# Service difficulty reports: N591FE A list on [N591FE](https://openairdocs.org/aircraft/N591FE.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 · 394 reports - [SDR FDEA202609281442](https://openairdocs.org/sdr/FDEA202609281442.md): Solenoid Valve · malfunctioned · Sep 28, 2026 · N591FE · Doug MD11F · Autopilot System > DURING TAKEOFF, PF NOTICED AN UNUSUAL AMOUNT OF FORCE TO ROTATE ACFT. DURING CLIMB, HAND FLYING, APPROX 3X AMOUNT OF USUAL FORCE REQUIRED TO MOVE ACFT IN PITCH AXIS. WHEN AP1 IN USE, AP FUNCTIONED NORMAL. ATTEMPT MADE TO SWITCH TO AP2, AP2 WAS NOT AVAIL. - [SDR FDEA202509231775](https://openairdocs.org/sdr/FDEA202509231775.md): Bracket · cracked · Sep 23, 2025 · N591FE · Doug MD11F · Leading Edge Devices > DURING APPROACH PHASE WE RECEIVED A LEVEL 2 SLAT DISAG. RAN QRH. CONTINUED APPROACH WITH NIL FURTHER ISSUES ON LANDING. REMOVED BROKEN PULLEY BRACKET MOUNT. REMOVED CRACKED CLIP. REMOVED CRACKED BRACKET REMOVED PULLEY CHANNEL. REMOVED CLIP. REMOVED CL - [SDR FDEA202410271583](https://openairdocs.org/sdr/FDEA202410271583.md): Skin · corroded · Oct 27, 2024 · N591FE · Doug MD11F · Fuselage Main, Plate/Skin > RIGHT HAND AFT FUSELAGE EXTERNAL SKIN SURFACE FOUND CORROSION BETWEEN STATION 2150 TO 2163. EMPENNAGE: RIGHT HAND AFT FUSELAGE EXTERNAL SURFACE BETWEEN STATION 2150 TO 2163 CORROSION AREA REPAIR CARRIED OUT AS PER MD-11 SRM 53-70-01-2R REPAIR 3 FIGURE 2 - [SDR FDEA202410271582](https://openairdocs.org/sdr/FDEA202410271582.md): Seat Track · corroded · Oct 27, 2024 · N591FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > FORWARD CABIN L1 DOOR WAY SEAT TRACK FOUND WITH CORROSION AT STATION 423. CABIN Ï¿½ FORWARD CABIN L1 DOOR WAY AT SEAT TRACK STATION 423, X=107.25 CORROSION EVALUATED, FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAM - [SDR FDEA202410201564](https://openairdocs.org/sdr/FDEA202410201564.md): Frame · dented · Oct 20, 2024 · N591FE · Doug MD11F · Fuselage Main, Frame > MAIN DECK CARGO COMPARTMENT LEFT HAND FRAME AT STATION 1741 L12 FOUND DENTED. CABIN Ï¿½ MAIN DECK CARGO COMPARTMENT DENT AT LEFT HAND FRAME STATION 1741 LONGERON 12 LEFT REPAIRED AS PER MD-11 SRM 53-00-07-2R FIGURE 201 REPAIR 2. REPETITIVE INSPECTION REQ - [SDR FDEA202410201563](https://openairdocs.org/sdr/FDEA202410201563.md): Cargo Track · worn · Oct 20, 2024 · N591FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 765, X = 8.5 FOUND CROWN WORN OUT. CABIN Ï¿½ MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 765, X= 8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE D - [SDR FDEA202410201562](https://openairdocs.org/sdr/FDEA202410201562.md): Cargo Track · worn · Oct 20, 2024 · N591FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1421, X = -47.5 FOUND CROWN WORN OUT. CABIN Ï¿½ MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 1421, X= -47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOW - [SDR FDEA202410201561](https://openairdocs.org/sdr/FDEA202410201561.md): Cargo Track · worn · Oct 20, 2024 · N591FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1421, X = -27.5 FOUND CROWN WORN OUT. CABIN Ï¿½ MAIN DECK CARGO COMPARTMENT 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 ALLOW - [SDR FDEA202410201560](https://openairdocs.org/sdr/FDEA202410201560.md): Cargo Track · worn · Oct 20, 2024 · N591FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1279, X = -8.5 FOUND CROWN WORN OUT. CABIN Ï¿½ MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 1279, X= -8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE - [SDR FDEA202410201559](https://openairdocs.org/sdr/FDEA202410201559.md): Cargo Track · worn · Oct 20, 2024 · N591FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1279, X = -27.5 FOUND CROWN WORN OUT. CABIN Ï¿½ MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 1279, X= -27.