# Service difficulty reports: N68050, cancelled Apr 13, 2024

A list on [N68050, cancelled Apr 13, 2024](https://openairdocs.org/deregistered/N68050-2024-04-13.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 · 63 reports

- [SDR FDEA201211093924](https://openairdocs.org/sdr/FDEA201211093924.md): Seal · failed · Nov 9, 2012 · N68050 · Doug MD1010F · APU Oil System
  > SHUTDOWN APU WITH FIRE HANDLE & DISCHARGED ONE FIRE BOTTLE AFTER ACFT FILLED WITH SMOKE DURING LOADING. APU RUNNING APPROX 15-20 MINUTES. RECEIVED AN ALERT FOR MAIN CARGO SMOKE & VISIBLE SMOKE IN COCKPIT/CARGO AREA. ASSUMED IT WAS COMING FROM THE APU AND PU
- [SDR FDEA201209213388](https://openairdocs.org/sdr/FDEA201209213388.md): Attach Bracket · failed · Sep 21, 2012 · N68050 · Doug MD1010F · Fuselage, Landing Gear Attach Fittings
  > UNSAFE NOSE GEAR INDICATION UPON EXTENSION. EXTENDED GEAR WITH ALTERNATE EXTENSION HANDLE. HEARD LOUD BANG ON RT SIDE ON TAKEOFF. NOTE: UPON CREW DEBRIEF. CAPT STATED THEY DID NOT FEEL THE NOSE GEAR EXTEND (AS THEY NORMALLY WOULD) WHEN SELECTED DOWN. R
- [SDR FDEA201209203366](https://openairdocs.org/sdr/FDEA201209203366.md): Mount · broken · Sep 20, 2012 · N68050 · Doug MD1010F · Fuselage, Landing Gear Attach Fittings
  > UNSAFE NOSE GEAR INDICATION ON EXTENSION. EXTENDED GEAR WITH ALTERNATE EXTENSION HANDLE. HEARD LOUD BANG ON RT SIDE AFTER TAKEOFF. CAPTAIN STATED THEY DID NOT FEEL THE NOSE GEAR EXTEND WHEN SELECTED DOWN. RT PSEU SHOWED NO NOSE GEAR CURRENT OR PREVIOUS F
- [SDR FDEA201206042126](https://openairdocs.org/sdr/FDEA201206042126.md): Bulkhead Web · cracked · Jun 4, 2012 · N68050 · Doug MD1010F · Fuselage Main, Bulkhead
  > LEFT MLG WW HAS A CRACK ON INBD BULKHEAD. REPAIRED IAW EA 8-5310-157338, PART 1, STEPS 1 THROUGH 4.
- [SDR FDEA201206042125](https://openairdocs.org/sdr/FDEA201206042125.md): Bulkhead Web · cracked · Jun 4, 2012 · N68050 · Doug MD1010F · Fuselage Main, Bulkhead
  > CRACK IN LT MLG WW INBD BULKHEAD, FWD UPPER SIDE PROTUDING OUT OF LIGHTNING HOLE THREE INCH CRACKS. MWT REPAIRED IAW EA 8-5310-157337, PART 1, STEPS 1- 4.
- [SDR FDEA201111184968](https://openairdocs.org/sdr/FDEA201111184968.md): Compressor · stalled · Nov 18, 2011 · N68050 · Doug MD1010F · Turbine Engine Compressor Section
  > AT ROTATION NR 1 ENG COMPRESSOR STALLED. HEARD A LOUD BANG WITH YAW AND TEMP AT 1097 DEGREES. N2 INDICATION HAD AN X WITH NO INFORMATION SHOWING. REMOVED AND REPLACED THE ENGINE.
