# Service difficulty reports: N68057, cancelled Apr 23, 2020

A list on [N68057, cancelled Apr 23, 2020](https://openairdocs.org/deregistered/N68057-2020-04-23.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 · 73 reports

- [SDR FDEA201503190989](https://openairdocs.org/sdr/FDEA201503190989.md): Switch · dirty · Mar 19, 2015 · N68057 · Doug MD1010F · Passenger/Crew Doors
  > DOOR 1 LT FAILED OPEN FROM OUTSIDE & INSIDE. CYCLED SLIDE ARM LEVER & OPENED WITH DOOR SWITCH. INSPECTED & CLEANED DOOR SWITCH IAW AMM 52-10-01-6. DOOR OPERATIONS CHECKED NORMAL IAW AMM 52-10-01-5. ACFT OK FOR SERVICE.
- [SDR FDEA201407191858](https://openairdocs.org/sdr/FDEA201407191858.md): Skin · cracked · Jul 19, 2014 · N68057 · Doug MD1010F · Fuselage Main, Plate/Skin
  > ON POST FLIGHT WALK AROUND FOUND FUSELAGE SKIN CRACKED AT NR 1 PACK DOOR CUT OUT UPPER AFT CORNER. INSTALLED DOUBLER, TRIPLER & FILLER IAW SRM 53-50-00 FIG 3A & EA.
- [SDR FDEA201406141448](https://openairdocs.org/sdr/FDEA201406141448.md): Skin · cracked · Jun 14, 2014 · N68057 · Doug MD1010F · Wing, Plate/Skin
  > FOUND A CRACK ON RT WING SKIN AT NR 3 SLAT TRACK BETWEEN NR 1 & 2 SLATS. TRIMMED OUT DAMAGED AREA. PERFORMED INTERNAL & EXTERNAL VISUAL INSPECTION WITH NO ADDITIONAL DAMAGE NOTED. HFEC INSPECTION DONE WITH NO CRACKS NOTED. REPAIRED IAW EA 8-5730-T0308776
- [SDR FDEA201406091367](https://openairdocs.org/sdr/FDEA201406091367.md): Skin · cracked · Jun 9, 2014 · N68057 · Doug MD1010F · Wing, Plate/Skin
  > FOUND TWO CRACKS ON RT WING TAI DUCT CUT OUT. VERIFIED CRACKS IAW NDT SPM PART 6. REPAIRED IAW EA 8-5710-T0308893 & SRM.
- [SDR FDEA201406091368](https://openairdocs.org/sdr/FDEA201406091368.md): Skin · cracked · Jun 9, 2014 · N68057 · Doug MD1010F · Wing, Plate/Skin
  > DURING POST FLIGHT INSPECTION, FOUND POSSIBLE LT WING LE CRACK AT REFUEL DOOR INBD CORNER CUT OUT. CONFIRMED CRACK BY HFEC INSPECTION IAW NDTSPM PT 6 CRACK TERMINATES AT FASTENER. CUT OUT CRACKED AREA IAW SRM 57-10-00 FIG 68 SHEET 2. COMPLIED WITH HFEC ON
- [SDR FDEA201406091366](https://openairdocs.org/sdr/FDEA201406091366.md): Skin · cracked · Jun 9, 2014 · N68057 · Doug MD1010F · Wing, Plate/Skin
  > FOUND TWO CRACKS IN LEFT WING TAI DUCT. VERIFIED CRACK IAW NDT SPM PART 6. REPAIRED IAW EA.
- [SDR FDEA201312223028](https://openairdocs.org/sdr/FDEA201312223028.md): Transmitter · failed · Dec 22, 2013 · N68057 · Doug MD1010F · Fuel Indicating System
  > AT FL 320, NOTICED NR 2 FUEL FLOW 16150 PPH, ALL OTHER INDICATIONS NORMAL. FUEL USED SHOWED NR 2 HAD USED 2200 LBS MORE THAN 1 & 3. FUEL REMAINING WAS IN AGREEMENT WITH FUEL USED. WHEN THROTTLE RETARDED, FUEL FLOW REDUCED TO APPROXIMATELY 11000 PPH AT IDLE
- [SDR FDEA201305100968](https://openairdocs.org/sdr/FDEA201305100968.md): Fitting · cracked · May 10, 2013 · N68057 · Doug MD1010F · Fuselage Main, Attach Fittings
  > MAIN CARGO DOOR FRAME NR 1 SPOOL LOWER FITTING CRACKED IN FOUR LOCATIONS. VERIFIED WITH HFEC IAW NDT SPM93K0393, CRACK RUNS THOUGH FITTING. R & R MAIN CARGO DOOR FRAME SPOOL LOWER FITTING. IAW SRM 51-33-01, VOL II.
