# Service difficulty reports: N623FE A list on [N623FE](https://openairdocs.org/aircraft/N623FE.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 5 · 246 reports - [SDR FDEA202402040135](https://openairdocs.org/sdr/FDEA202402040135.md): Control Unit · faulted · Feb 4, 2024 · N623FE · Doug MD11F · Battery/Charger System > ENROUTE LVL 1 BAT DISCHARGING ALERT. ALERT CAME ON MOMENTARILY SEVERAL TIMES AND THEN ALERT WAS CONTINUOUSLY ON AND OCCASIONALLY OFF REMAINDER OF FLIGHT. DECLARED EMERGENCY AND DIVERTED TO KORD. REMOVED AND REPLACED EPCU AS PRECAUTION PER AMM REF 24-0 - [SDR FDEA202302020201](https://openairdocs.org/sdr/FDEA202302020201.md): Slide · failed · Feb 2, 2023 · N623FE · Doug MD11F · Escape Slide > L1 DOOR SLIDE PARTIALLY DEPLOYED WHILE TROUBLESHOOTING NR0039 (L1 DOOR INOP). REMOVED AND REPLACED L1 DOOR SLIDE ASSEMBLY. REF MD11 AMM 25-61-01-4. SEE JPF FOR WORK ACCOMPLISHED. - [SDR FDEA202208161985](https://openairdocs.org/sdr/FDEA202208161985.md): Power Supply · inoperative · Aug 16, 2022 · N623FE · Doug MD11F · Emergency Lighting > ON PREFLIGHT OF EMER LTS, GOT LVL 1 ALERT EMER LT BAT 1 LO. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY POWER SUPPLY. OPERATIONAL CHECK GOOD. - [SDR FDEA202206061386](https://openairdocs.org/sdr/FDEA202206061386.md): None · none · Jun 6, 2022 · N623FE · Doug MD11 · Fuel Indicating System > PDIS 623 28-40 6983 06JUN22 CDG OPEN U LOGPAGES:385994 ON DESCENT FLT 200 RECEIVED LEVEL 2 FUEL QUANTITY FAULT TANK 1/3 FUEL QUANTITY LO - NOW W/ ARRIVED AT CDG DECLARED EMERGENCY FUEL PER QRH ADVISED AS A VALID ALERT. PERFORMED FUEL MIGRAT - [SDR FDEA202204120928](https://openairdocs.org/sdr/FDEA202204120928.md): Hinge · worn · Apr 12, 2022 · N623FE · Doug MD11F · Cargo/Baggage Doors > MAIN DECK CARGO DOOR UPPER EDGE, ATTACHED AFT HINGE FITTING #7 (PART NUMBER:ACA 7223-515) LOBES #12 TO #17 FOUND OUT OF TOLERANCE. MAIN DECK CARGO DOOR UPPER EDGE, ATTACHED AFT HINGE FITTING #7 (PART NUMBER:ACA 7223-515) LOBES #12 TO #17 REWORKED AND FOU - [SDR FDEA202204120927](https://openairdocs.org/sdr/FDEA202204120927.md): Support · worn · Apr 12, 2022 · N623FE · Doug MD11F · Cargo/Baggage Doors > MAIN DECK CARGO DOOR, UPPER EDGE ATTACHED FORWARD (#1) HINGE FITTING (PART NUMBER:ACA 7332-1) ALL 9 LOBES FOUND OUT OF TOLERANCE. MAIN DECK CARGO DOOR, UPPER EDGE ATTACHED FORWARD (#1) HINGE FITTING (PART NUMBER:ACA 7332-1) ALL 9 LOBES REWORKED AND FOUND - [SDR FDEA202204060871](https://openairdocs.org/sdr/FDEA202204060871.md): Longeron · cracked · Apr 6, 2022 · N623FE · Doug MD11F · Fuselage Main, Structure > CENTER CARGO - STATION 1581 TO STATION 1601 LONGERON 38 RIGHT SUSPECT CRACK. CENTER CARGO - STATION 1581 TO STATION 1601 LONGERON 38 RIGHT REPAIR CARRIED OUT AS PER SRM 53-00-05-2R FIGURE 202 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100. - [SDR FDEA202204040827](https://openairdocs.org/sdr/FDEA202204040827.md): Skin · cracked · Apr 4, 2022 · N623FE · Doug MD11F · Fuselage Main, Plate/Skin > EMPENNAGE - AFT FUSELAGE RIGHT HAND SIDE ON TOP OF APU EXHAUST DOOR AREA APPROXIMATE STATION 2140 LONGERON 36 RIGHT FOUND SKIN CRACK 2.2 INCH. EMPENNAGE -AFT FUSELAGE RIGHT HAND SIDE ON TOP OF APU EXHAUST DOOR AREA APPROXIMATE STATION 2140 LONGERON 36 RIGH - [SDR FDEA202203290738](https://openairdocs.org/sdr/FDEA202203290738.md): Seat