# Service difficulty reports: N68059, cancelled Jul 29, 2013

A list on [N68059, cancelled Jul 29, 2013](https://openairdocs.org/deregistered/N68059-2013-07-29.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 2 · 74 reports

- [SDR FDEA201105071778](https://openairdocs.org/sdr/FDEA201105071778.md): Battery Pack · discharged · May 7, 2011 · N68059 · Doug MD1010F · Emergency Lighting
  > EMERGENCY POWER BAT 1 LO ON PRE-FLIGHT. RELEASED FOR SERVICE IAW MEL: 33-50-02. REMOVED AND REPLACED EMERGENCY EXIT LIGHTS POWER SUPPLY IN ACCORDANCE WITH MD10-10 AMM 33-51-01-4,5; OPERATIONAL TEST SATISFACTORY. ACFT. OKAY FOR SERVICE.
- [SDR FDEA201105061765](https://openairdocs.org/sdr/FDEA201105061765.md): Latch · worn · May 6, 2011 · N68059 · Doug MD1010F · AC Generation System
  > DURING CLIMBOUT ADG DEPLOYED ON ITS OWN. AUX PUMP ON/ADG ELECTRIC ON ALL NORMAL. SLOWED TO A SLOWER CRUISE SPEED. R & R OTBD UPLATCH SPRING, AMM 24-25-01-2. CHECKED ROLLER. CHECKED NORMAL. AWAITING UPLATCH HOOK.
- [SDR FDEA201105021688](https://openairdocs.org/sdr/FDEA201105021688.md): Control Unit · failed · May 2, 2011 · N68059 · Doug MD1010F · AC Inverter
  > EMERGENCY POWER TEST INITIATES NORMALLY, AFTER 30SEC TEST APPEARS TO COMPLETE NORMALLY BUT EMERGENCY POWER TST FAIL ALERT APPEARS. DUE TO OTHER FAULTS NOTED ON ENG RUN ORDERED THE EPCU UNDER THE TSI. R & R EPCU OPS CHECK NORMAL. EMERGENCY POWER TEST ALSO CH
- [SDR FDEA201104281678](https://openairdocs.org/sdr/FDEA201104281678.md): Adg · unwanted deploy · Apr 28, 2011 · N68059 · Doug MD1010F · AC Inverter
  > PASSING FL14K, 320 KTS. NO TURBULANCE, THE ADG APPARENTLY DEPLOYED. HYD AUX PUMP LEVEL 0 ELEC CUE ON SD SHOWED GREEN ADG SYMBOL HYD CUE ON SD SHOWED AUX PUMP 1 ON. FULLY ENGAGED UPLOCK CLEVIS, AND STOWED ADG IAW MM 24-25-01-2 RII:036722.
- [SDR FDEA201005261661](https://openairdocs.org/sdr/FDEA201005261661.md): Unknown · malfunctioned · May 26, 2010 · N68059 · Doug MD1010F · Fuel Storage
  > ACFT LEFT AIRPORT WITH NR 1 TANK FUEL QTY DEFERRED. UPON ARRIVAL INTO,CREW REPORTED THAT ON APPROACH THEY GOT THE NR 1 TANK FUEL QTY LOW FAULT. CHECKED NR 1 TANK FUEL LEVEL STICKS AND FOUND ONLY 1200 LBS IN TANK NR 1,14600LBS IN TANK NR 2 AND 9100 LBS IN T
- [SDR FDEA200904161317](https://openairdocs.org/sdr/FDEA200904161317.md): Wire · unknown · Apr 16, 2009 · N68059 · Doug MD1010F · Engine Indicating System Wiring
  > CLIMBOUT PASSING 1000 FT RECEIVED ENG 2 EXCEEDANCE ALERT. RETARDED THROTTLE & N1 NOT EXCEEDED BUT HAD LARGE FLUCTUATIONS. ENG 2 N2 EGT NORMAL. PASSING 3000 FT RECEIVED ENG 2 RPM HI ALERT. ACCOMPLISHED CHECKLIST & ABLE TO KEEP NI RPM IN LIMITS WITH THROTTLE
- [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 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.