- [SDR FDEA201011174408](https://openairdocs.org/sdr/FDEA201011174408.md): Support · cracked · Nov 17, 2010 · N68050 · Doug MD1010F · Wing, Control Surface Attach Fittings
  > LEFT OTBD FLAP INBD HINGE-FWD FITTING ATTACHED TO THE WING HAS A CRACK ON INBD SIDE. REMOVED CRACKED SUPPORT FITTINGS IAW SRM 51-33-01. WORKED HOLES TO FINAL SIZE.325 ON OTBD FLALP SUPPORT FITTINGS COMPLIED WITH EA 8-5710-125587 FOR MISLOCATED HOLE REPAIR.
- [SDR FDEA200902120514](https://openairdocs.org/sdr/FDEA200902120514.md): Fuel Control · malfunctioned · Feb 12, 2009 · N68050 · Doug MD1010F · Fuel Control/Turbine Engines
  > NR 3 ENG ROLLBACK AT FL370, ENG IGN OVERRIDE ON. ENGINE RESTARTED ITSELF AT FL 270 IN CLOUDS -10C WITH ALL ENG ANTI-ICE ON. ROLL BACK RESULTED IN N1 OF 48 PERCENT & FUEL FLOW OF 1000. EGT OF 570. PERFORMED INSPECTION OF NR 3 ENGINE INLET & EXHAUST NO DEFE
- [SDR 08FDEA04876](https://openairdocs.org/sdr/08FDEA04876.md): Seat Track · worn · Nov 14, 2008 · N68050 · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO DECK SEAT TRACK AT STA 879 TO 919 LBL 107 HAS SEVERAL FASTENER HOLES DAMAGED ON THE OTBD LOWER LEG FROM PREVIOUS REWORK. REMOVED AND REPLACED SEAT TRACK, FAB NEW SEAT TRACK SECTION AND SPLICES IAW SRM 51-31-01, 53-70-00 FIG 1 SHEET 1 AND MAE TRAVEL
- [SDR 08FDEA04562](https://openairdocs.org/sdr/08FDEA04562.md): Seat Track · damaged · Oct 27, 2008 · N68050 · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MCDECK SEAT TRACK AT STA 1089 LBL 48 IS DAMAGED, REMOVED FLOORBOARDS FOR ACCESS. REMOVED SEAT TRACK, FABRICATED NEW TRACK. INSTALLED NEW TRACK AND REINSTALLED FLOORBOARDS IAW SRM 51-31-01, SRM 53-70-00 AND MAE TRAVELER T8/766008. MAJOR REPAIR AND RII.
- [SDR 07FDEA02341](https://openairdocs.org/sdr/07FDEA02341.md): Unknown · unknown · Jun 29, 2007 · N68050 · Doug MD1010F · Pneumatic Indicating System
  > EN ROUTE TO SEA, NOTICED ON PNEUMATIC PNL RED MANF NR 3 LIGHT AND AMBER BLEED OFF LIGHT. PNEUMATIC SYNOPTIC PG SHOWED NR 3 PNEU MANF IN THE RED AND PRESS IN MANF SLOWLY DROPPING. 2 MIN LATER RECEIVED LVL 3 ALERT "AIR MANF 3 FAIL". C/W QRH AND DIVERTED TO BO
- [SDR 07FDEA01983](https://openairdocs.org/sdr/07FDEA01983.md): Spar · cracked · May 25, 2007 · N68050 · Doug MD1010F · Horizontal Stabilizer, Spar/Rib
  > RT HORIZONTAL STABILIZER OUTBOARD LEADING BOTTOM ATTACH ANGLE CRACKED. REPAIRED IAW FEDEX EA NR 8-5510-109166 "STABILIZERS, RT STAB LOWER LEADING EDGE, SPAR CRACK REPAIR".
