# Service difficulty reports: N617FE A list on [N617FE](https://openairdocs.org/aircraft/N617FE.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 · 467 reports - [SDR FDEA202610061481](https://openairdocs.org/sdr/FDEA202610061481.md): Fire Loop · faulted · Oct 6, 2026 · N617FE · Doug MD11F · Fire Detection > FIRE DET 2 FAIL ILLUMINATED STEADY DURING FLIGHT AT CRUISE ALTITUDE. FIRE DET 2 FAIL LATER FLICKERED ON AND OFF FOR THE REMAINDER OF THE FLIGHT. REMOVED ENGINE NR 2 FIRE DETECTOR RAIL ASSY. FOR LOOP 'B' IAW AMM 26-11-03-4-1. RELEASED FOR SERVICE PER ME - [SDR FDEA202609261438](https://openairdocs.org/sdr/FDEA202609261438.md): Light Sys · no discrepancy · Sep 26, 2026 · N617FE · Doug MD11F · Emergency Lighting > DURING PREFLIGHT, EMERGENCY LIGHTS WILL NOT TEST COMPLETED EMERGENCY LIGHT TEST AND SYSTEM WORKED PROPERLY. - [SDR FDEA202609041262](https://openairdocs.org/sdr/FDEA202609041262.md): Doubler · no discrepancy · Sep 4, 2026 · N617FE · Doug MD11F · Standard Practices/Structures > EXISTING REPAIR AT CENTER WHEEL WELL LEFT HAND SIDE STATION 1380, X=31.5 LEFT HAND. EXISTING REPAIR AT CENTER WHEEL WELL LEFT HAND SIDE STATION 1380 X=31.5 LEFT HAND EVALUATED & FOUND DOUBLER REPLACED BY FABRICATION IN ACCORDANCE WITH SRM 51-33- 01-0G & D - [SDR FDEA202609031260](https://openairdocs.org/sdr/FDEA202609031260.md): Skin · corroded · Sep 3, 2026 · N617FE · Doug MD11F · Fuselage Main, Plate/Skin > AFT FUSELAGE, ACCESSORY BAY RT UPPER PNEUMATIC DUCT EXHAUST, AREA BS 2157 CORRODED. CORROSION REMOVED IAW SRM 51-21-01-0G, FOUND EXCEEDED LIMITS IAW SRM 53-70-01-2R, FIGURE 201, SHEET 3, REPAIR 3. CORRODED SKIN AT AFT FUSELAGE RT UPPER PNEUMATIC DUCT EXHA - [SDR FDEA202609021259](https://openairdocs.org/sdr/FDEA202609021259.md): Support Rod · corroded · Sep 2, 2026 · N617FE · Doug MD11F · Fuselage Main, Plate/Skin > AFT FUSELAGE ACCESSORY BAY RT PNEUMATIC DUCT SUPPORT ROD AREA BS 2159 CORRODED. CORROSION REMOVED IAW SRM 51-21-01-0G & FOUND EXCEEDED LIMIT IAW SRM 53-70-01-2R, FIGURE 201, SHEET 3, REPAIR 3 AT AFT ACCESSORY BAY. SKIN RIGHT PNEUMATIC DUCT SUPPORT ROD BS 2140 - [SDR FDEA202609011252](https://openairdocs.org/sdr/FDEA202609011252.md): Spar Cap · cracked · Sep 1, 2026 · N617FE · Doug MD11F · Nacelle/Pylon, Frame/Spar/Rib > TAIL PYLON UPPER SPAR, LT SIDE UPPER CAP VERTICAL FLANGE AT STA YID= 408.500, FOUND A CRACK INDICATION APPROX 0.35" IN LENGTH FROM FWD EDGE DURING ULTRASONIC INSPECTION. CRACK ON LEFT HAND SIDE UPPER CAP VERTICAL FLANGE AT STATION YID= 408.500 REPAIRED AS - [SDR FDEA202608291250](https://openairdocs.org/sdr/FDEA202608291250.md): Shear Tie · no discrepancy · Aug 29, 2026 · N617FE · Doug MD11F · Standard Practices/Structures > EXISTING REPAIR AT FUSELAGE FRAME BS 1902.15 SHEAR TIE, LONGERON 52. FUSELAGE FRAME STATION 1902.15 SHEAR CLIP AT LONGERON 52 CARRIED OUT REPAIR IN ACCORDANCE WITH EA 1-5330-T0388596 P1 TITLE: FUSELAGE - AFT FUSELAGE SKIN PANEL INSTL - ACCOMPLISHED NEW S - [SDR FDEA202608281243](https://openairdocs.org/sdr/FDEA202608281243.md): Skin · none · Aug 28, 2026 · N617FE · Doug MD11F · Fuselage Main, Plate/Skin > EXISTING REPAIR AT FUSELAGE SKIN - MAIN DECK CARGO DOOR CUTOUT - FORWARD LOWER CORNER STATION 623.065, LONGERON 27 LEFT HAND. EXISTING REPAIR AT FUSELAGE SKIN - MAIN DECK CARGO DOOR CUTOUT - FORWARD LOWER CORNER STATION 623.065 LONGERON 27 LEFT HAND EVALUA - [SDR FDEA202608281242](https://openairdocs.org/sdr/FDEA202608281242.md): Skin · none · Aug 28, 2026 · N617FE · Doug MD11F · Fuselage Main, Plate/Skin > EXISTING REPAIR AT FUSELAGE SKIN AT STATION 1894 TO STATION 