- [SDR 08FDEA01900](https://openairdocs.org/sdr/08FDEA01900.md): Skin · damaged · May 20, 2008 · N68059 · Doug DC1010 · Cargo/Baggage Doors
  > DURING DC10 CARGO MODIFICATION TO ACF DURING INSPECTION FOUND ON THE CENTER LOWER CARGO DOOR LATERAL SKIN DAMAGE. REPAIRED CENTER CARGO DOOR PAN ASSEMBLY FOR SRM 52-10-00 FIG 3 VOL 1.
- [SDR 08FDEA01833](https://openairdocs.org/sdr/08FDEA01833.md): Skin · damaged · May 13, 2008 · N68059 · Doug DC1010F · Wing, Plate/Skin
  > EXISTING EXTERNAL REPAIR DOUBLER AT FIXED L/E STA XIS 150 REMOVE REPAIR AND ACCOMPLISH A NEW IAW SRM 57-10-00 FIG 40 BECAUSE REPAIR DETECTED WAS FOUND WITH A SIGNIFICANT LOSS OF MATERIAL DUE TO A LIP CONTACT.
- [SDR 08FDEA01748](https://openairdocs.org/sdr/08FDEA01748.md): Skin · damaged · May 5, 2008 · N68059 · Doug DC1010F · Fuselage Main, Plate/Skin
  > DURING REPAIR ASSESSMENT WAS FOUND AN EXISTING EXTERNAL REPAIR AT FUSELAGE SKIN STA 1019, LONG NR 37R REPAIR FOUND NOT IN CONFORMITY WITH APPROVED DATA AND HAS BEEN REPLACED WITH A NEW IAW SRM 53-20-00 FIG 6 SH 3 AND 4.
- [SDR 08FDEA01698](https://openairdocs.org/sdr/08FDEA01698.md): Web · cracked · Apr 30, 2008 · N68059 · Doug DC1010F · Fuselage Miscellaneous Structure
  > DURING MD10 ACF MODIFICATION IN UPPER FUSELAGE AT STA 1305 JAMB DOOR L3 FOUND CRACK 0.5 INCH LONG ON THE WEB UPPER SIDE. PERFORMED REPAIR FOR SRM 53-50-00 FIG 19 VOL. I
- [SDR 08FDEA01637](https://openairdocs.org/sdr/08FDEA01637.md): Door Frame · cracked · Apr 28, 2008 · N68059 · Doug DC1010F · Fuselage Main, Structure
  > DURING MD10 ACF MODIFICATION IN UPPER FUSELAGE AT STA 1305 JAMB DOOR R3 FOUND CRACK 0.5 INCH LONG ON THE WEB. REPAIRED FOR SRM 53-50-00 FIG 19 VOL I.
- [SDR 08FDEA01636](https://openairdocs.org/sdr/08FDEA01636.md): Door Frame · cracked · Apr 28, 2008 · N68059 · Doug DC1010F · Fuselage Main, Structure
  > DURING MD10 ACF MODIFICATION ON UPPER FUSELAGE AT STA 1256 JAMB DOOR R3 FOUND N2 CRACK TO 2 INCH LONG ON THE WEB LOWER SIDE. REPAIRED FOR SRM 53-50-00 FIG 19 VOL I AND REPLACED CHANNEL P/N AEA0210-40.
- [SDR 08FDEA01635](https://openairdocs.org/sdr/08FDEA01635.md): Seat Track · corroded · Apr 28, 2008 · N68059 · Doug DC1010F · Fuselage, Seat/Cargo Attach Fittings
  > DURING MD10 ACF MODIFICATION IN UPPER FUSELAGE ON SEAT TRACK AT STA 502 X= 63, FOUND CORROSION AND SCREW BROKEN. REPLACED TRACK AFA7789-521 FOR DWG AND SRM 53-70-00 FIG 1 VOL I.
- [SDR 08FDEA01633](https://openairdocs.org/sdr/08FDEA01633.md): Door Frame · cracked · Apr 28, 2008 · N68059 · Doug DC1010F · Fuselage Main, Structure
  > DURING MD10 ACF MODIFICATION IN UPPER FUSELAGE AT STA 1256 JAMB DOOR R3 FOUND CRACK 0.5" LONG ON THE WEB UPPER SIDE REPAIRED FOR SRM 53-50-00 FIG 19 VOL I.