- [SDR 07FDEA01982](https://openairdocs.org/sdr/07FDEA01982.md): Floorbeam · corroded · May 25, 2007 · N68050 · Doug MD1010F · Fuselage Main, Floor Beam
  > FORWARD LOWER CARGO, DOOR TORQUE BOX FORWARD FRAME CORRODED. REMOVED CORROSION FROM FRAME AND SUPPORT BRACKET AND FOUND BOTH TO EXCEED ALLOWABLE LIMITS IAW MD/DC 10 SRM 53-00-01 VOL I FIG 1B. REPAIRED FRAME IAW FED EX EA NR 8-5350-109160 "FUSELAGE FWD LOWER
- [SDR 07FDEA01981](https://openairdocs.org/sdr/07FDEA01981.md): Frame · corroded · May 25, 2007 · N68050 · Doug MD1010F · Fuselage Main, Frame
  > FORWARD LOWER CARGO, DOOR TORQUE BOX FORWARD FRAME CORRODED. REMOVED CORROSION FROM FRAME AND WEB AND FOUND MATERIAL LOSS FOR BOTH TO EXCEED ALLOWABLE LIMITS IAW MD/DC 10 SRM53-00-01 VOL I FIG 1B. REPAIRED FRAME IAW FED EX EA NR 8-5350-109161 "FUSELAGE-FWD L
- [SDR 07FDEA01965](https://openairdocs.org/sdr/07FDEA01965.md): Wedge · dented · May 24, 2007 · N68050 · Doug MD1010F · Elevator, Plate/Skin
  > LEFT INBOARD ELEVATOR TRAILING EDGE DENTED AT MID-SECTION AREA. REMOVED DAMAGED SECTION OF LEFT INBOARD ELEVATOR PER DC/MD10 SRM 51-31-01 VOL 11. RECEIVED NEW TRAILING EDGE WEDGE SECTION, LOCATED AND DRILLED HOLES PER DC/MD10 SRM 51-31-01 PARAG 2 VOL11. AL
- [SDR 07FDEA01944](https://openairdocs.org/sdr/07FDEA01944.md): Fitting · corroded · May 22, 2007 · N68050 · Doug MD1010F · Cargo/Baggage Doors
  > MAIN CARGO DOOR NR 7 LATCH SPOOL AND FITTING IS CORRODED. REMOVED NR 7 SPOOL IAW FEDEX EA NR 8-5230-110663 REV A. " FUSELAGE-MAIN CARGO DOOR - LOWER JAMB SUPPORT FITTING INSPECTION AND DOOR RIG." CLEANED AND TREATED, PRIMED IAW FEDEX MD10 SRM 51-21-01 VOL
- [SDR 07FDEA01942](https://openairdocs.org/sdr/07FDEA01942.md): Fitting · corroded · May 22, 2007 · N68050 · Doug DC1010F · Fuselage Main, Attach Fittings
  > MAIN CARGO DOOR-LOWER JAMB FITTING NR 4 SHOWS CORROSION AT AFT UPPER HOLE. REPAIRED NR 4 LOWER JAMB FITTING AND WEB IAW FEDEX EA 8-5230-110663 REV A. "FUSELAGE-MAIN CARGO DOOR-LOWER JAMB SUPPORT FITTING INSPECTION AND DOOR RIG" LOWER SUPPORT FITTING REPLACED
- [SDR 07FDEA01941](https://openairdocs.org/sdr/07FDEA01941.md): Fitting · corroded · May 22, 2007 · N68050 · Doug MD1010F · Fuselage Main, Structure
  > MAIN CARGO DOOR-LOWER JAMB FITTING NR 5 SHOWS CORROSION AT LOWER FORWARD HOLE. REPAIRED NR 5 LOWER JAMB AND REPLACED SUPPORT FITTING IAW FEDEX EA 8-5230-110663 REV A " FUSELAGE-MAIN CARGO DOOR-LOWER JAMB SUPPORT FITTING INSPECTION AND DOOR RIG".
