# Service difficulty reports: N595FE A list on [N595FE](https://openairdocs.org/aircraft/N595FE.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 8 · 389 reports - [SDR FDEA202610051476](https://openairdocs.org/sdr/FDEA202610051476.md): Floor Panel · delaminated · Oct 5, 2026 · N595FE · Doug MD11F · Fuselage Floor Panel > MAIN DECK CARGO COMPARTMENT FLOOR PANEL #271EF FOUND DELAMINATED AT STATION 1361 TO STATION 1481. CABIN MAIN DECK CARGO COMPARTMENT DELAM FLOOR PANEL #271EF STATION 1351 TO 1481 REMOVED AND REPLACED WITH FABRICATED FLOOR PANEL AS PER AMM 53-21-04-4. PANEL - [SDR FDEA202610051475](https://openairdocs.org/sdr/FDEA202610051475.md): Floor Panel · delaminated · Oct 5, 2026 · N595FE · Doug MD11F · Fuselage Floor Panel > MAIN DECK CARGO COMPARTMENT FLOOR PANEL FOUND DELAMINATED AT BS 1361 TO 1481. CABIN MAIN DECK CARGO COMPARTMENT DELAM FLOOR PANEL #272EF STATION 1351 TO 1481 REMOVED AND REPLACED WITH FABRICATED FLOOR PANEL AS PER AMM 53-21-04-4. PANEL FABRICATED AS PER D - [SDR FDEA202610011462](https://openairdocs.org/sdr/FDEA202610011462.md): Floor Support · corroded · Oct 1, 2026 · N595FE · Doug MD11F · Fuselage Miscellaneous Structure > CABIN - MAIN DECK CARGO COMPARTMENT FLOOR PANEL SUPPORT AT STATION 735, X = -15" FOUND CORRODED. CABIN - MAIN DECK CARGO COMPARTMENT FLOOR PANEL SUPPORT CORRODED AT STATION 735 X = -15" EVALUATED, FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER MD - 11 SRM 53-0 - [SDR FDEA202610011461](https://openairdocs.org/sdr/FDEA202610011461.md): Floor Support · corroded · Oct 1, 2026 · N595FE · Doug MD11F · Fuselage Miscellaneous Structure > MAIN DECK CARGO COMPARTMENT FLOOR SUPPORT AT STATION 735, X = 0 FOUND WITH CORROSION. CABIN - MAIN DECK CARGO COMPARTMENT FLOOR SUPPORT CORRODED AT STATION 735 X = 0 EVALAUTED, FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER MD -11 SRM 53-00-00-2R FIGURE 202 - [SDR FDEA202609291449](https://openairdocs.org/sdr/FDEA202609291449.md): Seat Track · corroded · Sep 29, 2026 · N595FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO LEFT HAND AFT COMPARTMENT FLOOR SEAT TRACK FOUND WITH CORROSION AT STATION 1997 X= 107. SEAT TRACK BS 1997, X= 107 EVALUATED FOUND EXFOLIATION EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED - [SDR FDEA202609291448](https://openairdocs.org/sdr/FDEA202609291448.md): Longeron Splice · corroded · Sep 29, 2026 · N595FE · Doug MD11F · Fuselage Main, Longeron/Stringer > LOWER CENTER CARGO COMPARTMENT BILGE AREA LONGERON 48R SPLICE FOUND CORRODED AT BS 1705. EVALUATED AND FOUND EXFOLIATION OUT OF LIMITS IAW SRM 53-00-00-2R, FIGURE 205, SHEET 1. THE LONGERON SPLICE WAS REMOVED AND REPLACED WITH FABRICATED SPLICE IAW SRM 51-3 - [SDR FDEA202609291446](https://openairdocs.org/sdr/FDEA202609291446.md): Seat Track · corroded · Sep 29, 2026 · N595FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 715, X= 8.5" FOUND WITH CORROSION. SEAT TRACK EVALUATED AND FOUND EXFOLIATED AND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT AT EXISTING - [SDR FDEA202609241435](https://openairdocs.org/sdr/FDEA202609241435.md): Seat Track · corroded · Sep 24, 2026 · N595FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO BAY SEAT TRACK AT BS 775, X= -72.25" CROWN FOUND WORN. SEAT TRACK EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. - [SDR FDEA202609241434](https://openairdocs.org/sdr/FDEA202609241434.md): Seat Track · corroded · Sep 24, 2026 · N595FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO BAY SEAT TRACK AT BS 755, X= -8.5" CROWN FOUND WORN. SEAT TRACK EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. R - [SDR FDEA202609241433](https://openairdocs.org/sdr/FDEA202609241433.md): Seat Track · corroded · Sep 24, 2026 · N595FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO BAY SEAT TRACK AT BS 755, X= 27.5" CROWN FOUND WORN. THE SEAT TRACK WAS EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT IAW SRM 53-00-52-2R, FIGURE 201, REP - [SDR FDEA202609241432](https://openairdocs.org/sdr/FDEA202609241432.md): Seat Track · corroded · Sep 24, 2026 · N595FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO BAY SEAT TRACK AT BS 1431, X= 8.5" CROWN FOUND WORN. SEAT TRACK BS 1431, X= 8.5" WAS EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT AT EXISTING - [SDR FDEA202609241431](https://openairdocs.org/sdr/FDEA202609241431.md): Seat Track · corroded · Sep 24, 2026 · N595FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO BAY SEAT TRACK AT BS 1149, X= 47.5" CROWN FOUND WORN. MAIN DECK CARGO COMPARTMENT WORN CROWN AT SEAT TRACK STATION 1149 X= 47.5" EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT - [SDR FDEA202609241430](https://openairdocs.org/sdr/FDEA202609241430.md): Seat Track · corroded · Sep 24, 2026 · N595FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO BAY SEAT TRACK AT BS 1149, X= 27.5" CROWN FOUND WORN. SEAT TRACK, BS 1149, X= 27.5" EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT, BS 1169 TO EX - [SDR FDEA202609241429](https://openairdocs.org/sdr/FDEA202609241429.md): Seat Track · corroded · Sep 24, 2026 · N595FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO BAY SEAT TRACK AT BS 1681, X= 47.5" CROWN FOUND WORN. MAIN DECK CARGO COMPARTMENT WORN CROWN AT SEAT TRACK STATION 1681 X= 47.5" EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT - [SDR FDEA202609241428](https://openairdocs.org/sdr/FDEA202609241428.md): Seat Track · corroded · Sep 24, 2026 · N595FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 1381, X= -27.5" FOUND CORRODED. SEAT TRACK, BS 1381, X= -27.5" EVALUATED & FOUND EXFOLIATED, EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMEN - [SDR FDEA202609241427](https://openairdocs.org/sdr/FDEA202609241427.md): Seat Track · corroded · Sep 24, 2026 · N595FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 1431, X= -8.5" CROWN FOUND WORN. SEAT TRACK BS 1431 X= -8.5", EVALUATED & FOUND EXCEEDED LIMITS SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT, BS 1391 - 145 - [SDR FDEA202609241426](https://openairdocs.org/sdr/FDEA202609241426.md): Seat Track · corroded · Sep 24, 2026 · N595FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 1431, X= 47.5" CROWN FOUND WORN. MAIN DECK CARGO COMPARTMENT WORN CROWN