# Service difficulty reports: N68058, cancelled Mar 8, 2013

A list on [N68058, cancelled Mar 8, 2013](https://openairdocs.org/deregistered/N68058-2013-03-08.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 · 58 reports

- [SDR 07FDEA04612](https://openairdocs.org/sdr/07FDEA04612.md): Seat Track · corroded · Oct 16, 2007 · N68058 · Doug DC1010 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK (EQUIPMENT TIE DOWN TRACK) AT APPROX BL 91 LT AND BETWEEN FS 392 AND 25 HAS CORROSION. REMOVED, FAB'D AND INSTALLED SEAT TRACK IAW SRM 53-70-00 FIG 5 SHT 2 VOL I AND DAC DWG ABA 7680.
- [SDR 07FDEA04611](https://openairdocs.org/sdr/07FDEA04611.md): Seat Track · corroded · Oct 16, 2007 · N68058 · Doug DC1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN STA 880, RBL 76 SEAT TRACK CORRODED. REMOVED, FAB'D AND INSTALLED SEAT TRACK IAW DC/MD 10 SRM 51-31-01 VOL II PAGE 1 AND DAC DRAWING AFA 7433 REV AD. ALODINED AND PRIMED IAW DC/MD 10 SRM 51-21-01 VOL II PAGE 1 AND 21.
- [SDR 07FDEA04570](https://openairdocs.org/sdr/07FDEA04570.md): Seat Track · corroded · Oct 11, 2007 · N68058 · Doug DC1010F · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK BETWEEN STA 420 TO STA 448 RBL 27 REMOVED AND REPLACED SEAT TRACK ABA7684-507, STA 421.5 TO STA 484.7, RBL 27.5, IN REF TO DC10/MD10 SRM 51-33-01 VOL II PG 1.
- [SDR 07FDEA04566](https://openairdocs.org/sdr/07FDEA04566.md): Seat Track · gouged · Oct 10, 2007 · N68058 · Doug DC1010 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN, STN 1360 - STN 1364, RBL 46, "SEAT TRACK GOUGED" SCALLOPS ELONGATED CHECKED LIMITS, BLENDOUT AREA IS.510 OUT OF.500 MAX OUT OF LIMITS IAW DC/MD-10 SRM 53-70-00 VOL I PG 21 FIG 5 SHT 1. REMOVED DAMAGED SECTION AND INSTALLED NEW SECTION IAW DC/MD-
- [SDR 07FDEA04565](https://openairdocs.org/sdr/07FDEA04565.md): Seat Track · corroded · Oct 10, 2007 · N68058 · Doug DC1010 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN/CORROSION ON SEAT TRACK (EQUIPMENT TIE DOWN TRACK) AT BL 78 LT AND BETWEEN FS 374 AND 420 REMOVED CORROSION IAW MD/DC-10 SRM 53-70-00 FIG 5 SHEET 2 VOL I MIN THAT CAN BE REMAINING IS.060 IAW MD/DC-10 SRM 53-70-00 FIG 5 SHEET 2 VOL I OUT OF LIMITS IAW MD
- [SDR 07FDEA04564](https://openairdocs.org/sdr/07FDEA04564.md): Seat Track · gouged · Oct 10, 2007 · N68058 · Doug DC1010 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN, STN 1358, RBL 46, "SEAT TRACK GOUGED," SCALLOPS ELONGATED CHECKED LIMITS: REMAINING MATERIAL IS.170,.260 MIN REQ OUT OF LIMITS IAW DC/MD-10 SRM 53-70-00 VOL I PG 21 FIG 5 SHT 1. REMOVED DAMAGED SECTION AND INSTALLED NEW SECTION IAW DC/MD-10 SRM
- [SDR 07FDEA04563](https://openairdocs.org/sdr/07FDEA04563.md): Frame · chafed · Oct 10, 2007 · N68058 · Doug DC1010F · Fuselage Main, Frame
  > NR 1 AIR CONDITIONING COMPT BYPASS VALVE PUSH-PULL CABLE CHAFING AGAINST FRAME TOP CHORD STA 588. REPAIRED FRAME IAW EA 8-5310-10920B, FUSELAGE-AIR CONDITIONING BAY FRAME CHAFED. ON INNER FLANGE-REPAIR.
