# Service difficulty reports: N525FE A list on [N525FE](https://openairdocs.org/aircraft/N525FE.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 6 · 261 reports - [SDR FDEA202509151703](https://openairdocs.org/sdr/FDEA202509151703.md): Skin · ground damage · Sep 15, 2025 · N525FE · Doug MD11F · Fuselage Main, Plate/Skin > AFT CGO LOADER WENT UP (BY ITSELF PER RAMP) AND HITTED THE AFT FUSELAGE BELOW DOOR FRAME, LOADER STILL IN CONTACT CURRENTLY, BUT A HOLE IS VISIBLE ALREADY ABOUT 5 SQUARE INCHES. WILL EVALUATE WHEN LOADER IS REMOVED. OMPLIED WITH EA 1-5330-T0384834 PART 2 - [SDR FDEA202509051646](https://openairdocs.org/sdr/FDEA202509051646.md): Longeron Splice · damaged · Sep 5, 2025 · N525FE · Doug MD11F · Fuselage Main, Longeron/Stringer > DAMAGED LONGERON SPLICE AT STATION 1811 AND LONGERON 36 REWORKED DAMAGED SPLICES IAW 51-21-10. - [SDR FDEA202509051645](https://openairdocs.org/sdr/FDEA202509051645.md): Shear Tie · damaged · Sep 5, 2025 · N525FE · Doug MD11F · Fuselage Internal Mounting Structure > DAMAGED SHEAR TIE AT STA 1801 AND LONGERONS 37-39. REMOVED AND REPLACED THE SHEAR TIE AT STATION 1801 AND LONGERONS 37-39 IN REF TO SRM 51-33-01-0G - [SDR FDEA202506261050](https://openairdocs.org/sdr/FDEA202506261050.md): Skin · no discrepancy · Jun 26, 2025 · N525FE · Doug MD11F · Passenger/Crew Doors > AGING AIRCRAFT - EXISTING REPAIR AT L1 PASSENGER DOOR EXTERIOR SKIN FORWARD UPPER CORNER STATION 435. EXISTING REPAIR AT L1 PASSENGER DOOR EXTERIOR SKIN FORWARD UPPER CORNER STATION 435 EVALUATED AND FOUND REPAIRED IAW MD11 SRM 52-10-01-2R REPAIR 3 FIGURE - [SDR FDEA202506241033](https://openairdocs.org/sdr/FDEA202506241033.md): Spar Cap · corroded · Jun 24, 2025 · N525FE · Doug MD11F · Wing Spar > UPON UPPER SURFACE TRAILING EDGE FIXED PANEL REMOVAL FOR LOWER CAP CORROSION TREATMENT ACCESS UPPER CAP FOUND CORROSION AT STATION XORS 1031.5. RIGHT HAND WING UPPER CAP AT STATION XORS 1031.5 CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER MD-11 SRM 5 - [SDR FDEA202506241032](https://openairdocs.org/sdr/FDEA202506241032.md): Spar Cap · corroded · Jun 24, 2025 · N525FE · Doug MD11F · Wing Spar > UPON UPPER SURFACE TRAILING EDGE FIXED PANEL REMOVAL FOR LOWER CAP CORROSION TREATMENT ACCESS UPPER CAP FOUND CORROSION AT STATION XORS 1028.5. RIGHT HAND WING UPPER CAP AT STATION XORS 1028.5 CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57 - [SDR FDEA202506241031](https://openairdocs.org/sdr/FDEA202506241031.md): Spar Cap · corroded · Jun 24, 2025 · N525FE · Doug MD11F · Wing Spar > UPON UPPER SURFACE TRAILING EDGE FIXED PANEL REMOVAL FOR LOWER CAP CORROSION TREATMENT ACCESS, UPPER CAP FOUND CORROSION. AT STATION XORS 1035. RIGHT HAND WING UPPER CAP AT STATION XORS 1035 CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-00- - [SDR FDEA202506241030](https://openairdocs.org/sdr/FDEA202506241030.md): Spar Cap · corroded · Jun 24, 2025 · N525FE · Doug MD11F · Wing Spar > RIGHT HAND WING: UPON OUTBOARD TRAILING EDGE ISLAND REMOVAL FOR LOWER CAP CORROSION TREATMENT ACCESS, REAR SPAR UPPER CAP FOUND CORROSION FROM STATION XORS 1043 TO STATION XORS 1063. RIGHT HAND WING REAR SPAR UPPER CAP FROM STATION XORS 1043 TO STATION XO - [SDR FDEA202506201013](https://openairdocs.org/sdr/FDEA202506201013.md): Skin · worn · Jun 20, 2025 · N525FE · Doug MD11F · Standard Practices/Structures > AGING AIRCRAFT - EXISTING REPAIR ON DOUBLER EDGE AT FUSELAGE SKIN FWD CARGO DOOR CUTOUT AFT JAMB BS 1002 BETWEEN L38R TO L42R. (BLENDOOUT REPAIR). EXISTING REPAIR DOUBLER AT FUSELAGE SKIN FWD CARGO DOOR CUTOUT AFT JAMB BS 1002 BETWEEN L38R TO L42R EVALUATED - [SDR FDEA202506180979](https://openairdocs.org/sdr/FDEA202506180979.md): Skin · corroded · Jun 18, 2025 · N525FE · Doug MD11F · Fuselage Main, Plate/Skin > UPON REMOVED FAIRING FOR EXISTING REPAIR EVALUATION ACCESS FOUND CORROSION AT RIGHT HAND FUSELAGE SKIN AT APPROXIMATE STATION 2160 LONGERON 12 RIGHT AREA. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-70-01-2R FIGURE 201 SHEET 3 REPAIR 3 A - [SDR FDEA202506160959](https://openairdocs.org/sdr/FDEA202506160959.md): Cap · corroded · Jun 16, 2025 · N525FE · Doug MD11F · Wing Main, Frame Structure > RIGHT HAND WING OUTBOARD TRAILING EDGE LOWER CAP FOUND CORROSION AT STATION XORS 1044 - XORS 1077. RIGHT HAND WING OUTBOARD TRAILING EDGE LOWER CAP AT STATION XORS 1044 - XORS 1077 CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-00-10-1A ALLOW - [SDR FDEA202506160958](https://openairdocs.org/sdr/FDEA202506160958.md): Cap · corroded · Jun 16, 2025 · N525FE · Doug MD11F · Wing Main, Frame Structure > LEFT HAND WING OUTBOARD TRAILING EDGE LOWER CAP FOUND CORROSION AT STATION XORS 1052 - XORS 1083. LEFT HAND WING OUTBOARD TRAILING EDGE LOWER CAP AT STATION XORS 1052 - XORS 1083 CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-00-10-1A ALLOWAB - [SDR FDEA202506160957](https://openairdocs.org/sdr/FDEA202506160957.md): Longeron Splice · damaged · Jun 16, 2025 · N525FE · Doug MD11F · Fuselage Main, Longeron/Stringer > LOWER FORWARD CARGO COMPARTMENT RIGHT HAND TUNNEL AREA LONGERON SPLICE FITTING FOUND CRACK AT STATION 6-0 LONGERON 38 RIGHT. LOWER FORWARD CARGO COMPARTMENT RIGHT HAND TUNNEL AREA CRACKED LONGERON SPLICE FITTING AT STATION 6-0, LONGERON 38 RIGHT REMOVED AN - [SDR FDEA202506160956](https://openairdocs.org/sdr/FDEA202506160956.md): Longeron Splice · damaged · Jun 16, 2025 · N525FE · Doug MD11F · Fuselage Main, Longeron/Stringer > LOWER CENTER CARGO COMPARTMENT LEFT HAND TUNNEL AREA LONGERON SPLICE FITTING FOUND CRACK BETWEEN STATION 5-113 - 1542 LONGERON 38 LEFT. LOWER CENTER CARGO COMPARTMENT LEFT HAND TUNNEL AREA CRACK LONGERON SPLICE FITTING BETWEEN STATION 5-113 - 1542 LONGERON - [SDR FDEA202506140937](https://openairdocs.org/sdr/FDEA202506140937.md): Skin · corroded · Jun 14, 2025 · N525FE · Doug MD11F · Fuselage Main, Plate/Skin > AGING AIRCRAFT - EXISTING REPAIR AT AFT FUSELAGE SKIN BELOW HORIZONTAL STABILIZER RIGHT HAND SIDE STATION 2164, LONGERON 33 RIGHT EXISTING REPAIR AT AFT FUSELAGE SKIN BELOW HORIZONTAL STABILIZER RIGHT HAND SIDE STATION 2164 LONGERON 33 RIGHT EVALUATED AND - [SDR FDEA202506140936](https://openairdocs.org/sdr/FDEA202506140936.md): None · none · Jun 14, 2025 · N525FE · Doug MD11F · Wing Structure > AGING AIRCRAFT - EXISTING REPAIR AT RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT RIB DOUBLER STATION XOS 789.645 (REPLACED DOUBLER P/N ARB3954-8 BY FABRICATION) EXISTING REPAIR AT RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT RIB DOUBLER STATION XOS 789 - [SDR FDEA202506140935](https://openairdocs.org/sdr/FDEA202506140935.md): None · none · Jun 14, 2025 · N525FE · Doug MD11F · Wing Structure > AGING AIRCRAFT - EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE COMPARTMENT RIB DOUBLER STATION XOS 789.645 (REPLACED DOUBLER P/N ARB3954-7 BY FABRICATION) EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE COMPARTMENT RIB DOUBLER STATION XOS 789.6 - [SDR FDEA202506140934](https://openairdocs.org/sdr/FDEA202506140934.md): None · none · Jun 14, 2025 · N525FE · Doug MD11F · Wing Structure > AGING AIRCRAFT - EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE LOWER STRINGER DOUBLER STATION XOS 906.5607 EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE LOWER STRINGER DOUBLER STATION XOS 906.5607 EVALUATED AND FOUND REPAIRED IAW MD11 SRM 5 - [SDR FDEA202506140933](https://openairdocs.org/sdr/FDEA202506140933.md): None · none · Jun 14, 2025 · N525FE · Doug MD11F · Wing Main, Frame Structure > AGING AIRCRAFT - EXISTING REPAIR AT RIGHT HAND WING FIXED LEADING EDGE LOWER STRINGER DOUBLER STATION XOS 906.5607. EXISTING REPAIR AT RIGHT HAND WING FIXED LEADING EDGE LOWER STRINGER DOUBLER STATION XOS 906.5607 EVALUATED AND FOUND REPAIRED IAW MD11 SRM - [SDR FDEA202506130928](https://openairdocs.org/sdr/FDEA202506130928.md): Seat Track · none · Jun 13, 2025 · N525FE · Doug MD11F · Standard Practices/Structures > AGING AIRCRAFT - EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK BETWEEN STATION 1531 TO STATION 1551 X = -47.5 RIGHT HAND SIDE. EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK BETWEEN STATION 1531 TO STATION 1551 X = -47.5 - [SDR FDEA202506130927](https://openairdocs.org/sdr/FDEA202506130927.md): Skin · none · Jun 13, 2025 · N525FE · Doug MD11F · Standard Practices/Structures > AGING AIRCRAFT - EXISTING REPAIR AT RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER STATION XOS 993.237 EXISTING REPAIR AT RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER STATION XOS 993.237 EVALUATED AND FOUND REPAIRED NOT IAW - [SDR FDEA202506110916](https://openairdocs.org/sdr/FDEA202506110916.md): Stringer · cracked · Jun 11, 2025 · N525FE · Doug MD11F · Fuselage Main, Longeron/Stringer > DURING ACCOMPLISHING W/C: 57.11.01.1, FOUND CRACK ON UPPER AUXILLIARY TANK LOWER STRINGER S-47, ALONG XCW -17. (RIGHT HAND SIDE). CRACKED STRINGER S-47 ALONG XCW -17 AT UPPER AUXILLIARY TANK LOWER AREA REPAIRED AS PER MD-11 SRM 57-10-03-2R FIGURE 201 REPA - [SDR FDEA202506110915](https://openairdocs.org/sdr/FDEA202506110915.md): Stringer · cracked · Jun 11, 2025 · N525FE · Doug MD11F · Fuselage Main, Longeron/Stringer > DURING ACCOMPLISHING W/C: 57.11.01.1, FOUND CRACK ON UPPER AUXILLIARY TANK LOWER STRINGER S-47, ALONG XCW 17. CRACKED STRINGER S-47 ALONG XCW 17 AT UPPER AUXILLIARY TANK LOWER AREA REPAIRED AS PER MD-11 SRM 57-10-03-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIE - [SDR FDEA202506110914](https://openairdocs.org/sdr/FDEA202506110914.md): Stringer · cracked · Jun 11, 2025 · N525FE · Doug MD11F · Fuselage Main, Longeron/Stringer > DURING ACCOMPLISHING W/C: 57.11.01.1, FOUND CRACK AT UPPER AUXILLIARY TANK LOWER STRINGER S-47, ALONG XCW -46.5. (RIGHT HAND SIDE). CRACKED STRINGER S-47 ALONG XCW -46.5 AT UPPER AUXILLIARY TANK LOWER AREA REPAIRED AS PER MD-11 SRM 57-10-03-2R FIGURE 201 - [SDR FDEA202506110913](https://openairdocs.org/sdr/FDEA202506110913.md): Stringer · cracked · Jun 11, 2025 · N525FE · Doug MD11F · Fuselage Main, Longeron/Stringer > DURING ACCOMPLISHING W/C: 