/sdr/FDEA200904221381.md): Fitting · cracked · Apr 22, 2009 · N68053 · Doug DC1010F · Trailing Edge Flaps
  > LT WING INB FLAP SUPPORT STRUCTURE FOUND FITTING P/N ANB7394-501 WITH CRACK AND FOUR ATTACHMENT HOLES (FOR ANB7118-501 FITTING) WITH CORROSION ON BORES AND ON LUG FACES. REPAIRED AREA IAW EA NR 8-5340-128563.
- [SDR FDEA200904091238](https://openairdocs.org/sdr/FDEA200904091238.md): Door Frame · cracked · Apr 9, 2009 · N68053 · Doug DC1010F · Fuselage Main, Structure
  > MAIN CABIN, FOUND CRACKS ON LWR AFT JAMB DOOR 3 LT. REPAIRED LWR DOOR JAMB IAW SRM 53-50-00 FIGURE 19 SHT 2 VOL I.
- [SDR FDEA200904091237](https://openairdocs.org/sdr/FDEA200904091237.md): Door Frame · cracked · Apr 9, 2009 · N68053 · Doug DC1010F · Fuselage Main, Structure
  > MAIN CABIN, FOUND CRACK ON FWD UPPER JAMB DOOR 3 LT. REPAIRED UPPER DOOR JAMB WEB IAW SRM 53-50-00 FIGURE 19 SHT 1 VOL I.
- [SDR FDEA200903180957](https://openairdocs.org/sdr/FDEA200903180957.md): Support Fitting · corroded · Mar 18, 2009 · N68053 · Doug DC1010F · Trailing Edge Flaps
  > RT WING INBD FLAP SUPPORT STRUCTURE FOUND FITTING P/N ANB7394-502 WITH GOUGE AND 4 ATTACHMENT HOLES (FOR ANB7118-502 FITTING) WITH CORROSION ON BORES AND ON LUG FACES. REPAIRED AREA IAW EA 8-5340-128544.
- [SDR FDEA200903140917](https://openairdocs.org/sdr/FDEA200903140917.md): Attach Fitting · cracked · Mar 14, 2009 · N68053 · Doug DC1010F · Wing, Attach Fittings
  > LT UPPER BULKHEAD LUG CRACKED. REPAIRED AREA IAW SRM 57-20-00, FIG 38, STEP 1-6 AND 11/12, VOL I.
- [SDR FDEA200903090870](https://openairdocs.org/sdr/FDEA200903090870.md): Seat Track · corroded · Mar 9, 2009 · N68053 · Doug DC1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK FLOOR PANELS AND SEAT TRACKS 1 EA 1 INCH LONG MODERATE CORROSION LOWER CHANNEL. REPAIRED AREA IAW SRM 53-70-00, FIG 13, SHT 1, VOL I.
- [SDR FDEA200903040843](https://openairdocs.org/sdr/FDEA200903040843.md): Skin · worn · Mar 4, 2009 · N68053 · Doug DC1010F · Wing, Plate/Skin
  > RT WING L/E FOUND NR 2EA DEEP WEAR ON EXT SKIN.050 INCH BY.25 INCH DEEP.60 INCH. REPAIRED AREA IAW SRM 57-10-00, FIG 39 AND 15, VOL I.
- [SDR FDEA200903040842](https://openairdocs.org/sdr/FDEA200903040842.md): Skin · cracked · Mar 4, 2009 · N68053 · Doug DC1010F · Wing, Plate/Skin
  > RT WING EXT SKIN L/E FOUND CRACK ON UPPER EXT SKIN L/E. REPAIRED SKIN IAW SRM 57-10-00, FIG 68, SHT 2, VOL I.
- [SDR FDEA200903040841](https://openairdocs.org/sdr/FDEA200903040841.md): Skin · worn · Mar 4, 2009 · N68053 · Doug DC1010F · Leading Edge Devices
  > RT WING SLATS DROOPED FOUND DEEP WEAR ON ANTIFRICTION AND EXT SKIN. REPAIRED AREA IAW SRM 57-10-00, FIG 15, SHT 1, VOL I.
- [SDR FDEA200903040840](https://openairdocs.org/sdr/FDEA200903040840.md): Angle · cracked · Mar 4, 2009 · N68053 · Doug DC1010F · Leading Edge Devices
  > RT WING SLATS DROOPED FOUND ANGLES WITH CRACK ON INT DROOPED. REPAIRED AREA IAW SRM 57-00-01, FIG 10, SHT 1, VOL I.
