# Service difficulty reports: N603FE

A list on [N603FE](https://openairdocs.org/aircraft/N603FE.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 · 488 reports

- [SDR FDEA202609221404](https://openairdocs.org/sdr/FDEA202609221404.md): Light · no test · Sep 22, 2026 · N603FE · Doug MD11F · Emergency Lighting
  > EMER LT BAT 1 LO DURING EMER LT TEST. T/S IAW FIM 33-51 FT 104,REPLACED FAULTED BATTERY IAW AMM 33-51-01, OPS CHK OF EMER LTS TEST PASSED
- [SDR FDEA202607130918](https://openairdocs.org/sdr/FDEA202607130918.md): Bulkhead · misaligned · Jul 13, 2026 · N603FE · Doug MD11F · Nacelle/Pylon, Bulkhead/Firewall
  > RIGHT ENGINE #3 PYLON AFT BULKHEAD FOUND LUG BORE HOLE MISALIGN.YWN 418. RIGHT ENGINE #3 PYLON AFT BULKHEAD LUG BORE HOLE MISALIGN HOLE REWORKED AS PER EA #1-5440-T0387700 PART1.TITLE: NACELLES/PYLON - ATTACH /MOUNT/HINGE - NO 3 PYLON AFT BULKHEAD - MD11-B
- [SDR FDEA202607080862](https://openairdocs.org/sdr/FDEA202607080862.md): Fitting · chafed · Jul 8, 2026 · N603FE · Doug MD11F · Nacelle/Pylon, Main Frame
  > LEFT ENGINE PYLON - AFT PYLON BULKHEAD LUG FITTING FOUND WITH CHAFE AT EXTERIOR UPPER AREA.YWN-418. CARRIED OUT REPAIR IN ACCORDANCE WITH EA #1-5440-T0387673 PART 1 AND 2 TITLE: NACELLES/PYLON - ATTACH/MOUNT/HINGE- NR 1 PYLON AFT BULKHEAD LUG INSPECTION AND
- [SDR FDEA202606030669](https://openairdocs.org/sdr/FDEA202606030669.md): Lug · corroded · Jun 3, 2026 · N603FE · Doug MD11F · Nacelle/Pylon, Main Frame
  > RIGHT ENGINE PYLON AFT BULKHEAD LUG BORE HOLE FOUND WITH CORROSION AT 12 O'CLOCK, 3 O'CLOCK, 9 O'CLOCK AND 6 O'CLOCK POSITION AFTER SPHERICAL BEARING REMOVAL. CORROSION AT RIGHT ENGINE PYLON AFT BULKHEAD LUG BORE HOLE AT 12 O'CLOCK,3 O'CLOCK,9 O'CLOCK AND 6 O'
- [SDR FDEA202606030668](https://openairdocs.org/sdr/FDEA202606030668.md): Lug · corroded · Jun 3, 2026 · N603FE · Doug MD11F · Nacelle/Pylon, Main Frame
  > LEFT ENGINE PYLON AFT BULKHEAD LUG BORE HOLE FOUND WITH CORROSION AFTER SPHERICAL BEARING REMOVAL YWN 418. CORROSION AT LEFT ENGINE PYLON AFT BULKHEAD LUG BORE HOLE CARRIED OUT REPAIR IAW EA 1-5440-T0387673, PART 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-10
- [SDR FDEA202605180619](https://openairdocs.org/sdr/FDEA202605180619.md): Access Panel · cracked · May 18, 2026 · N603FE · Doug MD11F · Nacelle/Pylon, Plate/Skin
  > NR 3 PYLON COMPARTMENT THROUGH ACCESS PANEL 617BT OUTBOARD LOWER AFT WEB FOUND CRACK APPROXIMATELY 0.75" AT XFS 427 #3 PYLON COMPARTMENT ACCESS PANEL 617BT OUTBOARD LOWER AFT CRACKED WEB AT XFS 427 REMOVED AND REPLACED IN ACCORDANCE WITH SRM 51-31-01-0G. W
- [SDR FDEA202605180618](https://openairdocs.org/sdr/FDEA202605180618.md): Access Panel · cracked · May 18, 2026 · N603FE · Doug MD11F · Nacelle/Pylon, Plate/Skin
  > NR 1 PYLON COMPARTMENT THROUGH ACCESS PANEL 517BT OUTBOARD LOWER AFT WEB FOUND CRACK APPROXIMATELY 0.5" AT XFS 427. #1 PYLON COMPARTMENT ACCESS PANEL 517BT OUTBOARD LOWER AFT CRACKED WEB AT XFS 427 REMOVED AND REPLACED IN ACCORDANCE WITH SRM 51-31-01-0G. W
- [SDR FDEA202510312117](https://openairdocs.org/sdr/FDEA202510312117.md): Skin · corroded · Oct 31, 2025 · N603FE · Doug MD11F · Ailerons