57.11.01.1, FOUND CRACK ON UPPER AUXILLIARY TANK LOWER STRINGER S-47, ALONG XCW 46.5. CRACKED STRINGER S-47 ALONG XCW 46.5 AT UPPER AUXILLIARY TANK LOWER AREA REPAIRED AS PER MD-11 SRM 57-10-03-2R FIGURE 201 REPAIR 1. REPAIR CLA - [SDR FDEA202506110912](https://openairdocs.org/sdr/FDEA202506110912.md): Stringer · cracked · Jun 11, 2025 · N525FE · Doug MD11F · Fuselage Main, Longeron/Stringer > DURING ACCOMPLISHING W/C: 57.11.01.1, FOUND CRACK ON UPPER AUXILLIARY TANK LOWER STRINGER S-46, ALONG STATION XCW -46.5. (RIGHT HAND SIDE). REPAIR CARRIED OUT AT UPPER AUXILLIARY TANK LOWER STRINGER S-46, ALONG STATION XCW -46.5 (RIGHT HAND SIDE) AS PER - [SDR FDEA202506110911](https://openairdocs.org/sdr/FDEA202506110911.md): Longeron Splice · corroded · Jun 11, 2025 · N525FE · Doug MD11F · Fuselage Main, Longeron/Stringer > LOWER FORWARD CARGO COMPARTMENT BILGE AREA LONGERON SPLICE FITTING FOUND CRACK AT STATION 6-0 LONGERON 50 RIGHT. LOWER FORWARD CARGO COMPARTMENT BILGE AREA CRACKED LONGERON SPLICE FITTING AT STATION 6-0, LONGERON 50 RIGHT REMOVED AND REPLACED WITH FABRICAT - [SDR FDEA202506110910](https://openairdocs.org/sdr/FDEA202506110910.md): Longeron · corroded · Jun 11, 2025 · N525FE · Doug MD11F · Fuselage Main, Longeron/Stringer > LOWER FORWARD CARGO COMPARTMENT BILGE AREA LONGERON FOUND WITH CORROSION BETWEEN STATION 1038-1059 LONGERON 52. LOWER FORWARD CARGO COMPARTMENT BILGE AREA LONGERON 52 BETWEEN STATION 1038- 1059 CORROSION REMOVED AND FOUND OUT LIMIT PER MD-11 SRM 53-00-00-2R - [SDR FDEA202506100884](https://openairdocs.org/sdr/FDEA202506100884.md): Seat Track · corroded · Jun 10, 2025 · N525FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > CABIN - FLOOR SEAT TRACK STATION 850, X = - 8.5 FOUND WITH CORROSION. CABIN - AT SEAT TRACK STATION 850, X = - 8.5 CORROSION EVALUATED, FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPA - [SDR FDEA202506100883](https://openairdocs.org/sdr/FDEA202506100883.md): Seat Track · corroded · Jun 10, 2025 · N525FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > CABIN - FLOOR SEAT TRACK STATION 815, X = - 8.5 FOUND WITH CORROSION. CABIN - AT SEAT TRACK STATION 815, X = - 8.5 CORROSION EVALUATED, FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPA - [SDR FDEA202506100882](https://openairdocs.org/sdr/FDEA202506100882.md): Seat Track · corroded · Jun 10, 2025 · N525FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > CABIN - FLOOR SEAT TRACK STATION 795 X = - 8.5 FOUND WITH CORROSION. CABIN - AT SEAT TRACK STATION 795, X = - 8.5 CORROSION EVALUATED, FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAI - [SDR FDEA202506100880](https://openairdocs.org/sdr/FDEA202506100880.md): Seat Track · worn · Jun 10, 2025 · N525FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > CABIN - FLOOR PANEL SEAT TRACK STATION 1741 X = - 8.5 CROWN AREA FOUND WORN CABIN - AT SEAT TRACK STATION 1741, 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 REPAIR - [SDR FDEA202506100879](https://openairdocs.org/sdr/FDEA202506100879.md): Seat Track · worn · Jun 10, 2025 · N525FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > CABIN - FLOOR PANEL SEAT TRACK STATION 1661 X = - 8.5 CROWN AREA FOUND WORN. CABIN - SEAT TRACK AT 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 REPAI - [SDR FDEA202506100878](https://openairdocs.org/sdr/FDEA202506100878.md): Seat