AT SEAT TRACK STATION 1431 X= 47.5" EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN W - [SDR FDEA202609241425](https://openairdocs.org/sdr/FDEA202609241425.md): Seat Track · corroded · Sep 24, 2026 · N595FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO BAY SEAT TRACK AT STATION 1260, X= -8.5" CROWN FOUND WORN. SEAT TRACK EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT IAW SRM 53-00-52-2R, FIGURE 2 - [SDR FDEA202609241424](https://openairdocs.org/sdr/FDEA202609241424.md): Seat Track · corroded · Sep 24, 2026 · N595FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 1319, X= -27.5" FOUND CORRODED. SEAT TRACK BS 1319, X= -27.5", EVALUATED, FOUND EXFOLIATED & EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEME - [SDR FDEA202609231417](https://openairdocs.org/sdr/FDEA202609231417.md): Skin · cracked · Sep 23, 2026 · N595FE · Doug MD11F · Fuselage Main, Plate/Skin > NR 3 AIRCON COMPARTMENT ACCESS DOOR CUTOUT UPPER AFT CORNER FOUND CRACKED AT STATION 535. CRACKED SKIN AT FUSELAGE #3 AIRCON COMPARTMENT ACCESS DOOR CUTOUT UPPER AFT CORNER AT STATION 535 REPAIRED AS PER MD-11 SRM 53-20-15-2R REPAIR 3 FIGURE 201. INITIAL I - [SDR FDEA202609231416](https://openairdocs.org/sdr/FDEA202609231416.md): Attach Fitting · cracked · Sep 23, 2026 · N595FE · Doug MD11F · Wing, Attach Fittings > LEFT WING- LEADING EDGE COMPARTMENT ATTACH FORMER XOS 939 FOUND CRACK ABOUT 0.6 INCHES. LEFT HAND WING LEADING EDGE COMPARTMENT CRACKED FORMER AT XOS 939 REMOVED IAW SRM 51-33-01-0G AND MD-11 SRM 51-35-01-06. FABRICATED FORMER PER DRAWING ARB 1292 REVISION - [SDR FDEA202609221414](https://openairdocs.org/sdr/FDEA202609221414.md): Skin · cracked · Sep 22, 2026 · N595FE · Doug MD11F · Wing, Plate/Skin > HIGH FREQUENCY EDDY CURRENT INSPECTION FOUND CRACK INDICATION APPROXIMATE 0.25" IN LENGTH AT RIGHT HAND WING FIXED LEADING EDGE SKIN ADJACENT TO CUTOUT AT CORNER NUMBER 5 SLAT ACTUATOR ACCESS DOOR FORWARD INBOARD CORNER AT APPROXIMATE STATION XOS 484.511 - [SDR FDEA202609221413](https://openairdocs.org/sdr/FDEA202609221413.md): Skin · cracked · Sep 22, 2026 · N595FE · Doug MD11F · Wing, Plate/Skin > HIGH FREQUENCY EDDY CURRENT INSPECTION FOUND CRACK INDICATION APPROXIMATE 0.15" IN LENGTH AT LEFT HAND WING FIXED LEADING EDGE SKIN ADJACENT TO CUTOUT AT CORNER NUMBER 13 SLAT TRACK CUTOUT #10 AFT INBOARD CORNER AT APPROXIMATE STATION XOS 659.7174. - [SDR FDEA202609221412](https://openairdocs.org/sdr/FDEA202609221412.md): Skin · cracked · Sep 22, 2026 · N595FE · Doug MD11F · Wing, Plate/Skin > HIGH FREQUENCY EDDY CURRENT INSPECTION FOUND CRACK INDICATION APPROXIMATE 0.15" IN LENGTH AT LEFT HAND WING FIXED LEADING EDGE SKIN ADJACENT TO CUTOUT AT CORNER NUMBER 13 SLAT TRACK CUTOUT #10 AFT INBOARD CORNER AT APPROXIMATE STATION XOS 659.7174. CUTO - [SDR FDEA202609221411](https://openairdocs.org/sdr/FDEA202609221411.md): Angle · cracked · Sep 22, 2026 · N595FE · Doug MD11F · Wing Miscellaneous Structure > LEFT WING- LEADING EDGE COMPARTMENT ANGLE AT XOS 1083 FOUND CRACK ABOUT 0.4 INCHES. LEFT HAND WING LEADING EDGE COMPARTMENT CRACKED ANGLE AT XOS 1083 REMOVED PER MD-11 