# Service difficulty reports: N68054, cancelled Feb 3, 2024

A list on [N68054, cancelled Feb 3, 2024](https://openairdocs.org/deregistered/N68054-2024-02-03.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 4 · 186 reports

- [SDR FDEA201406081356](https://openairdocs.org/sdr/FDEA201406081356.md): Skin · cracked · Jun 8, 2014 · N68054 · Doug MD1010F · Wing, Plate/Skin
  > FOUND RT WING CRACKED JUST ABOVE ANTI-ICE TELESCOPING DUCT CUT OUT. ACCOMPLISH HFEC IAW NTM PT6 20-30-00. REPAIRED IAW EA 8-5710-T0308735 P1 AND SRM 57-40-01 REPAIR 10.
- [SDR FDEA201406081357](https://openairdocs.org/sdr/FDEA201406081357.md): Skin · cracked · Jun 8, 2014 · N68054 · Doug MD1010F · Wing, Plate/Skin
  > RIGHT WING FUEL PNL DOOR CUT OUT HAS A 1"X1/8" STRIP OF PAINT MISSING & LOOKS LIKE A POSSIBLE CRACK. REQUESTED NDT VERIFY. CONFIRMED & MARKED END CRACK LOCATED RT WING FUEL PNL DOOR CUT OUT IAW NDTSPM PT 6. FABRICATED DOUBLER & FILLER, TREATED & PRIMED RE
- [SDR FDEA201212134289](https://openairdocs.org/sdr/FDEA201212134289.md): Light · inoperative · Dec 13, 2012 · N68054 · Doug MD1010F · Escape Slide
  > R1 DOOR SLIDE TEST LIGHT INOPERATIVE. REMOVED AND REPLACED PRESSURE INDICATION LIGHT ASSY IAW AMM 25-61-03-2, OPS CHECKED GOOD. OK FOR SERVICE.
- [SDR FDEA201206072130](https://openairdocs.org/sdr/FDEA201206072130.md): Coalescer Bag · odor · Jun 7, 2012 · N68054 · Doug MD1010F · Humidity Control System
  > PACK ODOR LIKE DIRTY SOCK. R & R NR 2 AND NR 3 COALESCER BAGS IAW MM 21-54-03-2, RAN PACKS FOR 20 MIN AT FULL HOT, FOUND NO FOUL ODOR IN ACFT AT THIS TIME, OK TO CONTINUE.
- [SDR FDEA201206072129](https://openairdocs.org/sdr/FDEA201206072129.md): Unknown · odor · Jun 7, 2012 · N68054 · Doug MD1010F · Air Distribution System
  > PACK ONE HAS STRONG ODOR. NR 1 COALESCER ALREADY REPLACED, RAN PACKS, NO ODOR AT THIS TIME IAW M/M 21-54-03-2.
- [SDR FDEA201110254643](https://openairdocs.org/sdr/FDEA201110254643.md): Spar Cap · cracked · Oct 25, 2011 · N68054 · Doug MD1010F · Wing Spar
  > RT WING REAR SPAR LOWER CAP EO 8-5710-7-5007, PT 2 INSP FOUND CRACK AT FWD, OTBD HOLE COMPLIED WITH EA 8-5710-156726 FOR RT WING REAR SPAR LOWER CAP REPAIR OF FWD OTBD HOLE.