Track · worn · Jun 10, 2025 · N525FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > CABIN - FLOOR PANEL SEAT TRACK STATION 1631 X = - 8.5 CROWN AREA FOUND WORN. CABIN - AT SEAT TRACK STATION 1631, 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 REPAI - [SDR FDEA202506100877](https://openairdocs.org/sdr/FDEA202506100877.md): Seat Track · worn · Jun 10, 2025 · N525FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > CABIN - FLOOR PANEL SEAT TRACK STATION 1521 X = 8.5 CROWN AREA FOUND WORN. SEAT TRACK STA 1521, X = 8.5 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 SEAT TRACK R - [SDR FDEA202506100876](https://openairdocs.org/sdr/FDEA202506100876.md): Seat Track · worn · Jun 10, 2025 · N525FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > CABIN - FLOOR PANEL SEAT TRACK STATION 1139 X = 47.5 CROWN AREA FOUND WORN. CABIN - AT SEAT TRACK STATION 1139, 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 REPAIRE - [SDR FDEA202506100875](https://openairdocs.org/sdr/FDEA202506100875.md): Seat Track · worn · Jun 10, 2025 · N525FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > CABIN - FLOOR PANEL SEAT TRACK STATION 1541, X = - 8.5 CROWN AREA FOUND WORN. CABIN - AT SEAT TRACK STATION 1541, X = - 8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTI - [SDR FDEA202506100864](https://openairdocs.org/sdr/FDEA202506100864.md): Seat Track · worn · Jun 10, 2025 · N525FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > CABIN - FLOOR PANEL SEAT TRACK STATION 5-43 X = - 8.5 CROWN AREA FOUND WORN. CABIN - AT SEAT TRACK STATION 5-43, 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 REPAI - [SDR FDEA202412041775](https://openairdocs.org/sdr/FDEA202412041775.md): Light · failed · Dec 4, 2024 · N525FE · Doug MD11F · Emergency Lighting > EMER LT BAT 1 LO LEVEL ONE ALERT WHEN PERFORMING EMERGENCY LIGHTS TEST ON PREFLIGHT ACCOMPLISHED EMERGENCY LIGHTING BATTERY TEST. TEST PASSED. NO DEFECTS NOTED. OK FOR SERVICE. - [SDR FDEA202409081255](https://openairdocs.org/sdr/FDEA202409081255.md): Warning Message · illuminated · Sep 8, 2024 · N525FE · Doug MD11F · Fuel Indicating System > SHORTLY AFTER TOP OF CLIMB AT FL 370 RECEIVED LEVEL 1 TNK 1 TIP FUEL LO, FOLLOWED WITHIN 1 MINUTE BY TNK 3 TIP FUEL LO. RAN QRH, NO HELP. WHILE COORDINATING WITH GOC AND MOCC ABOUT THIS ISSUE, RECEIVED LEVEL 2 FUEL QTY/USED CHK ALERT. REPLACED STANDARD ELE - [SDR FDEA202311071842](https://openairdocs.org/sdr/FDEA202311071842.md): Collar · sheared · Nov 7, 2023 · N525FE · Doug MD11F · Landing Gear Steering System > DURING PUSHBACK, FOUND RH STEERING CYLINDER'S STEERING COLLAR PIN SHEARED OFF. INSTALLED NLG RT STEERING CYLINDER COLLAR PIN, REFERED AMM 32-52-30-4. NOSE GEAR STEERING CYLINDER OPS CHECK. A/C OK FOR SERVICE - [SDR FDEA202308131458](https://openairdocs.org/sdr/FDEA202308131458.md): Panel · cracked · Aug 13, 2023 · N525FE · Doug MD11F · Fuselage Main, Structure > WHILE TROUBLESHOOTING FOUND A CRACK IN THE LOWER TORQUE BOX PLANE PANEL AT STA. 2122. REPAIRED CRACK IN THE LOWER TORQUE BOX PLANE PANEL AT STA. 2122 IN REF. EA# 1-5310-T0375777 P1. FUSELAGE - MAINFRAME - CRACK IN LOWER TORQUE BOX WEB, APU COMPARTMENT CEILIN - [SDR FDEA202306081004](https://openairdocs.org/sdr/FDEA202306081004.md): Skin · chafed · Jun 8, 2023 · N525FE · Doug MD11F · Fuselage Main, Plate/Skin > FORWARD CARGO