- [SDR 07FDEA01940](https://openairdocs.org/sdr/07FDEA01940.md): Fitting · corroded · May 22, 2007 · N68050 · Doug MD1010F · Fuselage Main, Structure
  > MAIN CARGO DOOR LOWER JAMB FITTING NR 2 SHOWS CORROSION AT LOWER FORWARD HOLE. REPAIRED LOWER JAMB AND REPLACED SUPPORT FITTING NR 2 IAW FEDEX EA. 8-5230-110663 REV A. " FUSELAGE- MAIN CARGO DOOR-LOWER JAMB SUPPORT FITTING INSPECTION AND DOOR RIG." LOWER S
- [SDR 07FDEA01939](https://openairdocs.org/sdr/07FDEA01939.md): Fitting · corroded · May 22, 2007 · N68050 · Doug MD1010F · Fuselage Main, Structure
  > MAIN CARGO DOOR-LOWER JAMB FITTING NR 1 SHOWS CORROSION AT LOWER FORWARD HOLE. REPAIRED LOWER JAMB AND REPLACED SUPPORT FITTING NR 1 IAW FEDEX EA 8-5230-110663. "FUSELAGE- MAIN CARGO DOOR - LOWER JAMB FITTING INSPECTION AND DOOR RIG."
- [SDR 07FDEA01938](https://openairdocs.org/sdr/07FDEA01938.md): Fitting · corroded · May 22, 2007 · N68050 · Doug MD1010F · Fuselage Main, Structure
  > MAIN CARGO DOOR-LOWER JAMB FITTING NR 3 SHOWS CORROSION AT AFT LOWER HOLE. REPAIRED NR 3 LOWER JAMB WEB IAW FEDEX EA 8-5230-110663 REV. A. " FUSELAGE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING INSPECTION AND DOOR RIIG." FITTING(LOWER SUPPORT) REPLACED ON
- [SDR 07FDEA01937](https://openairdocs.org/sdr/07FDEA01937.md): Fitting · corroded · May 22, 2007 · N68050 · Doug MD1010F · Fuselage Main, Structure
  > MAIN CARGO DOOR LOWER JAMB FITTING NR 3 SHOWS CORROSION AT FORWARD LOWER HOLE. REPAIRED NR 3 LOWER JAMB AND REPLACED SUPPORT FITTING IAW FEDEX EA 8-5230-110663 REV A "FUSELAGE-MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING INSPECTION AND DOOR RIG."
- [SDR 07FDEA01945](https://openairdocs.org/sdr/07FDEA01945.md): Fitting · corroded · May 22, 2007 · N68050 · Doug MD1010F · Fuselage Miscellaneous Structure
  > MAIN CARGO DOOR NR 6 LATCH SPOOL AND FITTING IS CORRODED. REMOVED NR 6 SPOOL IAW DC/MD10 FEDEX EA NR 8-5230-110663 STEPS 5A AND B. CLEANED,TREATED AND PRIMED IAW FEDEX DC/MD10 SRM 51-21-01 VOL 11. INSTALLED NR 6 SPOOL AND FITTING IAW FEDEX EA NR 8-5230-1106
- [SDR 07FDEA01943](https://openairdocs.org/sdr/07FDEA01943.md): Fitting · corroded · May 22, 2007 · N68050 · Doug MD1010F · Fuselage Miscellaneous Structure
  > COMPLY WITH FEDEX EA NR 8-5230-110663 "FUSELAGE-MAIN CARGO DOOR - LOWER JAMB FITTING INSPECTION AND DOOR RIG". COMPLIED WITH FEDEX EA NR 8-5230-110663 "FUSELAGE- MAIN CARGO DOOR, LOWER JAMB FITTING INSPECTED AND RIGGED."