- [SDR FDEA200903040839](https://openairdocs.org/sdr/FDEA200903040839.md): Beam · corroded · Mar 4, 2009 · N68053 · Doug DC1010F · Fuselage Main, Structure
  > FWD CARGO COMP AREA INSP SEVERE CORROSION WITH EXFOLIATION ON BEAM. REPAIRED AREA IAW SRM 53-00-01, FIG 9, SHT 7, VOL I.
- [SDR FDEA200902280771](https://openairdocs.org/sdr/FDEA200902280771.md): Angle · corroded · Feb 28, 2009 · N68053 · Doug DC1010F · Fuselage Miscellaneous Structure
  > FWD CARGO COMPT AREA INSP MODERATE CORROSION CAP ANGLE. REPAIRED AREA IAW SRM 53-30-00, FIG 8 AND 5, VOL I.
- [SDR FDEA200902280770](https://openairdocs.org/sdr/FDEA200902280770.md): Floorbeam · corroded · Feb 28, 2009 · N68053 · Doug DC1010F · Fuselage Main, Floor Beam
  > FWD CARGO COMPT AREA INP SEVERE CORROSION ON BEAM LOWER PANEL FLOOR. REPAIRED BEAM IAW SRM 53-00-01, FIG 9, SHT 8, VOL I AND SRM 53-70-00, FIG 18, VOL I.
- [SDR FDEA200902280769](https://openairdocs.org/sdr/FDEA200902280769.md): Skin · cracked · Feb 28, 2009 · N68053 · Doug DC1010F · Wing, Plate/Skin
  > RT WING L/E FOUND CRACK ON LOWER EXT SKIN. REPAIRED AREA IAW SRM 57-10-00, FIG 68, SHT 2, VOL I.
- [SDR FDEA200902280768](https://openairdocs.org/sdr/FDEA200902280768.md): Rib · cracked · Feb 28, 2009 · N68053 · Doug DC1010F · Wing, Rib/Bulkhead
  > RT WING L/E FOUND CRACK ON INT RIB LOWER SIDE L/E. REPAIRED AREA IAW SRM 57-00-01, FIG 10, SHT 1, VOL I.
- [SDR FDEA200902280767](https://openairdocs.org/sdr/FDEA200902280767.md): Rib · cracked · Feb 28, 2009 · N68053 · Doug DC1010F · Wing, Rib/Bulkhead
  > RT WING L/E FOUND CRACK ON RIB LOWER INT L/E. REPAIRED AREA IAW SRM 57-00-01, FIG 10, SHT 1, VOL I.
- [SDR FDEA200902270756](https://openairdocs.org/sdr/FDEA200902270756.md): Skin · unknown · Feb 27, 2009 · N68053 · Doug DC1010F · Fuselage Main, Plate/Skin
  > EXTERNAL FUSELAGE EXISTING DOUBLER ON SKIN. REPAIRED SKIN IAW SRM 53-20-00, FIG 6, SHT 7 AND 8, VOL I.
- [SDR FDEA200902270755](https://openairdocs.org/sdr/FDEA200902270755.md): Skin · unknown · Feb 27, 2009 · N68053 · Doug DC1010F · Trailing Edge Flaps
  > LT WING INBD FLAP UPPER SKIN FOUND EXISTING FLUSH DOUBLER. REPAIRED AREA IAW SRM 57-10-00, FIG 85, VOL I.
- [SDR FDEA200902260731](https://openairdocs.org/sdr/FDEA200902260731.md): Skin · unknown · Feb 26, 2009 · N68053 · Doug DC1010F · Elevator, Plate/Skin
  > HORIZ STAB RT INBD ELEVATOR UPPER SKIN FOUND EXISTING DOUBLER. REPAIRED AREA IAW SRM 55-10-00, FIG 8, VOL I.
- [SDR FDEA200902260730](https://openairdocs.org/sdr/FDEA200902260730.md): Skin · unknown · Feb 26, 2009 · N68053 · Doug DC1010F · Elevator, Plate/Skin
  > HORIZ STAB RT INBD ELEVATOR UPPER SKIN FOUND, EXISTING DOUBLER. REPAIRED AREA IAW SRM 55-10-00, FIG 8, VOL I.
- [SDR FDEA200902260729](https://openairdocs.org/sdr/FDEA200902260729.md): Skin · unknown · Feb 26, 2009 · N68053 · Doug DC1010F · Elevator, Plate/Skin
  > HORIZ STAB RT INBD ELEVATOR UPPER SKIN FOUND, EXISTING DOUBLER. REPAIRED AREA IAW SRM 55-10-00, FIG 8, VOL I.
- [SDR FDEA200902260728](https://openairdocs.org/sdr/FDEA200902260728.md): Skin · unknown · Feb 26, 2009 · N68053 · Doug DC1010F · Trailing Edge Flaps
  > LT WING INBD FLAP UPPER SKIN FOUND EXISTING DOUBLER. REPAIRED AREA IAW SRM 57-00-01, FIG 86, VOL I AND EA NR 8-5750-128552.