- [SDR FDEA201110254641](https://openairdocs.org/sdr/FDEA201110254641.md): Door Frame · corroded · Oct 25, 2011 · N68054 · Doug MD1010F · Fuselage Main, Structure
  > AFT CARGO COMPARTMENT DOOR SILL HAS CORROSION AT NUTPLATE HOLES AS MARKED. REMOVED CORROSION AT 12 EA HOLES IAW SRM 51-21-01, 12 EA AREAS ARE WITHIN LIMITS IAW SRM 53-00-01. 1 NUTPLATE HOLE IS OUT OF LIMITS. CUT OUT DAMAGE AND REPAIRED IAW SRM 53-00-01,
- [SDR FDEA201110214618](https://openairdocs.org/sdr/FDEA201110214618.md): Skin · cracked · Oct 21, 2011 · N68054 · Doug MD1010F · Fuselage Main, Plate/Skin
  > AFT FUSELAGE OUTER SKIN IS CRACKED APPROX. 3" AT BS 2132 BETWEEN L4R AND L5R. REMOVED DAMAGE IAW SRM 53-00-01, NDT HFEC CHECKED GOOD IAW NTSPM 06-10-01, FABRICATED REPAIR USING 7075-T6.071 BATCH 0002069744 IAW SRM 53-00-01, FIG 4, SH 2 TREATED AND PRIMED AS
- [SDR FDEA201110214614](https://openairdocs.org/sdr/FDEA201110214614.md): Skin · cracked · Oct 21, 2011 · N68054 · Doug MD1010F · Trailing Edge Flaps
  > RT WING OTBD FLAP UPPER SURFACE 21" FROM THE OTBD EDGE HAS 3EA CRACKS AROUND FASTENER HOLES. REPAIRED RT WING OTBD FLAP UPPER SURFACE CRACKS AT 21" FROM OTBD EDGE IAW SRM 57-10-00, FIG 6, SH 1-3. MAJOR REPAIR.
- [SDR FDEA201110214613](https://openairdocs.org/sdr/FDEA201110214613.md): Skin · cracked · Oct 21, 2011 · N68054 · Doug MD1010F · Trailing Edge Flaps
  > RT WING OTBD FLAP UPPER SURFACE STA XORS 587 HAS 2 EA CRACKS AROUND FASTENER HOLES. REPAIRED RT WING OTBD FLAP UPPER SURFACE AT STA XORS 587 IAW SRM 57-10-00 VOL 1,FIG 85 SHEET 3. MAJOR REPAIR.
- [SDR FDEA201110174551](https://openairdocs.org/sdr/FDEA201110174551.md): Doubler · worn · Oct 17, 2011 · N68054 · Doug MD1010F · Fuselage Main, Plate/Skin
  > AFT FUSELAGE ACCESS DOOR 311AB CUTOUT DOUBLER WORN AND RT SIDE IS ALMOST KNIFE EDGE. REPAIRED IAW EA8-5310-150998
- [SDR FDEA201110164540](https://openairdocs.org/sdr/FDEA201110164540.md): Cargo Track · corroded · Oct 16, 2011 · N68054 · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > AFT CARGO COMPARTMENT SEAT TRACK, RBL 25 BETWEEN FS 1940 TO FS 1964, GOUGED AND CORRODED. R & R AFT CARGO COMPARTMENT SEAT TRACK AT IAW SRM 51-31-01, MAJOR REPAIR.
- [SDR FDEA201110164539](https://openairdocs.org/sdr/FDEA201110164539.md): Cargo Track · corroded · Oct 16, 2011 · N68054 · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > AFT CARGO COMPARTMENT SEAT TRACK AT RBL 25 BETWEEN FS 1800 TO 1920, HAS GOUGED AND CORRODED. R & R AFT CARGO COMPARTMENT SEAT TRACK IAW SRM 51-31-01, MAJOR REPAIR.
- [SDR FDEA201110154528](https://openairdocs.org/sdr/FDEA201110154528.md): Cargo Track · gouged · Oct 15, 2011 · N68054 · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > AFT CARGO BAY CARGO TRACK, LBL 25 BETWEEN BS 1920-1964 GOUGED AND CORRODED. REMOVED, AND FABRICATED, REPAIR SPLICES AND PLATES AND REPLACED CARGO TRACK IAW SRM 53-70-00 FIG.1 AND SRM 51-31-01. MAJOR REPAIR.
