# Service difficulty reports: N596FE

A list on [N596FE](https://openairdocs.org/aircraft/N596FE.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 9 · 417 reports

- [SDR FDEA202609091292](https://openairdocs.org/sdr/FDEA202609091292.md): Hydraulic Line · leaking · Sep 9, 2026 · N596FE · Doug MD11F · Hydraulic System, Main
  > PDIS 596 29-02 1798 09SEP26 12:57 PHX FACT LEVEL 1 HYD 2 OFF ALERT ABOUT 1.5 HRS AFTER TAKEOFF. LEVEL 2 HYD 2 FAIL AFTER PARKING BRAKE SET AT THE GATE. EMERGENCY DECLARED. PART 09SEP26 15:03 MC1 IDENTIFIED PARTS HYD LINE ASSEMBLY W/TEE
- [SDR FDEA202502050175](https://openairdocs.org/sdr/FDEA202502050175.md): Warning Message · illuminated · Feb 5, 2025 · N596FE · Doug MD11F · Landing Gear Position and Warning
  > AFTER TAKEOFF, MLG SELECTED UP, BOTH PRIMARY DISPLAY & SECONDARY SYNOPTIC DISPLAYED RED FOR LT MLG. RAN QRH & COORDINATED WITH GOC & MOCC FOR AIR TURN BACK. HANDLE DOWN, ALL PRIM DISPLAY & SEC SYNOPTIC DISPLAYED GREEN. SHORTLY SECONDARY SYNOPTIC DISPLAYED RED.
- [SDR FDEA202502040172](https://openairdocs.org/sdr/FDEA202502040172.md): Bracket · damaged · Feb 4, 2025 · N596FE · Doug MD11F · Landing Gear Position and Warning
  > DURING APPROACH TO LANDING, GEAR WAS EXT AND INITIALLY INDICATED 4 GREEN/SAFE. AFTER APPX. 1 MIN GEAR INDICATION ON LEFT GEAR TURNED RED AND ON SYNOPTIC FLASHED BETWEEN GREEN AND RED. AFTER APPX. 10 MIN LEFT GEAR INDICATED SOLID GREEN ON SYNOPTIC. CREW FO
- [SDR FDEA202412310005](https://openairdocs.org/sdr/FDEA202412310005.md): Door · slow · Dec 31, 2024 · N596FE · Doug MD11F · Passenger/Crew Doors
  > L SIDE MAIN DOOR CLOSES VERY SLOWLY AND WILL NOT OPEN. PRESSURE READING ZERO. WHILE T/S L1 DOOR FOUND PNEUMATIC CONTROL VALVE IN THE OPEN/ MANUAL CONFIG (AIR RESERVOIR EMPTY). RECONFIGURED PNEUMATIC CONTROL VALVE TO THE CLOSED POSITION AND SERVICED RESER
- [SDR FDEA202410101467](https://openairdocs.org/sdr/FDEA202410101467.md): Bracket · corroded · Oct 10, 2024 · N596FE · Doug MD11F · Trailing Edge Flaps
  > RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (HOLE #3) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-07. REPAIR BUSHING FABRIC
- [SDR FDEA202410101466](https://openairdocs.org/sdr/FDEA202410101466.md): Bracket · corroded · Oct 10, 2024 · N596FE · Doug MD11F · Trailing Edge Flaps
  > LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (HOLE #3) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-07. REPAIR BUSHING FABRICAT
- [SDR FDEA202410101465](https://openairdocs.org/sdr/FDEA202410101465.md): Skin · cracked · Oct 10, 2024 · N596FE · Doug MD11F · Fuselage Main, Plate/Skin
  > FORWARD CARGO - FORWARD CARGO DOOR LOWER AFT DOOR JAMB DOUBLER FOUND CHAFFED AT STATION 1002.3 LONGERON -40 RIGHT TO LONGERON -41 RIGHT. FORWARD CARGO - FORWARD CARGO DOOR LOWER AFT DOOR JAMB AT STATION 1002.3 LONGERON -40 RIGHT TO LONGERON -41 RIGHT CHAFF
- [SDR FDEA202410101464](https://openairdocs.org/sdr/FDEA202410101464.md): Skin · chafed · Oct 10, 2024 · N596FE · Doug MD11F · Fuselage Main, Plate/Skin
  > CENTER CARGO - AFT OF CENTER CARGO DOOR LOWER DOUBLER FOUND CHAFFED AT STATION 1781, LONGERON -38 RIGHT TO LONGERON -41 RIGHT. CENTER CARGO - AFT OF CENTER CARGO DOOR LOWER AT STATION 1781, LONGERON -38 RIGHT TO LONGERON -41 RIGHT DOUBLER CHAFFED AREA REPA