- [SDR FDEA201301140091](https://openairdocs.org/sdr/FDEA201301140091.md): Strut · damaged · Jan 14, 2013 · N68057 · Doug MD1010F · Nose/Tail Landing Gear Strut/Axle
  > AFTER T/O LDG GEAR HANDLE WOULD NOT RAISE. QRH C/W. HANDLE RAISED & ALL IN FLIGHT SYSTEMS OPERATED NORMALLY. R & R THE NLG ASSY, REF WC 32T2101 AND 32T2701.
- [SDR FDEA201301040056](https://openairdocs.org/sdr/FDEA201301040056.md): Intercostal · corroded · Jan 4, 2013 · N68057 · Doug MD1010F · Fuselage Miscellaneous Structure
  > LEFT MLG WHEEL WELL AFT WALL LOWER SHELF HAS THE INTERCOSTAL JUST BELOW THE FLAP BUSS CABLE PULLEYS WITH A LARGE AREA BULGED. INSTALLED NEW INTERCOSTAL REF. SRM 51-31-01.
- [SDR FDEA201212294396](https://openairdocs.org/sdr/FDEA201212294396.md): Control Unit · malfunctioned · Dec 29, 2012 · N68057 · Doug MD1010F · Landing Gear Retraction/Extension System
  > AFTER TAKEOFF LANDING GEAR HANDLE WOULD NOT RAISE. COMPLIED WITH QRH THEN GOT LEVEL 1 ANTI-SKID NO TEST ALERT. REMAINED ON UNTIL GEAR HANDLE DOWN. ANTI-SKID ALERT WENT OUT. ANTI-SKID WORKED ON LANDING ROLL OUT. LANDED WITHOUT INCIDENT. MX REMOVED AND REPL
- [SDR FDEA201209153328](https://openairdocs.org/sdr/FDEA201209153328.md): Scavenge Pump · leaking · Sep 15, 2012 · N68057 · Doug MD1010F · Turbine Engine Oil System
  > DURING CLIMB NR 1 OIL QUANTITY INDICATED '0'. ALL OTHER INDICATIONS NORMAL INITALLY. IN CRUISE NR 1 OIL PRESS DROPPED TO 14 PSI WITH AN AMBER INDICATION. CONFERRED WITH MAINT. THROUGHOUT, QRH COMPLIED WITH. DIVERTED. UPON ARRIVAL CHECKED NR 1 ENG. OIL, C
- [SDR FDEA201204241542](https://openairdocs.org/sdr/FDEA201204241542.md): Power Supply · failed · Apr 24, 2012 · N68057 · Doug MD1010F · Emergency Lighting
  > DURING PREFLIGHT EMERGENCY LIGHT TEST FAILED. R & R EMERGENCY LIGHTS POWER SUPPLY IAW MM 33-51-01-4, OPS CHECKS NORMAL.
- [SDR FDEA201111164931](https://openairdocs.org/sdr/FDEA201111164931.md): Sensor · failed · Nov 16, 2011 · N68057 · Doug MD1010F · Engine Indicating System
  > ON TAKEOFF ROLL N2 VIA FAIL. REJECT AT 60 KTS. R & R NR 1, ENG N1 SENSOR.
- [SDR FDEA201111154928](https://openairdocs.org/sdr/FDEA201111154928.md): Sensor · failed · Nov 15, 2011 · N68057 · Doug MD1010F · Engine RPM Indicating System
  > NR 3 ENGINE N1 GAUGE FAILED ON DEPARTURE ROLL ALONG WITH AUTOTHROTTLE OFF - "VIA 1 FAIL" AND "VIA 2 FAIL" LEVEL 1 ALERTS. VIA 1 FAULT HISTORY SHOWED NR 3 ENGINE N1 DISAGREE AND VIA 2 SHOWED NR 3 ENGINE N1 INTERMITTANT. FCC'S 1 & 2 LIST NR 3 ENG TACH FAULT
- [SDR FDEA201110124425](https://openairdocs.org/sdr/FDEA201110124425.md): Windshield · failed · Oct 12, 2011 · N68057 · Doug MD1010F · Flight Compartment Windows
  > CAPT'S WINDSHIELD ARCING & SHATTERED. SHORTED IN WINDOW AT 18000 FT. REPLACED THE CAPT'S WINDSHIELD REF MM 56-11-00-2.