- [SDR FDEA201110154530](https://openairdocs.org/sdr/FDEA201110154530.md): Floorbeam · corroded · Oct 15, 2011 · N68054 · Doug MD1010F · Fuselage Main, Floor Beam
  > AFT CARGO COMPARTMENT FLOORBEAM BS 1902 IS CORRODED FROM RBL15 TO LBL15. REMOVED DAMAGE IAWSRM 53-00-01 FIG.8 AND SRM 51-31-01. FABRICATED REPAIR ANGLE AND FILLER IAW SRM 53-00-01. INSTALLED REPAIR ANGLE AND FILLER IAW SRM 53-00-01 FIG 8 AND SRM 51-31-01. M
- [SDR FDEA201110144503](https://openairdocs.org/sdr/FDEA201110144503.md): Skin · punctured · Oct 14, 2011 · N68054 · Doug MD1010F · Trailing Edge Flaps
  > LEFT WING, INBD FLAP, LOWER OTBD SKIN PUNCTURED. TRIMMED OUT DAMAGE IAW 57-00-01, HFEC IAW NTSPM 06-10-01. NO CRACKS NOTED. FABRICATED SKIN DOUBLER, TEE DOUBLERS, TEE FILLER AND SKIN FILLER IAW SRM 57-00-01 FIG.3 INSTALLED ALL REPAIR PARTS IAW SRM 57-00-0
- [SDR FDEA201110124454](https://openairdocs.org/sdr/FDEA201110124454.md): Pulley · worn · Oct 12, 2011 · N68054 · Doug MD1010F · Passenger/Crew Doors
  > L1 DOOR FWD DRIVE TRACK, UPPER FORWARD PULLEY WORN. FURTHER INSPECTION FOUND PULLEY TO BE SPLIT. MINOR REPAIR R & R L1 DOOR UPPER FWD DRIVE PULLEY IAW SRM 51-31--01 AND MM 52-11-00. NO RIG DISTURBED AND OPS CHECKED GOOD IAW MM 52-11-00-5.
- [SDR FDEA201110114424](https://openairdocs.org/sdr/FDEA201110114424.md): Shear Tie · cracked · Oct 11, 2011 · N68054 · Doug MD1010F · Fuselage Internal Mounting Structure
  > MCD CABIN RT SIDEWALL AT STA 1800 AT L-18 SHEAR TIE CRACKED. REMOVED AND REPLACED DAMAGED SECTION OF SHEAR TIE IAW SRM 53-30-00 FIG 10, SRM 51-31-01 AND SRM 51-21-02. MAJOR REPAIR.
- [SDR FDEA201110104409](https://openairdocs.org/sdr/FDEA201110104409.md): Seat Track · damaged · Oct 10, 2011 · N68054 · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT RBL 45.5 BETWEEN FS 1821 AND FS 1841 UPPER LOBE HAS ELONGATED HOLE. REPLACEMENT ACCOMPLISHED ON NON-ROUTINE N00471 AND IS CLASSIFIED AS MAJOR REPAIR.
- [SDR FDEA201110104408](https://openairdocs.org/sdr/FDEA201110104408.md): Seat Track · damaged · Oct 10, 2011 · N68054 · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT RBL 45.5 BETWEEN FS 1801 AND FS 1821 UPPER LOBE HAS ELONGATED HOLES. REMOVED DAMAGED SEAT TRACK SECTION IAW SRM 53-70-00 FIG 1. FABRICATED SEAT TRACK SECTION, REPAIR SPLICES AND PLATES. INSTALLED REPAIR PARTS IAW SRM 53-70-00 AND SRM 51-31-01
- [SDR FDEA201110044289](https://openairdocs.org/sdr/FDEA201110044289.md): Seat Track · damaged · Oct 4, 2011 · N68054 · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT LBL45.5 BETWEEN FS 1621 AND 1641 UPPER LOBE HAS ELONGATED HOLE. REMOVED DAMAGED SEAT TRACK SECTION, FABRICATED TRACK, REPAIR SPLICES AND PLATES IAW SRM 53-70 00 FIG.1 VOL. 1. INSTALLED SEAT TRACK, SPLICES AND PLATES IAW SRM 53-70-00 FIG.1.