1914 LONGERON 47 LEFT HAND TO LONGERON 50 RIGHT. FUSELAGE SKIN AT STATION 1894 TO STATION 1914 LONGERON 47 LEFT HAND TO LONGERON 50 RIGHT HAND CARRIED OUT REPAIR IN ACCORDANCE WITH EA 1-5330-T03 - [SDR FDEA202608271237](https://openairdocs.org/sdr/FDEA202608271237.md): Seat Track · corroded · Aug 27, 2026 · N617FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT, ON REMOVAL OF FLOOR PANELS FOR ACCESS, FOUND SEAT TRACK CORRODED AT BS 1169 X= -27.5. THE SEAT TRACK WAS EVALUATED, FOUND EXFOLIATED & EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS RE - [SDR FDEA202608271236](https://openairdocs.org/sdr/FDEA202608271236.md): Seat Track · corroded · Aug 27, 2026 · N617FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT UPON REMOVAL OF FLOOR PANELS FOR ACCESS, FOUND SEAT TRACK CORRODED AT BS 1149, X= 8.5. THE SEAT TRACK WAS EVALUATED, FOUND EXFOLIATED AND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS RE - [SDR FDEA202608271235](https://openairdocs.org/sdr/FDEA202608271235.md): Seat Track · corroded · Aug 27, 2026 · N617FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT, UPON REMOVAL OF FLOOR PANELS FOR ACCESS, FOUND SEAT TRACK CORRODED AT BS 1149, X= -8.5. THE SEAT TRACK WAS EVALUATED, FOUND EXFOLIATED & EXCEEDS LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REP - [SDR FDEA202608271234](https://openairdocs.org/sdr/FDEA202608271234.md): Seat Track · corroded · Aug 27, 2026 · N617FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO BAY, UPON REMOVAL OF FLOOR PANELS FOR ACCESS, FOUND SEAT TRACK CORRODED AT BS 6-90 X= -8.5. THE SEAT TRACK WAS EVALUATED, FOUND EXFOLIATION EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SE - [SDR FDEA202608261231](https://openairdocs.org/sdr/FDEA202608261231.md): Seat Track · no discrepancy · Aug 26, 2026 · N617FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT - EXISTING SEAT TRACK REPAIR BETWEEN STATION 1651 - 1691, X= 8.5 REQUIRES EVALUATION FOR CONDITION AND CONFORMITY TO APPROVED DATA. MAIN DECK CARGO COMPARTMENT. EXISTING SEAT TRACK REPAIR BETWEEN STATION 1651 - 1691, X=8.5 EVALUATE - [SDR FDEA202608261227](https://openairdocs.org/sdr/FDEA202608261227.md): Seat Track · worn · Aug 26, 2026 · N617FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO BAY SEAT TRACK AT BS 755, X= -47.5" FOUND CROWN 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, BS 725 TO EXISTING SPLICE BS 765, X= -4 - [SDR FDEA202608261226](https://openairdocs.org/sdr/FDEA202608261226.md): Floor Support · corroded · Aug 26, 2026 · N617FE · Doug MD11F · Fuselage Miscellaneous Structure > MAIN DECK CARGO AFT FLOOR SUPPORT FOUND WITH CORROSION BETWEEN BS 1931-1941, X= 3. CORROSION ON FLOOR SUPPORT MAIN DECK CARGO AFT COMPARTMENT BETWEEN STATION 1931-1941 X= 3 EVALUATED AND FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER MD-11 SRM 53- 00-00-2R FIG - [SDR FDEA202608261225](https://openairdocs.org/sdr/FDEA202608261225.md): Floor Support · dented · Aug 26, 2026 · N617FE · Doug MD11F · Fuselage Miscellaneous Structure > AFT CABIN COMPARTMENT FLOOR SUPPORT FOUND WITH CORROSION AT BS 1996, X= 27. CORROSION ON FLOOR SUPPORT AT AFT CABIN COMPARTMENT STATION 1996 X= 27 EVALUATED AND FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-00-2R FIGURE 206 REPAIR GENERAL. CO - [SDR FDEA202608221215](https://openairdocs.org/sdr/FDEA202608221215.md): Seat Track · worn · Aug 22, 2026 · N617FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 5-10, X= -47.5" 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 SPLI - [SDR FDEA202608221214](https://openairdocs.org/sdr/FDEA202608221214.md): Seat