- [SDR 07FDEA01846](https://openairdocs.org/sdr/07FDEA01846.md): Frame · cracked · May 18, 2007 · N68050 · Doug MD1010F · Wing Spar
  > RIGHT WING LEADING EDGE FORMER CRACKED AT XOS625.5 STOP DRILLED CRACK AND INSTALLED REPAIR CLIP PER MD/DC 10-10 SRM 57-20-00 FIG 1 VOL I. FUEL CONTROL PANEL WAS REMOVED. REINSTALLED AND OPS CHECKED TO FACILITATE REPAIR IN REF TO MD10-10 MM 28-00-00-5. OPS
- [SDR 07FDEA01835](https://openairdocs.org/sdr/07FDEA01835.md): Bushing · loose · May 17, 2007 · N68050 · Doug MD1010F · Elevator Structure
  > LEFT OUTBD ELEVATOR THIRD HINGE FROM INBD SIDE HAT BUSHINGS LOOSE IN FITTING BORE FOR OUTBOARD DAMPNER. REMOVED AND REPLACED LT O/B ELEVATOR THIRD HINGE FROM I/B SIDE HAT BUSHINGS IAW CMM 55-21-01 AND FEDEX 8-5520-10913-63. ORIGINAL ATTACHED TO FEDEX N/R N0
- [SDR 07FDEA01834](https://openairdocs.org/sdr/07FDEA01834.md): Bushing · corroded · May 17, 2007 · N68050 · Doug MD1010F · Rudder Control System
  > RT O/B ELEVATOR I/B ACTUATOR MOUNT FITTING (ON ELEVATOR) CORRODED ON I/B SIDE. REMOVED CORROSION/DAMAGE IAW DAC CMM 55-21-01. REMOVED, FABRICATED AND INSTALLED BUSHINGS IAW DAC CMM 55-21-01 AND FEDEX 8-5520-109163. TITLE; " STABILIZER- LT AND RT ELEVATOR HI
- [SDR 07FDEA01833](https://openairdocs.org/sdr/07FDEA01833.md): Bushing · loose · May 17, 2007 · N68050 · Doug MD1010F · Elevator Structure
  > RT O/B ELEVATOR I/B DAMPNER HINGE FITTING HAT BUSHINGS ARE LOOSE. REMOVED AND REPLACED RT O/B ELEVATOR I/B DAMPNER HINGE FITTING HAT BUSHINGS IAW CMM 55-21-01 AND FEDEX EA 8-5520-109163. ORIGINAL ATTACHED TO FEDEX N/R N00836.
- [SDR 07FDEA01832](https://openairdocs.org/sdr/07FDEA01832.md): Bushing · loose · May 17, 2007 · N68050 · Doug MD1010F · Elevator Structure
  > RT O/B ELEVATOR O/B DAMPER HINGE FITTING HAT BUSHINGS ARE LOOSE. REMOVED AND REPLACED RT O/B ELEVATOR O/B ELEVATOR O/B DAMPNER HINGE FITTING HAT BUSHINGS IAW CMM 55-21-01 AND FEDEX EA 8-5520-109163. TITLE; LT AND RT ELEVATOR HINGE FITTING OVERSIZE HOLE-RE
- [SDR 07FDEA01825](https://openairdocs.org/sdr/07FDEA01825.md): Skin · cracked · May 16, 2007 · N68050 · Doug MD1010F · Elevator, Plate/Skin
  > RT INBOARD ELEVATOR UPPER SKIN IS CRACKED ON EDGE. CUT OUT DAMAGED SKIN, FABRICATED REPAIR DOUBLER AND FILLER, AND INSTALLED REF. DC/MD 10 SRM 55-00-01 FIG 3 VOL I AND 51-31-01 VOL II. ALODINED AND PRIMERED PER REF MD/DC 10 SRM 51-21-01 VOL II. THIS IS A
- [SDR 07FDEA01824](https://openairdocs.org/sdr/07FDEA01824.md): Skin · cracked · May 16, 2007 · N68050 · Doug MD1010F · Elevator, Plate/Skin
