# Service difficulty reports: N572FE A list on [N572FE](https://openairdocs.org/aircraft/N572FE.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 · 258 reports - [SDR FDEA202506010827](https://openairdocs.org/sdr/FDEA202506010827.md): Lamp · failed · Jun 1, 2025 · N572FE · Doug MD11F · Landing Gear Position and Warning > NOSE GEAR GREEN LIGHT ON FORWARD PANEL INOP RELAMPED NOSE LANDING GEAR DOWN INDICATING BULB PER AMM 33-11-17-2. OPS CHECK GOOD. A/C OK FOR SERVICE. - [SDR FDEA202505180766](https://openairdocs.org/sdr/FDEA202505180766.md): Test Switch · misinstalled · May 18, 2025 · N572FE · Doug MD11F · Escape Slide > DURING PREFLIGHT, THE R1 PRESS TO TEST LIGHT DID NOT ILLUMINATE ON THE DOOR WHEN PRESSED. RELEASED FOR SERVICE PER MEL: 25-61-02 CATEGORY C. FOUND PUSH TO TEST SWITCH JAMMED IN TEST POSTION. REMOVED LAMP HOUSING FROM INDICATOR LAMP ASSY AND FOUND TO HAV - [SDR FDEA202502270301](https://openairdocs.org/sdr/FDEA202502270301.md): Rib · cracked · Feb 27, 2025 · N572FE · Doug MD11F · Leading Edge Devices > RIGHT WING, LEADING EDGE SLAT ASSEMBLY #5, THIRD FROM INBOARD EDGE, STATION XOS 670.495 RIB FOUND WITH CRACK, 0.3 INCH. RIGHT WING, LEADING EDGE SLAT ASSEMBLY #5, THIRD FROM INBOARD EDGE, STATION XOS 670.495 CRACKED RIB REPAIRED AS PER EA # 1-5750-T0382398 - [SDR FDEA202502270300](https://openairdocs.org/sdr/FDEA202502270300.md): Rib · cracked · Feb 27, 2025 · N572FE · Doug MD11F · Leading Edge Devices > RIGHT WING, LEADING EDGE SLAT ASSEMBLY #5, SECOND FROM INBOARD EDGE, STATION XOS 665.296 RIB FOUND WITH CRACK, 0.4 INCH. RIGHT WING, LEADING EDGE SLAT ASSEMBLY #5, SECOND FROM INBOARD EDGE, STATION XOS 665.296 CRACKED RIB REPAIRED AS PER EA # 1-5750-T03823 - [SDR FDEA202502250291](https://openairdocs.org/sdr/FDEA202502250291.md): Frame · dented · Feb 25, 2025 · N572FE · Doug MD11F · Fuselage Main, Frame > CABIN - LEFT HAND FRAME AT STATION 1641 LONGERON S 12L FOUND DENT. CABIN - DENT AT LEFT HAND FRAME STATION 1641 LONGERON 12 LEFT, REPAIRED AS PER MD-11 SRM 53-00-07-2R FIGURE 201 REPAIR 2. REPETITIVE INSPECTION REQUIRED - INITIAL AT 14,500 CYCLES AND REP - [SDR FDEA202502250290](https://openairdocs.org/sdr/FDEA202502250290.md): Seat Track · worn · Feb 25, 2025 · N572FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1239 X = 8.5 FOUND CROWN WORN. MAIN DECK - AT SEAT TRACK STATION 1239, 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 TRA - [SDR FDEA202502250289](https://openairdocs.org/sdr/FDEA202502250289.md): Seat Track · worn · Feb 25, 2025 · N572FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1425 X = 8.5 FOUND CROWN WORN. MAIN DECK - AT SEAT TRACK STATION 1425, 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 TRA - [SDR FDEA202502250288](https://openairdocs.org/sdr/FDEA202502250288.md): Seat Track · worn · Feb 25, 2025 · N572FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1425 X = 47.5 FOUND CROWN WORN. MAIN DECK - AT SEAT TRACK STATION 1425, 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 T - [SDR FDEA202502250287](https://openairdocs.org/sdr/FDEA202502250287.md): Seat Track · worn · Feb 25, 2025 · N572FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1425 X = - 8.5 FOUND CROWN WORN. MAIN DECK - AT SEAT TRACK STATION 1425, 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 - [SDR FDEA202502250286](https://openairdocs.org/sdr/FDEA202502250286.md): Seat Track · worn · Feb 25, 2025 · N572FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 879 X = 8.5 FOUND CROWN WORN. MAIN DECK - AT 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 ALLOABLE DAMAGE 1. CROWN WORN SEAT TRACK RE - [SDR FDEA202502250285](https://openairdocs.org/sdr/FDEA202502250285.md): Seat Track · worn · Feb 25, 2025 · N572FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1541 X = 47.5 FOUND CROWN WORN. MAIN DECK Ï¿½ AT STATION 1541, X = 47.5 WORN SEAT TRACK CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT - [SDR FDEA202502250284](https://openairdocs.org/sdr/FDEA202502250284.md): Seat Track · worn · Feb 25, 2025 · N572FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1256 X = - 8.5 FOUND CROWN WORN. MAIN DECK - AT SEAT TRACK STATION 1256, 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 - [SDR FDEA202502250283](https://openairdocs.org/sdr/FDEA202502250283.md): Seat Track · worn · Feb 25, 2025 · N572FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1256 X = -27.5 FOUND CROWN WORN. MAIN DECK - AT SEAT TRACK STATION 1256, 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 SEA - [SDR FDEA202502250282](https://openairdocs.org/sdr/FDEA202502250282.md): Seat Track · worn · Feb 25, 2025 · N572FE · Doug MD11F · Fuselage Floor Panel > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1545 X = -47.5 FOUND CROWN WORN. MAIN DECK - AT SEAT TRACK STATION 1545, 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 S - [SDR FDEA202502250281](https://openairdocs.org/sdr/FDEA202502250281.md): Seat Track · worn · Feb 25, 2025 · N572FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1009 X = 27.5 FOUND CROWN WORN. MAIN DECK - AT SEAT TRACK STATION 1009, 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 T - [SDR FDEA202502250280](https://openairdocs.org/sdr/FDEA202502250280.md): Seat Track · worn · Feb 25, 2025 · N572FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 6-10 X = -75.5 FOUND CROWN WORN. MAIN DECK Ï¿½ 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 DAMAGE 1. CROWN WORN SE - [SDR FDEA202502250279](https://openairdocs.org/sdr/FDEA202502250279.md): Seat Track · worn · Feb 25, 2025 · N572FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1239 X = -75.25 FOUND CROWN WORN. MAIN DECK - AT SEAT TRACK STATION 1239, X = - 75.25 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN S - [SDR FDEA202502250277](https://openairdocs.org/sdr/FDEA202502250277.md): Skin · cracked · Feb 25, 2025 · N572FE · Doug MD11F · Wing Main, Frame Structure > RIGHT WING LEADING EDGE, SLAT ASSEMBLY NUMBER 5 UNDERSIDE COVE PANEL INBOARD EDGE FOUND WITH CRACKLINE FROM RIVETED HOLE, AT STATION XOS 660.537. RIGHT WING LEADING EDGE, SLAT ASSEMBLY NUMBER 5 UNDERSIDE COVE PANEL INBOARD EDGE AT STATION XOS 660.537 REPAI - [SDR FDEA202502250276](https://openairdocs.org/sdr/FDEA202502250276.md): Skin · chafed · Feb 