- [SDR FDEA202410101462](https://openairdocs.org/sdr/FDEA202410101462.md): Floor Support · corroded · Oct 10, 2024 · N596FE · Doug MD11F · Fuselage Miscellaneous Structure
  > FORWARD CABIN - FLOOR PANEL SUPPORT AT RIGHT HAND STATION 436 X = -77 FOUND CORRODED. FORWARD CABIN AT RIGHT HAND STATION 386 TO STATION 459 X = -77 FLOOR PANEL SUPPORT REMOVED AND REPLACED AS PER MD-11 SRM 51-33-01-0G. REWORKED FLOOR PANEL SUPPORT AS
- [SDR FDEA202410091452](https://openairdocs.org/sdr/FDEA202410091452.md): Floorbeam · corroded · Oct 9, 2024 · N596FE · Doug MD11F · Fuselage Main, Floor Beam
  > FORWARD CABIN - FLOOR PANEL SUPPORT AT RIGHT HAND STATION 436 X = -77 FOUND CORRODED. FORWARD CABIN AT RIGHT HAND STATION 386 TO STATION 459 X = -77 FLOOR PANEL SUPPORT REMOVED AND REPLACED AS PER MD-11 SRM 51-33-01-0G. REWORKED FLOOR PANEL SUPPORT AS PE
- [SDR FDEA202409241348](https://openairdocs.org/sdr/FDEA202409241348.md): Doubler · chafed · Sep 24, 2024 · N596FE · Doug MD11F · Fuselage Main, Plate/Skin
  > CENTER CARGO - AFT OF CENTER CARGO DOOR LOWER DOUBLER FOUND CHAFFED AT STATION 1781, LONGERON -38 RIGHT TO LONGERON -41 RIGHT. CENTER CARGO - AFT OF CENTER CARGO DOOR LOWER AT STATION 1781, LONGERON -38 RIGHT TO LONGERON -41 RIGHT DOUBLER CHAFFED AREA REPA
- [SDR FDEA202409231338](https://openairdocs.org/sdr/FDEA202409231338.md): Bracket · corroded · Sep 23, 2024 · N596FE · Doug MD11F · Trailing Edge Flaps
  > RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (HOLE #3) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-07. REPAIR BUSHING FABRIC
- [SDR FDEA202409231337](https://openairdocs.org/sdr/FDEA202409231337.md): Bracket · corroded · Sep 23, 2024 · N596FE · Doug MD11F · Trailing Edge Flaps
  > LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (HOLE #3) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-07. REPAIR BUSHING FABRICAT
- [SDR FDEA202409191325](https://openairdocs.org/sdr/FDEA202409191325.md): Doubler · chafed · Sep 19, 2024 · N596FE · Doug MD11F · Fuselage Main, Plate/Skin
  > FORWARD CARGO - FORWARD CARGO DOOR LOWER AFT DOOR JAMB DOUBLER CHAFFED AT STATION 1002.3 LONGERON -40 RIGHT TO LONGERON -41 RIGHT. FORWARD CARGO - FORWARD CARGO DOOR LOWER AFT DOOR JAMB AT STATION 1002.3 LONGERON -40 RIGHT TO LONGERON -41 RIGHT CHAFFED DOU
- [SDR FDEA202409111300](https://openairdocs.org/sdr/FDEA202409111300.md): Seat Track · cracked · Sep 11, 2024 · N596FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK - CARGO COMPARTMENT SEAT TRACK AT STATION 635 X=- 8.5 CRACKED. APPROXIMATELY 2.5 INCHES. MAIN DECK - CARGO COMPARTMENT CRACKED SEAT TRACK APPROXIMATELY 2.5 INCHES AT STATION 635 X= -8.5 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM EXISTING
- [SDR FDEA202409111299](https://openairdocs.org/sdr/FDEA202409111299.md): Slide · cracked · Sep 11, 2024 · N596FE · Doug MD11F · Escape Slide
  > EMERGENCY EVACUATION SLIDE ASSEMBLY WARNING LIGHT INOPERATIVE-BUZZER OPERATIVE PERFORMED OPS CHECK OF SLIDE TEST SWITCH PER AMM 52-73-14/401. OPS CHECK NORMAL. LIGHT AND HORN FUNCTION NORMAL.