- [SDR 08FDEA01631](https://openairdocs.org/sdr/08FDEA01631.md): Seat Track · corroded · Apr 28, 2008 · N68059 · Doug DC1010F · Fuselage, Seat/Cargo Attach Fittings
  > DURING MD10 ACF MODIFICATION IN UPPER FUSELAGE ON SEAT TRACK X -107 STA 1581 TO 1661 FOUND SEVERAL POINT OF CORROSION. REPAIRED FOR SRM 53-70-00 FIG 1 VOL I.
- [SDR 08FDEA01629](https://openairdocs.org/sdr/08FDEA01629.md): Seat Track · worn · Apr 28, 2008 · N68059 · Doug DC1010F · Fuselage, Seat/Cargo Attach Fittings
  > DURING MD10 ACF MODIFICATION IN UPPER FUSELAGE ON SEAT TRACK STA 635- 615 X -28, FOUND USURED AND MISSING MATERIAL REPAIRED FOR SRM 53-70-00 FIG 1 VOL I.
- [SDR 08FDEA01478](https://openairdocs.org/sdr/08FDEA01478.md): Seat Track · damaged · Apr 23, 2008 · N68059 · Doug DC1010F · Fuselage, Seat/Cargo Attach Fittings
  > DURING MD10 ACF MODIFICATION IN UPPER FUSELAGE AT STA 1273 AND X -47.250 FOUND MISSING MATERIAL ON SEAT TRACK. REPAIRED SEAT TRACK FOR SRM 53-10-00 FIG 1 VOL I.
- [SDR 08FDEA01477](https://openairdocs.org/sdr/08FDEA01477.md): Frame · cracked · Apr 23, 2008 · N68059 · Doug DC1010 · Fuselage Main, Frame
  > DURING MODIFICATION IN CENTER ACCESSORY COMPARTMENT AT STA 1099 FROM LONGERON 49 TO LONGERON 48 RT SIDE FOUND LIGHT CORROSION AND CRACK LONG 0.5" ON CAP FRAME. REMOVED CORROSION FOR SRM 51-21-01 VOL II AND PERFORMED FRAME CAP REPAIR FOR SRM 53-30-00 FIG 8 VOL
- [SDR 08FDEA01441](https://openairdocs.org/sdr/08FDEA01441.md): Seat Track · damaged · Apr 17, 2008 · N68059 · Doug DC1010F · Fuselage, Seat/Cargo Attach Fittings
  > DURING MD10 ACF MODIFICATION IN UPPER FUSELAGE AT STA 1209 X= 47.250 SEAT TRACK WITH MISSING MATERIAL. REPAIRED FOR SRM 53-70-00 FIG 1 VOL I.
- [SDR 08FDEA01440](https://openairdocs.org/sdr/08FDEA01440.md): Seat Track · damaged · Apr 17, 2008 · N68059 · Doug DC1010F · Fuselage, Seat/Cargo Attach Fittings
  > DURING MD10 ACF MODIFICATION IN UPPER FUSELAGE FROM STA 1099 TO STA 1159 ON SEAT TRACK FOUND HOLES OVALIZED REPAIRED FROM SRM 53-70-00 FIG 1 VOL I.
- [SDR 08FDEA01439](https://openairdocs.org/sdr/08FDEA01439.md): Seat Track · cracked · Apr 17, 2008 · N68059 · Doug DC1010F · Fuselage, Seat/Cargo Attach Fittings
  > DURING MD10 ACF MODIFICATION IN UPPER FUSELAGE AT STA 1341 X = -75.250 FOUND SEAT TRACK WITH CRACK.5" LONG REPAIRED FOR SRM 53-70-00 FIG 1 VOL I.
- [SDR 08FDEA01438](https://openairdocs.org/sdr/08FDEA01438.md): Rib · damaged · Apr 17, 2008 · N68059 · Doug DC1010F · Wing, Rib/Bulkhead
  > DURING MD10 ACF MODIFICATION ON SLAT NR 3 RT WING FOUND RIB P/N ARB1666-502 WITH HOLE OVALIZED REPLACED RIB FOR SRM 51-35-01 VOL II AND DWG NRB6027.