Track · corroded · Aug 22, 2026 · N617FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO BAY SEAT TRACK AT BS 1721, X= -27.5" FOUND WITH EXFOLIATION CORROSION. THE SEAT TRACK WAS EVALUATED & FOUND EXFOLIATED AND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEME - [SDR FDEA202608211210](https://openairdocs.org/sdr/FDEA202608211210.md): Seat Track · worn · Aug 21, 2026 · N617FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO BAY SEAT TRACK AT BS 1541, X= -8.5" CROWN WAS FOUND 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 BS 5-123/1531 - 1571 EXIS - [SDR FDEA202608211209](https://openairdocs.org/sdr/FDEA202608211209.md): Seat Track · worn · Aug 21, 2026 · N617FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > CABIN- MAIN DECK CARGO BAY SEAT TRACK BS 1541, 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 BS 1571 - 5-123/1531 EXIST - [SDR FDEA202608211208](https://openairdocs.org/sdr/FDEA202608211208.md): Seat Track · worn · Aug 21, 2026 · N617FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 1541, X= 47.5" FOUND CROWN WORN. THE SEAT TRACK EVALUATED & FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT BS 1571 - 5-123/1531 IAW - [SDR FDEA202608211207](https://openairdocs.org/sdr/FDEA202608211207.md): Seat Track · worn · Aug 21, 2026 · N617FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO BAY SEAT TRACK AT STATION 1421, X= -47.5" FOUND CROWN WORN. SEAT TRACK CROWN EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT AT EXISTING SPLICES BS 1411 - 1 - [SDR FDEA202608211206](https://openairdocs.org/sdr/FDEA202608211206.md): Seat Track · damaged · Aug 21, 2026 · N617FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 1421, 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, BS 1391 -1431, X = - [SDR FDEA202608211205](https://openairdocs.org/sdr/FDEA202608211205.md): Seat Track · damaged · Aug 21, 2026 · N617FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO BAY SEAT TRACK AT BS 1421, X= 47.5" 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 FROM BS 1391- 1431 IAW SRM 53 - [SDR FDEA202608211204](https://openairdocs.org/sdr/FDEA202608211204.md): Seat Track · damaged · Aug 21, 2026 · N617FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT SEAT TRACK, BS 1421, 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 FROM BS 1391 - 1431 IAW - [SDR FDEA202608211203](https://openairdocs.org/sdr/FDEA202608211203.md): Seat Track · damaged · Aug 21, 2026 · N617FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO BAY SEAT TRACK AT BS 1411, X= -27.5" FOUND 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 FROM BS 1391 - 1431 IAW SRM 53-00 - [SDR FDEA202608211202](https://openairdocs.org/sdr/FDEA202608211202.md): Seat Track · damaged · Aug 21, 2026 · N617FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > CABIN- MAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 1279, X= 8.5", FOUND CROWN WORN. FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM BS 1269 - 1331, X= 8.5 IAW SRM 53-00-52-2R, REPA - [SDR FDEA202608211200](https://openairdocs.org/sdr/FDEA202608211200.md): Seat Track · worn · Aug 21, 2026 · N617FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO BAY SEAT TRACK AT STATION 1165, X= -47.5" FOUND CROWN WORN. 