25, 2025 · N572FE · Doug MD11F · Standard Practices/Structures > FORWARD CARGO DOOR FUSELAGE CUTOUT FORWARD LOWER AREA FOUND EXISTING REPAIR CHAFE AT STATION 889. EXISTING CHAFFED REPAIR DOUBLERS AT FORWARD CARGO DOOR FUSELAGE CUTOUT FORWARD LOWER AREA AT STATION 889 REMOVED AS PER MD-11 SRM 51-33-01-0G. REPAIR CARRIE - [SDR FDEA202502210266](https://openairdocs.org/sdr/FDEA202502210266.md): Seat Track · worn · Feb 21, 2025 · N572FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 5-10 X = 27.5 FOUND CROWN WORN. MAIN DECK Ï¿½ AT SEAT TRACK STATION 5-10 X = 27.5 CROWN WORN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT - [SDR FDEA202502210265](https://openairdocs.org/sdr/FDEA202502210265.md): Seat Track · worn · Feb 21, 2025 · N572FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 5-10 X = 47.5 FOUND CROWN WORN. MAIN DECK Ï¿½ AT SEAT TRACK STATION 5-10 X = 47.5 CROWN WORN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT - [SDR FDEA202502210264](https://openairdocs.org/sdr/FDEA202502210264.md): Seat Track · worn · Feb 21, 2025 · N572FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1169 X = 47.5 FOUND CROWN WORN. MAIN DECK Ï¿½ AT SEAT TRACK STATION 1169, X = 47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. WORN CROWN SEAT - [SDR FDEA202502210262](https://openairdocs.org/sdr/FDEA202502210262.md): Seat Track · worn · Feb 21, 2025 · N572FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1169 X = -8.5 FOUND CROWN WORN. MAIN DECK Ï¿½ 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 - [SDR FDEA202502210261](https://openairdocs.org/sdr/FDEA202502210261.md): Seat Track · worn · Feb 21, 2025 · N572FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 829 X = 8.5 FOUND CROWN WORN. MAIN DECK Ï¿½ AT SEAT TRACK STATION 829, 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 - [SDR FDEA202502210260](https://openairdocs.org/sdr/FDEA202502210260.md): Seat Track · worn · Feb 21, 2025 · N572FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 849 X = -8.5 FOUND CROWN WORN. MAIN DECK Ï¿½ AT SEAT TRACK STATION 849, 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 TRA - [SDR FDEA202502010164](https://openairdocs.org/sdr/FDEA202502010164.md): Coupler · failed · Feb 1, 2025 · N572FE · Doug MD11F · Communications System Wiring > HF2 WILL NOT ALLOW FREQUENCY CHANGES NOR TUNE ANYWHERE. FAIL DISPLAYED IN FREQUENCY WINDOW. CFDS HF2 FAULT, CODE 231114 HF2/COAX. EMERGENCY DECLARED. TUNED HF 2 TO 15MHZ UTC CLOCK FREQ, RECEIVED AUDIO BUT VERY WEAK, AFTER SEVERAL ATTEMPTS, NO LONGER RECEIV - [SDR FDEA202501310158](https://openairdocs.org/sdr/FDEA202501310158.md): Warning Message · false activation · Jan 31, 2025 · N572FE · Doug MD11F · Emergency Lighting > RECEIVED 'BAT 1 LO' ALERT DURING EMERGENCY LIGHT TEST. PERFORMED SUCESSFUL EMERGENCY LIGHTING ADJ/TEST PROCEDURE IAW AMM 33-50-00-5, SYSTEM OK FOR SERVICE. - [SDR FDEA202501260137](https://openairdocs.org/sdr/FDEA202501260137.md): Warning Message · illuminated · Jan 26, 2025 · N572FE · Doug MD11F · Emergency Lighting > RECEIVED AN EMER LT BAT 1 LO ALERT. PERFORMED FUNCTIONAL TEST OF THE EMERGENCY LIGHTING SYSTEM AS REQUIRED PER M/M 33-50-00-5. 