  > RIGHT INBD AILERON UPPER SURFACE OUTBOARD SIDE TRAILING EDGE AREA FOUND CORRODED. RIGHT HAND INBOARD AILERON ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-10-20-4. NEUTRAL POSITION ADJUSTMENT AND TEST CARRIED OUT FOUND SATISFACTORY AS PER AMM 27-10-00-5. R
- [SDR FDEA202510292102](https://openairdocs.org/sdr/FDEA202510292102.md): Floor Panel · damaged · Oct 29, 2025 · N603FE · Doug MD11F · Fuselage Floor Panel
  > FLOOR PANEL #231HF AT LEFT BS 595 TO 675 SURFACE FOUND DAMAGED. DAMAGED FLOOR PANEL #231HF AT CABIN LEFT HAND STATION 595 TO STATION 675 REMOVED AND REPLACED IAW AMM 53-25-04-4. FLOOR PANEL #231HF FABRICATED AS PER DRAWING SRZ-25-005 REVISION R. REPAIR CLA
- [SDR FDEA202510272095](https://openairdocs.org/sdr/FDEA202510272095.md): Beam · cracked · Oct 27, 2025 · N603FE · Doug MD11F · Passenger/Crew Doors
  > CABIN L2 DOOR NR 6 BEAM FORWARD STOP FOUND CRACKED AT BS 794 CRACK LENGTH 1.0". AT L2 DOOR CRACKED NR 6 STOP BEAM. R & R IAW SRM 51-31-01-0G & DRAWING ADA3462, REVISION AC. L2 DOOR NR 6 STOP BEAM FABRICATED BY MACHINING IAW EA 1-5210-T0385415 PART 1. REPA
- [SDR FDEA202510242087](https://openairdocs.org/sdr/FDEA202510242087.md): Hinge Bracket · corroded · Oct 24, 2025 · N603FE · Doug MD11F · Trailing Edge Flaps
  > RIGHT WING:(FLAP SIDE) RIGHT INBOARD FLAP OUTBOARD AFTER HINGE OUTBOARD PIVOT HOLE AREA FOUND CORROSION. CORRROSION AT RIGHR HAND WING: (FLAP SIDE) RIGHT HAND INBOARD FLAP OUTBOARD AFT HINGE OUTBOARD PIVOT HOLE AREA REWORKED AND FOUND EXCEED LIMIT AS PER
- [SDR FDEA202510242086](https://openairdocs.org/sdr/FDEA202510242086.md): Hinge Bracket · corroded · Oct 24, 2025 · N603FE · Doug MD11F · Trailing Edge Flaps
  > RIGHT WING:(FLAP SIDE) RIGHT INBOARD FLAP OUTBOARD AFTER HINGE INBOARD PIVOT HOLE AREA FOUND CORROSION. CORROSION AT RIGHT HAND WING: ( FLAP SIDE) RIGHT HAND INBOARD FLAP OUTBOARD AFT HINGE INBOARD PIVOT HOLE AREA REWORKED AND FOUND EXCEED LIMIT AS PE
- [SDR FDEA202510242085](https://openairdocs.org/sdr/FDEA202510242085.md): Hinge Bracket · corroded · Oct 24, 2025 · N603FE · Doug MD11F · Trailing Edge Flaps
  > LEFT WING:(FLAP SIDE) LEFT INBOARD FLAP OUTBOARD AFTER HINGE OUTBOARD PIVOT HOLE AREA FOUND CORROSION. CORROSION AT LEFT HAND WING: ( FLAP SIDE) LEFT HAND INBOARD FLAP OUTBOARD AFT HINGE OUTBOARD PIVOT HOLE AREA REWORKED AND FOUND EXCEED LIMIT AS PER M
- [SDR FDEA202510242084](https://openairdocs.org/sdr/FDEA202510242084.md): Hinge Bracket · corroded · Oct 24, 2025 · N603FE · Doug MD11F · Trailing Edge Flaps
  > LEFT WING:(FLAP SIDE) LEFT HAND INBOARD FLAP OUTBOARD AFTER HINGE INBOARD PIVOT HOLE AREA FOUND CORROSION. CORROSION AT LEFT HAND WING ( FLAP SIDE) LEFT HAND INBOARD FLAP OUTBOARD AFT HINGE INBOARD PIVOT HOLE AREA REWORKED AND FOUND EXCEED LIMIT AS PER
- [SDR FDEA202510242083](https://openairdocs.org/sdr/FDEA202510242083.md): Hinge Bracket · corroded · Oct 24, 2025 · N603FE · Doug MD11F · Trailing Edge Flaps
  > RIGHT WING: WING SIDE RIGHT INBOARD FLAP OUTBOARD HINGE PIVOT HOLE SURFACE AREA FOUND CORROSION. CORROSION AT RIGHT HAND WING: WING SIDE RIGHT HAND INBOARD FLAP OUTBOARD HINGE PIVOT HOLE SURFACE AREA REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44
