# Service difficulty reports: N588FE

A list on [N588FE](https://openairdocs.org/aircraft/N588FE.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 7 · 346 reports

- [SDR FDEA202404110456](https://openairdocs.org/sdr/FDEA202404110456.md): Sensor · failed · Apr 11, 2024 · N588FE · Doug MD11F · Landing Gear Position and Warning
  > UNSAFE RIGHT GEAR UP INDICATION PRIMARY AND SECONDARY ON DEPARTURE PHNL. CYCLED LANDING GEAR PER QRH GEAR PRIMARY AND SECONDARY GEAR INDICATED UP AND LOCKED. PROCEEDED ON ROUTE PER FLIGHT PLAN. REMOVED AND REPLACED RIGHT GEAR UP AND LATCH SENSOR, CRIMPED N
- [SDR FDEA202312061919](https://openairdocs.org/sdr/FDEA202312061919.md): Module · failed · Dec 6, 2023 · N588FE · Doug MD11F · Leading Edge Slat Control System
  > ON DOWNWIND FOR APPROACH AT 4000FT, EXTENDED THE SLATS AND RECEIVED A LEVEL 2 SLAT DISAG ALERT. WE DISCONTINUED THE APPROACH AND RAN THE QRH. DECLARED AN EMERGENCY WITH ATC AND PERFORMED A NO SLAT/FLAPS 28 APPROACH. LANDING ON KIND RUNWAY 05L UNEVENTFU
- [SDR FDEA202311191863](https://openairdocs.org/sdr/FDEA202311191863.md): Pseu · failed · Nov 19, 2023 · N588FE · Doug MD11F · Leading Edge Slat Control System
  > SLAT DISAG ON EXTENSION DURING APPROACH PHASE. COMPLIED WITH QRH RESULTING IN FLAP 28/SLATS RETRACT LANDING. EMERGENCY DECLARED. REPLACED PSEU PER ABOVE REFERENCE, OPS CHECKS OK. PANELS OPENED FOR ACCESS FOR SLAT LUBE. LUBRICATED INBOARD AND OTBOARD SL
- [SDR FDEA202302070244](https://openairdocs.org/sdr/FDEA202302070244.md): Unknown · unknown · Feb 7, 2023 · N588FE · Doug MD11F · Fuselage Main, Structure
  > AFT ACCESSORY COMPARTMENT HAS CORROSION ON ROW OF NUT PLATES ON RH SIDE AFT. MWT REPAIRED IAW SRM 53-70-01-2R
- [SDR FDEA202210112538](https://openairdocs.org/sdr/FDEA202210112538.md): Doubler · cracked · Oct 11, 2022 · N588FE · Doug MD11F · Fuselage Main, Plate/Skin
  > REFERENCE TO SNRM #N01411 - UPON REMOVAL OF DOUBLER NCA 6244-3 FOUND INNER WEB DOUBLER NCA 6244-85 CRACKED (01 EACH OF APPROXIMATELY 0.5" LENGTH). FUSELAGE - MAIN FRAME AT STATION 595 CRACKED WEB DOUBLER NCA 6244-85 CARRIED OUT REPAIR IN ACCORDANCE WITH EA
- [SDR FDEA202209082248](https://openairdocs.org/sdr/FDEA202209082248.md): Doubler · cracked · Sep 8, 2022 · N588FE · Doug MD11F · Fuselage Main, Plate/Skin
  > REFERENCE TO SNRM # N01369 HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION CARRIED OUT ON ACCESSED FASTENER HOLES WITHIN THE AREA OF THE REMOVED NCA6244-3 DOUBLER FOOTPRINT AREA AT STATION 595 AND FOUND 03 EACH HOLES WITH CRACK INDICATION. FUSELAGE - MA
- [SDR FDEA202209052205](https://openairdocs.org/sdr/FDEA202209052205.md): Skin · dented · Sep 5, 2022 · N588FE · Doug MD11F · Fuselage Main, Plate/Skin
  > LEFT SKIN BETWEEN STATION 595 TO 615 AND LONGERON 37 AND LONGERON 46 FOUND DENT. REPAIR CARRIED OUT AS PER EA NUMBER: 1-5330-T0370337 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. ORIG SUB DATE: 9/6/2022
- [SDR FDEA202209022144](https://openairdocs.org/sdr/FDEA202209022144.md): Longeron · corroded · Sep 2, 2022 · N588FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > REFERENCE SNRM NUMBER N01369, AFTER ADDITIONAL REMOVAL FOUND LONGERON NUMBER 49 LEFT CORRODED BETWEEN STATION 535 TO STATION 575. STATION 535 TO STATION 575 LONGERON NUMBER 49 LEFT CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-00-2R FIGURE 20
- [SDR FDEA202208292097](https://openairdocs.org/sdr/FDEA202208292097.md): Support · cracked · Aug 29, 2022 · N588FE · Doug 600N · Fuselage Main, Structure
  > CABIN - WHILE ACCOMPLISHING FLOOR BEAM REPAIR PER SPECIAL/NONROUTINE MAINTENANCE FORM N01209 FOUND CHANNEL (SUPPORT) AT LEFT HAND STATION 1256 X=116 CRACKED. CRACKED CHANNEL ( SUPPORT) AT LEFT HAND STATION 1256 X=116 REMOVED AND REPLACED IN ACCORDANCE WI
- [SDR FDEA202208292096](https://openairdocs.org/sdr/FDEA202208292096.md): Longeron · cracked · Aug 29, 2022 · N588FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > REFERENCE SPECIAL/NONROUTINE MAINTENANCE FORM N00314, TO INSPECT STATION 595 BULKHEAD FOUND FUSELAGE NO.1 AIRCON BAY AFT BULKHEAD STATION 595 APPROXIMATE LONGERON NO.42 SUSPECTED CRACK. FUSELAGE STATION 595 BULKHEAD NO.1 AIRCON BAY CRACKED AT DOUBLER AND