- [SDR FDEA201107192814](https://openairdocs.org/sdr/FDEA201107192814.md): Floorbeam · cracked · Jul 19, 2011 · N68057 · Doug MD1010F · Fuselage Main, Floor Beam
  > FLOORBEAM TEE CRACKED THROUGH ALL SIDES AT STA 1156 L29R. REPAIRED CRACKED FLOORBEAM REF SRM 53-30-00 FIG 7. COMPLIED WITH EA 8-5310-147795.
- [SDR FDEA201012024537](https://openairdocs.org/sdr/FDEA201012024537.md): Lamp · inoperative · Dec 2, 2010 · N68057 · Doug MD1010F · Emergency Equipment
  > R1 DOOR PRESSURE, PRESS TO TEST INDICATOR INOP. FOUND P/N 387 HIGH VOLTAGE LAMPS IN DOOR SLIDE PUSH BUTTON SWT. INSTALED P/N 368 LAMPS PER IPC. GRD OPS CHECKS OK.
- [SDR FDEA200911093915](https://openairdocs.org/sdr/FDEA200911093915.md): Actuator · damaged · Nov 9, 2009 · N68057 · Doug MD1010F · Trailing Edge Flap Actuator
  > DURING WALK AROUND, FOUND LT OTBD FLAP INBD ACT BROKEN. INSPECTED FLAP FOR ANY PULLED RIVETS AND NONE FOUND. INSPECTED OTBD FLAP ACT"S ATTACKING POINTS TO MAKE SURE NO OTHER DAMAGE TO FLAPS, NONE FOUND. INSPECTED ALL OTHER FLAPS AND NO DAMAGE FOUND IAW AMM-
- [SDR FDEA200906102018](https://openairdocs.org/sdr/FDEA200906102018.md): Smoke Detector · malfunctioned · Jun 10, 2009 · N68057 · Doug MD1010F · Smoke Detection
  > DECENDING THRU 14,000` RECEIVED "CARGO FIRE ALERT" COMPLIED WITH QRH AND DISCHARGED BOTH FIRE BOTTLES. NEVER HAD ANY SECONDARY INDICATIONS OF FIRE. REMOVED AND REPLACED ALL LOWER CARGO COMPARTMENT SMOKE DETECTOR PER MM 26-14-01-4. INSTALLED NR 2 CARGO
- [SDR FDEA200807012617](https://openairdocs.org/sdr/FDEA200807012617.md): Seal · worn · Jul 1, 2008 · N68057 · Doug MD1010F · Flight Compartment Windows
  > LOUD NOISE THAT APPEARED TO COME FROM THE CAPT'S SLIDING WINDOW AREA. A VIBRATION COULD BE FELT ON THE POST IN THE WINDOW ARM. BUT COMMUNICATION WAS NEARLY IMPOSSIBLE WITH ATC. EVENTUALLY AN EMERGENCY WAS DECLARED. LOWER ALTITUDE AND LOWER AIRSPEED HELPED
- [SDR 08FDEA02617](https://openairdocs.org/sdr/08FDEA02617.md): Window Frame · damaged · Jul 1, 2008 · N68057 · Doug MD1010F · Fuselage Main, Structure
  > LOUD NOISE THAT APPEARED TO COME FROM THE CAPT'S SLIDING WINDOW AREA. A VIBRATION COULD BE FELT ON THE POST IN THE WINDOW ARM. BUT COMMUNICATION WAS NEARLY IMPOSSIBLE WITH ATC. EVENTUALLY AN EMERGENCY WAS DECLARED. LOWER ALTITUDE AND LOWER AIRSPEED HELPED.
- [SDR 07FDEA03587](https://openairdocs.org/sdr/07FDEA03587.md): Skin · damaged · Sep 11, 2007 · N68057 · Doug MD1010F · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN AND FRAME AT STA 642 HAVE OVERSIZED FASTENER HOLE. REPAIRED IAW EA 8-53-109196-FUSELAGE-EXISTING BUSHINGS FOUND AT STA 641.5 MCD, LOWER SILL-REPAIR. MAJOR REPAIR.