- [SDR FDEA202510242082](https://openairdocs.org/sdr/FDEA202510242082.md): Hinge Bracket · corroded · Oct 24, 2025 · N603FE · Doug MD11F · Trailing Edge Flaps
  > LEFT WING: (ON WING SIDE), LEFT INBOARD FLAP OUTBOARD FORWARD HINGE PIVOT HOLE SPOTFACE AREA FOUND CORRODED. CORRODED AT LEFT HAND WING: (ON WING SIDE), LEFT HAND INBOARD FLAP OUTBOARD FORWARD HINGE PIVOT HOLE SPOT FACE AREA REWORKED AND FOUND EXCEED L
- [SDR FDEA202510242081](https://openairdocs.org/sdr/FDEA202510242081.md): Hinge Bracket · corroded · Oct 24, 2025 · N603FE · Doug MD11F · Trailing Edge Flaps
  > LEFT WING: WING SIDE LEFT INBOARD FLAP OUTBOARD HINGE PIVOT HOLE SURFACE AREA FOUND CORRODED. ORROSION AT LEFT HAND WING: WING SIDE LEFT HAND INBOARD FLAP OUTBOARD HINGE PIVOT HOLE SURFACE AREA REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. R
- [SDR FDEA202510222069](https://openairdocs.org/sdr/FDEA202510222069.md): Doubler · cracked · Oct 22, 2025 · N603FE · Doug MD11F · Fuselage Main, Plate/Skin
  > FUSELAGE: #1 AIRCONDITION RAM AIR EXHAUST ASSY CUT OUT PRODUCTION DOUBLER SUSPECT CRACKED. CRACKED DOUBLER AT FUSELAGE #1 AIRCONDITION RAM AIR EXHAUST ASSEMBLY AT LEFT HAND STATION 561.667 REMOVED AND REPLACED WITH FABRICATED DOUBLER AS PER MD-11 SRM 51-
- [SDR FDEA202510222068](https://openairdocs.org/sdr/FDEA202510222068.md): Doubler · cracked · Oct 22, 2025 · N603FE · Doug MD11F · Fuselage Main, Plate/Skin
  > FUSELAGE: #1 AIRCONDITION RAM AIR EXHAUST ASSY CUT OUT PRODUCTION DOUBLER SUSPECT CRACKED. CRACKED DOUBLER AT FUSELAGE #1 AIRCONDITION RAM AIR EXHAUST ASSEMBLY AT LEFT HAND STATION 561.667 REMOVED AND REPLACED WITH FABRICATED DOUBLER AS PER MD-11 SRM 51-
- [SDR FDEA202510222063](https://openairdocs.org/sdr/FDEA202510222063.md): Beam · cracked · Oct 22, 2025 · N603FE · Doug MD11F · Fuselage Main, Structure
  > LOWER CENTER CARGO DOOR UPPER DOOR JAMB CENTER BEAM FOUND CRACKED AT BS 1746.925. LOWER CENTER CARGO DOOR UPPER DOOR JAMB CENTER BEAM CRACKED AT STATION 1746.925 REPAIRED AS PER MD-11 SRM 53-50-15-2R FIGURE 201 REPAIR 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2
- [SDR FDEA202510162032](https://openairdocs.org/sdr/FDEA202510162032.md): Floor Panel · delaminated · Oct 16, 2025 · N603FE · Doug MD11F · Fuselage Floor Panel
  > CABIN LEFT HAND FLOOR PANEL 231CF AT BS 495 TO 595 BETWEEN X=27.5 TO X=47.25 ACCESS CUT OUT FOUND DELAMINATED. REMOVED AND REPLACED AS PER AMM 53-25-04-4. FLOOR PANEL 231CF FABRICATED IAW DRAWING SRZ-25-005 REVISION R. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-
- [SDR FDEA202510162031](https://openairdocs.org/sdr/FDEA202510162031.md): Seat Track · worn · Oct 16, 2025 · N603FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN-SEAT TRACK AT STAION 1275 X= -8.5 FOUND CROWN WORN. SEAT TRACK BS 1275 X= -8.5 CROWN EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT AT CABIN FROM BS 1264 TO BS 1313
- [SDR FDEA202510162030](https://openairdocs.org/sdr/FDEA202510162030.md): Seat Track · worn · Oct 16, 2025 · N603FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK BS 1275 X= 8.5, FOUND THE CROWN WORN. THE SEAT TRACK CROWN WAS EVALUATED & 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 201, REPAIR 1.