- [SDR FDEA201110044288](https://openairdocs.org/sdr/FDEA201110044288.md): Seat Track · gouged · Oct 4, 2011 · N68054 · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT LBL 45.5 BETWEEN FS 1721 AND FS1741 LOBE IS GOUGED. REMOVED DAMAGED SEAT TRACK SECTION, FABRICATED TRACK, REPAIR SPLICES AND PLATES IAW SRM 53-70-00 FIG.1 VOL.1. INSTALLED SEAT TRACK, SPLICES AND PLATES IAW SRM 53-70-00 FIG.1. MAJOR REPAIR
- [SDR FDEA201110044290](https://openairdocs.org/sdr/FDEA201110044290.md): Seat Track · gouged · Oct 4, 2011 · N68054 · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT LBL 45.5 BETWEEN FS 1621 AND FS 1641 UPPER SURFACE IS GOUGED. REMOVED DAMAGED SEAT TRACK SECTION IAW SRM 53-70-00 FIG.1 FABRICATED REPAIR SLICES AND PLATES IAW SRM 53-70-00 FIG 1. INSTALLED TRACK SECTION, SPLICES AND PLATES IAW SRM 53-70-00 F
- [SDR FDEA201110044291](https://openairdocs.org/sdr/FDEA201110044291.md): Seat Track · damaged · Oct 4, 2011 · N68054 · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT LBL 45.5, FS 1721-1741 UPPER LOBE HAS ELONGATED HOLES. REMOVED DAMAGED SEAT TRACK SECTION, FABRICATED REPAIR SLICES AND PLATES AND INSTALLED IAW SRM 53-70-00 FIG 1.
- [SDR FDEA201102260785](https://openairdocs.org/sdr/FDEA201102260785.md): Oxygen Mask · leaking · Feb 26, 2011 · N68054 · Doug MD1010F · Crew Oxygen System
  > AFTER O2 MASK WERE USED IN FLIGHT ALL 3 O2 BOTTLES DROPPED TO 0 PSI. SERVICED ALL 3, CREW O2 BOTTLES PER AMM 12-14-35. CHECKED ALL BOTTLES AND MASK SYSTEMS FOR LEAKS PER AMM 35-11-00-06-0. FOUND ONE RT COURIER MASK SLIGHTLY LEAKING AT INTIAL BOTTLE RESERVI
- [SDR FDEA201010284183](https://openairdocs.org/sdr/FDEA201010284183.md): Bungee Cylinder · damaged · Oct 28, 2010 · N68054 · Doug MD1010F · Landing Gear Retraction/Extension System
  > AFTER T/O, LT MAIN REMAINED UNSAFE FOLLOWED QRH CYCLED NO CHANGE. GEAR APPEARED TO BE DOWN ENTIRE TIME. UNEVENTFUL LANDING. REMOVED & REPLACED L/H MLG BUNGEE CYCLINDER ASSY ACFT OK FOR SERVICE.
- [SDR 07FDEA05029](https://openairdocs.org/sdr/07FDEA05029.md): Seat Track · damaged · Dec 11, 2007 · N68054 · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN, BS 1240, LBL 48, SEAT TRACK SCALLOP CHIPPED AND WORN RE-EVALUATED TRACK. TRACK HAS CHIPPED/BROKEN AREAS. OUT OF LIMITS IAW DC/MD10-10 SRM 53-70-00 VOL I PG 21 AND 22. REMOVED DAMAGED SECTION AND INSTALLED FABED/NEW SECTION IAW DC/MD10-10 SRM 51-
- [SDR 07FDEA05016](https://openairdocs.org/sdr/07FDEA05016.md): Door Frame · corroded · Dec 7, 2007 · N68054 · Doug MD1010F · Fuselage Main, Structure
  > MAIN CARGO DOOR JAMB TOP SURFACE UNDER NR 5 SPOOL FITTING HAS EXFOLIATION, STA 712. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IN REF TO MD/DC10-10 SRM 53-00-01 FIG 1 VOL I. ORIGIONAL.100, REMOVED.047, REMAINING.053. LOCATION OF DAMAGE AT STA 712
- [SDR 07FDEA05015](https://openairdocs.org/sdr/07FDEA05015.md): Door Frame · corroded · Dec 7, 2007 · N68054 · Doug MD1010F · Fuselage Main, Structure
  > MAIN CARGO DOOR LOWER JAMB TOP SURFACE MOST AFT PART OF JAMB AT STA 766 HAS SURFACE CORROSION. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IN REF TO MD/DC10-10 SRM 53-00-01 VOL I. ORIGIONAL.100, REMOVED.027, REMAINING.073. LOCATION OF DAMAGE STA 766,
- [SDR 07FDEA04989](https://openairdocs.org/sdr/07FDEA04989.md): Seat Track · damaged · Dec 3, 2007 · N68054 · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN APPROX AT STA 1256 AND STA 1264 SEAT TRACK SCALLOPS (3EA) ELONGATED (N7513) AT LBL 48 EVALUATED SEAT TRACK FOUND TO BE OUT OF LIMITS IAW DC/MD10 SRM 53-70-00 VOL I PG 21 AND 22. MAT ID S4929150 PO NR 595343.1 IAW DC/MD10 SRM 53-42-01 FIG 5 VOL III.