Track · corroded · Mar 29, 2022 · N623FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT FLOOR, SEAT TRACK ALONG X = - 8.5 STATION 1641 FOUND WITH CORROSION AT FLANGE. MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK FLANGE AT STATION 1641 X = -8.5, CORROSION REMOVED AS PER SRM 51-21-01-0G AND EXCEED LIMIT AS PER SRM - [SDR FDEA202203290737](https://openairdocs.org/sdr/FDEA202203290737.md): Frame · dented · Mar 29, 2022 · N623FE · Doug MD11F · Fuselage Main, Frame > MAIN DECK CARGO COMPARTMENT LEFT HAND STATION 1761 FRAME FLANGE FOUND DENTED AT LONGERON 12 LEFT LOCATION. FRAME FLANGE REPAIRED AS PER SRM 53-00-07-2R FIGURE 201 REPAIR 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. I - [SDR FDEA202203220636](https://openairdocs.org/sdr/FDEA202203220636.md): Doubler · unknown · Mar 22, 2022 · N623FE · Doug MD11F · Wing, Plate/Skin > AGING AIRCRAFT - EXISTING RIB DOUBLER REPAIR FOUND AT RIGHT HAND WING LEADING EDGE CAVITY STATION XOS= 789. - [SDR FDEA202203220635](https://openairdocs.org/sdr/FDEA202203220635.md): Doubler · unknown · Mar 22, 2022 · N623FE · Doug MD11F · Wing, Plate/Skin > AGING AIRCRAFT - EXISTING RIB DOUBLER REPAIR FOUND AT RIGHT HAND WING LEADING EDGE CAVITY STATION XOS= 667. - [SDR FDEA202203220634](https://openairdocs.org/sdr/FDEA202203220634.md): Doubler · unknown · Mar 22, 2022 · N623FE · Doug MD11F · Wing, Plate/Skin > AGING AIRCRAFT - EXISTING DOUBLER REPAIR FOUND AT RIGHT HAND WING LOWER SKIN LEADING EDGE CAVITY STATION XOS= 584 TO XOS= 610. - [SDR FDEA202203220633](https://openairdocs.org/sdr/FDEA202203220633.md): Doubler · unknown · Mar 22, 2022 · N623FE · Doug MD11F · Wing, Plate/Skin > AGING AIRCRAFT - EXISTING RIB DOUBLER REPAIR FOUND AT LEFT HAND WING LEADING EDGE CAVITY STATION XOS= 789. EVALUATED AND FOUND DOUBLER REPLACED BY FABRICATION IN ACCORDANCE WITH SRM 51-33-01-0G AND DOUGLAS DRAWING ARB3954 REVISION K. EO 1-5100-7-5001 B7 P - [SDR FDEA202203220632](https://openairdocs.org/sdr/FDEA202203220632.md): Doubler · unknown · Mar 22, 2022 · N623FE · Doug MD11F · Wing, Plate/Skin > AGING AIRCRAFT - EXISTING RIB DOUBLER REPAIR FOUND AT LEFT HAND WING LEADING EDGE CAVITY STATION XOS= 667. EVALUATED AND FOUND DOUBLER REPLACED BY FABRICATION IN ACCORDANCE WITH SRM 51-33-01-0G AND DOUGLAS DRAWING ARB3954 REVISION K. EO 1-5100-7-5001 B7 P - [SDR FDEA202203220631](https://openairdocs.org/sdr/FDEA202203220631.md): Former · unknown · Mar 22, 2022 · N623FE · Doug MD11F · Wing, Plate/Skin > AGING AIRCRAFT - EXISTING FORMER REPAIR FOUND AT LEFT HAND WING LEADING EDGE CAVITY STATION XOS= 559. EVALUATED AND FOUND FORMER REPLACED BY FABRICATION IN ACCORDANCE WITH SRM 51- 33-01-0G AND DOUGLAS DRAWING ARB1162 REVISION S. EO 1-5100-7-5001 B7 PART 1, - [SDR FDEA202203210620](https://openairdocs.org/sdr/FDEA202203210620.md): Track · cracked · Mar 21, 2022 · N623FE · Doug MD11 · Fuselage Floor Panel > MAIN DECK CARGO COMPARTMENT FLOOR, SEAT TRACK ALONG X = 47.5 CROWN FOUND CRACKED OFF AT STATION 755. MAIN DECK CARGO COMPARTMENT FLOOR CRACKED SEAT TRACK AT STATION 755 X = 47.5 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 725 TO EXISTING SPL - [SDR FDEA202203210619](https://openairdocs.org/sdr/FDEA202203210619.md): Seat Track · cracked · Mar 21, 2022 · N623FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT FLOOR, SEAT