- [SDR FDEA202409111298](https://openairdocs.org/sdr/FDEA202409111298.md): Seat Track · cracked · Sep 11, 2024 · N596FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK - CARGO COMPARTMENT SEAT TRACK AT STATION 755 X=- 8.5 CRACKED. APPROXIMATELY 2 INCHES. MAIN DECK - CARGO COMPARTMENT CRACKED SEAT TRACK APPROIMATELY 2 INCHES AT STATION 755 X= -8.5 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM EXISTING SPLICE
- [SDR FDEA202409111297](https://openairdocs.org/sdr/FDEA202409111297.md): Intercostal · cracked · Sep 11, 2024 · N596FE · Doug MD11F · Turbine Engine Air Inlet Section
  > EMPENNAGE: FROM #2 ENG INTAKE DUCT ACCESS PANEL FOUND RIGHT HAND INTERCOSTAL AFT EDGE CRACKED (LENGTH:1 INCH) BETWEEN STATION 2161 REAR CENTER SPAR TO REAR SPAR. EMPENNAGE RIGHT HAND INTERCOSTAL AFT EDGE BETWEEN STATION 2161 REAR CENTER SPAR TO REAR SPAR
- [SDR FDEA202409111295](https://openairdocs.org/sdr/FDEA202409111295.md): Stringer · cracked · Sep 11, 2024 · N596FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > DURING ACCOMPLISHING WORKCARD 57.20.01.2, FOUND CRACK ON CENTER UPPER AUXILLARY TANK STRINGER 47 AT STATION XCW -46.5. CENTER UPPER AUXILLARY TANK STRINGER 47 STATION XCW -46.5 AREA REPAIR CARRIED OUT AS PER MD11 SRM57-10-03-2R FIGURE 201 REPAIR 1. FUEL LE
- [SDR FDEA202409111294](https://openairdocs.org/sdr/FDEA202409111294.md): Stringer · cracked · Sep 11, 2024 · N596FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > DURING ACCOMPLISHING WORKCARD 57.20.01.2, FOUND CRACK ON CENTER UPPER AUXILLARY TANK STRINGER 47 AT STATION XCW -17. CENTER UPPER AUXILLARY TANK STRINGER 47 STATION XCW -17 AREA REPAIR CARRIED OUT AS PER MD11 SRM57-10-03-2R FIGURE 201 REPAIR 1. FUEL LEAK C
- [SDR FDEA202409111293](https://openairdocs.org/sdr/FDEA202409111293.md): Stringer · cracked · Sep 11, 2024 · N596FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > DURING ACCOMPLISHING WORKCARD 57.20.01.2, FOUND CRACK ON CENTER UPPER AUXILLARY TANK STRINGER 47 AT STATION XCW 46.5. CENTER UPPER AUXILLARY TANK STRINGER 47 STATION XCW 46.5 AREA REPAIR CARRIED OUT AS PER MD11 SRM57-10-03-2R FIGURE 201 REPAIR 1. FUEL LEAK
- [SDR FDEA202409111292](https://openairdocs.org/sdr/FDEA202409111292.md): Stringer · cracked · Sep 11, 2024 · N596FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > DURING ACCOMPLISHING WORKCARD 57.20.01.2, FOUND CRACK ON CENTER UPPER AUXILLARY TANK STRINGER 47 AT STATION XCW 17. CENTER UPPER AUXILLARY TANK STRINGER 47 STATION XCW 17 AREA REPAIR CARRIED OUT AS PER MD11 SRM57-10-03-2R FIGURE 201 REPAIR 1. FUEL LEAK CHE
- [SDR FDEA202409091263](https://openairdocs.org/sdr/FDEA202409091263.md): Cargo Track · gouged · Sep 9, 2024 · N596FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK - CARGO COMPARTMENT SEAT TRACK AT STATION 1289 X= 27.5 FOUND CROWN DAMAGED. MAIN DECK - CARGO COMPARTMENT SEAT TRACK AT STATION 1289 X= 27.5 CROWN GOUGE MARK ON EDGE AREA REMOVED AS PER MD11 SRM 51-21-01-0G AND FOUND EXCEEDED LIMIT AS PER MD11
