# Service difficulty reports: N610FE

A list on [N610FE](https://openairdocs.org/aircraft/N610FE.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 10 · 497 reports

- [SDR FDEA202610151589](https://openairdocs.org/sdr/FDEA202610151589.md): Rib · broken · Oct 15, 2026 · N610FE · Doug MD11F · Leading Edge Devices
  > LEFT WING, NR 8 LEADING EDGE SLAT INNER RIB AT XOS 1135.627 FOUND BROKEN, AFTER REMOVAL OF LOWER SURFACE SKIN.
- [SDR FDEA202610151588](https://openairdocs.org/sdr/FDEA202610151588.md): Rib · broken · Oct 15, 2026 · N610FE · Doug MD11F · Leading Edge Devices
  > LEFT WING, NR 8 LEADING EDGE SLAT LOWER SURFACE HAD A LOOSE FASTENER, INNER RIB AT XOS 1141.221 FOUND BROKEN.
- [SDR FDEA202610101550](https://openairdocs.org/sdr/FDEA202610101550.md): Seat Track · worn · Oct 10, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO BAY SEAT TRACK AT BS 1139, X= -27.5, 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 BTWN EXISTING SPLICES BS 1129/6-100
- [SDR FDEA202610101549](https://openairdocs.org/sdr/FDEA202610101549.md): Seat Track · worn · Oct 10, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO BAY SEAT TRACK AT BS 1209, X= 47.5, 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 BTWN EXISTING SPLICES BS 1169 - 122
- [SDR FDEA202610091522](https://openairdocs.org/sdr/FDEA202610091522.md): Seat Track · worn · Oct 9, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO BAY SEAT TRACK AT BS 1249, X= -47.5, 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 BTWN BS 1311 TO EXISTING SPLICE BS
- [SDR FDEA202610091513](https://openairdocs.org/sdr/FDEA202610091513.md): Seat Track · worn · Oct 9, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO BAY SEAT TRACK AT BS 1139, X=47.5" 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 SPLICES BS 1129/6-100 - B
- [SDR FDEA202610091504](https://openairdocs.org/sdr/FDEA202610091504.md): Seat Track · worn · Oct 9, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN - FORWARD MIAN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 755, X=-8.5" FOUND CROWN WORN. CABIN - FWD MAIN DECK CARGO COMPARTMENT WORN CROWN AT SEAT TRACK STATION 755 X=-8.5" EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101
- [SDR FDEA202610091502](https://openairdocs.org/sdr/FDEA202610091502.md): Seat Track · worn · Oct 9, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > FORWARD MIAN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 755, X=47.5" FOUND CROWN WORN. CABIN - FWD MAIN DECK CARGO COMPARTMENT WORN CROWN AT SEAT TRACK STATION 755 X=47.5" EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOW
- [SDR FDEA202610091501](https://openairdocs.org/sdr/FDEA202610091501.md): Seat Track · worn · Oct 9, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > FORWARD MIAN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 635, X= 47.5" FOUND CROWN WORN. CABIN - FWD MAIN DECK CARGO COMPARTMENT WORN CROWN AT SEAT TRACK STATION 635 X= 47.5" EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALL
- [SDR FDEA202610091533](https://openairdocs.org/sdr/FDEA202610091533.md): Seat Track · worn · Oct 9, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO BAY SEAT TRACK AT BS 1671, X= -8.5" FOUND 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 BTWN BS 1651- 1691, X= -8.5 IA
- [SDR FDEA202610091532](https://openairdocs.org/sdr/FDEA202610091532.md): Seat Track · worn · Oct 9, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1671, X= 8.5" FOUND 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 1651 TO
- [SDR FDEA202610091531](https://openairdocs.org/sdr/FDEA202610091531.md): Seat Track · worn · Oct 9, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1551, X= 27.5" FOUND THE CROWN WORN. THE SEAT TRACK WAS EVALUATED AND FOUND EXCEEDED LIMITS SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT BTWN BS 1571 T