- [SDR 08FDEA01424](https://openairdocs.org/sdr/08FDEA01424.md): Skin · dented · Apr 16, 2008 · N68059 · Doug DC1010F · Fuselage Main, Plate/Skin
  > DURING MD10 ACF MODIFICATION ON LOWER FUSELAGE EXTERNAL FOUND DENT 0.047" BY 2" BY 1.5 INCH LONG ON EXTERNAL SKIN STA 1049 RT SIDE LONGERON 46 TO LONGERON 47. REPAIRED FOR SRM 53-20-00 FIG 6 VOL I.
- [SDR 08FDEA01423](https://openairdocs.org/sdr/08FDEA01423.md): Rib · damaged · Apr 16, 2008 · N68059 · Doug DC1010F · Wing, Rib/Bulkhead
  > DURING MD10 ACF MODIFICATION ON WING LT SIDE OUTBOARD SLAT NR 3 FOUND RIB P/N ARB1666-501 WITH EA 7 HOLES OVALIZED. REPLACED RIB FOR SRM 51-35-01 VOL II AND DWG ARB1666.
- [SDR 08FDEA01401](https://openairdocs.org/sdr/08FDEA01401.md): Frame · cracked · Apr 14, 2008 · N68059 · Doug DC1010F · Fuselage Main, Frame
  > DURING MD10 MODIFICATION TO ACF IN AVIONIC COMPARTMENT RT SIDE STA 469 X =-61 FOUND FRAME WITH CRACK 1 INCH REPAIRED FOR SRM 53-30-00 FIG 11 VOL I.
- [SDR 08FDEA01400](https://openairdocs.org/sdr/08FDEA01400.md): Floorbeam · damaged · Apr 14, 2008 · N68059 · Doug DC1010F · Fuselage Main, Floor Beam
  > DURING MD10 MODIFICATION ACF FOUND IN AFT CARGO COMPT STA 1857 AT X 30 BEAM FLOOR WITH DOUBLE HOLE. REPAIRED FOR SRM 53-60-01 FIG 3 VOL I.
- [SDR 08FDEA01399](https://openairdocs.org/sdr/08FDEA01399.md): Seat Track · damaged · Apr 14, 2008 · N68059 · Doug DC1010F · Fuselage, Seat/Cargo Attach Fittings
  > DURING MD10 ACF MODIFICATION IN UPPER FUSELAGE AT STA.939 X -47.50 FOUND SEAT TRACK WITH HOLE OVALIZED REPAIRED FOR SRM 53-70-00 FIG 1 VOL I.
- [SDR 08FDEA01331](https://openairdocs.org/sdr/08FDEA01331.md): Skin · cracked · Apr 7, 2008 · N68059 · Doug DC1010F · Fuselage Main, Plate/Skin
  > DURING MD10 ACF MODIFICATION FOUND ON UPPER FUSELAGE AT STA 1305 JAMB DOOR R NR 3 NUMBER 2 CRACK 2 INCHES LONG ON THE WEB IN POSITION LOWER REPAIRED FOR SRM 53-50-00 FIG 19 VOL I.
- [SDR 08FDEA01330](https://openairdocs.org/sdr/08FDEA01330.md): Skin Panel · delaminated · Apr 7, 2008 · N68059 · Doug DC1010F · Horizontal Stabilizer, Plate/Skin
  > DURING MD10 ACF MODIFICATION ON HORIZONTAL STABILIZER RT SIDE FOUND DISBONDING THE UPPER SKIN TIP OUTBOARD ELEVATOR REPLACED SKIN ASSY FOR SRM 51-35-01 AND DWG ALC7347,ALC7348, ALC7602.
- [SDR 08FDEA01297](https://openairdocs.org/sdr/08FDEA01297.md): Frame · cracked · Apr 4, 2008 · N68059 · Doug DC1010F · Fuselage Main, Frame
  > DURING MD10 ACF MODIFICATION ON UPPER FUSELAGE AT STA 1781 LT STRINGER 13 FOUND FRAME WITH CRACK 5 INCHES LONG. REPAIRED FOR SRM 53-30-00 FIG 5 SECT.
- [SDR 08FDEA01209](https://openairdocs.org/sdr/08FDEA01209.md): Skin · misrepaired · Mar 31, 2008 · N68059 · Doug DC1010F · Fuselage Main, Plate/Skin
  > DURING REPAIR ASSESSMENT AN EXISTING REPAIR AT FUSELAGE SKIN WAS FOUND NOT IN CONFORMITY WITH APPROVED DATA REPAIR HAS BEEN REPLACED WITH A NEW IAW SRM 53-50-00 FIG 26, VOL I.