- [SDR 07FDEA04988](https://openairdocs.org/sdr/07FDEA04988.md): Seat Track · damaged · Dec 3, 2007 · N68054 · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN FLOOR TRACK SCALLOP BROKEN OUT AT STA 1139 LBL 48 EVALUATED SEAT TRACK, FOUND BROKEN SCALLOP, OUT OF LIMITS IAW DC/MD10 SRM 53-70-00 VOL I PG 21 AND 22. REMOVED AND REPLACED OUT OF LIMIT SECTION IAW DC/MD10 SRM 51-31-01 VOL II PG 1 AND DC/MD10 SRM 51-
- [SDR 07FDEA04987](https://openairdocs.org/sdr/07FDEA04987.md): Seat Track · corroded · Dec 3, 2007 · N68054 · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN APPROX AT STA 1531 LBL 27 SEAT TRACK HAS CORROSION. REMOVED AND REPLACED SEAT TRACK AT STA 1490 TO 1531 LBL 27 IAW DC-10/MD-10 SRM 53-70-00, VOL I, FIG 1.
- [SDR 07FDEA04931](https://openairdocs.org/sdr/07FDEA04931.md): Seat Track · damaged · Nov 26, 2007 · N68054 · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN FLOOR TRACK SCALLOP BROKEN OUT AT STA 792 LBL 49. CHECK LIMITS AND IS OUT OF LIMITS IAW DC/MD10-10 SRM 53-70-00 VOL I PG 21. REMOVED SEAT TRACK IAW DC/MD10-10 SRM 51-31-01 VOL II PG 1. FABRICATED SPLICE PLATE AND SPLICE HAT IAW DC/MD10-10 S
- [SDR 07FDEA04930](https://openairdocs.org/sdr/07FDEA04930.md): Seat Track · damaged · Nov 26, 2007 · N68054 · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN FLOOR TRACK SCALLOP BROKEN OUT AT STA 1059 LBL 48. FOUND TO BE OUT OF LIMITS IAW DC/MD10-10 SRM 53-70-00 PGS 21 & 22 VOL I REMOVED TRACK IAW DC/MD10-10 SRM 51-31-01 VOL II PGS 1-10. IAW DC/MD10-10 SRM 53-42-01 VOL III PGS 13 & 14. FABRICATED SEAT T
- [SDR 07FDEA04929](https://openairdocs.org/sdr/07FDEA04929.md): Seat Track · gouged · Nov 26, 2007 · N68054 · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN FLOOR TRACK GOUGED AT STA 1119 RBL 48 2 EACH SCALLOPS.
- [SDR 07FDEA04928](https://openairdocs.org/sdr/07FDEA04928.md): Seat Track · gouged · Nov 26, 2007 · N68054 · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN FLOOR TRACK GOUGED AT STA 1119 RBL 48 2 EACH SCALLOPS. BLENDED AREA.500 MAX LIMIT GAP.510 REMAIN. OUT OF LIMITS IAW DC/MD10-10 SRM 53-70-00 VOL I PG 21 & 22. MAT ID TRACK, SPLICE HAT & PLATE. REMOVED DAMAGED TRACK INSTALLED NEW SECTION IAW DC/MD10-1
- [SDR 07FDEA04927](https://openairdocs.org/sdr/07FDEA04927.md): Seat Track · worn · Nov 26, 2007 · N68054 · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > FOUND MAIN CABIN AT STA 1441 RBL 48 SEAT TRACK WORN. BLENDED SEAT TRACK, WIDTH OF SCALOP HAS.200 REMAINING MIN IS.260 OUT OF LIMITS IAW DC 10 SRM 53-70-00 VOL I PG 21". REMOVED AND REPLACED DAMAGED SECTION OF TRACK IAW DC/MD10 51-31-01. ALODINED & PRIME