- [SDR 07FDEA02662](https://openairdocs.org/sdr/07FDEA02662.md): Support Bracket · cracked · Jul 29, 2007 · N68058 · Doug DC1010 · Wing Miscellaneous Structure
  > RT WING O/B FLAP, I/B HINGE, O/B ATTACH BRACE CRACKED AT REAR SPAR. REMOVED AND REPLACED CRACKED SUPPORT ARB0029-506. REF SRM 57-00-01.
- [SDR 07FDEA02436](https://openairdocs.org/sdr/07FDEA02436.md): Inu · failed · Jul 5, 2007 · N68058 · Doug DC1010 · Inertial Guidance System
  > NR 1 INU FAILED AFTER PUSH BACK. REPLACED NR 1 INU GRD, OPS CK NORMAL MM 34-43-04-2, OFF MFG 463001-6130-0413, POS 1 SRL 0341, TAG 0357A9, ON MFG 463001-6130-0413, SRL 2223, TAG 572A32.
- [SDR 06FDEA1942](https://openairdocs.org/sdr/06FDEA1942.md): Filler · cracked · May 17, 2006 · N68058 · Doug DC1010 · Nacelle/Pylon, Main Frame
  > NR2 ENGINE SAIL TAIL FILLER AT EXHAUST NOZZLE HAS NUMEROUS CRACKS AS MARKED, 2 DEEP CHAF MARKS AND RIGHT FWD CORNER IS BROKEN. REMOVED SAIL TAIL FILLER IAW SRM 51-31-01. REPAIRED FILLER AS REQUIRED BY WELDING CRACKS AND CHAF MARKS ON MAE TRAVLER T6/593345.
- [SDR 06FDEA1940](https://openairdocs.org/sdr/06FDEA1940.md): Wedge · cracked · May 17, 2006 · N68058 · Doug DC1010F · Trailing Edge Flaps
  > LT WING I/B FLAP UPPER SKIN HAS A CRACK NEAR O/B END. CLEANED AREA IAW M/M 12-22-02-7, HFEC INSP PER NTM 51-00-00 CRACK FOUND 3 EA. REMOVED T/E SECTION IAW SRM 51-31-01. REMOVED DAMAGED AREA IAW SRM 57-10-00, FIG 85. FAB DOUBLER AND FILLER MAT THICKNESS 2
- [SDR 06FDEA0920](https://openairdocs.org/sdr/06FDEA0920.md): Connector · damaged · Mar 2, 2006 · N68058 · Doug DC1010 · Door Warning System
  > AT FL 290 A/C DOOR LIGHT ILLUMINATED ON SECOND OFFICERS PANEL. CREW RAN RED TAB CHECKLIST AND LANDED AT MEMPHIS. DOOR LIGHT EXT DESCENDING THROUGH 16,000 FT. AIR CONDITIONING DOOR CAUTION LIGHT SYSTEM(S) INOP. VERIFY AND RECORD IN AML/EAML THE AFFECTED AIR
- [SDR 05FDEA03180](https://openairdocs.org/sdr/05FDEA03180.md): Warning Light · illuminated · Sep 28, 2005 · N68058 · Doug DC1010 · Engine Thrust Reverser
  > WHILE IN FLIGHT CLIMBING-OUT OF 15000 FT, THE NR 2 THRUST REVERSER UNLOCK LIGHT WAS FLICKERING ON AND OFF. THRUST REV CHECKLIST WAS COMPLETED AND RETURN AND LANDED ACN RELEASED FOR SERVICE PER MEL/CDL: 78-01-01-B
- [SDR 05FDEA00504](https://openairdocs.org/sdr/05FDEA00504.md): Skin · torn · Mar 10, 2005 · N68058 · Doug DC1010 · Fuselage Main, Plate/Skin