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOW - [SDR FDEA202410201558](https://openairdocs.org/sdr/FDEA202410201558.md): Cargo Track · worn · Oct 20, 2024 · N591FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > CABIN MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1279, X = -47.5 FOUND CROWN WORN OUT. CABIN MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 1279, X= -47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 - [SDR FDEA202410201557](https://openairdocs.org/sdr/FDEA202410201557.md): Cargo Track · worn · Oct 20, 2024 · N591FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1279, X = 47.5 FOUND CROWN WORN OUT. CABIN Ï¿½ MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 1279, X= 47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE - [SDR FDEA202410201556](https://openairdocs.org/sdr/FDEA202410201556.md): Cargo Track · worn · Oct 20, 2024 · N591FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1279, X = 27.5 FOUND CROWN WORN OUT. CABIN Ï¿½ MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 1279, X= 27.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE - [SDR FDEA202410201555](https://openairdocs.org/sdr/FDEA202410201555.md): Cargo Track · worn · Oct 20, 2024 · N591FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > CABIN MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1279, X = 8.5 FOUND CROWN WORN OUT. CABIN MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 1279, X= 8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOW - [SDR FDEA202410171532](https://openairdocs.org/sdr/FDEA202410171532.md): Doubler · cracked · Oct 17, 2024 · N591FE · Doug MD11F · Wing, Plate/Skin > LEFT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACKED AT STATION XOS 1047. LEFT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER AT STATION XOS 1047 CRACKED AREA REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. - [SDR FDEA202410171531](https://openairdocs.org/sdr/FDEA202410171531.md): Doubler · cracked · Oct 17, 2024 · N591FE · Doug MD11F · Wing, Plate/Skin > LEFT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACKED AT STATION XOS 561. LEFT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER AT STATION XOS 561 CRACKED AREA REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. RE - [SDR FDEA202410171530](https://openairdocs.org/sdr/FDEA202410171530.md): Doubler · cracked · Oct 17, 2024 · N591FE · Doug MD11F · Wing, Plate/Skin > RIGHT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACKED AT STATION XOS 696. RIGHT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER AT STATION XOS 696 CRACKED AREA REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. - [SDR FDEA202410161526](https://openairdocs.org/sdr/FDEA202410161526.md): Cargo Track · cracked · Oct 16, 2024 · N591FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > CABIN MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1149, X= 8.5 FOUND CROWN WORN OUT. CABIN MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 1149, X= 8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALL - [SDR FDEA202410161525](https://openairdocs.org/sdr/FDEA202410161525.md): Cargo Track · cracked · Oct 16, 2024 · N591FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1149, X= -27.5Ï¿½ FOUND CROWN WORN OUT. CABIN Ï¿½ MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 1149, X= -27.