- [SDR 07FDEA04926](https://openairdocs.org/sdr/07FDEA04926.md): Seat Track · damaged · Nov 26, 2007 · N68054 · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > FOUND MAIN CABIN, BS 1085, RBL 28, SEAT TRACK SCALLOP CHIPPED. BLENDED AREA; CHECKED LIMITS. GAP BETWEEN SCALLOPS IS.520 MAX ALLOWED IS.500 OUT OF LIMITS IAW DC/MD10-10 SRM 53-70-00 VOL I PG 21. REMOVED DAMAGED TRACK SECTION AND INSTALLED NEW SECTION IAW
- [SDR 07FDEA04925](https://openairdocs.org/sdr/07FDEA04925.md): Angle · chafed · Nov 26, 2007 · N68054 · Doug MD1010F · Nacelle/Pylon Miscellaneous Structure
  > NR 1 PYLON THRUST LINK RUBBING AGAINST WING O/B THRUST ANGLE, STA YN348 CENTERED THRUST LINK, CLEANED AREA AROUND ATTACHMENT PIN & BUSHING, INSPECTED AREA OF BEARING & BUSHING IAW FEDEX WORK CARD 54X1201ALI-P1 LUBED THRUST LINK BEARING IAW FEDEX MM 12-21-02
- [SDR 07FDEA04924](https://openairdocs.org/sdr/07FDEA04924.md): Seat Track · damaged · Nov 26, 2007 · N68054 · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN FLOOR TRACK SCALLOP BROKEN OUT AT STA 814 LBL 29. CHECKED LIMITS ON SEAT TRACK SCALLOPS. SCALLOPS TO SCALLOPS IS.510 OUT OF LIMITS IAW DC/MD10-10 SRM 53-70-00 VOL I PG 21. DIAL CALIPERS USED T8278D. REMOVED SEAT TRACK IAW DC/MD10-10 SRM 51-
- [SDR 07FDEA04909](https://openairdocs.org/sdr/07FDEA04909.md): Door Frame · corroded · Nov 23, 2007 · N68054 · Doug MD1010F · Fuselage Main, Structure
  > MAIN CARGO DOOR LOWER JAMB AT NR 7 SPOOL LOCATION, ALL FOUR HOLES (A, B, C, D) HAD EVIDENCE OF CORROSION. REAMED HOLES A,B,D TO.517 AND HOLE D TO.484 TO REMOVE CORROSION IN REF TO MD/DC10-10 SRM 53-50-01 FIG 17 VOL I. ACCOMPLISHED BHEC IN REF TO NTSPM 06-
- [SDR 07FDEA04908](https://openairdocs.org/sdr/07FDEA04908.md): Door Frame · corroded · Nov 23, 2007 · N68054 · Doug MD1010F · Fuselage Main, Structure
  > MAIN CARGO DOOR LOWER JAMB AT NR 6 SPOOL LOCATION, ALL 4 HOLES (A, B, C, D) HAD EVIDENCE OF CORROSION. REAMED HOLES A,B,C TO 0517 AND HOLE D TO.484 TO REMOVE CORROSION IN REF TO MD/DC10-10 SRM 53-50-00 FIG 17 VOL I. ACCOMPLISHED BHEC IN REF TO NTSPM 06-10-
- [SDR 07FDEA04907](https://openairdocs.org/sdr/07FDEA04907.md): Door Frame · corroded · Nov 23, 2007 · N68054 · Doug MD1010F · Fuselage Main, Structure
  > MAIN CARGO DOOR LOWER JAMB AT NR 5 SPOOL LOCATION, ALL 4 HOLES (A, B, C, D) HAD EVIDENCE OF CORROSION. REAMED HOLES A,B,D TO.517 AND HOLE D TO.484 TO REMOVE CORROSION IN REF TO MD/DC10-10 SRM 53-50-01 FIG 17 VOL I. ACCOMPLISHED BHEC IN REF TO NTSPM 06-10-
- [SDR 07FDEA04906](https://openairdocs.org/sdr/07FDEA04906.md): Door Frame · corroded · Nov 23, 2007 · N68054 · Doug MD1010F · Fuselage Main, Structure
  > MAIN CARGO DOOR LOWER JAMB AT NR 4 SPOOL LOCATION, ALL 4 HOLES (A, B, C, D) HAD EVIDENCE OF CORROSION. REAMED HOLES A,B,C TO.460 TO REMOVE CORROSION. WITHIN LIMITS OF MD/DC10-10 SRM 53- 50-00 FIG 17 VOL I. HOLE D REAMED TO REMOVE CORROSION AND INSTALLED B