- [SDR FDEA200902260727](https://openairdocs.org/sdr/FDEA200902260727.md): Skin · unknown · Feb 26, 2009 · N68053 · Doug DC1010F · Fuselage Main, Plate/Skin
  > EXTERNAL FUSELAGE SKIN EXISTING FLUSH DOUBLER. REPAIRED AREA IAW SRM 53-20-00, FIG 6, SHT 7 AND 8, VOL I.
- [SDR FDEA200902250716](https://openairdocs.org/sdr/FDEA200902250716.md): Skin · dented · Feb 25, 2009 · N68053 · Doug DC1010F · Cargo/Baggage Doors
  > AFT CARGO COMPT DOOR FOUND DENT 2 INCH BY 3 INCH DEPTH.14 INCH ON EXTERNAL SKIN. REPAIRED AREA IAW SRM 52-10-00, FIG 17, VOL I.
- [SDR FDEA200902250715](https://openairdocs.org/sdr/FDEA200902250715.md): Seat Track · corroded · Feb 25, 2009 · N68053 · Doug DC1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK BALLMATS SEAT TRACK FOUND CORROSION WITH EXFOLIATION ON SEAT TRACK. REPAIRED AREA IAW SRM 53-70-00, FIG 1, VOL I.
- [SDR FDEA200902190580](https://openairdocs.org/sdr/FDEA200902190580.md): Channel · corroded · Feb 19, 2009 · N68053 · Doug DC1010F · Fuselage Miscellaneous Structure
  > FWD CARGO COMPT AREA DURING INSP FOUND SEVERE CORROSION WITH EXFOLIATION ON CHANNEL. REPAIRED CHANNEL IAW SRM 53-70-00, FIG 7, SHT 2, VOL I.
- [SDR FDEA200902190579](https://openairdocs.org/sdr/FDEA200902190579.md): Skin · cracked · Feb 19, 2009 · N68053 · Doug DC1010F · Wing, Plate/Skin
  > LT WING OTBD FLAP OTBD HINGE FOUND CRACK ON SKIN. REMOVED PART.
- [SDR FDEA200902190578](https://openairdocs.org/sdr/FDEA200902190578.md): Skin · cracked · Feb 19, 2009 · N68053 · Doug DC1010F · Wing, Plate/Skin
  > LT WING OTBD FLAP INBD HINGE (ONBOARD) FOUND CRACK ON SKIN (REMOVED PART). REPAIRED AREA IAW SRM 57-00-01, FIG 4, SHT 2, VOL I.
- [SDR FDEA200902190577](https://openairdocs.org/sdr/FDEA200902190577.md): Skin · cracked · Feb 19, 2009 · N68053 · Doug DC1010F · Trailing Edge Flaps
  > LT WING INBD FLAP LWR SKIN BROKEN. REPAIRED AREA IAW SRM 57-00-01, FIG 4, SHT 2, VOL I.
- [SDR FDEA200902110504](https://openairdocs.org/sdr/FDEA200902110504.md): Seat Track · corroded · Feb 11, 2009 · N68053 · Doug DC1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK FLOOR PANELS AND SEAT TRACKS SEVERE CORROSION ON SEAT TRACK AND SPLICES. REPAIRED SEAT TRACK IAW SRM 53-70-00, FIG 1, VOL I.
- [SDR FDEA200902060468](https://openairdocs.org/sdr/FDEA200902060468.md): Door Frame · cracked · Feb 6, 2009 · N68053 · Doug DC1010F · Fuselage Main, Structure
  > MAIN CABIN CRACK ON FWD UPPER WEB JAMB DOOR NR 3 RT. REPAIRED DOOR JAMB IAW SRM 53-50-00 FIG 19 SHEET VOL I.
- [SDR FDEA200902060467](https://openairdocs.org/sdr/FDEA200902060467.md): Door Frame · cracked · Feb 6, 2009 · N68053 · Doug DC1010F · Fuselage Main, Structure
  > MAIN CABIN CRACKS ON LOWER AFT JAMB DOOR WEB NR 3 RT. REPAIRED AREA IAW SRM 53-50-00, FIG 19, SHT 2, VOL I.
- [SDR FDEA200902050459](https://openairdocs.org/sdr/FDEA200902050459.md): Beam · cracked · Feb 5, 2009 · N68053 · Doug DC1010F · Fuselage Main, Structure
  > FWD CARGO COMPT AREA INSPECTION FOUND CRACK ON BEAM. REPAIRED BEAM IAW SRM 53-60-01, FIG 3, VOL I.