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 6-10 - [SDR FDEA202608211199](https://openairdocs.org/sdr/FDEA202608211199.md): Doubler · cracked · Aug 21, 2026 · N617FE · Doug MD11F · Fuselage Main, Plate/Skin > NR 1 AIRCON RAM AIR EXHAUST CUTOUT PRODUCTION DOUBLER FOUND CRACKED AT STATION Y= 561.667. PRODUCTION DOUBLER ON NR 1 AIRCON RAM AIR EXHAUST CUTOUT AT STATION Y=561.667 REMOVED IAW SRM 51-31-01-0G. DOUBLER FABRICATED IAW DWG ACA3850 REV AA & INSTALLED IAW SRM - [SDR FDEA202608201189](https://openairdocs.org/sdr/FDEA202608201189.md): Doubler · damaged · Aug 20, 2026 · N617FE · Doug MD11F · Wing, Plate/Skin > AGING AIRCRAFT - LEFT WING LEADING EDGE COMPARTMENT FOUND WITH EXISTING BEADED DOUBLER REPAIR BETWEEN STATION XOS 772 TO XOS 776. EVALUATED AND FOUND REPAIRED IN ACCORDANCE WITH MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. ENGINEERING ORDER 1-5100- 7-5001 - [SDR FDEA202608201188](https://openairdocs.org/sdr/FDEA202608201188.md): Doubler · damaged · Aug 20, 2026 · N617FE · Doug MD11F · Wing, Plate/Skin > AGING AIRCRAFT - LEFT HAND WING LEADING EDGE COMPARTMENT FOUND WITH EXISTING BEADED DOUBLER REPAIR BETWEEN STATION XOS 759 TO XOS 763. EVALUATED AND FOUND REPAIRED IN ACCORDANCE WITH MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. ENGINEERING ORDER 1-5100- 7 - [SDR FDEA202608201187](https://openairdocs.org/sdr/FDEA202608201187.md): Doubler · damaged · Aug 20, 2026 · N617FE · Doug MD11F · Wing, Plate/Skin > AGING AIRCRAFT - LEFT HAND WING LEADING EDGE COMPARTMENT FOUND WITH EXISTING BEADED DOUBLER REPAIR BETWEEN STATION XOS 625 TO XOS 629. EVALUATED AND FOUND REPAIRED IN ACCORDANCE WITH MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. ENGINEERING ORDER 1-5100- 7 - [SDR FDEA202608201186](https://openairdocs.org/sdr/FDEA202608201186.md): Doubler · damaged · Aug 20, 2026 · N617FE · Doug MD11F · Wing, Plate/Skin > AGING AIRCRAFT - LEFT WING LEADING EDGE COMPART FOUND WITH EXISTING BEADED DOUBLER REPAIR BETWEEN STATION XOS 616 TO XOS 621. LEFT WING LEADING EDGE COMPARTMENT FOUND WITH EXISTING BEADED DOUBLER REPAIR BETWEEN STATION XOS 616 TO XOS 621 EVALUATED AND FOU - [SDR FDEA202608201183](https://openairdocs.org/sdr/FDEA202608201183.md): Seat Track · worn · Aug 20, 2026 · N617FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > CABIN- MAIN DECK CARGO BAY SEAT TRACK AT STATION 1165, X= 27.5" FOUND CROWN WORN. FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM BS 1169 TO EXISTING SPLICE STATION 6-100/11 - [SDR FDEA202608201182](https://openairdocs.org/sdr/FDEA202608201182.md): Seat Track · worn · Aug 20, 2026 · N617FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 1150, X= 47.5" 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 BS 1169 TO EXISTING S - [SDR FDEA202608201181](https://openairdocs.org/sdr/FDEA202608201181.md): Seat Track · worn · Aug 20, 2026 · N617FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > CABIN- MAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 6-10, X= -8.5" FOUND CROWN WORN. SEAT TRACK EVALUATED & FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT BS 6-60 TO EXISTING SP - [SDR FDEA202608201180](https://openairdocs.org/sdr/FDEA202608201180.md): Seat Track · worn · Aug 20, 2026 · N617FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 6-50, X= 8.5" FOUND CROWN WORN. SEAT TRACK EVALUATED & FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT BS 6-60 TO EXISTING SPLICE BS - [SDR FDEA202608201179](https://openairdocs.org/sdr/FDEA202608201179.md): Seat Track · worn · Aug 20, 2026 · N617FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > CABIN- MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 6-10, X= 47.5" FOUND CROWN WORN. SEAT TRACK EVALUATED & FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT BS 6-60 TO EXISTING S - [SDR FDEA202608201178](https://openairdocs.org/sdr/FDEA202608201178.md): Seat