- [SDR 07FDEA04905](https://openairdocs.org/sdr/07FDEA04905.md): Door Frame · corroded · Nov 23, 2007 · N68054 · Doug MD1010F · Fuselage Main, Structure
  > MAIN CARGO DOOR LOWER JAMB AT NR 2 SPOOL LOCATION, ALL 4 HOLES (A, B, C, D) HAD EVIDENCE OF CORROSION. REAMED HOLES A,B,C,D TO REMOVE CORROSION AND INSTALLED REPAIR BUSHINGS. FOUND REPAIR BUSHINGS WOULD NOT MEET THE LIMITS STATED IN MD/DC10-10 SRM 53-50-00
- [SDR 07FDEA04904](https://openairdocs.org/sdr/07FDEA04904.md): Door Frame · corroded · Nov 23, 2007 · N68054 · Doug MD1010F · Fuselage Main, Structure
  > MAIN CARGO DOOR LOWER JAMB AT NR 1 SPOOL LOCATION, ALL 4 HOLES (A, B, C, D) HAD EVIDENCE OF CORROSION. REAMED HOLES A,B,C,D TO REMOVE COROSION AND INSTALLED REPAIR BUSHINGS. FOUND REPAIR BUSHINGS WOULD NOT MEET THE LIMITS STATED IN MD/DC10-10 SRM 53-50-00 F
- [SDR 07FDEA04903](https://openairdocs.org/sdr/07FDEA04903.md): Beam · corroded · Nov 23, 2007 · N68054 · Doug MD1010F · Fuselage Main, Structure
  > MAIN CARGO DOOR JAMB TOP SURFACE UNDER CENTERING GUIDE HAS SURFACE CORROSION, STA 660. REMOVED AND REPLACED BEAMS ACA7225-1 AND ACA7226-1 IN REF TO DAC DRAWING ACA7224 REV G AND DC/MD10-10 SRM 51-31-01 VOL II PG 1, MD/DC10-10 SRM 51-33-01 VOL II PG 1 AND DC/
- [SDR 07FDEA04799](https://openairdocs.org/sdr/07FDEA04799.md): Skin · cracked · Nov 15, 2007 · N68054 · Doug MD1010F · Horizontal Stabilizer, Plate/Skin
  > RT HORIZONTAL STAB UPPER REAR SKIN PANEL HAS APPROXIMATELY A I/2 INCH LONG CRACK INDICATION. REPAIRED RIGHT HAND HORIZONTAL STAB SKIN PANEL IN REFERENCE TO EA 8-5510-109228.
- [SDR 07FDEA02092](https://openairdocs.org/sdr/07FDEA02092.md): Door Frame · corroded · Jun 7, 2007 · N68054 · Doug MD1010F · Fuselage Main, Structure
  > EXFOLIATION CORROSION LOCATED AT LOWER AFT CARGO DOOR CUTOUT, FWD LOWER CORNER. CORROSION EXCEEDED SRM LIMITS AFTER REMOVAL, REQUIRED EA TO FLY UNTIL NEXT C CHECK.
- [SDR 06FDEA03090](https://openairdocs.org/sdr/06FDEA03090.md): Loop · faulty · Aug 26, 2006 · N68054 · Doug MD1010F · Pneumatic Indicating System
  > CLIMBOUT FROM MEMPHIS GOT A LEVEL 3 AIR MAN NR 2 FAILED WARNING WENT AWAY AFTER THROTTLE WAS AT IDLE FOR A COUPLE OF MINUTES, DUMPED 6000 LBS FUEL FOR LANDING. ACN RELEASED FOR SERVICE PER MEL/CDL: 36-23-01-02 CATEGORY: C EXPIRATION: 05SEP06 "MEL 36-23-01-02

Next page: https://openairdocs.org/deregistered/N68054-2024-02-03/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 = 'N68054' AND deregistration_id = 'N68054-2024-02-03'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N68054-2024-02-03/reports

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OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.