  > INSPECTED DAMAGED AREA, FOUND A LARGE TEAR IN SKIN APPROX 16 X 6 INCH FWD OF FR959 L AND ABOVE STRINGER 41L. STOP DRILLED TEARS AND CUT OUT DAMAGE PER DC10 SRM 53-20-00 VOL 1 FIG 6 SHEET 7. UPON REMOVAL OF SKIN FOUND TEAR STRIP AT FR 959L/ STRINGER 41L CRACK
- [SDR 04FDEA03388](https://openairdocs.org/sdr/04FDEA03388.md): Connector · dirty · Dec 7, 2004 · N68058 · Doug DC1010 · Passenger/Crew Doors
  > AFTER TAKEOFF R1 DOOR LIGHT CAME ON AND WOULD NOT PRESSURIZE. ATB TO MEM. MEL 52-04-02: FWD CABIN DOOR CAUTION LIGHT INOPERATIVE. CHECKED WIRING ON R-1 DOOR, CLEANED CONNECTOR TO ACTUATOR. PRECAUTIONARY, ACTUATED DOOR MULTIPLE TIMES INSIDE AND OUT, CLEANE
- [SDR 04FDEA02886](https://openairdocs.org/sdr/04FDEA02886.md): Longeron · corroded · Oct 7, 2004 · N68058 · Doug DC1010F · Fuselage Main, Longeron/Stringer
  > LOWER FUSELAGE UNDERWING LONGERON 48R IS CORRODED FROM STATION 1368 TO STATION 1521. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW DC10 SRM 53-00-01 VOL I PAGE 8, FIGURE 1B. REMOVED DAMAGE SECTION OF LONGERON 48R FROM STATION 1330 TO 1521. INSTALLED LONG
- [SDR 04FDEA02885](https://openairdocs.org/sdr/04FDEA02885.md): Longeron · corroded · Oct 7, 2004 · N68058 · Doug DC1010F · Fuselage Main, Longeron/Stringer
  > LOWER FUSELAGE UNDERWING LONGERON 49R IS CORRODED FROM STATION 1368 TO 1521. REMOVED CORROSION LONGERON 49R, FOUND TO BE OUT OF LIMITS. REMOVED LONGERON 49R FROM STATION 1330 TO 1521. FABRICATED LONGERON 49R IAW DAC DWG 7013 AND SPLICE REPAIR IAW DC10 SRM 5
- [SDR 04FDEA02884](https://openairdocs.org/sdr/04FDEA02884.md): Fitting · migrated · Oct 7, 2004 · N68058 · Doug DC1010F · Horizontal Stabilizer Structure
  > LEFT HORIZONTAL STABILIZER INBOARD TRAILING EDGE, STABILIZER TO STABILIZER BOX SAFETY LINK, OUTBOARD ATTACH CLEVIS BUSHING WORN AND MIGRATED THROUGH STABILIZER LOWER INBOARD ACCESS PANEL 334MB. REMOVED FITTING FOR INSTALLATION OF REPAIR BUSHING IAW FEDEX DC10
- [SDR 04FDEA02883](https://openairdocs.org/sdr/04FDEA02883.md): Panel · delaminated · Oct 7, 2004 · N68058 · Doug DC1010F · Horizontal Stabilizer, Plate/Skin
  > LEFT HORIZONTAL STABILIZER 1 EACH PANEL AT STATION XE122 COMPOSITE PANEL AT AFT SPAR TOP SIDE IS DELAMINATED. REPAIRED PANEL BY FABRICATING AND BONDING NEW OUTER SKIN, INNER SKIN, INNER DOUBLER AND CORE IAW DWG ALC7429 AND EA 8-5510-81439 AND TPS 1001 REV E.