- [SDR FDEA200902040447](https://openairdocs.org/sdr/FDEA200902040447.md): Fitting · cracked · Feb 4, 2009 · N68053 · Doug DC1010F · Wing, Attach Fittings
  > FITTING CRACKED. REPAIRED AREA IAW SRM 57-00-01, FIG 11, VOL I.
- [SDR FDEA200902040449](https://openairdocs.org/sdr/FDEA200902040449.md): Fitting · cracked · Feb 4, 2009 · N68053 · Doug DC1010F · Fuselage Main, Attach Fittings
  > CAC CRACK ON FITTING FRAME. REPAIRED AREA IAW SRM 53-30-00, FIG 7, VOL I.
- [SDR FDEA200902040448](https://openairdocs.org/sdr/FDEA200902040448.md): Seat Track · corroded · Feb 4, 2009 · N68053 · Doug DC1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK FLOOR PANELS AND SEAT TRACKS FOUND CORROSION WITH EXFOLIATION ON TRACK. REPAIRED AREA IAW SRM 53-70-00, FIG 1, SHT 1 AND 2, VOL I.
- [SDR 22AA20081101](https://openairdocs.org/sdr/22AA20081101.md): Anti-Ice Valve · inoperative · Nov 18, 2008 · N68041 · Doug DC1010F · Cabin Cooling System
  > STRONG BURNING SMELL COMING FROM NR 1 AIR CONDITIONING PACK AFTER TAKEOFF AT HIGH POWER SETTINGS, PACK INLET & DISCHARGE TEMPERATURE NORMAL NR 1 AIR CONDITIONING PACK OPERATION NORMAL ON GROUND. REMOVED AND REPLACED WATER SEPARATOR CONICAL COALESCER IAW MM 21
- [SDR 08FDEA04420](https://openairdocs.org/sdr/08FDEA04420.md): Cable · inoperative · Oct 17, 2008 · N68059 · Doug DC1010F · Auto Throttle System
  > NR 2 THROTTLE STUCK DURING CRUISE. ENGINE SHUTDOWN DURING DESCENT. NR 2 THROTTLE MOVED BACK ON SHORT FINAL AFTER LANDING NR 2 THROTTLE COULD BE MOVED TO IDLE. CABLE COMING FROM OAK. REPLACED #2 THROTTLE CABLE PER MM 76-11-01-2, OP'S CHEKS NORMAL. PERFORMED
- [SDR 08FDEA02120](https://openairdocs.org/sdr/08FDEA02120.md): Skin · failed · Jun 3, 2008 · N68059 · Doug DC1010F · Fuselage Main, Plate/Skin
  > DURING REPAIR ASSESSMENT AN EXISTING REPAIR WAS FOUND AT FUSELAGE SKIN REPLACED EXISTING REPAIR IAW SRM53-50-00 FIG 9 BECAUSE IT IS NOT IN COMPLIANCE WITH APPROVED DATA.
- [SDR 08FDEA02021](https://openairdocs.org/sdr/08FDEA02021.md): Floorbeam · corroded · May 29, 2008 · N301FE · Doug DC1010F · Fuselage Main, Floor Beam
  > AFT LOWER PIT STA 1841 FLOORBEAM IS CORRODED FROM LBL 20 TO RBL 20. AFTER CORROSION REMOVAL, FOUND OUT OF REPAIR LIMIT IAW SRM 53-00-01, REMOVED FLOORBEAM AND REPLACED NEW FLOORBEAM IAW SRM 51-31-01, CLASSIFIED AS MAJOR REPAIR.
- [SDR 08FDEA02018](https://openairdocs.org/sdr/08FDEA02018.md): Door Frame · misrepaired · May 28, 2008 · N68059 · Doug DC1010F · Fuselage Main, Structure
  > DURING REPAIR ASSESSMENT WAS FOUND AN EXISTING REPAIR AT CTR CARGO FUSELAGE DOOR JAMB REPAIR HAS BEEN REPLACED BECAUSE IT FOUND NOT IN CONFORMITY WITH APPROVED DATA.
- [SDR 08FDEA02017](https://openairdocs.org/sdr/08FDEA02017.md): Structure · misrepaired · May 28, 2008 · N68059 · Doug DC1010F · Fuselage Main, Structure
  > DURING REPAIR ASSESSMENT WAS FOUND AN EXISTING REPAIR AT CENTER FUSELAGE DOOR JAMB LT SIDE REPAIR HAS BEEN REPLACED BECAUSE IT FOUND NOT IN CONFORMITY WITH APPROVED DATA.

Next page: https://openairdocs.org/model/mcdonnell-douglas-dc-10-10f/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 = 'DC1010F'
ORDER BY difficulty_date DESC
```

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

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