- [SDR FDEA202610091530](https://openairdocs.org/sdr/FDEA202610091530.md): Seat Track · worn · Oct 9, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1551, 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 BTWN BS 157
- [SDR FDEA202610091529](https://openairdocs.org/sdr/FDEA202610091529.md): Seat Track · worn · Oct 9, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 5-11, X= 47.5" FOUND 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 AT S
- [SDR FDEA202610091528](https://openairdocs.org/sdr/FDEA202610091528.md): Seat Track · worn · Oct 9, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 5-11, 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 BTWN BS 5-43 TO E
- [SDR FDEA202610091527](https://openairdocs.org/sdr/FDEA202610091527.md): Seat Track · worn · Oct 9, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 5-11, X= 8.5" FOUND 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 AT ST
- [SDR FDEA202610091526](https://openairdocs.org/sdr/FDEA202610091526.md): Seat Track · worn · Oct 9, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 1421, 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 BTWN BS 1391 A
- [SDR FDEA202610091525](https://openairdocs.org/sdr/FDEA202610091525.md): Seat Track · worn · Oct 9, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1421, X= -8.5" FOUND 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 AT STATION 1
- [SDR FDEA202610091524](https://openairdocs.org/sdr/FDEA202610091524.md): Seat Track · worn · Oct 9, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 1421, 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 1391 T
- [SDR FDEA202610091523](https://openairdocs.org/sdr/FDEA202610091523.md): Seat Track · worn · Oct 9, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1421, X= 27.5" FOUND 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 AT STATION 14
- [SDR FDEA202610091521](https://openairdocs.org/sdr/FDEA202610091521.md): Seat Track · worn · Oct 9, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO BAY SEAT TRACK AT BS 1296, X= -47.5, 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 BTWN BS 1311 TO EXISTING SPLICE B
- [SDR FDEA202610091520](https://openairdocs.org/sdr/FDEA202610091520.md): Seat Track · worn · Oct 9, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 1296, 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 1311 TO
- [SDR FDEA202610091519](https://openairdocs.org/sdr/FDEA202610091519.md): Seat Track · worn · Oct 9, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO BAY SEAT TRACK AT BS 1296, X= -8.5, 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 BTWN BS 1311 TO EXISTING SPLICE BS 1
- [SDR FDEA202610091518](https://openairdocs.org/sdr/FDEA202610091518.md): Seat Track · worn · Oct 9, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO BAY SEAT TRACK AT BS 1296, X= 8.5", 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 BTWN BS 1269 - 1311 IAW SRM 53-00-5
- [SDR FDEA202610091517](https://openairdocs.org/sdr/FDEA202610091517.md): Seat Track · worn · Oct 9, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO BAY SEAT TRACK AT BS 1296, X= 27.5" CROWN WORN. THE SEAT TRACK WAS EVALUATED & FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT BTWN BS 1249 - 1311 IAW SRM 53-00-52-2R
- [SDR FDEA202610091516](https://openairdocs.org/sdr/FDEA202610091516.md): Seat Track · worn · Oct 9, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO BAY SEAT TRACK AT BS 1159, X= 47.5" 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 BTWN EXISTING SPLICES BS 1129/6-100
- [SDR FDEA202610091515](https://openairdocs.org/sdr/FDEA202610091515.md): Seat Track · worn · Oct 9, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO BAY SEAT TRACK AT BS 1139, X= -8.5" 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 EXISTING SPLICES BS 1129/6-1