TRACK ALONG X = 8.5 CROWN AT STATION 1541 FOUND CRACKED. MAIN DECK CARGO COMPARTMENT FLOOR, CRACKED SEAT TRACK AT STATION 1541 X = 8.5 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM EXISTING SPLICE STATION 5-12 - [SDR FDEA202203200606](https://openairdocs.org/sdr/FDEA202203200606.md): Frame · cracked · Mar 20, 2022 · N623FE · Doug MD11F · Fuselage Main, Structure > AGING AIRCRAFT - EXISTING REPAIR AT MAIN DECK CARGO FRAME STATION 1781 LONGERON 12 RIGHT HAND TO 13 RIGHT HAND. EXISTING REPAIR AT MAIN DECK CARGO FRAME AT ACTUAL CORRECT STATION 1781 LONGERON 11 RIGHT HAND TO 14 RIGHT HAND EVALUATED AND FOUND FRAME CRACK - [SDR FDEA202203170543](https://openairdocs.org/sdr/FDEA202203170543.md): Doubler · cracked · Mar 17, 2022 · N623FE · Doug MD11 · Wing, Plate/Skin > RIGHT HAND WING - LEADING EDGE CAVITY BEADED DOUBLER AT STATION XOS = 696 FOUND CRACK. RIGHT HAND WING LEADING EDGE CAVITY DOUBLER AT STATION XOS 696 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 1 - [SDR FDEA202203170542](https://openairdocs.org/sdr/FDEA202203170542.md): Doubler · cracked · Mar 17, 2022 · N623FE · Doug MD11 · Wing, Plate/Skin > RIGHT HAND WING - LEADING EDGE CAVITY BEADED DOUBLER AT STATION XOS = 737 FOUND CRACK. RIGHT HAND WING LEADING EDGE CAVITY DOUBLER AT STATION XOS 737 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 1 - [SDR FDEA202203170540](https://openairdocs.org/sdr/FDEA202203170540.md): Doubler · cracked · Mar 17, 2022 · N623FE · Doug MD11 · Wing, Plate/Skin > RIGHT HAND WING - LEADING EDGE CAVITY BEADED DOUBLER AT STATION XOS = 793 FOUND CRACK. RIGHT HAND WING LEADING EDGE CAVITY DOUBLER AT STATION XOS 793 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 1 - [SDR FDEA202109042217](https://openairdocs.org/sdr/FDEA202109042217.md): Warning Message · false indication · Sep 4, 2021 · N623FE · Doug MD11F · Central Warning > ENROUTE RECEIVED A LEVEL 2 ALERT, FUEL QTY/USED CHK, AND POSSIBLE FUEL LEAK MESSAGE. COMPLIED WITH QRH. WE SHOWED A DISCREPANCY IN FUEL OF 5000 LBS AND WHEN DIVERTED BECAUSE OF POSSIBLE FUEL LEAK IT WAS 7500 LBS DISCREPANCY. IT WAS UNUSUAL THAT FUEL WAS - [SDR FDEA202101220179](https://openairdocs.org/sdr/FDEA202101220179.md): Probe · failed · Jan 22, 2021 · N623FE · Doug MD11F · Altimeter, Barometric/Encoder > PASSING FL270, ALL DATA DROPPED OFF PFD (AUTOPILOTS, AUTOTHOTTLES, NAV DATA, FLIGHT DIRECTOR ETC), RAN QRH TO STABILIZE AIRPLANE, PER QRH SWITCHED CADC 1 TO AUX & DATA RETURNED. AIR TURNBACK TO ONT, HAD IDENTICAL FAILURE USING AUX. DATA RETURNED ON ITS OWN - [SDR FDEA2020041760751](https://openairdocs.org/sdr/FDEA2020041760751.md): Support Fitting · damaged · Apr 16, 2020 · N623FE · Doug MD11F · Fuselage Main, Attach Fittings > FUSELAGE Ï¿½ CENTER STRUCTURE INSTALLATION Ï¿½ WHILE ACCOMPLISHING INSPECT/REPLACE HI-LOKS ON LEFT HAND INBOARD FLAP SUPPORT FITTING AT YIFH 61 FOUND THE EXISTING INSTALLED HI-LOKS EXCEEDS LIMITS AS PER WORKCARD E1-5310-7-5004 PART 5 STEP 13. COMPLIED WITH - [SDR FDEA2020041760750](https://openairdocs.org/sdr/FDEA2020041760750.md): Support Fitting · damaged · Apr 16, 2020 · N623FE · Doug MD11F · Fuselage Main, Attach Fittings > FUSELAGE Ï¿½ CENTER STRUCTURE INSTALLATION Ï¿½ WHILE ACCOMPLISHING INSPECT/REPLACE HI-LOKS ON RIGHT HAND INBOARD FLAP SUPPORT FITTING AT YIFH 61 FOUND THE EXISTING INSTALLED