SRM 51-35-01-0G. FABRICATED ANGLE PER DOUGLAS DRAWING ARB 2920 REVISION BB. FABRICATE - [SDR FDEA202609221410](https://openairdocs.org/sdr/FDEA202609221410.md): Skin · cracked · Sep 22, 2026 · N595FE · Doug MD11F · Wing, Plate/Skin > RIGHT HAND WING- LEADING EDGE COMPARTMENT ANGLE AT XOS 1083 FOUND CRACK ABOUT 0.5 INCHES. RIGHT HAND WING LEADING EDGE COMPARTMENT CRACKED ANGLE AT XOS 1083 REMOVED PER MD-11 SRM 51-33-01-0G AND MD-11 SRM 51-35-01-0G. FABRICATED ANGLE PER DOUGLAS DRAWING - [SDR FDEA202609221409](https://openairdocs.org/sdr/FDEA202609221409.md): Doubler · cracked · Sep 22, 2026 · N595FE · Doug MD11F · Wing, Plate/Skin > LEFT HAND WING- LEADING EDGE COMPARTMENT BEADED DOUBLER AT XOS 688 FOUND CRACK ABOUT 0.2 INCH. LEFT HAND WING LEADING EDGE COMPARTMENT CRACKED BEADED DOUBLER AT XOS 688 CARRIED OUT REPAIR PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED A - [SDR FDEA202609221408](https://openairdocs.org/sdr/FDEA202609221408.md): Skin · cracked · Sep 22, 2026 · N595FE · Doug MD11F · Wing, Plate/Skin > RIGHT HAND WING- LEADING EDGE COMPARTMENT BEADED DOUBLER AT XOS 762 FOUND CRACK ABOUT 0.2 INCH. RIGHT HAND WING LEADING EDGE COMPARTMENT CRACKED BEADED DOUBLER AT XOS 762 CARRIED OUT REPAIR PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED - [SDR FDEA202609221407](https://openairdocs.org/sdr/FDEA202609221407.md): Skin · cracked · Sep 22, 2026 · N595FE · Doug MD11F · Wing, Plate/Skin > RIGHT HAND WING- NUMBER 11 SLAT TRACK LOWER CUT OUT OUTBOARD CORNER FOUND CRACK ABOUT 0.5 INCH AT XOS 717. RIGHT WING NUMBER 11 SLAT TRACK CRACKED SKIN AT XOS 717 LOWER CUTOUT FASTENERS REMOVED PER MD-11 SRM 51-33-01-0G AND MD-11 SRM 51-35-01-0G AND TRIMM - [SDR FDEA202609221406](https://openairdocs.org/sdr/FDEA202609221406.md): Skin · cracked · Sep 22, 2026 · N595FE · Doug MD11F · Leading Edge Devices > RIGHT HAND WING- NUMBER 14 SLAT TRACK LOWER CUT OUT OUTBOARD CORNER FOUND CRACK ABOUT 0.5 INCH AT XOS 889. RIGHT WING NUMBER 14 SLAT TRACK CRACKED SKIN AT XOS 889 LOWER CUTOUT FASTENERS REMOVED AS PER MD-11 SRM 51-33-01-0G AND MD-11 SRM 51-35-01-0G AND TR - [SDR FDEA202609211389](https://openairdocs.org/sdr/FDEA202609211389.md): Seat Track · worn · Sep 21, 2026 · N595FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 6-10, X= -27.5 FOUND THE CROWN WORN. THE SEAT TRACK WAS EVALUATED & FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT AT EXISTING SPLIC - [SDR FDEA202609211388](https://openairdocs.org/sdr/FDEA202609211388.md): Seat Track · worn · Sep 21, 2026 · N595FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 6-10, X= -47.5 FOUND THE CROWN WORN. SEAT TRACK EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT BTWN EXISTING SPLICES - [SDR FDEA202609211387](https://openairdocs.org/sdr/FDEA202609211387.md): Seat Track · worn · Sep 21, 2026 · N595FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 6-10, X= -8.5 FOUND THE CROWN WORN. SEAT TRACK EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT BTWN EXISTING SPLICES BS - [SDR FDEA202609211386](https://openairdocs.org/sdr/FDEA202609211386.md): Seat Track · worn · Sep 21, 2026 · N595FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 6-10, X= 8.5 FOUND THE CROWN WORN. THE SEAT TRACK WAS EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT BTWN EXISTING S - [SDR FDEA202609211385](https://openairdocs.org/sdr/FDEA202609211385.md): Seat Track · worn · Sep 21, 2026 · N595FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 6-10, X= 27.5 FOUND THE CROWN WORN. THE SEAT TRACK WAS EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT BTWN BS 6-60 - - [SDR FDEA202609211384](https://openairdocs.org/sdr/FDEA202609211384.md): Seat Track · worn · Sep 21, 2026 · N595FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 6-10, X= 47.5 FOUND THE CROWN WORN. THE SEAT TRACK WAS EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM EXISTING SPLICES BS - [SDR FDEA202609211383](https://openairdocs.org/sdr/FDEA202609211383.md): Seat Track · worn · Sep 21, 2026 · N595FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 1010 X= 47.5 FOUND THE CROWN WORN. THE SEAT TRACK WAS EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT, BS 969 - 1029, - [SDR FDEA202609211382](https://openairdocs.org/sdr/FDEA202609211382.md): Seat Track · worn · Sep 21, 2026 · N595FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 1010 X= 8.5 FOUND THE CROWN WORN. THE SEAT TRACK WAS EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT, BS 989 - 1029, X= - [SDR FDEA202609211381](https://openairdocs.org/sdr/FDEA202609211381.md): Seat Track · worn · Sep 21, 2026 · N595FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 1010 X= -8.5 FOUND THE CROWN WORN. SEAT TRACK BS 1010 X= -8.5", EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT, BS 989 - [SDR FDEA202609211380](https://openairdocs.org/sdr/FDEA202609211380.md): Seat Track · worn · Sep 21, 2026 · N595FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 1010 X= -47.5 FOUND THE CROWN WORN. SEAT TRACK EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT BS 989 - 1029 X= -47.5" IAW - [SDR FDEA202608211201](https://openairdocs.org/sdr/FDEA202608211201.md): Bulkhead · damaged · Aug 21, 2026 · N595FE · Doug MD11F · Nacelle/Pylon, Main Frame > NR 1 PYLON AFT SPHERICAL BEARING EXISTING BORE HOLE MEASURED DIAMETER = 2.9995. AND FOUND CORROSION. CORROSION AT NR 1 PYLON AFT BULKHEAD CARRIED OUT REPAIR IAW EA 1-5440-T0388481, PART1. THIS EA DEVIATES FROM EO 1-5440-E0385675, PART 1. REPAIR CLASSIFIED - [SDR FDEA202608191154](https://openairdocs.org/sdr/FDEA202608191154.md): Bearing · damaged · Aug 19, 2026 · N595FE · Doug MD11F · Nacelle/Pylon, Main Frame > NR 3 PYLON AFT SPHERICAL BEARING EXISTING BORE HOLE MEASURED DIAMETER=3.040" AND FOUND CORRODED. NR 3 PYLON AFT BULKHEAD CARRIED OUT REPAIR AS PER EA 1-5440-T0388374 PART1, PART 2 AND PART 3. CLASSIFIED AS MAJOR PER GMM 6-2-100. - [SDR FDEA202506050840](https://openairdocs.org/sdr/FDEA202506050840.md): Battery · inoperative · Jun 5, 2025 · N595FE · Doug MD11F · Emergency Equipment > L1 PRESS TO TEST REMOTE SLIDE LIGHT IS INOP. REPLACED BATTERIES & BULBS, PREFORMED SLIDE FUNCTIONAL TEST IAW MM 25-61-05-01, OPS CHECKED GOOD, A/C OK FOR FLIGHT. - [SDR