'EMER LT BAT 1 LO' DID NOT SHOW UP. OPS CHECKED NORMAL. OK FOR SERVICE. - [SDR FDEA202407151015](https://openairdocs.org/sdr/FDEA202407151015.md): Slide · dislodged · Jul 15, 2024 · N572FE · Doug MD11F · Escape Slide > R1 SLIDE/RAFT FELL OUT OF DOOR UNTO CREW STAIRS. ( DOOR WAS ARMED BT RAMP CREW) 1R CABIN ENTRY SLIDE/RAFT - REMOVED - EXTENDED OVERWATER OPS REQUIRES TWO SLIDE/RAFTS AND/OR PORTABLE RAFTS. MEL: 52-10-03-03 REMOVED R1 DOOR SLIDE/RAFT PER MM 25-61-15- - [SDR FDEA202402220208](https://openairdocs.org/sdr/FDEA202402220208.md): Girt Bar · out of alignment · Feb 22, 2024 · N572FE · Doug MD11F · Emergency Equipment > DURING PREFLIGHT 1L DOOR WILL NOT CLOSE AND ARM PROPERLY DUE TO GIRT BAR MISALIGNMENT MEL 22FEB24 04:40 IND U RELEASED FOR SERVICE PER MEL: 52-10-03-03. 1L CABIN ENTR Y SLIDE/RAFT - REMOVED) - EXTENDED OVERWATER OPS REQ UIRES TWO SLIDE/RAFTS AND/OR P - [SDR FDEA202303040376](https://openairdocs.org/sdr/FDEA202303040376.md): Skin · chafed · Mar 4, 2023 · N572FE · Doug MD11F · Fuselage Main, Plate/Skin > REWORK REQUIRED: UPON PERFORMING WORKCARD # 52C3204-02 STEP 03, LOWER CENTER CARGO DOOR AFT CUTOUT STATION 1781, LOWER DOUBLER FOUND CHAFFED AT LONGERON 40 RIGHT LOWER CENTER CARGO DOOR AFT CUTOUT STATION 1781 AT LONGERON 40 RIGHT CHAFFED LOWER DOUBLER R - [SDR FDEA202302230338](https://openairdocs.org/sdr/FDEA202302230338.md): Skin · cracked · Feb 23, 2023 · N572FE · Doug MD11F · Wing, Plate/Skin > DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION FOUND 02 EACH FASTENER HOLES WITH CRACK INDICATION AT LEFT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS = 683.4 AND STATION XORS = 713.6 ON HOLE #29 AND #30 (REFERENCE TO SNRM N00938 - [SDR FDEA202302210324](https://openairdocs.org/sdr/FDEA202302210324.md): Rib · cracked · Feb 21, 2023 · N572FE · Doug MD11F · Wing Main, Frame Structure > WHILE CARRIED OUT INTERNAL BORESCOPE INSPECTION ON RIGHT HAND NUMBER 8 SLAT LOOSE RIVETS AREA (SNRM N00487), FOUND THE SLAT INTERNAL RIB CRACK AT STATION XOS 1152.408. CRACKED RIB AT RIGHT HAND NUMBER 8 SLAT LOOSE RIVETS AREA (SNRM N00487) INTERNAL STATI - [SDR FDEA202302210323](https://openairdocs.org/sdr/FDEA202302210323.md): Rib · cracked · Feb 21, 2023 · N572FE · Doug MD11F · Wing Main, Frame Structure > WHILE CARRIED OUT INTERNAL BORESCOPE INSPECTION ON RIGHT HAND NUMBER 8 SLAT LOOSE RIVETS AREA (SNRM N00487), FOUND THE SLAT INTERNAL RIB CRACK AT STATION XOS 1146.814. CRACKED RIB AT RIGHT HAND NUMBER 8 SLAT LOOSE RIVETS AREA (SNRM N00487) INTERNAL STATI - [SDR FDEA202302210322](https://openairdocs.org/sdr/FDEA202302210322.md): Rib · cracked · Feb 21, 2023 · N572FE · Doug MD11F · Wing Main, Frame Structure > WHILE CARRIED OUT INTERNAL BORESCOPE INSPECTION ON RIGHT HAND NUMBER 8 SLAT LOOSE RIVETS AREA (SNRM N00487), FOUND THE SLAT INTERNAL RIB CRACK AT STATION XOS 1141.221. CRACKED RIB AT RIGHT HAND NUMBER 8 SLAT LOOSE RIVETS AREA (SNRM N00487) INTERNAL STATI - [SDR FDEA202302210321](https://openairdocs.org/sdr/FDEA202302210321.md): Rib · cracked · Feb 21, 2023 · N572FE · Doug MD11F · Wing Main, Frame Structure > WHILE