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALL - [SDR FDEA202410161524](https://openairdocs.org/sdr/FDEA202410161524.md): Cargo Track · cracked · Oct 16, 2024 · N591FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > CABIN MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1149, X= 47.5 FOUND CROWN WORN OUT. CABIN MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 1149, X= 47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 A - [SDR FDEA202410161523](https://openairdocs.org/sdr/FDEA202410161523.md): Cargo Track · cracked · Oct 16, 2024 · N591FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > CABIN MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1010, X= -47.5 FOUND CROWN WORN. CABIN MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 1010, X= -47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALL - [SDR FDEA202410161522](https://openairdocs.org/sdr/FDEA202410161522.md): Doubler · cracked · Oct 16, 2024 · N591FE · Doug MD11F · Wing, Plate/Skin > RIGHT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACKED AT STATION XOS 990. RIGHT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER AT STATION XOS 990 CRACKED AREA REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. - [SDR FDEA202410161521](https://openairdocs.org/sdr/FDEA202410161521.md): Doubler · cracked · Oct 16, 2024 · N591FE · Doug MD11F · Wing, Plate/Skin > RIGHT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACKED AT STATION XOS 628. RIGHT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER AT STATION XOS 628 CRACKED AREA REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. - [SDR FDEA202410161520](https://openairdocs.org/sdr/FDEA202410161520.md): Doubler · cracked · Oct 16, 2024 · N591FE · Doug MD11F · Wing, Plate/Skin > RIGHT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACKED AT STATION XOS 614. RIGHT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER AT STATION XOS 614 CRACKED AREA REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. - [SDR FDEA202410161519](https://openairdocs.org/sdr/FDEA202410161519.md): Cargo Track · worn · Oct 16, 2024 · N591FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 805, X= 8.5Ï¿½ FOUND CROWN WORN. CABIN Ï¿½ MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 805, X= 8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAM - [SDR FDEA202410161518](https://openairdocs.org/sdr/FDEA202410161518.md): Cargo Track · worn · Oct 16, 2024 · N591FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 805, X= -8.5Ï¿½ FOUND CROWN WORN. CABIN Ï¿½ MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 805, X= -8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE D - [SDR FDEA202410161517](https://openairdocs.org/sdr/FDEA202410161517.md): Cargo Track · worn · Oct 16, 2024 · N591FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > CABIN MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1010, X= 27.5 FOUND CROWN WORN. CABIN MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 1010, X= 27.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOW - [SDR FDEA202410161516](https://openairdocs.org/sdr/FDEA202410161516.md): Cargo Track · worn · Oct 16, 2024 · N591FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 6-10, X= 47.5Ï¿½ FOUND CROWN WORN. CABIN Ï¿½ MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 6-10, X= 47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE - [SDR FDEA202410161515](https://openairdocs.org/sdr/FDEA202410161515.md): Cargo Track · worn · Oct 16, 2024 · N591FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > CABIN MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1010, X= 47.5 FOUND CROWN WORN. CABIN MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 1010, X= 47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOW - [SDR FDEA202410161514](https://openairdocs.org/sdr/FDEA202410161514.md): Cargo Track · worn · Oct 16, 2024 · N591FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 6-10, X= 27.5Ï¿½ FOUND CROWN WORN. CABIN Ï¿½ MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 6-10, X= 27.