- [SDR 04FDEA02859](https://openairdocs.org/sdr/04FDEA02859.md): Panel · delaminated · Oct 1, 2004 · N68058 · Doug DC1010F · Wing, Plate/Skin
  > PANEL 66CT HAS SEVERAL AREAS OF DELAMINATION. REPAIRED BY REMOVING DAMAGE, FABRICATING AND BONDING NEW SKIN, CORE AND DOUBLERS IAW DAC DWG ARC0627 AND EA 8-5710-77619, REFERENCE NON-ROUTINE N00129.
- [SDR 04FDEA02856](https://openairdocs.org/sdr/04FDEA02856.md): Static Port · failed · Oct 1, 2004 · N68058 · Doug DC1010F · Pitot/Static System
  > LEFT PRIMARY STATIC PORT FAILS WAVINESS CHECK. REMOVED LEFT HAND STATIC PORT AND REPLACED HEAT SINK IAW FEDEX DC10 MM 34-11-01-2. REMOVED STATIC PORT AND BLENDED OUT GOUGE ON LEFT HAND RUB PLATE IAW DC10 SRM 53-00-02 VOL 1 AND DC10 SRM 51-71-00 VOL II. INS
- [SDR 04FDEA02855](https://openairdocs.org/sdr/04FDEA02855.md): Ventilator Panel · cracked · Oct 1, 2004 · N68058 · Doug DC1010F · Nacelle/Pylon, Main Frame
  > NR 3 PYLON TOP PANEL 487DR HAS THREE AREAS OF CRACKS. REPAIRED VENTILATOR ASSY P/N AUB7054-501 IAW FEDEX EA 8-5480-77611. LOCATED AND DRILLED VENTILATOR ASSY IAW DC10 SRM 51-31-01 VOL II. VENTILATOR ASSEMBLY TO BE INSTALLED UNDER FEDEX OPS 43R-FIT. REFERE
- [SDR 04FDEA02861](https://openairdocs.org/sdr/04FDEA02861.md): Skin Panel · corroded · Oct 1, 2004 · N68058 · Doug DC1010F · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE CENTER SKIN REQUIRES REMOVAL DUE TO CORROSION FROM STATION 1350 TO 1521, L48L TO L48R. COMPLIED WITH FEDEX EA 8-5330-77624, SKIN SPLICE REPAIR AT STATION 1350-1521 REPAIR. REFERENCE NON-ROUTINE N01775.
- [SDR 04FDEA02819](https://openairdocs.org/sdr/04FDEA02819.md): Panel · delaminated · Sep 27, 2004 · N68058 · Doug DC1010F · Wing, Plate/Skin
  > PANEL 541EB HAS SEVERAL AREAS OF DELAMINATION. REPAIRED PANEL BY FABRICATING AND BONDING NEW INNER SKIN, OUTERSKIN, DOUBLER AND CORE IAW DC10 DRAWING ARC0264 AND EA8-5710-77620.
- [SDR 04FDEA02818](https://openairdocs.org/sdr/04FDEA02818.md): Tube · cracked · Sep 27, 2004 · N68058 · Doug DC1010F · Aircraft Fuel Distribution System
  > LEFT WING LEADING EDGE UPPER PYLON FUEL SAXAPHONE LINE IS CRACKED AT MOUNTING POINT. REMOVED, REPAIRED, REINSTALLED FUEL LINE IAW FEDEX EA 8-2822-77635.
- [SDR 04FDEA02823](https://openairdocs.org/sdr/04FDEA02823.md): Panel · delaminated · Sep 27, 2004 · N68058 · Doug DC1010F · Wing, Plate/Skin
  > PANEL 641CR HAS SEVERAL AREAS OF DELAMINATION. REPAIRED PANEL IAW FEDEX EA 8-5710-77617. REFERENCE NON ROUTINE N00169.
- [SDR 04FDEA02822](https://openairdocs.org/sdr/04FDEA02822.md): Hinge · corroded · Sep 27, 2004 · N68058 · Doug DC1010F · Trailing Edge Flaps
  > LEFT HAND INBOARD FLAP OUTBOARD SUPPORT PIVOT ATTACH POINT OUTBOARD BORE CORRODED. CORROSION EXCEEDS CMM 57-52-01 LIMITS. REPAIRED IAW FEDEX EA 8-5750-77622. REFERENCE NON ROUTINE N00490.