  > DURING DENT EVALUATION ON RT OUTBOARD ELEVATOR UPPER SKIN HFEC INSPECTION REVEALED A 1" CRACK. CUT OUT DAMAGED SKIN, FABRICATED REPAIR DOUBLER AND FILLER AND INSTALLED REF. DC/MD10 55-00-01 FIG 3, VOL I. ALODINED AND PRIMERED PER REF DC/MD 10 SRM 51-21-01
- [SDR 07FDEA01736](https://openairdocs.org/sdr/07FDEA01736.md): Seat Track · corroded · May 10, 2007 · N68050 · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > AFT LOWER CARGO, CORROSION AT TIEDOWN SEAT TRACK SURFACE AND AT NUT PLATES HOLES UPPER AND LOWER SURFACES, FS 1790-167 LBL 21". REMOVED DAMAGE SEAT TRACK SECTIONS AND FABRICATED NEW SECTIONS AND SPLICES IAW MD/DC 10 SRM 53-70-00 FIG 1 VOL I. ALODINED AND PRI
- [SDR 07FDEA01709](https://openairdocs.org/sdr/07FDEA01709.md): Seat Track · broken · May 6, 2007 · N68050 · Doug DC1010 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN FLOOR SEAT TRACK LUG BROKEN OUT AT STA 635 LBL47. REMOVED AND REPLACED CABIN FLOOR SEAT TRACK SECTION FROM STA 622 TO STA 746 LBL47 IAW DC/MD10 SRM 53-70-00 FIG 5, VOL 1.
- [SDR 07FDEA01708](https://openairdocs.org/sdr/07FDEA01708.md): Seat Track · gouged · May 6, 2007 · N68050 · Doug DC1010 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN FLOOR SEAT TRACK GOUGED AT STA 1161 TO STA 1171 LBL 48. REMOVED AND REPLACED CABIN SEAT TRACK FROM STA 1129 TO STA 1189, LBL 48 IAW DC/MD10 SRM 53-70-00 FIG 1, VOL 1.
- [SDR 07FDEA01707](https://openairdocs.org/sdr/07FDEA01707.md): Seat Track · worn · May 4, 2007 · N68050 · Doug DC1010 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK WORN STA 635 BL 8.5. REMOVED AND REPLACED SEAT TRACK REF DC/MD 10 SRM 51-10-01 VOL III PG 85 53-70-00 VOL I FIG 1, 51-31-01 VOL II PG 4, 51-33-01 VOL II PG 4.
- [SDR 07FDEA01706](https://openairdocs.org/sdr/07FDEA01706.md): Seat Track · gouged · May 4, 2007 · N68050 · Doug DC1010 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN FLOOR SEAT TRACK GOUGED BETWEEN STA-1019 AND STA 1039 LBL 50. REMOVED AND REPLACED MAIN CABIN FLOOR SEAT TRACK AT LBL 50 FROM STA 1006 TO STA 1046 IAW DC/MD 10 SRM 53-70-00 FIG 1 VOL 1.
- [SDR 07FDEA01685](https://openairdocs.org/sdr/07FDEA01685.md): Doubler · corroded · May 2, 2007 · N68050 · Doug DC1010 · Fuselage Miscellaneous Structure
  > AFT FUSELAGE WASTE TANK COMPT, FRAME LWR FWD AND AFT CHORDS AT LONGERONS ATTACH FASTENERS HAVE CORROSION BETWEEN L49R AND L52 AT STA 1997 REMOVED FASTENERS FROM FRAME STA 1997 L49-52 PER MD/DC 10 SRM 51-31-01 VOL 2. REMOVED CORROSION PER MD/DC10 SRM 51-21-01
- [SDR 07FDEA01679](https://openairdocs.org/sdr/07FDEA01679.md): Fitting · cracked · May 1, 2007 · N68050 · Doug MD1010F · Fuselage Miscellaneous Structure
  > MAIN CARGO DOOR-LOWER JAMB FITTING NR 5 SHOWS CRACK/CORROSION AT LOWER HOLE.