- [SDR FDEA202409091262](https://openairdocs.org/sdr/FDEA202409091262.md): Cargo Track · gouged · Sep 9, 2024 · N596FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK - CARGO COMPARTMENT SEAT TRACK AT STATION 1289 X= 47.5 FOUND CROWN DAMAGED. MAIN DECK - CARGO COMPARTMENT SEAT TRACK AT STATION 1289 X= 47.5 CROWN GOUGE MARK ON EDGE AREA REMOVED AS PER MD11 SRM 51-21-01-0G AND FOUND EXCEEDED LIMIT AS PER MD11
- [SDR FDEA202409091261](https://openairdocs.org/sdr/FDEA202409091261.md): Cargo Track · gouged · Sep 9, 2024 · N596FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CARGO COMPARTMENT SEAT TRACK AT STATION 1506 X= -27.5 FOUND CROWN DAMAGED. MAIN DECK - CARGO COMPARTMENT SEAT TRACK AT STATION 1506 X= -27.5 CROWN GOUGE ON EDGE REMOVED AS PER MD11 SRM 51-21-01-0G AND FOUND EXCEEDED LIMIT AS PER MD11 SRM 53-00-52-1A FIGU
- [SDR FDEA202409091260](https://openairdocs.org/sdr/FDEA202409091260.md): Cargo Track · gouged · Sep 9, 2024 · N596FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK - CARGO COMPARTMENT SEAT TRACK AT STATION 5-10 X= 47.5 FOUND CROWN DAMAGED. MAIN DECK - CARGO COMPARTMENT SEAT TRACK AT STATION 5-10 X= 47.5 CROWN GOUGE ON EDGE AREA REMOVED AS PER MD11 SRM 51-21-01-0G AND FOUND EXCEEDED LIMIT AS PER MD11 SRM 53-00-5
- [SDR FDEA202409091258](https://openairdocs.org/sdr/FDEA202409091258.md): Cargo Track · gouged · Sep 9, 2024 · N596FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK - CARGO COMPARTMENT SEAT TRACK AT STATION 1384 X= -8.5 FOUND CROWN DAMAGED. MAIN DECK - CARGO COMPARTMENT SEAT TRACK AT STATION 1384 X= -8.5 CROWN GOUGE MARK ON EDGE AREA REMOVED AS PER MD11 SRM 51-21-01-0G AND FOUND EXCEEDED LIMIT AS PER MD11
- [SDR FDEA202409091257](https://openairdocs.org/sdr/FDEA202409091257.md): Cargo Track · gouged · Sep 9, 2024 · N596FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK - CARGO COMPARTMENT SEAT TRACK AT STATION 1750 X= 8.5 FOUND CROWN DAMAGED. MAIN DECK - CARGO COMPARTMENT SEAT TRACK AT STATION 1750 X= 8.5 CROWN GOUGE ON EDGE AREA REMOVED AS PER MD11 SRM 51-21-01-0G AND FOUND EXCEEDED LIMIT AS PER MD11 SRM 53-
- [SDR FDEA202409091256](https://openairdocs.org/sdr/FDEA202409091256.md): Cargo Track · gouged · Sep 9, 2024 · N596FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK - CARGO COMPARTMENT SEAT TRACK AT STATION 1166 X= 47.5 FOUND CROWN DAMAGED. MAIN DECK - CARGO COMPARTMENT SEAT TRACK AT STATION 1166 X= 47.5 CROWN GOUGE MARK ON EDGE AREA REMOVED AS PER MD11 SRM 51-21-01-0G AND FOUND EXCEEDED LIMIT AS PER MD11
- [SDR FDEA202409061249](https://openairdocs.org/sdr/FDEA202409061249.md): Skin · cracked · Sep 6, 2024 · N596FE · Doug MD11F · Wing, Plate/Skin