- [SDR 04FDEA02821](https://openairdocs.org/sdr/04FDEA02821.md): Frame · corroded · Sep 27, 2004 · N68058 · Doug DC1010F · Fuselage Main, Frame
  > MAIN CABIN FUSELAGE STATION 1821 HAS CORROSION AT LOWER FRAME END, AS SEEN FROM BULK PIT UPPER TORQUE BOX. CORROSION EXCEEDS LIMITS IAW DC10 SRM 53-00-01 VOL 1. FABRICATED AND INSTALLED REPAIR IAW DC10 SRM 50-30-00 FIGURE 5, VOLUME 1. REFERENCE NON ROUTINE
- [SDR 04FDEA02820](https://openairdocs.org/sdr/04FDEA02820.md): Skin · corroded · Sep 27, 2004 · N68058 · Doug DC1010F · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE CENTER SKIN REQUIRES REMOVAL DUE TO CORROSION, FROM STATION 1350 TO 1521 L48L TO L48R. COMPLIED WITH FEDEX EA 8-5330-77624, SKIN SPLICE REPAIR AT STATION 1350-1521. REFERENCE NON ROUTINE N01775.
- [SDR 04FDEA02832](https://openairdocs.org/sdr/04FDEA02832.md): Panel · corroded · Sep 27, 2004 · N68058 · Doug DC1010F · Horizontal Stabilizer, Plate/Skin
  > RIGHT HORIZONTAL STABILIZER PANEL 344JB HAS CORROSION ON NUMEROUS SPOTS ON INTERIOR SURFACE. REPAIRED PANEL BY FABRICATING AND BONDING NEW OUTER SKIN, INNER SKIN, INNER DOUBLER, OUTER DOUBLER AND CORE IAW TPS 1001 REV E AND FEDEX EA 8-5510-81466. RIGHT HAND
- [SDR 04FDEA02831](https://openairdocs.org/sdr/04FDEA02831.md): Liner · punctured · Sep 27, 2004 · N68058 · Doug DC1010F · Fuselage Main, Structure
  > AFT PIT DOOR JAMB AFT SIDE THRESHOLD PANEL HAS HOLE PUNCTURES ON IT. WELD REPAIRED IAW FEDEX EA 8-5320-77632, REFERENCE NON-ROUTINE.
- [SDR 04FDEA02830](https://openairdocs.org/sdr/04FDEA02830.md): Beam · damaged · Sep 27, 2004 · N68058 · Doug DC1010F · Fuselage, Landing Gear Attach Fittings
  > DURING REMOVAL OF ZERT FITTING BUSHING ON LEFT HAND MAIN LANDING GEAR TRUCK BEAM, FOUND BUSHING TO BE THREADED BUSHINGS, NOT PRESS BUSHING. INSTALLED NEW ZERK FITTING IAW FEDEX EA 8-3212-81257 PART 1 DC10 LANDING GEAR MAIN LANDING GEAR TRUCK BEAM BORE REPAIR
- [SDR 04FDEA02829](https://openairdocs.org/sdr/04FDEA02829.md): Panel · delaminated · Sep 27, 2004 · N68058 · Doug DC1010F · Wing, Plate/Skin
  > PANEL 541CR HAS MANY AREA OF DELAMINATION. REPAIRED PANEL 541CR BY FABRICATING AND BONDING NEW SKINS, DOUBLERS AND CORE IAW TPS 1001 REV E, DAC DWG ARC2906 AND FEDEX EA 8-5710-77618. REFERENCE NON-ROUTINE N00163.