- [SDR 07FDEA03403](https://openairdocs.org/sdr/07FDEA03403.md): Floorbeam · corroded · Sep 6, 2007 · N68057 · Doug MD1010F · Fuselage Main, Floor Beam
  > AFT CABIN BULKHEAD FLOOR TEE ANGLE SUPPORT CORRODED UNDER FLOOR PANEL SUPPORT AT RBL 20 REMOVED CORROSION IAW MD10 SRM 53-40-00 VOL1 FIG 18. ORIGINAL THICKNESS.125 IAW MD10 SRM 53-40-00 VOL 1 FIG 18, REMAINING.094 MATERIAL REMOVED.031. REPAIRED IAW MD10
- [SDR 07FDEA03234](https://openairdocs.org/sdr/07FDEA03234.md): Seat Track · corroded · Aug 29, 2007 · N68057 · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK HAS CORROSION AT STA.720 AT LBL 107. REMOVED, FABRICATED AND INSTALLED SPLICED PLATE, SPLICE HAT AND SEAT TRACK IAW MD/DC10 SRM 53-70-00 VOL I PGE 3-4,51-31-01 VOL II PGE 1-10,53-70-00 PG E51 VOL I AND PART MARKED IAW FED EX GMM 7-0-1000
- [SDR 07FDEA03006](https://openairdocs.org/sdr/07FDEA03006.md): Stringer · corroded · Aug 21, 2007 · N68057 · Doug MD1010F · Fuselage Main, Longeron/Stringer
  > CENTER W/WELL AREA L48L END FITTING CORRODED IN AREAS STA 1509 TO 1521. REMOVED, FABRICATED AND INSTALLED FITTING P/N AYB7020-1 STA 1509-1521 L48L IAW DC/MD10 SRM 51-33-01 VOL II, 53-00-01 FIG 1B VOLII, 51-21-01 VOL1, 51-21-02 VOLII AND DAC DWG AYB 7020.
- [SDR 07FDEA02982](https://openairdocs.org/sdr/07FDEA02982.md): Seat Track · cracked · Aug 20, 2007 · N68057 · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK FLANGE IS CRACKED AT STA 449 LBL 28.5 REMOVED SEAT TRACK AT STA 449 LBL 28.5 IAW DC-10 SRM 51-31-01 VOL 2 PG 1-10. FABRICATED IAW DC-10 SRM 53-70-00 PG 51 VOL 1. INSTALLED SEAT TRACK AT STA 449LBL 28.5 IAW DC 10 SRM 51-51-01 VOL 2 PG 1-2.
- [SDR 07FDEA02980](https://openairdocs.org/sdr/07FDEA02980.md): Seat Track · gouged · Aug 20, 2007 · N68057 · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > GOUGED CABIN SEAT TRACK SCALLOPS AT STA 879 TO 899 LBL 85 REMOVED AND REPLACED SEAT TRACK IAW DC-10 SRM 53-70-00 VOL 1 PG 51. FABRICATED SPLICE PLATES AND SPLICE HATS IAW DC-10 SRM 53-70-00 PG 4 VOL 1. INSTALLED SEAT TRACK SPLICE PLATE AND SPLICE HAT IAW DC1
- [SDR 07FDEA02879](https://openairdocs.org/sdr/07FDEA02879.md): Spar · cracked · Aug 14, 2007 · N68057 · Doug MD1010F · Horizontal Stabilizer, Spar/Rib
  > RT HORIZONTAL STAB REAR SPAR CAP CRACKED ON AFT SIDE NEAR RT UPPER AFT BARREL NUT AT STA XE 48.500 CRACK EXTENDS APPROX 3.0", HORIZONTALLY FROM INBD END OF FITTING PER EDDY CURRENT TEST. ACCOMPLISHED EA 8-5510-109187"STABILIZER-HORIZ- AD92-22-10-RH UPPER AFT
- [SDR 07FDEA02877](https://openairdocs.org/sdr/07FDEA02877.md): Door Frame · corroded · Aug 14, 2007 · N68057 · Doug MD1010F · Fuselage Main, Structure
  > FOUND MAIN CARGO LOWER DOOR JAMB HAS CORROSION ON LOWER BEAM AT STA 750. 09-04-07 REMOVED AND REPLACED MAIN CARGO DOOR JAMB LOWER DOOR JAMB LOWER BEAM IN REF TO DC/MD10 SRM 51-33-01 VOL II PAGE 1, AND DAC DRAWING ACA7224 REV.G. MAJOR REPAIR.