  > RIGHT WING - NUMBER 12 LEADING EDGE SLAT TRACK CUTOUT OUTBOARD LOWER CORNER SKIN FOUND CRACK AT STATION XOS 776. REPAIR CARRIED OUT AT RIGHT WING - NUMBER 12 LEADING EDGE SLAT TRACK CUTOUT OUTBOARD LOWER CORNER SKIN AT STATION XOS 776 AS PER MD-11 SRM 57-4
- [SDR FDEA202409051241](https://openairdocs.org/sdr/FDEA202409051241.md): Doubler · corroded · Sep 5, 2024 · N596FE · Doug MD11F · Wing Main, Frame Structure
  > RIGHT WING - UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER BETWEEN INNER REAR SPAR AND YW 467, BETWEEN XW 212 AND XW 230 FOUND CORROSION AS MARKED. RIGHT WING - UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER BETWEEN INNER REAR SPAR
- [SDR FDEA202409051240](https://openairdocs.org/sdr/FDEA202409051240.md): Doubler · corroded · Sep 5, 2024 · N596FE · Doug MD11F · Wing, Plate/Skin
  > LEFT WING - UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER BETWEEN AUXILLARY SPAR AND YW 467 FOUND CORROSION LEFT WING - UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER BETWEEN AUXILLARY SPAR AND YW 467 AREA CORROSION REMOVED AND FOU
- [SDR FDEA202409041236](https://openairdocs.org/sdr/FDEA202409041236.md): Doubler · cracked · Sep 4, 2024 · N596FE · Doug MD11F · Wing, Plate/Skin
  > RIGHT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 764 FOUND CRACK ABOUT 0.3". REPAIR CARRIED OUT AT LEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 654 AS PER MD - 11 SRM 57 - 40 - 02 - 2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS
- [SDR FDEA202409041235](https://openairdocs.org/sdr/FDEA202409041235.md): Doubler · cracked · Sep 4, 2024 · N596FE · Doug MD11F · Wing, Plate/Skin
  > RIGHT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 676 FOUND CRACK ABOUT 0.3". REPAIR CARRIED OUT AT RIGHT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 676 AS PER MD - 11 SRM 57 - 40 - 02 - 2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED A
- [SDR FDEA202409041234](https://openairdocs.org/sdr/FDEA202409041234.md): Doubler · cracked · Sep 4, 2024 · N596FE · Doug MD11F · Wing, Plate/Skin
  > RIGHT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 619 FOUND CRACK ABOUT 0.2". REPAIR CARRIED OUT AT RIGHT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 619 AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR
- [SDR FDEA202409041233](https://openairdocs.org/sdr/FDEA202409041233.md): Doubler · cracked · Sep 4, 2024 · N596FE · Doug MD11F · Wing, Plate/Skin
  > LEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 749 FOUND CRACK ABOUT 0.3 INCH. REPAIR CARRIED OUT AT LEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 794 AS PER MD - 11 SRM 57 - 40 - 02 - 2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED
- [SDR FDEA202409041232](https://openairdocs.org/sdr/FDEA202409041232.md): Doubler · cracked · Sep 4, 2024 · N596FE · Doug MD11F · Wing, Plate/Skin
  > LEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 688 FOUND CRACK ABOUT 0.2 INCH. REPAIR CARRIED OUT AT LEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 688 AS PER MD - 11 SRM 57 - 40 - 02 - 2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED
- [SDR FDEA202409041231](https://openairdocs.org/sdr/FDEA202409041231.md): Doubler · cracked · Sep 4, 2024 · N596FE · Doug MD11F · Wing, Plate/Skin
  > LEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 654 FOUND CRACK ABOUT 0.3 INCH. REPAIR CARRIED OUT AT LEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 654 AS PER MD - 11 SRM 57 - 40 - 02 - 2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED
- [SDR FDEA202409041230](https://openairdocs.org/sdr/FDEA202409041230.md): Doubler · cracked · Sep 4, 2024 · N596FE · Doug MD11F · Wing, Plate/Skin
  > LEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 618 FOUND CRACK ABOUT O.2 INCH. REPAIR CARRIED OUT AT LEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 618 AS PER MD - 11 SRM 57 - 40 - 02 - 2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED
- [SDR FDEA202409041229](https://openairdocs.org/sdr/FDEA202409041229.md): Trunnion · cracked · Sep 4, 2024 · N596FE · Doug MD11F · Fuselage, Landing Gear Attach Fittings
  > NOSE LANDING GEAR LEFT HAND EXISTING TRIMMED OUT AREA TRUNNION FITTING STATION 595 CRACK APPROXIMATE 0.200". HIGH FREQUENCY EDDY CURRENT AT EXISTING TRIMMED OUT AREA ON NOSE LANDING GEAR LEFT HAND TRUNNION FITTING ADJACENT AREA AT APPROXIMATE STATION Y=59
- [SDR FDEA202407141001](https://openairdocs.org/sdr/FDEA202407141001.md): Deu · faulted · Jul 14, 2024 · N596FE · Doug MD11F · Engine Indicating System
  > ENGINE FAIL LIGHT ILLUMINATED AT ABOUT 100 KTS ON THE TAKEOFF ROLL. THE TAKEOFF WAS REJECTED. ALL ENGINES WERE OPERATING NORMALLY AFTER THE REJECT. REPLACED DEU-3. OPS CKS GOOD.
- [SDR FDEA202405140666](https://openairdocs.org/sdr/FDEA202405140666.md): Actuator · cracked · May 14, 2024 · N596FE · Doug MD11F · Nose/Tail Landing Gear
  > APPROX 2 MIN AFTER GEAR RETRACTION, LEVEL 2 HYD 3 FAIL CAUTION. TURNED BACK TOWARDS MEMPHIS AND PROCEEDED WITH QRH FOR HYD 3 FAIL. NOSE GEAR SHOWED UNSAFE, AFTER DISCUSSION WITH MOC, FLEET CAPTAIN, AND TECH PILOT A LOW APPROACH WAS CONDUCTED TO VERIFY NOS
- [SDR FDEA202211042727](https://openairdocs.org/sdr/FDEA202211042727.md): Skin · cracked · Nov 4, 2022 · N596FE · Doug MD11F · Fuselage Main, Plate/Skin
  > AGING AIRCRAFT - EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT LEFT 3 DOOR FORWARD FUSELAGE JAMB WEB AT STATION 1255 BETWEEN LONGERON 26 TO LONGERON 27 LEFT HAND. EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT LEFT 3 DOOR FORWARD FUSELAGE JAMB WEB AT S
- [SDR FDEA202211032720](https://openairdocs.org/sdr/FDEA202211032720.md): Skin · none · Nov 3, 2022 · N596FE · Doug MD11F · Wing Miscellaneous Structure
  > DURING ULTRASONIC INSPECTION AT RIGHT HAND WING FUEL TANK CUTOUT BETWEEN STATION XORS = 683.4 AND STATION XORS = 713.6 FOUND EXISTING REPAIR BUSHING AT HOLE ( #8, #9, #10, #11, #13, #29, #30, #31, #32, #33, #34, #36). RIGHT WING FUEL TANK CUTOUT EXIS