- [SDR FDEA202510162029](https://openairdocs.org/sdr/FDEA202510162029.md): Seat Track · worn · Oct 16, 2025 · N603FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT STATION 1541 X= -8.5 FOUND CROWN WORN. SEAT TRACK STATION 1541 X= -8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT AT CABIN
- [SDR FDEA202510162028](https://openairdocs.org/sdr/FDEA202510162028.md): Seat Track · worn · Oct 16, 2025 · N603FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT STATION 1661 X= -8.5 FOUND CROWN WORN. SEAT TRACK STATION 1661 X= -8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT AT CABIN
- [SDR FDEA202510162027](https://openairdocs.org/sdr/FDEA202510162027.md): Seat Track · worn · Oct 16, 2025 · N603FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT BS 1801 X= -8.5 FOUND CROWN WORN. SEAT TRACK BS 1801, X= -8.5 WORN CROWN EVALUATED & FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT AT CABIN FROM EXISTING SPLICE
- [SDR FDEA202510162026](https://openairdocs.org/sdr/FDEA202510162026.md): Seat Track · worn · Oct 16, 2025 · N603FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT STATION 1661 X= 47.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 1661 X= 47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT AT CABIN FR
- [SDR FDEA202510162025](https://openairdocs.org/sdr/FDEA202510162025.md): Seat Track · worn · Oct 16, 2025 · N603FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT STATION 1661 X= 8.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 1661 X= 8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT AT
- [SDR FDEA202510162024](https://openairdocs.org/sdr/FDEA202510162024.md): Seat Track · worn · Oct 16, 2025 · N603FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT STATION 1541 X= 8.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 1541 X= 8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REP
- [SDR FDEA202510162023](https://openairdocs.org/sdr/FDEA202510162023.md): Seat Track · worn · Oct 16, 2025 · N603FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT STATION 5-10 X= -8.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 5-10 X= -8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK R
- [SDR FDEA202510162022](https://openairdocs.org/sdr/FDEA202510162022.md): Seat Track · worn · Oct 16, 2025 · N603FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT BS 1421 X= -47.5 FOUND CROWN WORN. SEAT TRACK CROWN EVALUATED & 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 201, REPAIR 1. REPAIR
- [SDR FDEA202510162021](https://openairdocs.org/sdr/FDEA202510162021.md): Seat Track · worn · Oct 16, 2025 · N603FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT STAION 1275 X= -27.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 1275 X= -27.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK
- [SDR FDEA202510162020](https://openairdocs.org/sdr/FDEA202510162020.md): Seat Track · worn · Oct 16, 2025 · N603FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT BS 1275 X= 27.5, FOUND THE CROWN WORN. THE SEAT TRACK CROWN 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 FROM BS 1247 TO BS 1331IAW SRM 53-00-5
- [SDR FDEA202510162019](https://openairdocs.org/sdr/FDEA202510162019.md): Seat Track · worn · Oct 16, 2025 · N603FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN-SEAT TRACK AT STAION 1421 X= 27.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 1421, X= 27.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT T
- [SDR FDEA202510162018](https://openairdocs.org/sdr/FDEA202510162018.md): Seat Track · worn · Oct 16, 2025 · N603FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT STATION 1401 X= -8.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 1401, X= -8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK
- [SDR FDEA202510162017](https://openairdocs.org/sdr/FDEA202510162017.md): Seat Track · worn · Oct 16, 2025 · N603FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT STATION 879 X= 47.5 FOUND CROWN WORN. SEAT TRACK STATION 879, X= 47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT AT CABIN
- [SDR FDEA202510162016](https://openairdocs.org/sdr/FDEA202510162016.md): Seat Track · worn · Oct 16, 2025 · N603FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT STATION 879 X= -8.5 FOUND CROWN WORN. SEAT TRACK STATION 879 X= -8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT AT CABIN ST
- [SDR FDEA202510162015](https://openairdocs.org/sdr/FDEA202510162015.md): Seat Track · worn · Oct 16, 2025 · N603FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT STATION 879 X= -27.5 FOUND CROWN WORN. SEAT TRACK STATION 879 X= -27.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT AT CABIN
- [SDR FDEA202510141991](https://openairdocs.org/sdr/FDEA202510141991.md): Seat Track · worn · Oct 14, 2025 · N603FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT BS 1169 X= -27.5 FOUND THE CROWN WORN. THE SEAT TRACK CROWN 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 FROM EXISTING SPLICE BS 1129 TO BS 11
- [SDR FDEA202510141990](https://openairdocs.org/sdr/FDEA202510141990.md): Seat Track · worn · Oct 14, 2025 · N603FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT BS 1169 X= 47.5 FOUND CROWN WORN. THE SEAT TRACK CROWN 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 IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1.