- [SDR 07FDEA02864](https://openairdocs.org/sdr/07FDEA02864.md): Seat Track · gouged · Aug 13, 2007 · N68057 · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > GOUGED/SCUFFED SCALLOPS ON CABIN SEAT TRACK AT STA 1199, TO 1219, RBL 47.5 REMOVED SEAT TRACK SECTION AT STA 1209-1269 RBL 47 IAW DC-10/MD-10 SRM 51-31-01, VOL2, PG 1. MAT ID FOR SEAT TRACK SECTION IS S4929405 PO 571558.2 IAW DC-10/MD10 SRM 53-42-01, VOL 2 PG
- [SDR 07FDEA02863](https://openairdocs.org/sdr/07FDEA02863.md): Seat Track · gouged · Aug 13, 2007 · N68057 · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > GOUGED, CABIN SEAT TRACK AT STA 1039 TO 1059, LBL 27.5 CHECKED LIMITS, GAP BETWEEN SCALLOPS FOUND TO BE GREATER THAN.500 (MAX ALLOWED) OUT OF LIMITS IAW DC/MD-10 SRM 53-70-00 VOL 1 PG 21. REMOVED DAMAGE SEAT TRACK SECTION AND INSTALLED FAB`D SEAT TRACK SECTI
- [SDR 07FDEA02862](https://openairdocs.org/sdr/07FDEA02862.md): Seat Track · damaged · Aug 13, 2007 · N68057 · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > ELONGATED SCALLOPS AT CABIN SEAT TRACK, STA 899 TO 919, RBL47.5. [08-29-07] CHECKED LIMITS, MAX ALLOW BETWEEN EDGE OF SCALLOP IS.500. FOUND TO BE GREATER THAN.500. OUT OF LIMITS IAW DC/MD-10 SRM 53-70-00 VOL 1 PG 21. DIAL CALIPER T8878F REMOVED AND
- [SDR 07FDEA02797](https://openairdocs.org/sdr/07FDEA02797.md): Seat Track · damaged · Aug 8, 2007 · N68057 · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > ELONGATED SCALLOPS AT CABIN SEAT TRACK LBL 47.5, STA 939 TO 1019 (2-PLACES) REMOVED SEAT TRACK AT STA 879-1019 IAW DC10-SRM 53-70-00 VOL 1 PG5. SEAT TRACK WAS OUT OF LIMITS IAW DC10 SRM 53-20-00 PG 21. REPLACED SEAT TRACK IAW DC10 SRM 53-70-00 VOL 1 PG 1-10,
- [SDR 07FDEA02796](https://openairdocs.org/sdr/07FDEA02796.md): Seat Track · damaged · Aug 8, 2007 · N68057 · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > BROKEN SCALLOPS ON CABIN SEAT TRACK AT STA 755 REMOVED FLOOR PANEL IAW DC10/MD10 SRM 51-31-01 VOL 2 PGS 1-5. REMOVED SEAT TRACK AT STA 700-760 LBL 47.5 IAW DC10/MD10 SRM 51-31-01 VOL 2 PG 1-5, MAT ID 54929405 AND PO NR 570769.5 FOR SEAT TRACK IAW DC10/MD10 SR
- [SDR 07FDEA02795](https://openairdocs.org/sdr/07FDEA02795.md): Seat Track · worn · Aug 8, 2007 · N68057 · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > ELONGATED SCALLOPS ON CABIN SEAT TRACK AT RBL 47.5, STA 1019 TO 1039 CHECKED LIMITS, SEAT TRACK HAS SEVERAL BROKEN SCALLOPS OUT OF LIMITS IAW DC/MD10 SRM 53-70-00 VOL 1 PG 21. REMOVED OLD TRACK AND INSTALLED NEW TRACK IAW MD-DC10 SRM 53-42-01 VOL 3 PG 13/14
- [SDR 07FDEA02794](https://openairdocs.org/sdr/07FDEA02794.md): Seat Track · gouged · Aug 8, 2007 · N68057 · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > GOUGED, CABIN SEAT TRACK SCALLOPS AT STA 1159 TO STA 1099, RBL 27.5 STA 1099-1119, RBL 27.5 REMOVED GOUGE, REMAINING.434, FOUND TO BE WITHIN LIMITS IAW DC10/MD10 SRM 53-70-00, FIGURE 5 VOL 1 STA 1119-1159 RBL 27.5. REMOVED GOUGE AND FOUND TO BE OUT OF LIMITS
- [SDR 07FDEA02780](https://openairdocs.org/sdr/07FDEA02780.md): Stringer · corroded · Aug 6, 2007 · N68057 · Doug MD1010F · Fuselage Main, Longeron/Stringer
  > CENTER WHEEL AREA L48L END FITTING CORRODED IN AREAS STA1509 TO 1521. [08-21-07] ALL WORK ACCOMPLISHED ON SDR 07-3006 -W/O 37284.