- [SDR FDEA202610091514](https://openairdocs.org/sdr/FDEA202610091514.md): Seat Track · worn · Oct 9, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO BAY SEAT TRACK AT BS 1159, X=8.5" 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 BTWN EXISTING SPLICES BS 1129/6-100 -
- [SDR FDEA202610091512](https://openairdocs.org/sdr/FDEA202610091512.md): Seat Track · worn · Oct 9, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO BAY SEAT TRACK AT BS 1149, X=-47.5" 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 SPLICES BS 1129/6-100 TO
- [SDR FDEA202610091511](https://openairdocs.org/sdr/FDEA202610091511.md): Seat Track · worn · Oct 9, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO BAY SEAT TRACK AT BS 879, X=47.5" 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 BTWN BS 869 TO EXISTING SPLICE BS 929
- [SDR FDEA202610091510](https://openairdocs.org/sdr/FDEA202610091510.md): Seat Track · worn · Oct 9, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO BAY SEAT TRACK AT BS 806, X=-27.5" CROWN WAS 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 BTWN BS 816 TO EXISTING SPLICE BS
- [SDR FDEA202610091509](https://openairdocs.org/sdr/FDEA202610091509.md): Seat Track · worn · Oct 9, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO BAY SEAT TRACK AT BS 806, X=-47.5, CROWN WAS 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 SECTIONALREPLACEMENT BTWN EXISTING SPLICES BS 765 - 816
- [SDR FDEA202610091508](https://openairdocs.org/sdr/FDEA202610091508.md): Seat Track · worn · Oct 9, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 829, X=8.5" FOUND 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 909 TO EXIST
- [SDR FDEA202610091506](https://openairdocs.org/sdr/FDEA202610091506.md): Seat Track · worn · Oct 9, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > FORWARD MAIN DECK CARGO BAY SEAT TRACK AT BS 755, X=-47.5. 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 BTWN BS 725 TO EXIS
- [SDR FDEA202610091505](https://openairdocs.org/sdr/FDEA202610091505.md): Seat Track · worn · Oct 9, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > FORWARD MIAN DECK CARGO BAY SEAT TRACK AT BS 755, 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 BS 816 TO EXIST
- [SDR FDEA202610091503](https://openairdocs.org/sdr/FDEA202610091503.md): Seat Track · worn · Oct 9, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > FORWARD MAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 755, X=27.5", FOUND 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 SPL
- [SDR FDEA202610091500](https://openairdocs.org/sdr/FDEA202610091500.md): Fitting · cracked · Oct 9, 2026 · N610FE · Doug MD11F · Fuselage Main, Structure
  > CENTER W/W - CENTER W/W FORWARD BULKHEAD LEFT HAND T - FITTING UPPER CORNER SUSPECT CRACK AT STATION 1368.650
- [SDR FDEA202610091499](https://openairdocs.org/sdr/FDEA202610091499.md): Fitting · cracked · Oct 9, 2026 · N610FE · Doug MD11F · Fuselage Main, Structure
  > CENTER W/W - CENTER W/W FORWARD BULKHEAD RIGHT HAND T - FITTING UPPER CORNER SUSPECT CRACK AT STATION 1368.650.
- [SDR FDEA202610091498](https://openairdocs.org/sdr/FDEA202610091498.md): Fitting · cracked · Oct 9, 2026 · N610FE · Doug MD11F · Fuselage Main, Structure
  > PER E.A.#1-5310-T0378549 REVISION.A PART 3 TITLE: FUSELAGE-MAINFRAME-CRACK REPAIR ON LEFT HAND NOSE LANDING GEAR TRUNNION FITTING, STATION 595, REQUIRES REPLACEMENT OF FITTING OR CONTACT FEDEX ES FOR PERMANENT REPAIR PLAN.(FITTING ASSEMBLY PART NUMBER: A
- [SDR FDEA202610081495](https://openairdocs.org/sdr/FDEA202610081495.md): Doubler · cracked · Oct 8, 2026 · N610FE · Doug MD11F · Wing, Plate/Skin
  > RIGHT WING, FIXED LEADING EDGE RIB DOUBLER AT STATION XOS 667 FOUND CRACK ABOUT 0.2". RIGHT WING FIXED LEADING EDGE CRACKED RIB DOUBLER AT STATION XOS 667 REMOVED AND INSTALLED WITH FABRICATED RIB DOUBLER AS PER MD-11 SRM 51-31-01-0G.RIB DOUBLER FABRICATE
- [SDR FDEA202610081494](https://openairdocs.org/sdr/FDEA202610081494.md): Doubler · cracked · Oct 8, 2026 · N610FE · Doug MD11F · Wing, Plate/Skin