- [SDR 07FDEA01676](https://openairdocs.org/sdr/07FDEA01676.md): Flange · cracked · May 1, 2007 · N68050 · Doug DC1010 · Horizontal Stabilizer Miscellaneous Structure
  > RT HORIZONTAL STAB CENTER LE SECTION OB UPPER ATTACH POINT FLANGE CRACKED AT NUTPLATES. REMOVED AND REPLACED RT HORIZONTAL LE SECTIONS CENTER OUTBOARD UPPER "T" CAP CHORD AT XFS 241, IAW DC/MD 10-10 SRM 51-31-01 VOL II AND 51-33-01 VOL II.
- [SDR 07FDEA01673](https://openairdocs.org/sdr/07FDEA01673.md): Rib · cracked · Apr 30, 2007 · N68050 · Doug MD1010F · Horizontal Stabilizer, Spar/Rib
  > RT HORIZONTAL STABILIZER I/B L/E SECTION NOSE O/B RIB FLANGE CRACKED XFS108, AND ATTACHED CLIP HAS SHEARED FASTENER. INSTALLED REPAIR ANGLE AND STOP DRILLED CRACK IN RT HORIZONTAL STABILIZER IN/B L/E SECTION FORMER RIB AT XFS 108 AND INSTALLED NEW FASTENERS I
- [SDR 07FDEA01672](https://openairdocs.org/sdr/07FDEA01672.md): Seat Track · bent · Apr 30, 2007 · N68050 · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK BENT SEVERAL AREAS BETWEEN STA. 625 AND STA. 775, BL107.5. REMOVED BENT AREAS IAW EA NR 8-5310-11060411, (FUSELAGE MAINFRAME-SEAT TRACK BETWEEN STA. 635-765/X=107.25. TRIMMED SEAT TRACK LOBES), ALODINED AND PRIMED IAW SRM 51-21-01 PG.1
- [SDR 07FDEA01671](https://openairdocs.org/sdr/07FDEA01671.md): Angle · cracked · Apr 30, 2007 · N68050 · Doug MD1010F · Horizontal Stabilizer Miscellaneous Structure
  > RT HORIZONTAL L/E CENTER I/B SECTION UPPER I/B ATTACHED FLANGE CRACKED MARKED. REMOVED CRACKED RT HORIZ L/E T-CAP SECTION AT UPPER I/B STA XFS 166 IAW DC/MD 10 SRM 55-00-01 FIG, 6 VOL 1, AND INSTALLED ANGLE REPAIR PER MD/DC10 SRM 55-00-01 FIG, 6 VOL 1.
- [SDR 07FDEA01634](https://openairdocs.org/sdr/07FDEA01634.md): Door · corroded · Apr 26, 2007 · N68050 · Doug MD1010F · Cargo/Baggage Doors
  > FWD PIT HAS CORROSION IN THE AFT CORNER BETWEEN DOOR SEAL AND BEAM. [SUP 05-30-07] REMOVED CORROSION FROM RAIL AND FOUND MATERIAL LOSS TO WITHIN ALLOWABLE LIMITS IAW DC/MD 10 SRM 53-50-00 VOL I FIG. 15A. ALODINED AND PRIMED REWORK AREA IAW DC/MD 10 SRM 51-
- [SDR 07FDEA01631](https://openairdocs.org/sdr/07FDEA01631.md): Beam · corroded · Apr 26, 2007 · N68050 · Doug DC1010 · Fuselage Main, Structure
  > FWD PIT HAS CORROSION IN THE FORWARD LOWER CORNER BETWEEN DOOR SEAL AND BEAM. [SUP 05-30-07] REMOVED CORROSION FROM RAIL, VERIFIED BLEND OUT AND REMAINING THICKNESS, PER FEDEX EA 8-5350-109152.