- [SDR 08FDEA01208](https://openairdocs.org/sdr/08FDEA01208.md): Skin · misrepaired · Mar 31, 2008 · N68059 · Doug DC1010F · Fuselage Main, Plate/Skin
  > DURING REPAIR ASSESSMENT AN EXISTING REPAIR AT FUSELAGE SKIN WAS FOUND NOT IN CONFORMITY WITH APPROVED DATA REPAIR HAS BEEN REPLACED WITH A NEW IAW SRM 53-20-00 FIG 6, SH 3/4.
- [SDR 08FDEA01187](https://openairdocs.org/sdr/08FDEA01187.md): Fitting · corroded · Mar 28, 2008 · N68059 · Doug DC1010F · Fuselage Main, Structure
  > DURING MD10 ACF MODIFICATION MAIN CARGO DOOR LOWER JAM SUPPORT FITTING AFTER INSPECTION FOUND BORE "B", "A" AND "D" OF FITTING NR 4 WITH CORROSION (DIAMETER.456") (REF EO FEDEX 8-5230-117635. PERFORMED REWORK HOLE FOR SRM 53-50-00 FIG 17, PERFORMED NDI AN
- [SDR 08FDEA01185](https://openairdocs.org/sdr/08FDEA01185.md): Fitting · corroded · Mar 28, 2008 · N68059 · Doug DC1010F · Fuselage Main, Structure
  > DURING MD10 ACF MODIFICATION MAIN CARGO DOOR LOWER JAM SUPPORT FITTING AFTER INSPECTION FOUND BORE "C" OF FITTING NR 1 WITH CORROSION (DIAMETER.456"), REF EO FEDEX 8-5230-117635. PERFORMED REWORK HOLE FOR SRM 53-50-00 FIG 17, PERFORMED NDI AND INSTALLED BUSH
- [SDR 08FDEA01183](https://openairdocs.org/sdr/08FDEA01183.md): Fitting · corroded · Mar 28, 2008 · N68059 · Doug DC1010F · Fuselage Main, Structure
  > DURING MD10 ACF MODIFICATION MAIN CARGO DOOR LOWER JAM SUPPORT FITTING AFTER INSPECTION FOUND BORE "B", "C" AND "D" OF FITTING NR 7 WITH CORROSION DIAMETER.456 INCH (REF.E.O. FEDEX 8-5230-117635). PERFORMED REWORK HOLE FOR SRM 53-50-00 FIG 17, PERFORMED NDI
- [SDR 08FDEA01182](https://openairdocs.org/sdr/08FDEA01182.md): Fitting · corroded · Mar 28, 2008 · N68059 · Doug DC1010F · Fuselage Main, Structure
  > DURING MD10 ACF MODIFICATION MAIN CARGO DOOR COVER JAM SUPPORT FITTING AFTER INSPECTION FOUND BORE "B" OF FITTING NR 3 WITH CORROSION (DIAMETER.58") (REF EO FEDEX 8-5230-117635). PERFORMED REWORK HOLE FOR SRM 53-50-00 FIG 17, PERFORMED NDI AND INSTALLED BUS
- [SDR 08FDEA01180](https://openairdocs.org/sdr/08FDEA01180.md): Seat Track · corroded · Mar 28, 2008 · N68059 · Doug DC1010F · Fuselage, Seat/Cargo Attach Fittings
  > DURING MD10 ACF MODIFICATION IN UPPER FUSELAGE AT STA 1099 BETWEEN SEAT TRACK X= -78 AND X=-81 FOUND CORROSION ON FLOOR SUPPORT REMOVED CORROSION IS OUT LIMIT THE REWORK. REPLACED SUPPORT FOR DWG ADA3615 AND SRM 51-35-01 VOL II.
- [SDR 08FDEA01151](https://openairdocs.org/sdr/08FDEA01151.md): Hinge Bracket · corroded · Mar 26, 2008 · N68059 · Doug DC1010F · Trailing Edge Flaps
  > DURING MODIFICATION MD10 ACF RT OUTBOARD FLAP INBOARD HINGE WITH RUST, BUSHING WITH PLAY AND SHIM WITH OXIDE. REPLACED HINGE FLAP P/N ARC0502-501 FOR DWG ARC0504.