CARRIED OUT INTERNAL BORESCOPE INSPECTION ON RIGHT HAND NUMBER 8 SLAT LOOSE RIVETS AREA (SNRM N00487), FOUND THE SLAT INTERNAL RIB CRACK AT STATION XOS 1135.627. CRACKED RIB AT RIGHT HAND NUMBER 8 SLAT LOOSE RIVETS AREA (SNRM N00487) INTERNAL STATI - [SDR FDEA202302210320](https://openairdocs.org/sdr/FDEA202302210320.md): Rib · cracked · Feb 21, 2023 · N572FE · Doug MD11F · Wing Main, Frame Structure > WHILE CARRIED OUT INTERNAL BORESCOPE INSPECTION ON RIGHT HAND NUMBER 8 SLAT LOOSE RIVETS AREA (SNRM N00487), FOUND THE SLAT INTERNAL RIB CRACK AT STATION XOS 1130.033. CRACKED RIB AT RIGHT HAND NUMBER 8 SLAT LOOSE RIVETS AREA (SNRM N00487) INTERNAL STATI - [SDR FDEA202302210319](https://openairdocs.org/sdr/FDEA202302210319.md): Rib · cracked · Feb 21, 2023 · N572FE · Doug MD11F · Wing Main, Frame Structure > WHILE CARRIED OUT INTERNAL BORESCOPE INSPECTION ON RIGHT HAND NUMBER 8 SLAT LOOSE RIVETS AREA (SNRM N00487), FOUND THE SLAT INTERNAL RIB CRACK AT STATION XOS 1124.439. CRACKED RIB AT RIGHT HAND NUMBER 8 SLAT LOOSE RIVETS AREA (SNRM N00487) INTERNAL STATI - [SDR FDEA202302210318](https://openairdocs.org/sdr/FDEA202302210318.md): Rib · cracked · Feb 21, 2023 · N572FE · Doug MD11F · Wing Main, Frame Structure > WHILE CARRIED OUT INTERNAL BORESCOPE INSPECTION ON RIGHT HAND NUMBER 8 SLAT LOOSE RIVETS AREA (SNRM N00487), FOUND THE SLAT INTERNAL RIB CRACK AT STATION XOS 1118.845. CRACKED RIB AT RIGHT HAND NUMBER 8 SLAT LOOSE RIVETS AREA (SNRM N00487) INTERNAL STATI - [SDR FDEA202302210317](https://openairdocs.org/sdr/FDEA202302210317.md): Rib · cracked · Feb 21, 2023 · N572FE · Doug MD11F · Wing Main, Frame Structure > WHILE CARRIED OUT INTERNAL BORESCOPE INSPECTION ON RIGHT HAND NUMBER 8 SLAT LOOSE RIVETS AREA (SNRM N00487), FOUND THE SLAT INTERNAL RIB CRACK AT STATION XOS 1050.641. CRACKED RIB AT RIGHT HAND NUMBER 8 SLAT LOOSE RIVETS AREA (SNRM N00487) INTERNAL STATI - [SDR FDEA202302210316](https://openairdocs.org/sdr/FDEA202302210316.md): Rib · cracked · Feb 21, 2023 · N572FE · Doug MD11F · Wing Main, Frame Structure > WHILE CARRIED OUT INTERNAL BORESCOPE INSPECTION ON RIGHT HAND NUMBER 8 SLAT LOOSE RIVETS AREA (SNRM N00487), FOUND THE SLAT INTERNAL RIB CRACK AT STATION XOS 1045.622. CRACKED RIB AT RIGHT HAND NUMBER 8 SLAT LOOSE RIVETS AREA (SNRM N00487) INTERNAL STATI - [SDR FDEA202302210315](https://openairdocs.org/sdr/FDEA202302210315.md): Rib · cracked · Feb 21, 2023 · N572FE · Doug MD11F · Wing Main, Frame Structure > WHILE CARRIED OUT INTERNAL BORESCOPE INSPECTION ON RIGHT HAND NUMBER 8 SLAT LOOSE RIVETS AREA (SNRM N00487), FOUND THE SLAT INTERNAL RIB CRACK AT STATION XOS 1035.585. CRACKED RIB AT RIGHT HAND NUMBER 8 SLAT LOOSE RIVETS AREA (SNRM N00487) INTERNAL STATI - [SDR FDEA202302210314](https://openairdocs.org/sdr/FDEA202302210314.md): Rib · cracked · Feb 21, 2023 · N572FE · Doug MD11F · Wing Main, Frame Structure > WHILE CARRIED OUT INTERNAL BORESCOPE INSPECTION ON RIGHT HAND NUMBER 8 SLAT LOOSE RIVETS AREA (SNRM N00487), FOUND THE SLAT INTERNAL RIB CRACK AT STATION XOS 1040.604. CRACKED RIB AT RIGHT HAND NUMBER 8 SLAT LOOSE RIVETS AREA (SNRM N00487) INTERNAL