- [SDR 04FDEA02828](https://openairdocs.org/sdr/04FDEA02828.md): Panel · delaminated · Sep 27, 2004 · N68058 · Doug DC1010F · Horizontal Stabilizer, Plate/Skin
  > LEFT HORIZONTAL STABILIZER, 1 EACH PANEL AT STA XE203.5, COMPOSITE PANEL AT AFT SPAR TOP DELAMINATED. REPAIRED BY FABRICATION AND BONDING NEW OUTER AND INNER SKIN, DOUBLERS AND CORE IAW TPS 1001 REV E AND FEDEX EA 8-5510-81441. REFERENCE NON-ROUTINE N00148.
- [SDR 04FDEA02827](https://openairdocs.org/sdr/04FDEA02827.md): Panel · corroded · Sep 27, 2004 · N68058 · Doug DC1010F · Horizontal Stabilizer, Plate/Skin
  > RIGHT HORIZONTAL STABILIZER PANEL 344JB HAS CORROSION ON NUMEROUS SPOTS ON INTERIOR SURFACE. REPAIRED PANEL IAW FEDEX EA 8-5510-81466.
- [SDR 04FDEA02826](https://openairdocs.org/sdr/04FDEA02826.md): Panel · delaminated · Sep 27, 2004 · N68058 · Doug DC1010F · Wing, Plate/Skin
  > RIGHT WING TRAILING EDGE PANEL 641BB DELAMINATED. REPAIRED PANEL IAW FEDEX EA 8-5710-77621, REFERENCE NON ROUTINE N00419.
- [SDR 04FDEA02825](https://openairdocs.org/sdr/04FDEA02825.md): Panel · delaminated · Sep 27, 2004 · N68058 · Doug DC1010F · Wing, Plate/Skin
  > PANEL 636HL HAS SEVERAL AREAS OF DELAMINATION. REPAIRED PANEL IAW FEDEX EA 8-5710-77614. REFERENCE NON ROUTINE N00323.
- [SDR 04FDEA02824](https://openairdocs.org/sdr/04FDEA02824.md): Panel · delaminated · Sep 27, 2004 · N68058 · Doug DC1010F · Wing, Plate/Skin
  > PANEL 541EB HAS SEVERAL AREAS OF DELAMINATION. REPAIRED PANEL IAW FEDEX EA 8-5710-77620, REFERENCE NON ROUTINE N00125.
- [SDR 04FDEA02637](https://openairdocs.org/sdr/04FDEA02637.md): Skin · damaged · Sep 4, 2004 · N68058 · Doug DC1010F · Wing, Plate/Skin
  > LEFT WING TRAILING EDGE SKIN AFT OF MAIN LANDING GEAR LOWER SURFACE REQUIRES FABRICATION. FABRICATED DOUBLER AND SKIN IAW DAC DWG ARC0468, BONDED SKIN AND DOUBLER IAW TPS 1001 REV E AND DAC DWG ARC0468 AND EA 9-5710-81448. ALODINED AND PRIMED CONTACT UPPER S
- [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 04FDEA02643](https://openairdocs.org/sdr/04FDEA02643.md): Pan · gouged · Sep 4, 2004 · N68058 · Doug DC1010F · Nacelle/Pylon, Main Frame
  > NR 2 ENGINE RIGHT HAND 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 DC10 SRM 51-35-01 VOL II. WELD REPAIRED IAW FEDEX EA 8-5410-81450. INSTALLED PAN I
- [SDR 04FDEA02642](https://openairdocs.org/sdr/04FDEA02642.md): Panel · delaminated · Sep 4, 2004 · N68058 · Doug DC1010F · Wing, Plate/Skin
  > PANEL 636 DL HAS SEVERAL AREA OF DELAMINATION. REPAIRED PANEL P/N ARC0566-2 BY FABRICATING AND BONDING NEW SKIN, DOUBLERS AND CORE IAW FEDEX EA 8-5710-77513, DAC DWG ARC0566 AND TPS 1001 REV E, REFERENCE N/R N00321.