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE - [SDR FDEA202401190089](https://openairdocs.org/sdr/FDEA202401190089.md): Anti-Ice Valve · inoperative · Jan 19, 2024 · N591FE · Doug MD11F · Air Intake Anti/De-Ice System > CLIMBING OUT, WE TURNED ON ALL ANTI-ICE SYSTEMS ENTERING CLOUDS. HAD AN AMBER TAIL ANTI- DISAG WARNING N EIS, FOLLOWED SHORTLY BY LEVEL 2 TAIL A-ICE DISAG. RAN QRH, TURNED OFF SYSTEM AND RETURNED TO DEPARTURE BASE. REPEAT WRITE UP. REMOVED AND REPLACED HO - [SDR FDEA202312031903](https://openairdocs.org/sdr/FDEA202312031903.md): Power Supply · failed · Dec 3, 2023 · N591FE · Doug MD11 · Emergency Lighting > EMER LT BAT 1 LO LEVEL 1 ALERT ON EMERGENCY LIGHTS TEST. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY, REF AMM 33-51-01-4, OPS CHECKS GOOD. A/C OK FOR SERVICE. REMOVED POWER SUPPLY, EMERGENCY EXIT LIGHTS. MFG: GRIMES, P/N 60-4411-5, S/N 0555 - [SDR FDEA202310221787](https://openairdocs.org/sdr/FDEA202310221787.md): Pressure Switch · failed · Oct 22, 2023 · N591FE · Doug MD11F · Escape Slide > R1 DOOR EVAC SLIDE PRESSURE PRESS-TO-TEST INDICATING SYSTEM INOP. REMOVED AND REPLACED REMOTE PRESSURE INDICATOR ASSY. OPS GOOD OK FOR SERVICE - [SDR FDEA202301110069](https://openairdocs.org/sdr/FDEA202301110069.md): Skin · cracked · Jan 11, 2023 · N591FE · Doug MD11F · Wing, Plate/Skin > R/H FIXED LEADING EDGE SKIN HAS A.250 IN. CRACK AT SLAT TRACK #10 CUT OUT AFT I/B CORNER. (MARKED) INSTALLED REPAIR FILLER AND DOUBLER PER SRM 57-40-02-2R FIGURE 201. REPAIR OF WING FIXED LEADING EDGE, LOWER SURFACE AT SLAT TRACK CUTOUT. "MAJOR REPAIR". - [SDR FDEA202212112906](https://openairdocs.org/sdr/FDEA202212112906.md): Skin · cracked · Dec 11, 2022 · N591FE · Doug MD11F · Wing, Plate/Skin > RIGHT FIXED LEADING EDGE SKIN HAS A.250 IN. CRACK AT SLAT TRACK NR 10 CUT OUT AFT INBD CORNER. INSTALLED A REPAIR FILLER AND DOUBLER IAW SRM 57-40-02-2R FIGURE 201. MAJOR REPAIR. - [SDR FDEA202212092899](https://openairdocs.org/sdr/FDEA202212092899.md): Web · corroded · Dec 9, 2022 · N591FE · Doug MD11 · Wing Structure > OVERWING FUEL TANK-STA 1372X=97;DURING CLEANUP/INSPECTION WE FOUND 1 HOLE IN THE WEB CORRODED. THE HOLE IS NOT IN THE CORROSION REPAIR AREA. THE HOLE WAS PART OF THE STRUCTURE REMOVED FOR ACCESSIBILITY TO CORRODED AREA. REPAIRED PER E.A. # 1-5730-T0371173 - [SDR FDEA202211282902](https://openairdocs.org/sdr/FDEA202211282902.md): Support · unknown · Nov 28, 2022 · N591FE · Doug MD11 · Wing, Plate/Skin > FUEL TANK RAIL SUPPORT REQUIRES FABRICATION APB7277-1. TEMPLATE PROVIDED. REF EA 1- 5730-T0371173 R1. 0000329719: MAHER, PATRICK L - 02-DEC-2022 20:28 FABRICATED RAIL SUPPORT REF DAC DWG APB7277. 0000329719: MAHER, PATRICK L - 02-DEC-2022 20:34 RES - [SDR FDEA202211232847](https://openairdocs.org/sdr/FDEA202211232847.md): Stiffener · unknown · Nov 23, 2022 · N591FE · Doug MD11F · Wing Main, Frame Structure > STIFFNER APB 7278-1 REQUIRES FABRICATION. 0003883811: CORDOVA, CARLOS - 27-NOV-2022 07:15 FABRICATED STIFFENER P/N APB7278-1 IAW DOUGLAS DWG APB7278 - [SDR FDEA202211102748](https://openairdocs.org/sdr/FDEA202211102748.md): None · none · Nov 10, 2022 · N591FE · Doug MD11F · Standard Practices/Structures > CTR CARGO COMPT - FRAME AT STA 1661 L48R REQUIRED TO BE SPLIT FOR ACCESS TO LONGERON REPAIR. TOP STRAP OF REPAIR NEEDS TO BE INSTALLED REF SRM 53-00-07-2R NOTE 15-C STEP 1(REF. N1289) INSTALLED STRAP AT FRAME STA 1661 IN BETWEEN L47R AND L48R REF MD11 SRM - [SDR FDEA202211082905](https://openairdocs.org/sdr/FDEA202211082905.md): Skin · corroded · Nov 8, 2022 · N591FE · Doug MD11 · Wing Main, Frame Structure > BUSHING FOR DRAIN HOLE AT CENTER WING UPPER SKIN AT REAR SPA APPROX BETWEEN XCW 101 AND XCW 118 REQUIRES TO BE FABRICATED WITH DIM. AS FOLLOW: DIA = 0.750, HEIGHT = 0.675 FABRICATED BUSHING PER EA 1-5710-T0370445 P3 WINGS - PLATES AND SKIN - CENTER WING - - [SDR FDEA202210282688](https://openairdocs.org/sdr/FDEA202210282688.md): Floorboard · delaminated · Oct 28, 2022 · N591FE · Doug MD11F · Fuselage Floor Panel > MAIN DECK - FLOORBOARD 252BF IS DELAMINATED FABRICATED MAIN CARGO FLOORBOARD 252BF IAW FEDEX DRAWING SRZ-25-005. MAJOR REPAIR - [SDR FDEA202210282681](https://openairdocs.org/sdr/FDEA202210282681.md): Intercostal · cracked · Oct 28, 2022 · N591FE · Doug MD11F · Empennage Structure > INTERCOSTAL P/N AJC 7582-3 IS CRACKED AT AFT UPPER CONRER ACCESED THOUGH PANEL 363 PL. REPAIRED INTERCOSTAL P/N AJC 7582-3 UPPER AFT CORNER REF SRM 55-30-02-2R REPAIR 7 FIGURE 203 AND E.A.#: 1-5530-T0371227 A MAJOR REPAIR. - [SDR FDEA202210282680](https://openairdocs.org/sdr/FDEA202210282680.md): Intercostal · cracked · Oct 28, 2022 · N591FE · Doug MD11F · Empennage Structure > INTERCOSTAL P/N AJC 7582-3 IS CRACKED AT FWD UPPER CORNER ACCESED THOUGH PANEL 363 PL. REPAIRED INTERCOSTAL P/N AJC 7582-3 FWD CORNER REF SRM 55-30-02-2R FIGURE 201 REPAIR 7 - [SDR FDEA202210162673](https://openairdocs.org/sdr/FDEA202210162673.md): Attach Bracket · cracked · Oct 16, 2022 · N591FE · Doug MD11F · Elevator Structure > R/H OUTBOARD ELEVATOR, UPPER OUTBOARD ATTACH BRACKET FOR WRAP-AROUND PANEL 346BB IS BENT/HAS CRACK. REMOVED AND REPLACED ALC8830-8 CLIP, REF DWG ALC8830. - [SDR FDEA202210112639](https://openairdocs.org/sdr/FDEA202210112639.md): Support Angle · corroded · Oct 11, 2022 · N591FE · Doug MD11F · Trailing Edge Flaps > RT INBD TE FLAP, CORROSISON ON PANEL SUPPORT ANGLE AT PANEL LAND FOR 641FB NSTALLED RT INBD TE FLAP FABRICATED TEE ARC0307-4 REF B/P DAC DWG ARC0307 & SRM 51-31- 01-OG. - [SDR FDEA202210112638](https://openairdocs.org/sdr/FDEA202210112638.md): Support Angle · corroded · Oct 11, 2022 · N591FE · Doug MD11F · Trailing Edge Flaps > RT INBD TE FLAP, CORROSISON ON PANEL SUPPORT ANGLE AT PANEL LAND FOR 641GB 0000435071: HARPER, RICHARD R - 21-OCT-2022 19:54 REMOVED AND REPLACED WITH NEW TEE ON RT INBD TE FLAP ARC0307-6 REF B/P DAC DWG ARC0307 & SRM 51-31-01-OG. SEE JPF FOR DETAILS OF RE - [SDR FDEA202210072820](https://openairdocs.org/sdr/FDEA202210072820.md): Skin · corroded · Oct 7, 2022 · N591FE · Doug MD11F · Fuselage Main, Plate/Skin > FABRICATE -5 REPAIR FILLER OVER TANK. FABRICATED -5 REPAIR FILLER ACCORDING TO EA 1-5710-T0370445. MAJOR REPAIR. ORIG SUB DATE: 11/18/2022 - [SDR FDEA202210072821](https://openairdocs.org/sdr/FDEA202210072821.md): Fuel Tank · corroded · Oct 7, 2022 · N591FE · Doug MD11F · Fuel Storage > FABRICATE -4 REPAIR FILLER OVER TANK. FABRICATED IN TANK WING -4 REPAIR FILLER IAW EA 1-5710-T0370445. MAJOR REPAIR. - [SDR FDEA202210062504](https://openairdocs.org/sdr/FDEA202210062504.md): Skin · dented · Oct 6, 2022 · N591FE · Doug MD11F · Trailing Edge Flaps > L/H I/B FLAP BOTTOM SKIN HAS A DENT. CUT OUT GOUGE FROM L/H INBD FLAP BOTTOM SKIN, INSTALLED EXTERNAL DOUBLER PER SRM 57-00-01-2R FIG 201 SHEET 2 "MAJOR REPAIR" - [SDR FDEA202210062502](https://openairdocs.org/sdr/FDEA202210062502.md): Tripler · damaged · Oct 6, 2022 · N591FE · Doug MD11F · Fuselage Main, Plate/Skin > FABRICATE IN TANK CENTER WING REPAIR TRIPLER. REPAIRED PER EA 1-5710-T0370445 Next page: https://openairdocs.org/aircraft/N591FE/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 = 'N591FE' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N591FE/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.