Track · worn · Aug 20, 2026 · N617FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 6-10, X= -47.5" FOUND CROWN WORN. SEAT TRACK EVALUATED, & FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM BS 6-60 TO EXISTING SPLIC - [SDR FDEA202608201177](https://openairdocs.org/sdr/FDEA202608201177.md): Seat Track · worn · Aug 20, 2026 · N617FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 6-10, X= -27.5" FOUND CROWN WORN. SEAT TRACK EVALUATED & FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT BS 6-60 TO EXISTING SP - [SDR FDEA202608201176](https://openairdocs.org/sdr/FDEA202608201176.md): Seat Track · worn · Aug 20, 2026 · N617FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > CABIN- MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1019, X= -47.5" FOUND CROWN WORN. EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM BS 989 - 1029, X= -47.5, EXIS - [SDR FDEA202608201175](https://openairdocs.org/sdr/FDEA202608201175.md): Seat Track · worn · Aug 20, 2026 · N617FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 879, X= 8.5" FOUND CROWN WORN. SEAT TRACK EVALUATED & FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT, BS 909 TO EXISTING SPLICE BS 869 - [SDR FDEA202608201174](https://openairdocs.org/sdr/FDEA202608201174.md): Seat Track · worn · Aug 20, 2026 · N617FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > CABIN- MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 879, X= 27.5" FOUND CROWN WORN. SEAT TRACK, BS 879 X= 27.5" EVALUATED & FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM BS 9 - [SDR FDEA202608201173](https://openairdocs.org/sdr/FDEA202608201173.md): Doubler · cracked · Aug 20, 2026 · N617FE · Doug MD11F · Wing, Plate/Skin > LEFT WING- LEADING EDGE COMPARTMENT BEADED DOUBLER AT XOS 745 FOUND CRACK ABOUT 0.2 INCH. LEFT WING LEADING EDGE COMPARTMENT CRACKED BEADED DOUBLER AT XOS 745. CARRIED OUT REPAIR IAW SRM 57-40-02-2R, REPAIR 15, FIGURE 203. REPAIR CLASSIFIED MAJOR IAW GMM 6-2- - [SDR FDEA202608201172](https://openairdocs.org/sdr/FDEA202608201172.md): Former · cracked · Aug 20, 2026 · N617FE · Doug MD11F · Wing Main, Frame Structure > LEFT HAND WING- LEADING EDGE COMPARTMENT FORMER AT STATION XOS 1025 FOUND CRACKED, ABOUT 0.5 INCHES. LEFT WING LEADING EDGE COMPARTMENT CRACKED FORMER REMOVED AT STATION XOS 1025 IAW SRM 51-35-01-0G. FABRICATED FORMER IAW DRAWING ARB2920, REVISION BB. INSTA - [SDR FDEA202606030666](https://openairdocs.org/sdr/FDEA202606030666.md): Bulkhead · worn · Jun 3, 2026 · N617FE · Doug MD11F · Nacelle/Pylon, Bulkhead/Firewall > #3 AFT PYLON BULKHEAD WORN REMOVED AND REPLACED AFT BULKHEAD. - [SDR FDEA202605050557](https://openairdocs.org/sdr/FDEA202605050557.md): Fastener · loose · May 5, 2026 · N617FE · Doug MD11F · Nacelle/Pylon, Main Frame > ENG PYLON HAS SEVERAL LOOSE FASTENERS ON OUTSIDE NEAR AFT MOUNT - [SDR FDEA202605050556](https://openairdocs.org/sdr/FDEA202605050556.md): Skin · pulled · May 5, 2026 · N617FE · Doug MD11F · Nacelle/Pylon, Plate/Skin > NR 1 ENG PYLON HAS 3 PULLED FASTENERS ON SKIN O/B SIDE ABOVE AFT ENG MOUNT POINT. - [SDR FDEA202605050555](https://openairdocs.org/sdr/FDEA202605050555.md): Fastener · loose · May 5, 2026 · N617FE · Doug MD11F · Nacelle/Pylon, Main Frame > SEVERAL LOOSE FASTENERS ON O/B SIDE OF # 1ENG PYLON JUST BELOW THE FWD PYLON ATTACH FITTING. Next page: https://openairdocs.org/aircraft/N617FE/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 = 'N617FE' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N617FE/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.