FDEA202503300539](https://openairdocs.org/sdr/FDEA202503300539.md): Engine · failed · Mar 30, 2025 · N595FE · Doug MD11F · Engine (Turbine/Turboprop) > PDIS 595 79-36 8740 30MAR25 02:47 NRT OPEN ENG 3 OIL FILTER LEVEL 2 ALERT @FL350. AIRFRAME VIBRATION STARTED JUST PRIOR TO ALERT AND CONTINUED UNTIL THROTTLE AT IDLE. ENGINE PARAMETERS NORMAL. CONSULTED QRH. SHUT DOWN #3 ENGINE AS ALERT WOULD - [SDR FDEA202501310160](https://openairdocs.org/sdr/FDEA202501310160.md): Bulb · wrong part · Jan 31, 2025 · N595FE · Doug MD11F · Emergency Equipment > 1L ESCAPE SLIDE BOTTLE PRESSURE LIGHT WILL NOT ILLUMINATE UPON TESTING. AMM: 25-61-04-5 T/S AND FOUND WRONG BULBS INSTALLED IN LIGHT ASSY. RELAMPED WITH PROPER 368 BULBS NOW L1 DOOR SLIDE REMOTE PRESSURE INDICATOR OPS CHECKS NORMAL REF MM 25-61-04-5. ACFT O - [SDR FDEA202410011410](https://openairdocs.org/sdr/FDEA202410011410.md): Floor Panel · delaminated · Oct 1, 2024 · N595FE · Doug MD11F · Fuselage Floor Panel > FLIGHT COMPARTMENT FLOOR PANEL #215BF FOUND DELAMINATED STATION 335. FLIGHT COMPARTMENT STATION 335 DELAMINATED FLOOR PANEL #215BF REMOVED AND REPLACED AS PER MD-11 AMM 53-21-02-4. FLOOR PANEL #215BF FABRICATED AS PER FEDEX DRAWING SRZ-25-005 REVISION R. R - [SDR FDEA202410011409](https://openairdocs.org/sdr/FDEA202410011409.md): Floor Panel · delaminated · Oct 1, 2024 · N595FE · Doug MD11F · Fuselage Floor Panel > FLIGHT COMPARTMENT FLOOR PANEL #216AF FOUND DELAMINATED STATION 330. FLIGHT COMPARTMENT STATION 330 DELAMINATED FLOOR PANEL #216AF REMOVED AND REPLACED AS PER MD-11 AMM 53-21-02-4. FLOOR PANEL #216AF FABRICATED AS PER FEDEX DRAWING SRZ-25-005 REVISION R. R - [SDR FDEA202410011408](https://openairdocs.org/sdr/FDEA202410011408.md): Floor Panel · delaminated · Oct 1, 2024 · N595FE · Doug MD11F · Fuselage Floor Panel > FLIGHT COMPARTMENT FLOOR PANEL #215DF FOUND DELAMINATED STATION 350. FLIGHT COMPARTMENT, STATION 350 DELAMINATED FLOOR PANEL #215DF REMOVED AND REPLACED AS PER MD-11 AMM 53-21-02-4. FLOOR PANEL #215DF FABRICATED AS PER FEDEX DRAWING SRZ-25-005 REVISION R. - [SDR FDEA202409271379](https://openairdocs.org/sdr/FDEA202409271379.md): Floor Panel · delaminated · Sep 27, 2024 · N595FE · Doug MD11F · Fuselage Floor Panel > CABIN - MAIN DECK CARGO COMPARTMENT FLOOR PANEL #231HF DELAM. CABIN - MAIN DECK CARGO COMPARTMENT, DELAMINATED FLOOR PANEL #231HF REMOVED AND REPLACED AS PER MD-11 AMM 53-21-04-4. FLOOR PANEL #231HF FABRICATED AS PER FEDEX DRAWING SRZ-25-005 REVISION R. RE - [SDR FDEA202409271378](https://openairdocs.org/sdr/FDEA202409271378.md): Floor Panel · delaminated · Sep 27, 2024 · N595FE · Doug MD11F · Fuselage Floor Panel > CABIN - MAIN DECK CARGO COMPARTMENT FLOOR PANEL #231GF DELAM. CABIN - MAIN DECK CARGO COMPARTMENT, DELAMINATED FLOOR PANEL #231GF REMOVED AND REPLACED AS PER MD-11 AMM 53-21-04-4. FLOOR PANEL #231GF FABRICATED AS PER FEDEX DRAWING SRZ-25-005 REVISION R. RE Next page: https://openairdocs.org/aircraft/N595FE/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 = 'N595FE' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N595FE/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.