- [SDR FDEA202211032719](https://openairdocs.org/sdr/FDEA202211032719.md): Skin · none · Nov 3, 2022 · N596FE · Doug MD11F · Wing Structure
  > DURING ULTRASONIC INSPECTION AT LEFT HAND WIING FUEL TANK CUTOUT BETWEEN STATION XORS = 683.4 AND STATION XORS = 713.6 FOUND EXISTING REPAIR BUSHING AT HOLE ( #7,#8,#9,#10,#11,#13,#14,#16,#28,#29,#30,#31,#32,#33,#36). LEFT HAND WING FUEL TANK CUTOUT EXIST
- [SDR FDEA202211022711](https://openairdocs.org/sdr/FDEA202211022711.md): None · none · Nov 2, 2022 · N596FE · Doug MD11F · Standard Practices/Structures
  > AGING AIRCRAFT - EXISTING REPAIR DOUBLER FOUND AT LEFT HAND HORIZONTAL STABILIZER LEADING EDGE APPROXIMATELY BETWEEN XFS = 228.840 AND XFS = 246.301. EXISTING REPAIR DOUBLER AT LEFT HAND HORIZONTAL STABILIZER LEADING EDGE APPROXIMATELY BETWEEN XFS=228.840
- [SDR FDEA202210292690](https://openairdocs.org/sdr/FDEA202210292690.md): Longeron Splice · cracked · Oct 29, 2022 · N596FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > CENTER CARGO - BILGE STATION 5-113 TO STATION 1541 LONGERON 45 RIGHT SPLICE FOUND CRACKED. SPLICE AT CENTER CARGO - BILGE STATION 5-113 TO STATION 1541 LONGERON 45 RIGHT REMOVED AS PER SRM 51-33-01-0G. SPLICE FABRICATED BY MACHINING AS PER DOUGLAS DRAWI
- [SDR FDEA202210292693](https://openairdocs.org/sdr/FDEA202210292693.md): Longeron Splice · cracked · Oct 29, 2022 · N596FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > CENTER CARGO - BILGE STATION 5-113 TO STATION 1541 LONGERON 45 RIGHT SPLICE FOUND CRACKED. CRACKED SPLICE AT CENTER CARGO - BILGE STATION 5-113 TO STATION 1541 LONGERON 45 RIGHT REMOVED AS PER SRM 51-33-01-0G. SPLICE FABRICATED BY MACHINING AS PER DOUGLA
- [SDR FDEA202210292692](https://openairdocs.org/sdr/FDEA202210292692.md): Longeron Splice · cracked · Oct 29, 2022 · N596FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > CENTER CARGO - BILGE STATION 5-113 TO STATION 1541 LONGERON 45 RIGHT SPLICE FOUND CRACKED. CRACKED SPLICE AT CENTER CARGO - BILGE STATION 5-113 TO STATION 1541 LONGERON 45 RIGHT REMOVED AS PER SRM 51-33-01-0G. SPLICE FABRICATED BY MACHINING AS PER DOUGLA
- [SDR FDEA202210292691](https://openairdocs.org/sdr/FDEA202210292691.md): Longeron Splice · cracked · Oct 29, 2022 · N596FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > CENTER CARGO - BILGE STATION 5-113 TO STATION 1541 LONGERON 45 RIGHT SPLICE FOUND CRACKED. CRACKED SPLICE AT CENTER CARGO - BILGE STATION 5-113 TO STATION 1541 LONGERON 45 RIGHT REMOVED AS PER SRM 51-33-01-0G. SPLICE FABRICATED BY MACHINING AS PER DOUGLA

Next page: https://openairdocs.org/aircraft/N596FE/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 = 'N596FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N596FE/reports

---
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.