- [SDR 07FDEA02779](https://openairdocs.org/sdr/07FDEA02779.md): Stringer · corroded · Aug 6, 2007 · N68057 · Doug MD1010F · Fuselage Main, Longeron/Stringer
  > CENTER WHEEL WELL AREA L52 END FITTING HAS CORROSION IN AREAS STA1509 TO 1521. [08-21-07] RMEOVED, FABRICATED, INSTALLED FITTING P/N AYB7020-2 IAW DC/MD10 SRM 51-33-01 VOLII, 53-00-01FIG 1B VOLII, 51-21-01 VOLII, 51-21-02 VOL II AND DAC DWG AYB 7020.
- [SDR 07FDEA02778](https://openairdocs.org/sdr/07FDEA02778.md): Stringer · corroded · Aug 6, 2007 · N68057 · Doug MD1010F · Fuselage Main, Longeron/Stringer
  > CENTER WHEEL WELL AREA L51R END FITTING HAS CORROSION IN AREAS STA 1509 TO 1521. [08-21-07] REMOVED, FABRICATED, AND INSTALLED FITTING P/N AYB 7020-1 STA.1509 TO 1521 L51R IAW DC/MD10 SRM 51-33-01 VOLII,53-00-01 FIG. 1B VOLII,51-21-01 VOLII,51-21-02 VOLII
- [SDR 07FDEA02728](https://openairdocs.org/sdr/07FDEA02728.md): Fitting · cracked · Aug 2, 2007 · N68057 · Doug MD1010F · Fuselage Main, Attach Fittings
  > MAIN CARGO DOOR FITTING NR 3 BORES A, C AND D SHOWS CRACK INDICATION WITH BHEC BORES MARKE DIN BLACK. 09-04-07 REMOVED AND REPLACED NR 3 DOOR FITTING AT STA 666 IN REF TO DC/MD10 SRM 51-33-01 VOL II PAGE 1. MAJOR REPAIR.
- [SDR 07FDEA02727](https://openairdocs.org/sdr/07FDEA02727.md): Door Frame · corroded · Aug 2, 2007 · N68057 · Doug MD1010F · Fuselage Main, Structure
  > MAIN CARGO DOOR CUT-OUT LOWER JAMB TOP SIDE, JUST FWD OF NR 3 LATCH SPOOL FITTING WEB CORRODED. 09-04-07 REMOVED AND REPLACED MAIN CARGO DOOR JAMB UPPER BEAM ACA7226-1 IN REF TO DC/MD10 SRM 51-33-01 VOL II PAGE1 AND DAC DRAWING ACA7224 REV G. MAJOR REPAIR
- [SDR 07FDEA02726](https://openairdocs.org/sdr/07FDEA02726.md): Fitting · cracked · Aug 2, 2007 · N68057 · Doug MD1010F · Fuselage Main, Attach Fittings
  > MAIN CARGO DOOR FITTING NR 7 BORES A, B, C AND D SHOW CRACK INDICATIONS WITH BHEC BORES MARKED IN BLACK. 09-04-07 REMOVED AND REPLACED FITTING NR 7 IN REF TO DC/MD10 SRM 51-33-01 VOLI PAGE 1. MAJOR REPAIR MECH 3934 QC348
- [SDR 07FDEA01117](https://openairdocs.org/sdr/07FDEA01117.md): Bolt · corroded · Mar 23, 2007 · N68057 · Doug MD1010F · Wing, Landing Gear Attach Fittings
  > LT MAIN LANDING GEAR SUPPORT FITTING-FWD TRUNNION BOLT DOES NOT TAKE GREASE AND IS FROZEN. UPON REMOVAL, FOUND BOLT CORRODED. REPAIRED BOLT PER SEQ NR 13 EA 8-5710-10593 "LT MLG SUPPORT FITTING, FWD TRUNNION BOLT (FROZEN)".