- [SDR FDEA202510141989](https://openairdocs.org/sdr/FDEA202510141989.md): Seat Track · cracked · Oct 14, 2025 · N603FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT STATION 685 X= 27.5 FOUND CRACKED. CRACKED SEAT TRACK AT STATION 695 X= 27.5 REMOVED FROM EXISTING SPLIES STATION 665 TO STATION 745 X=27.5 AS PER MD-11 SRM 51-31-01-0G. CRACKED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT AT CABIN FROM EXIS
- [SDR FDEA202510141988](https://openairdocs.org/sdr/FDEA202510141988.md): Seat Track · cracked · Oct 14, 2025 · N603FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT STATION 755 X= -8.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 755 X= -8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REP
- [SDR FDEA202510141987](https://openairdocs.org/sdr/FDEA202510141987.md): Seat Track · worn · Oct 14, 2025 · N603FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT STATION 919 X= 47.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 919 X= 47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REP
- [SDR FDEA202510141986](https://openairdocs.org/sdr/FDEA202510141986.md): Seat Track · worn · Oct 14, 2025 · N603FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK BS 1249 X= 75.25 FOUND THE CROWN WORN. THE SEAT TRACK CROWN 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 1169 - BS 1264, X= 75.25 IAW SRM 53-0
- [SDR FDEA202510141985](https://openairdocs.org/sdr/FDEA202510141985.md): Seat Track · worn · Oct 14, 2025 · N603FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT STATION 1169 X= 8.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 1169, X= 8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK RE
- [SDR FDEA202510141984](https://openairdocs.org/sdr/FDEA202510141984.md): Seat Track · worn · Oct 14, 2025 · N603FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN-SEAT TRACK AT STATION 635 X= -47.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 635, X= -47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT
- [SDR FDEA202510141983](https://openairdocs.org/sdr/FDEA202510141983.md): Seat Track · worn · Oct 14, 2025 · N603FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT STATION 1169 X= -8.5 FOUND CROWN WORN. SEAT TRACK CROWN 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 IAW SRM 53-00-52-2R FIGURE 201, REPAIR 1.
- [SDR FDEA202510141982](https://openairdocs.org/sdr/FDEA202510141982.md): Seat Track · worn · Oct 14, 2025 · N603FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT STATION 1169 X= 27.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 1169 X= 27.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT
- [SDR FDEA202510141981](https://openairdocs.org/sdr/FDEA202510141981.md): Door Frame · cracked · Oct 14, 2025 · N603FE · Doug MD11F · Fuselage Main, Structure
  > LEFT 3 AFT DOOR JAME LOWER WEB AT STATION 1310 FOUND CRACKED. CANIN-LEFT 3 AFT DOOR JAME LOWER WEB AT STATION 1310 CRACKED REPAIR CARRIED OUT AS PER MD-11 SRM 53-40-15-2R FIGURE 201 REPAIR 3. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA202510121972](https://openairdocs.org/sdr/FDEA202510121972.md): Spar Cap · corroded · Oct 12, 2025 · N603FE · Doug MD11F · Wing Spar
  > RIGHT WING LOCATED BETWEEN OUTBOARD TRAILING EDGE ISLAND AND RIGHT HAND OUTBOARD AILERON, OUTBOARD TRAILING EDGE LOWER CAP XORS 1048 FOUND CORRODED. CORROSION REMOVED & FOUND EXCEEDED LIMIT IAW SRM 57-00-01-1A ALLOWABLE DAMAGE 1. REAR SPAR LOWER CAP CARRIE

Next page: https://openairdocs.org/aircraft/N603FE/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 = 'N603FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N603FE/reports

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