  > LEFT WING, FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 705 FOUND CRACK ABOUT 0.3". LEFT WING FIXED LEADING EDGE CRACKED BEADED DOUBLER AT STATION XOS 705 CARRIED OUT REPAIR AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJ
- [SDR FDEA202610081493](https://openairdocs.org/sdr/FDEA202610081493.md): Doubler · cracked · Oct 8, 2026 · N610FE · Doug MD11F · Wing, Plate/Skin
  > LEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 682 FOUND CRACK ABOUT 0.2". LEFT WING FIXED LEADING EDGE CRACKED BEADED DOUBLER AT STATION XOS 682 CARRIED OUT REPAIR AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MA
- [SDR FDEA202610081492](https://openairdocs.org/sdr/FDEA202610081492.md): Doubler · cracked · Oct 8, 2026 · N610FE · Doug MD11F · Wing, Plate/Skin
  > RIGHT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 705 FOUND CRACK ABOUT 0.2". RIGHT WING FIXED LEADING EDGE CRACKED BEADED DOUBLER AT STATION XOS 705 CARRIED OUT REPAIR AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS
- [SDR FDEA202509281843](https://openairdocs.org/sdr/FDEA202509281843.md): Deu · failed · Sep 28, 2025 · N610FE · Doug MD11F · Central Display
  > AT CRUISE FL370 GOT MULTIPLE CAUTIONS: LEVEL1 SELECT PACK 1 OFF, WITH MULTIPLE ELECTRICAL LEVEL1 DC TIE 3 OFF AND BUS R EMER DC OFF, ALSO LEVEL 0 GLY EXT POWER ON, THE ELECTRICAL ISSUES TRIGGERED A LEVEL2 FLAP DISAG WITH LEFT INBOARD FLAP INDICATING 22 D
- [SDR FDEA202502140232](https://openairdocs.org/sdr/FDEA202502140232.md): Battery · no test · Feb 14, 2025 · N610FE · Doug MD11F · Emergency Lighting
  > DURING POST FLIGHT CHECK FOUND EMGENCEY LIGHT TEST FAILED WITH ALERT EMER LT BAT 1 LO. REMOVED AND INSTALLED EMERGENCEY LIGHTING BATTERY POWER SUPPLY REF MM 33-51-01-4. OPS CHECKS NORMAL REF MM 33-51-01-5. ACFT OK FOR SERVICE.
- [SDR FDEA202501240136](https://openairdocs.org/sdr/FDEA202501240136.md): Warning Message · illuminated · Jan 24, 2025 · N610FE · Doug MD11F · Emergency Lighting
  > DURING PREFLIGHT LEVEL 1 EMER LT BAT 1 LO. T/S REF MD11 FIM 33-51-02-00 FIG. 104, AND ACCOMPLISHED OPS TEST REF MD11 AMM 33-51-01-5 MULTI. TIMES DURING GRD TIME AND ALL OPS CK GOOD.
- [SDR FDEA202407090975](https://openairdocs.org/sdr/FDEA202407090975.md): Engine · vibration · Jul 9, 2024 · N610FE · Doug MD11F · Engine Pressure Ratio (EPR)
  > NR 3 ENGINE HIGH VIBE 5.0 & ABOVE.VERBAL FROM FLIGHT CREW. REF ER 24-01792 COMPLETED #3 ENGINE INSTALLATION REF WIC 7100000-03-91. REPLACED THE ENGINE
- [SDR FDEA202404040437](https://openairdocs.org/sdr/FDEA202404040437.md): Spar Cap · corroded · Apr 4, 2024 · N610FE · Doug MD11F · Wing Spar
  > RIGHT WING - TRAILING EDGE REAR SPAR LOWER CAP FOUND CORROSION AT XORS 1051. ROHT WING TRAILING EDGE REAR SPAR LOWER CAP AT XORS 1051 CORROSION REMOVED AND FOUD EXCEEDED LIMIT AS PER MD-11 SRM 57-00-10-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED AREA REPAIR
- [SDR FDEA202404040436](https://openairdocs.org/sdr/FDEA202404040436.md): Spar Cap · corroded · Apr 4, 2024 · N610FE · Doug MD11F · Wing Spar
  > LEFT WING - TRAILING EDGE REAR SPAR LOWER CAP FOUND CORROSION AT XORS 1068. LEFT WING TRAILING EDGE REAR SPAR LOWER CAP AT XORS 1068 CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 57-00-10-1A FIGURE 101 ALLOWABLE DAMGE 1. CORRODED AREA REPAIR
- [SDR FDEA202403250365](https://openairdocs.org/sdr/FDEA202403250365.md): Doubler · cracked · Mar 25, 2024 · N610FE · Doug MD11F · Wing, Plate/Skin
  > LEFT WING - FIXED LEADING EDGE BEADED DOUBLER FOUND CRACK AT STATION XOS 635. LEFT WING FIXED LEADING EDGE AT STATION XOS 635 CRACKED BEADED DOUBLER REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-

Next page: https://openairdocs.org/aircraft/N610FE/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 = 'N610FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N610FE/reports

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