- [SDR 06FDEA04310](https://openairdocs.org/sdr/06FDEA04310.md): Engine · making metal · Dec 22, 2006 · N68057 · Doug MD1010F · Engine (Turbine/Turboprop)
  > SHUT DOWN NR 3 ENGINE IN FLIGHT BECAUSE OF LEVEL 2 ALERT, ENG NR 3 OIL FILTER. BEFORE SHUT DOWN OIL PRESS WAS NORMAL. OIL TEMP WAS 20 PERCENT HIGHER THAN OTHER ENGINES. AFTER SHUT DOWN IT WIND MILLED FOR 25 MIN WITH SOME OIL PRESS. CHECKED AIU FAULTS LAS
- [SDR 06FDEA03439](https://openairdocs.org/sdr/06FDEA03439.md): Cylinder · failed · Sep 26, 2006 · N68057 · Doug MD1010F · Main Landing Gear
  > RT MAIN GEAR DOWN ON RETRACTION AFTER T/O. LIGHT WENT RED AND STAYED RED UNTIL GEAR HANDLE PLACED DOWN. RECYCLED, SAME THING. LANDED @ KOAK. PER CREW DEBRIEF, APPARENTLY THE RT MLG NEVER MOVED FROM THE DOWN AND LOCKED POSITION. SUSPECT RT MAIN DOWNLOCK CYC
- [SDR 06FDEA1616](https://openairdocs.org/sdr/06FDEA1616.md): Dimmer · failed · Apr 25, 2006 · N68057 · Doug MD1010F · Flight Compartment Lighting
  > APPROACHING TOP OF DESCENT A SLIGHT ELECTRICAL ODOR WAS NOTED IN COCKPIT. UNABLE TO LOCATE SOURCE, BUT A BRIEF SQUEAL WAS HEARD NEAR COCKPIT DOOR, FOLLOWED SHORTLY AFTER BY UNCOMMAND IRCD OPENING. DEACTIVATED IRCD AS A PRECAUTION. CONFIRMED ELECTRICAL ODOR
- [SDR 06FDEA1276](https://openairdocs.org/sdr/06FDEA1276.md): Seal · leaking · Mar 31, 2006 · N68057 · Doug MD1010F · Flight Compartment Windows
  > 1 40 INTO FLIGHT AT FL370, WINDOW SEAL ON CAPT SIDE DEVELOPED LOUD SQUEAL. TOO LOUD TO CONTINUE FLIGHT. NOISE DISSIPATED UPON DESCENT THRU 15,000'. REMOVED AND REPLACED LEFT SLIDING CLEAR WINDOW PER MD-10-10 AMM 56-12-00-4. PRESSURIZED A/C PER MD10-10 AMM 2
- [SDR 06FDEA0953](https://openairdocs.org/sdr/06FDEA0953.md): Repair · none · Mar 6, 2006 · N68057 · Doug MD1010F · Standard Practices/Structures
  > REPAIR DOUBLER STATION 1059 - 1085 L51 - L52 MARKED NR 15 REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. VISUALLY INSPECTED REPAIR LOCATED AT STA 1059 - 1085 L51 - L52. ACCOMPLISHED PART
- [SDR 06FDEA0924](https://openairdocs.org/sdr/06FDEA0924.md): Repair · unknown · Mar 2, 2006 · N68057 · Doug MD1010F · Standard Practices/Structures
  > REPAIR LT OB FLAP UPPER SKIN,STA.XOF 587 MARKED NR 71. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. VISUALLY INSPECTED REPAIR AT LT OB FLAP UPPER SKIN, FOUND TO BE WITHIN SRM 57-20-00 FI

Next page: https://openairdocs.org/deregistered/N68057-2020-04-23/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 = 'N68057' AND deregistration_id = 'N68057-2020-04-23'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N68057-2020-04-23/reports

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