DOOR FORWARD DOOR JAMB LOWER EXISTING REPAIR DOUBLER AT STATION 895.700 LONGERON 38 RIGHT TO LONGERON 42 RIGHT FOUND CHAFFED. FORWARD CARGO DOOR FORWARD DOOR JAMB LOWER EXISTING REPAIR DOUBLER AT STATION 895.700 LONGERON 38 RIGHT TO LONGERON - [SDR FDEA202306081003](https://openairdocs.org/sdr/FDEA202306081003.md): Skin · chafed · Jun 8, 2023 · N525FE · Doug MD11F · Fuselage Main, Plate/Skin > FORWARD CARGO DOOR AFT DOOR JAMB LOWER EXISTING REPAIR DOUBLER AT STATION 1002.300 LONGERON 38 RIGHT TO LONGERON 42 RIGHT FOUND CHAFFED. FORWARD CARGO DOOR AFT DOOR JAMB LOWER EXISTING REPAIR DOUBLER AT STATION 1002.300 LONGERON 38 RIGHT TO LONGERON 42 RIG - [SDR FDEA202305270961](https://openairdocs.org/sdr/FDEA202305270961.md): Skin · cracked · May 27, 2023 · N525FE · Doug MD11F · Wing, Plate/Skin > 06 EACH FASTENER HOLE #7,#10,#11,#16,#37,#38 FOUND CRACK INDICATION DURING OPEN-HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT LEFT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS=683.4 AND STATION XORS=713.6. LEFT HAND WING LOWER SKIN ACCE - [SDR FDEA202305270960](https://openairdocs.org/sdr/FDEA202305270960.md): Skin · cracked · May 27, 2023 · N525FE · Doug MD11F · Wing Structure > 08 EACH FASTENER HOLES #7,#10,#11,#12,#15,#16,#34,#36 FOUND CRACK INDICATION DURING OPEN-HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT RIGHT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS=683.4 AND STATION XORS=713.6. LOWER SKIN ACCESS DOO - [SDR FDEA202305240930](https://openairdocs.org/sdr/FDEA202305240930.md): Seat Track · corroded · May 24, 2023 · N525FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > CABIN - MAIN DECK CARGO COMPARTMENT RIGHT HAND SEAT TRACK AT STATION 1421 X = -8.5" FOUND WITH CORROSION. MAIN DECK CARGO COMPARTMENT SEAT TRACK CORROSION AT STATION 1421 X = -8.5" REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 SHEET 1 - [SDR FDEA202305240929](https://openairdocs.org/sdr/FDEA202305240929.md): Seat Track · damaged · May 24, 2023 · N525FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > CABIN - MAIN DECK CARGO COMPARTMENT RIGHT HAND SEAT TRACK AT STATION 1341 X= -8.5" FOUND WITH CORROSION. MAIN DECK CARGO COMPARTMENT CORRODED SEAT TRACK AT STATION 1341 X = -8.5" REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 SHEET 1. - [SDR FDEA202305240928](https://openairdocs.org/sdr/FDEA202305240928.md): Seat Track · damaged · May 24, 2023 · N525FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > CABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1289 X = -8.5" FOUND CROWN DAMAGED. MAIN DECK CARGO COMPARTMENT DAMAGED SEAT TRACK AT STATION 1289 X= -8.5" MEASURED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 SHEET 1. SEAT TRAC - [SDR FDEA202305230919](https://openairdocs.org/sdr/FDEA202305230919.md): Skin · cracked · May 23, 2023 · N525FE · Doug MD11F · Wing, Plate/Skin > HIGH FREQUENCY EDDY CURRENT INSPECTION FOUND CRACK INDICATION APPROXIMATELY 0.15" IN LENGTH AT RIGHT HAND WING FIXED LEADING EDGE SKIN ADJACENT TO CUTOUT AT CORNER NUMBER 2 SLAT ANTI-ICE TELESCOPIC DUCT CUTOUT UPPER OUTBOARD CORNER AT APPROXIMATELY STA X Next page: https://openairdocs.org/aircraft/N525FE/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 = 'N525FE' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N525FE/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.