- [SDR 08FDEA01137](https://openairdocs.org/sdr/08FDEA01137.md): Hinge Bracket · corroded · Mar 25, 2008 · N68059 · Doug DC1010 · Trailing Edge Flaps
  > DURING MD10 ACF MODIFICATION FOUND RT OUTBOARD FLAP, OUTBOARD HINGE WITH RUT AND CORROSION. REPLACED BRACKET ASSY OUT FLAP FOR DWG ARC0503-502
- [SDR 08FDEA01136](https://openairdocs.org/sdr/08FDEA01136.md): Hinge Bracket · corroded · Mar 25, 2008 · N68059 · Doug DC1010F · Trailing Edge Flaps
  > DURING MD10 ACF MODIFICATION, FOUND LT OUTBOARD FLAP OUTBOARD HINGE WITH ATTACH POINTS WITH OXIDE. REPLACED BRACKET ASSY P/N ARC0503-501 FOR DWG ARC0505.
- [SDR 08FDEA01135](https://openairdocs.org/sdr/08FDEA01135.md): Hinge Bracket · corroded · Mar 25, 2008 · N68059 · Doug DC1010F · Trailing Edge Flaps
  > DURING MD10 ACF MODIFICATION, FOUND LT OUTBOARD INBOARD FLAP HINGE WITH ATTACH POINT (FWD) RUST AND BUSHING WITH PLAY. REPLACED BRACKET ASSY FOR DWG ARC0504.
- [SDR 08FDEA00872](https://openairdocs.org/sdr/08FDEA00872.md): Frame · cracked · Mar 11, 2008 · N68059 · Doug DC1010F · Fuselage Main, Frame
  > DURING MODIFICATION DC10 CARGO TO MD10 ACF, AT REMOVAL BRACKET IS NOTED CRACK 1.5 INCH LONG ON FRAME STA 1851 RT SIDE LONGERON 10 TO 11. PERFORMED REPAIR FOR EA FEDEX 8-5310-111515.
- [SDR 08FDEA00774](https://openairdocs.org/sdr/08FDEA00774.md): Bracket · damaged · Mar 7, 2008 · N68059 · Doug DC1010F · Nacelle/Pylon Miscellaneous Structure
  > FOUND ON PYLON NR 3 ON STA YN=240 THE BRACKET WITH DAMAGED AND DO NOT INSTALLED FOR DWG REPLACE WEB FOR SRM 51-33-01 VOL II AND DWG AUB7027.
- [SDR 08FDEA00678](https://openairdocs.org/sdr/08FDEA00678.md): Fitting · cracked · Mar 3, 2008 · N68059 · Doug DC1010F · Fuselage Miscellaneous Structure
  > DURING MODIFICATION DC10 FREIGHTER TO MD10 ACF, FOUND IN AIR CONDITION COMPARTMENT NR 3 RT SIDE STA 555 X= -96 Z=-37,50 THE END FITTING FRAME WITH CRACK. INSPECTED AREA AND REPLACED SUPPORT P/N ACA3137-1.
- [SDR 06FDEA2434](https://openairdocs.org/sdr/06FDEA2434.md): Unknown · unknown · Jun 30, 2006 · N68059 · Doug DC1010 · Standard Practices/Structures
  > REPAIR DOUBLER STA 620 FWD LOWER CORNER MAIN CARGO DOOR CUT-OUT MARKED NR 73. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. COMPLIED WITH FEDEX EA 8-5330-100785, FUSELAGE, MAIN CARGO DOOR O
- [SDR 06FDEA2413](https://openairdocs.org/sdr/06FDEA2413.md): Bolt · sheared · Jun 27, 2006 · N68059 · Doug DC1010 · Trailing Edge Flaps
  > RIGHT WING TRAILING EDGE INTERIOR STRUCTURE, OUTBOARD FLAP INBOARD TRACK SUPPORT FITTING LOWER OUTBOARD ATTACH BOLT SHEARED AT AFT SPAR. COMPLIED WITH E8-5710-100781 PT 1, LOWER ATTACH STUD BOLT REPLACED. MAJOR REPAIR.

Next page: https://openairdocs.org/deregistered/N68059-2013-07-29/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 n_number = 'N68059' AND deregistration_id = 'N68059-2013-07-29'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N68059-2013-07-29/reports

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