HI-LOKS EXCEEDS LIMITS AS PER WORKCARD E1-5310-7-5004 PART 6 STEP 13. COMPLIED WIT - [SDR FDEA2020041740745](https://openairdocs.org/sdr/FDEA2020041740745.md): Hinge Bracket · corroded · Apr 14, 2020 · N623FE · Doug MD11F · Wing, Control Surface Attach Fittings > RIGHT HAND WING, WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT HAND WING, WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE (NR4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57 - [SDR FDEA2020041740744](https://openairdocs.org/sdr/FDEA2020041740744.md): Hinge Bracket · corroded · Apr 14, 2020 · N623FE · Doug MD11F · Wing, Control Surface Attach Fittings > RIGHT HAND WING, WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT HAND WING, WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE (NR4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-4 - [SDR FDEA2020041740743](https://openairdocs.org/sdr/FDEA2020041740743.md): Hinge Bracket · corroded · Apr 14, 2020 · N623FE · Doug MD11F · Wing, Control Surface Attach Fittings > RIGHT HAND WING, WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT RIGHT HAND WING, WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (NR3 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-44-07. REPAIR BUSHING FABRICATE - [SDR FDEA2020041740742](https://openairdocs.org/sdr/FDEA2020041740742.md): Hinge Bracket · corroded · Apr 14, 2020 · N623FE · Doug MD11F · Wing, Control Surface Attach Fittings > LEFT HAND WING, WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT HAND WING, WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE (NR4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-4 - [SDR FDEA2020041740741](https://openairdocs.org/sdr/FDEA2020041740741.md): Hinge Bracket · corroded · Apr 14, 2020 · N623FE · Doug MD11F · Wing, Control Surface Attach Fittings > LEFT HAND WING, WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT HAND WING, WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE (NR4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-44 - [SDR FDEA2020041740740](https://openairdocs.org/sdr/FDEA2020041740740.md): Hinge Bracket · corroded · Apr 14, 2020 · N623FE · Doug MD11F · Wing, Control Surface Attach Fittings > LEFT HAND WING, WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT LEFT HAND WING, WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (NR3 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-44-07. REPAIR BUSHING FABRICATED - [SDR FDEA202004100729](https://openairdocs.org/sdr/FDEA202004100729.md): Door Frame · cracked · Apr 10, 2020 · N623FE · Doug MD11F · Air Conditioning Doors > FUSELAGE - # 2 AIR - CONDITIONING COMPARTMENT DOOR INTERIOR UPPER EDGE FOUND CRACKED BETWEEN STATION YFAD -0.437 AND YFAD -12.422 FUSELAGE - # 2 AIR - CONDITIONING COMPARTMENT DOOR INTERIOR UPPER EDGE CRACKED FRAME BETWEEN STATION YFAD -0.437 AND YFAD -12. - [SDR FDEA202004080722](https://openairdocs.org/sdr/FDEA202004080722.md): Support Fitting · corroded · Apr 8, 2020 · N623FE · Doug MD11F · Trailing Edge Flaps > RIGHT HAND WING - OUTBOARD FLAP VANE # 5 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSION CORROSION AT RIGHT HAND WING - OUTBOARD FLAP VANE # 5 SUPPORT FITTING ECCENTRIC HOLE BORE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02- - [SDR FDEA202004080721](https://openairdocs.org/sdr/FDEA202004080721.md): Support