STATI - [SDR FDEA202302210313](https://openairdocs.org/sdr/FDEA202302210313.md): Rib · cracked · Feb 21, 2023 · N572FE · Doug MD11F · Wing Main, Frame Structure > WHILE CARRIED OUT INTERNAL BORESCOPE INSPECTION ON RIGHT HAND NUMBER 8 SLAT LOOSE RIVETS AREA (SNRM N00487), FOUND THE SLAT INTERNAL RIB CRACK AT STATION XOS 1030.567. CRACKED RIB AT RIGHT HAND NUMBER 8 SLAT LOOSE RIVETS AREA (SNRM N00487) INTERNAL STATI - [SDR FDEA202302200310](https://openairdocs.org/sdr/FDEA202302200310.md): Rib · cracked · Feb 20, 2023 · N572FE · Doug MD11F · Wing Main, Frame Structure > WHILE CARRIED OUT INTERNAL BORESCOPE INSPECTION ON LEFT HAND NUMBER 6 SLAT LOOSE RIVETS AREA (SNRM N00480), FOUND THE SLAT INTERNAL RIB CRACK AT STATION XOS 873.627. CRACKED RIB AT LEFT HAND NUMBER 6 SLAT LOOSE RIVETS AREA (SNRM N00480) INTERNAL STATION XO - [SDR FDEA202302200309](https://openairdocs.org/sdr/FDEA202302200309.md): Rib · corroded · Feb 20, 2023 · N572FE · Doug MD11F · Wing Main, Frame Structure > WHILE CARRIED OUT INTERNAL BORESCOPE INSPECTION ON LEFT HAND NUMBER 6 SLAT LOOSE RIVETS AREA (SNRM N00480), FOUND THE SLAT INTERNAL RIB CRACK AT STATION XOS 822.022. CRACKED RIB AT LEFT HAND NUMBER 6 SLAT LOOSE RIVETS AREA (SNRM N00480) INTERNAL STATION XO - [SDR FDEA202302200308](https://openairdocs.org/sdr/FDEA202302200308.md): Rib · cracked · Feb 20, 2023 · N572FE · Doug MD11F · Wing Main, Frame Structure > WHILE CARRIED OUT INTERNAL BORESCOPE INSPECTION ON LEFT HAND NUMBER 6 SLAT LOOSE RIVETS AREA (SNRM N00480), FOUND THE SLAT INTERNAL RIB CRACK AT STATION XOS 816.822. CRACKED RIB AT LEFT HAND NUMBER 6 SLAT LOOSE RIVETS AREA (SNRM N00480) INTERNAL STATION XO - [SDR FDEA202302200307](https://openairdocs.org/sdr/FDEA202302200307.md): Rib · cracked · Feb 20, 2023 · N572FE · Doug MD11F · Wing Main, Frame Structure > WHILE CARRIED OUT INTERNAL BORESCOPE INSPECTION ON LEFT HAND NUMBER 6 SLAT LOOSE RIVETS AREA (SNRM N00480), FOUND THE SLAT INTERNAL RIB CRACK AT STATION XOS 811.623. CRACKED RIB AT LEFT HAND NUMBER 6 SLAT LOOSE RIVETS AREA (SNRM N00480) INTERNAL STATION XO - [SDR FDEA202302200306](https://openairdocs.org/sdr/FDEA202302200306.md): Rib · cracked · Feb 20, 2023 · N572FE · Doug MD11F · Wing Main, Frame Structure > WHILE CARRIED OUT INTERNAL BORESCOPE INSPECTION ON LEFT HAND NUMBER 6 SLAT LOOSE RIVETS AREA (SNRM N00480), FOUND THE SLAT INTERNAL RIB CRACK AT STATION XOS 806.424. CRACKED RIB AT LEFT HAND NUMBER 6 SLAT LOOSE RIVETS AREA (SNRM N00480) INTERNAL STATION XO - [SDR FDEA202302200305](https://openairdocs.org/sdr/FDEA202302200305.md): Rib · cracked · Feb 20, 2023 · N572FE · Doug MD11 · Wing Main, Frame Structure > WHILE CARRIED OUT INTERNAL BORESCOPE INSPECTION ON LEFT HAND NUMBER 6 SLAT LOOSE RIVETS AREA (SNRM N00480), FOUND THE SLAT INTERNAL RIB CRACK AT STATION XOS 796.025 REPAIRED AS PER EA# 1-5750-T0373019 P1 TITLE: WINGS-FLIGHT SURFACES -LH WING SLAT NO.6-RIBS Next page: https://openairdocs.org/aircraft/N572FE/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 = 'N572FE' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N572FE/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.