- [SDR 07FDEA01587](https://openairdocs.org/sdr/07FDEA01587.md): Handle · worn · Apr 24, 2007 · N68050 · Doug MD1010F · Passenger/Crew Doors
  > R1 DOOR EMERGENCY HANDLE BACKLOCK DOES NOT HOLD HANDLE ONCE HANDLE IS MOVED TO EMERGENCY POSITION. FOUND OVERRIDE LEVER BINDING WITH BACKLOCK. REPLACED BUSHING, SEAL AND LEVER IAW MD10-10 MM 52-11-14-2 AXIAL PLAY CK GOOD. PERFORMED PNEUMATIC TEST TO CK BA
- [SDR 07FDEA01534](https://openairdocs.org/sdr/07FDEA01534.md): Skin · gouged · Apr 22, 2007 · N68050 · Doug MD1010F · Trailing Edge Flaps
  > LT WING O/B FLAP O/B LOWER SKIN GOUGED ON INTERIOR SIDE. CUT OUT DAMAGED PART REF; DC/MD10-10 SRM 57-10-00 FIG 85 VOL 1. FABBED DOUBLER REF; DC/MD10-10 SRM 57-10-00 VOL1. ALODINED AND PRIMED REF; DC/MD10-10 SRM 51-21-01 VOL 11. INSTALLED DOUBLER REF; DC/MD
- [SDR 07FDEA01533](https://openairdocs.org/sdr/07FDEA01533.md): Skin · gouged · Apr 22, 2007 · N68050 · Doug MD1010F · Trailing Edge Flaps
  > LT WING O/B FLAP O/B LOWER SKIN GOUGED ON INTERIOR SIDE. CUT OUT DAMAGE REF; DC/MD10-10 SRM 57-10-00 FIG 85 VOL 1. FABBED REPAIR DOUBLER. [SUP 04-30-07] REF; DC/MD10 -10 SRM 57-10-00 VOL 1. ALODINED AND PRIMED REF; DC/MD10-10 SRM 51-21-01 VOL 11. INSTALLE
- [SDR 06FDEA03143](https://openairdocs.org/sdr/06FDEA03143.md): Shutoff Valve · inoperative · Aug 30, 2006 · N68050 · Doug DC1010 · Airfoil Anti/De-ice System
  > LEVEL 3 MANF FAIL SYS 1 RAN QRH, DIVERTED TO SMF PER CREW VERBAL, ALERT APPEARED WHEN WING ANTI-ICE MEL. ACN RELEASED FOR SERVICE PER MEL/CDL: 30-11-01 CATEGORY: C EXPIRATION: 09SEP06 "MEL 30-11-01: (LEFT) WING A/I SHUTOFF VALVE(S) - INOP. DO NOT OPERATE A
- [SDR 06FDEA1114](https://openairdocs.org/sdr/06FDEA1114.md): Warning System · malfunctioned · Mar 12, 2006 · N68050 · Doug MD1010F · Landing Gear Position and Warning
  > UNSAFE GEAR IND RT MAIN AFTER T/O PRI AND SEC DISPLAY. FOLLOWED CHECKLIST TO SAFE GEAR UP CONDITION. FACT INSP RT GEAR AND DOOR AREA FOR DAMAGE OR DEFECTS WITH NONE FOUND. CHECKED PSEU NO CURRENT FAULTS OR FAULTS ON THE INBD LEG. FAULTS ON LEGS 7 AND 8 FOR
- [SDR 06FDEA0868](https://openairdocs.org/sdr/06FDEA0868.md): Finger Doubler · corroded · Feb 28, 2006 · N68050 · Doug MD1010F · Ailerons
  > LT OUTBOARD AILERON, I/B UPPER SKIN FINGER DOUBLERS DELAMINATED WITH CORROSION. FABRICATED AND INSTALLED NEW SKIN IAW DC 10 SRM 51-35-01 VOL II AND DAC DWG ARC1110, AND EA 8-5710-92633 WINGS - LT AILERON SKIN CORRODED.

Next page: https://openairdocs.org/deregistered/N68050-2024-04-13/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 = 'N68050' AND deregistration_id = 'N68050-2024-04-13'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N68050-2024-04-13/reports

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