- [SDR 04FDEA02638](https://openairdocs.org/sdr/04FDEA02638.md): Panel · delaminated · Sep 4, 2004 · N68058 · Doug DC1010F · Wing, Plate/Skin
  > RIGHT WING TRAILING EDGE PANEL 641 EB HAS MANY AREA OF DELAMINATION. REPAIRED RIGHT WING TRAILING EDGE PANE 641EB BY FABRICATING AND BONDING INNER AND OUTER SKIN, HONEYCOMB CORE AND INNER DOUBLER IAW EA 8-5710-7763, DAC DWG ARC0264 AND TPS 1001 REV E, REFEREN
- [SDR 04FDEA02538](https://openairdocs.org/sdr/04FDEA02538.md): Floorbeam · corroded · Aug 21, 2004 · N68058 · Doug DC1010F · Fuselage Main, Floor Beam
  > AFT PIT, FLOORBEAM CAP BEAM AT STATION 1887.0 HAS EXFOLIATION. REMOVED FLOORBEAM IAW SRM 51-33-01 VOL II. INSTALLED NEW FLOORBEAM AGA 3849-15, (FABRICATED ON NON-ROUTINE N01875) IAW DWG AGA 3849 AND SRM 51-33-01 VOL II. REFERENCE NON-ROUTINE N01814.
- [SDR 04FDEA02491](https://openairdocs.org/sdr/04FDEA02491.md): Duct · gouged · Aug 17, 2004 · N68058 · Doug DC1010F · Engine Thrust Reverser
  > SEVERAL GOUGES ON FORWARD COMPARTMENT COOLING DUCT INSIDE NR 1 OUTBOARD THRUST REVERSER AT NR 1 ENGINE, (NR 1 OUTBOARD THRUST REVERSER UPPER COOLING DUCT). REMOVED DUCT, REPAIRED IAW EA 8-7830-77634, AND DC10 SRM 51-21-01 VOL 2, AND REINSTALLED IAW DC10 MM 20
- [SDR 04FDEA02484](https://openairdocs.org/sdr/04FDEA02484.md): Skin · damaged · Aug 16, 2004 · N68058 · Doug DC1010F · Fuselage Main, Plate/Skin
  > RIGHT HAND PRIMARY STATIC PORT HAS EXTERNAL DOUBLER WITHIN 18 INCHES OF CONTROLLED AREA AT FOUR O'CLOCK POSITION AT FUSELAGE STATION 869 AT LONGERON 48 RIGHT. REMOVED AND REPLACED SKIN AND DOUBLERS IAW FEDEX EA 8-5330-81438, FUSELAGE SKIN SPLICE REPAIR AT ST
- [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 04FDEA02347](https://openairdocs.org/sdr/04FDEA02347.md): Fitting · cracked · Aug 2, 2004 · N68058 · Doug DC1010F · Wing, Center Box
  > CRACKED FITTING, CENTER WING SECTION TO FUSELAGE SPLICE, STATION 1157, LEFT HAND SIDE AT LONGERON 37L, EXTERNAL FITTING. REMOVED DAMAGED FITTING IAW DC10 SRM 51-33-01 VOL II. NEW FITTING FABBED ON FEDEX CARD N00880. LOCATED AND DRILLED FITTING IAW DC10 SRM 51
- [SDR 04FDEA02346](https://openairdocs.org/sdr/04FDEA02346.md): Fitting · corroded · Aug 2, 2004 · N68058 · Doug DC1010F · Fuselage Miscellaneous Structure
  > CORROSION AT THE INTERIOR OF AFT CARGO DOOR UPPER BOX AT LONGERON 27L FITTING AND SEVERAL HARDWARE, STA 1787 TO STA 1841, LONGERON 27L, LBL 101.0 TO LBL 106.0. REMOVED CORROSION, EXCEEDS LIMITS IAW DC10 SRM 53-00-01 VOL I, REMOVED AND REPLACED HEADER BEAM,
- [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

Next page: https://openairdocs.org/deregistered/N68058-2013-03-08/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 = 'N68058' AND deregistration_id = 'N68058-2013-03-08'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N68058-2013-03-08/reports

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