Fitting · corroded · Apr 8, 2020 · N623FE · Doug MD11F · Trailing Edge Flaps > RIGHT HAND WING - OUTBOARD FLAP VANE # 4 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSION CORROSION AT RIGHT HAND WING - OUTBOARD FLAP VANE # 4 SUPPORT FITTING ECCENTRIC HOLE BORE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02- - [SDR FDEA202004080720](https://openairdocs.org/sdr/FDEA202004080720.md): Support Fitting · corroded · Apr 8, 2020 · N623FE · Doug MD11F · Trailing Edge Flaps > RIGHT HAND WING OUTBOARD FLAP VANE NR 2 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSION. SUPPORT FITTING REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R REPAIR 5 FIGURE 201. OVERSIZED ECCENTRIC BUSHING FABRICATED BY MACHINING AS PER SRM - [SDR FDEA202004060702](https://openairdocs.org/sdr/FDEA202004060702.md): Hinge Bracket · corroded · Apr 6, 2020 · N623FE · Doug MD11F · Wing, Control Surface Attach Fittings > RIGHT HAND WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE SURFACE FOUND CORROSION CORROSION AT RIGHT HAND WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-07. REPAIR EVALUATED - [SDR FDEA2020040650699](https://openairdocs.org/sdr/FDEA2020040650699.md): Hinge Bracket · corroded · Apr 5, 2020 · N623FE · Doug MD11F · Wing, Control Surface Attach Fittings > LEFT HAND WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE SURFACE FOUND CORROSION CORROSION AT LEFT HAND WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-07. REPAIR EVALUATED A - [SDR FDEA2020040650696](https://openairdocs.org/sdr/FDEA2020040650696.md): Skin · cracked · Apr 5, 2020 · N623FE · Doug MD11F · Wing, Plate/Skin > 03EA FASTENER HOLES #30, #31, #32 FOUND WITH CRACK INDICATION DURING ACCOMPLISHMENT OF OPEN-HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT RIGHT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS = 690 AND STATION XORS = 700. REPAIR CARRIED OUT - [SDR FDEA2020040650695](https://openairdocs.org/sdr/FDEA2020040650695.md): Doubler · cracked · Apr 5, 2020 · N623FE · Doug MD11F · Wing, Plate/Skin > LEFT HAND WING FIXED LEADING EDGE COMPARTMENT AT APPROXIMATELY STATION XOS 794 FOUND BEADED DOUBLER CRACKED. REPAIR CARRIED OUT AT LEFT HAND WING FIXED LEADING EDGE COMPARTMENT AT APPROXIMATELY STATION XOS 794 DOUBLER AS PER SRM 57-40-02-2R FIGURE 203 REPA - [SDR FDEA2020040650694](https://openairdocs.org/sdr/FDEA2020040650694.md): Doubler · cracked · Apr 5, 2020 · N623FE · Doug MD11F · Wing, Plate/Skin > LEFT HAND WING FIXED LEADING EDGE COMPARTMENT AT APPROXIMATELY STATION XOS 764 FOUND BEADED DOUBLER CRACKED. REPAIR CARRIED OUT AT LEFT HAND WING FIXED LEADING EDGE COMPARTMENT AT APPROXIMATELY STATION XOS 764 DOUBLER AS PER SRM 57-40-02-2R FIGURE 203 REPA - [SDR FDEA2020040650693](https://openairdocs.org/sdr/FDEA2020040650693.md): Former · cracked · Apr 5, 2020 · N623FE · Doug MD11F · Wing, Rib/Bulkhead > LEFT HAND WING FIXED LEADING EDGE COMPARTMENT AT APPROXIMATELY STATION XOS 993 FOUND FORMER CRACKED. CRACKED FORMER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED FORMER PER DOUGLAS DRAWING ARB 1164 REVISION M. INSTALLED FABRICATED FORMER AT LEFT HAND WIN - [SDR FDEA2020040650692](https://openairdocs.org/sdr/FDEA2020040650692.md): Angle · cracked · Apr 5, 2020 · N623FE · Doug MD11F · Wing Miscellaneous Structure > LEFT HAND WING FIXED LEADING EDGE COMPARTMENT AT APPROXIMATELY STATION XOS 1084 FOUND ANGLE CRACKED. CRACKED ANGEL REMOVED AS PER SRM 51-31-01-0G AND FABRICATED ANGLE AS PER DOUGLAS DRAWING ARB 2920 REVISION BB. INSTALLED FABRICATED ANGLE AT LEFT HAND WI - [SDR FDEA2020040650691](https://openairdocs.org/sdr/FDEA2020040650691.md): Former · cracked · Apr 5, 2020 · N623FE · Doug MD11F · Wing, Rib/Bulkhead > LEFT HAND WING FIXED LEADING EDGE COMPARTMENT AT APPROXIMATELY STATION XOS 1025 FOUND FORMER CRACKED. CRACKED FORMER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED FORMER AS PER DOUGLAS DRAWING ARB 2920 REVISION BB. INSTALLED FABRICATED FORMER AT LEFT HAND - [SDR FDEA2020040640688](https://openairdocs.org/sdr/FDEA2020040640688.md): Hinge Fitting · corroded · Apr 4, 2020 · N623FE · Doug MD11F · Trailing Edge Flaps > LEFT HAND WING - FLAP SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT HOLE OUTBOARD LUG HOLE BORE FOUND CORRSION. CORROSION AT LEFT HAND WING - FLAP SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT HOLE OUTBOARD LUG HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 C - [SDR FDEA2020040640687](https://openairdocs.org/sdr/FDEA2020040640687.md): Hinge Fitting · corroded · Apr 4, 2020 · N623FE · Doug MD11F · Trailing Edge Flaps > LEFT HAND WING - FLAP SIDE OUTBOARD FLAP INBOARD HINGE PIVOT HOLE INBOARD LUG HOLE BORE FOUND CORRSION. CORROSION AT LEFT HAND WING - FLAP SIDE OUTBOARD FLAP INBOARD HINGE PIVOT HOLE INBOARD LUG HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 5 - [SDR FDEA202004030671](https://openairdocs.org/sdr/FDEA202004030671.md): Hinge Bracket · corroded · Apr 3, 2020 · N623FE · Doug MD11F · Trailing Edge Flaps > LEFT HAND WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE OUTBOARD LUG HOLE SURFACE FOUND CORROSION. CORROSION AT LEFT HAND WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE OUTBOARD LUG HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD- - [SDR FDEA202004030670](https://openairdocs.org/sdr/FDEA202004030670.md): Hinge Bracket · corroded · Apr 3, 2020 · N623FE · Doug MD11F · Trailing Edge Flaps > LEFT HAND WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE INBOARD LUG HOLE SURFACE FOUND CORROSION. CORROSION AT LEFT HAND WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE INBOARD LUG HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 - [SDR FDEA202004030669](https://openairdocs.org/sdr/FDEA202004030669.md): Hinge Bracket · corroded · Apr 3, 2020 · N623FE · Doug MD11F · Trailing Edge Flaps > LEFT HAND WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT HAND WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE OUTBOARD LUG HOLE BORE (A AND B HOLE) REWORKED AND FOUND EXCEED LIMIT A - [SDR FDEA202004030668](https://openairdocs.org/sdr/FDEA202004030668.md): Hinge Bracket · corroded · Apr 3, 2020 · N623FE · Doug MD11F · Trailing Edge Flaps > LEFT HAND WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT HAND WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE INBOARD LUG HOLE BORE (G AND F HOLE) REWORKED AND FOUND EXCEED LIMIT AS Next page: https://openairdocs.org/aircraft/N623FE/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 = 'N623FE' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N623FE/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.