- [SDR FDEA202208252048](https://openairdocs.org/sdr/FDEA202208252048.md): Skin · dented · Aug 25, 2022 · N588FE · Doug MD11F · Fuselage Main, Plate/Skin
  > RIGHT SKIN BETWEEN BS 595 AND 615, BETWEEN LONGERON 44R-46R DENTED. CARRIED OUT REPAIR IN ACCORDANCE WITH EA 1-5330-T0370284 P1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA202208222024](https://openairdocs.org/sdr/FDEA202208222024.md): Former · cracked · Aug 22, 2022 · N588FE · Doug MD11F · Wing Main, Frame Structure
  > LEFT HAND WING - OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 757 FORMER CRACKED. LEFT HAND WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 757 CRACKED FORMER REMOVED AND FABRICATED PER DOUGLAS DRAWIING ARB 2930 REV F. INSTALLED FABRICAT
- [SDR FDEA202208151977](https://openairdocs.org/sdr/FDEA202208151977.md): Spar · cracked · Aug 15, 2022 · N588FE · Doug MD11F · Wing Spar
  > HIGH FREQUENCY EDDY CURRENT AND ULTRASONIC INSPECTION CARRIED OUT ON UPPER SPAR ASSEMBLY, TAIL PYLON MANUFACTURING JOINT SPAR BETWEEN STATION YID 408.5 TO 413.2 AND FOUND CRACK INDICATION PROPAGATE IN AFT DIRECTION FROM THE EDGE OF LEFT HAND SIDE UPPER C
- [SDR FDEA202208121970](https://openairdocs.org/sdr/FDEA202208121970.md): Floorbeam · cracked · Aug 12, 2022 · N588FE · Doug MD11F · Fuselage Main, Floor Beam
  > HIGH FREQUENCY EDDY CURRENT SURFACE INSPECTION CARRIED OUT ON LEFT HAND SIDE OVERWIING FLOOR BEAM AT STATION Y=1256 AND FOUND CRACK INDICATION ON THE OVERWING FLOOR BEAM WEB AND UPPER FLANGES BETWEEN STATION X = 107 AND STATION X = 116 APPROXIMATELY 1 I
- [SDR FDEA202208121969](https://openairdocs.org/sdr/FDEA202208121969.md): Longeron Splice · cracked · Aug 12, 2022 · N588FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > FORWARD CARGO COMPARTMENT, FOUND UNDERFLOOR LONGERON SPLICE BETWEEN STATION 755 TO STATION 775, LONGERON - 44 LEFT SUSPECT CRACKED. REMOVED AND REPLACED PER SRM 51-31- 01-OG. LONGERON SPLICE FABRICATED BY MACHINING PER DOUGLAS DRAWING ACA7150 REVISION
- [SDR FDEA202208121968](https://openairdocs.org/sdr/FDEA202208121968.md): Skin · cracked · Aug 12, 2022 · N588FE · Doug MD11F · Wing, Plate/Skin
  > LEFT HAND WING - OUTBOARD FIXED LEADING EDGE #11 SLAT TRACK CUTOUT STATION XOS 714 CRACKED. REPAIR CARRIED OUT PER SRM 57-40-02-2R REPAIR 7 FIGURE 201 REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA202208121967](https://openairdocs.org/sdr/FDEA202208121967.md): Slat Track · cracked · Aug 12, 2022 · N588FE · Doug MD11F · Leading Edge Devices
  > LEFT HAND WING - OUTBOARD FIXED LEADING EDGE #15 SLAT TRACK CUTOUT STATION XOS 949 CRACKED. REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 7 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA202208121966](https://openairdocs.org/sdr/FDEA202208121966.md): Skin · cracked · Aug 12, 2022 · N588FE · Doug MD11F · Wing, Plate/Skin
  > LEFT HAND WING - OUTBOARD FIXED LEADING EDGE #16 SLAT TRACK CUTOUT STATION XOS 1003 CRACKED. LEFT HAND WING - OUTBOARD FIXED LEADING EDGE NUMBER 16 SLAT TRACK CUTOUT STATION XOS 1003 CRACKED AREA REPAIR CARRIED OUT AS PER EA: 1-5730-T0370336 PART 1. TITLE
- [SDR FDEA202208111959](https://openairdocs.org/sdr/FDEA202208111959.md): Skin · cracked · Aug 11, 2022 · N588FE · Doug MD11F · Wing, Plate/Skin
  > RIGHT HAND WING - OUTBOARD FIXED LEADING EDGE NUMBER 15 SLAT TRACK CUTOUT STATION XOS 950 CRACKED. SKIN REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 7 FIGURE 201. REPAIR CLASSIFED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA202208111958](https://openairdocs.org/sdr/FDEA202208111958.md): Skin · cracked · Aug 11, 2022 · N588FE · Doug MD11F · Wing, Plate/Skin
  > RIGHT HAND WING - OUTBOARD FIXED LEADING EDGE NUMBER 16 SLAT TRACK CUTOUT STATION XOS 1007 CRACKED. SKIN REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 7 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA202208111957](https://openairdocs.org/sdr/FDEA202208111957.md): Doubler · cracked · Aug 11, 2022 · N588FE · Doug MD11F · Wing, Plate/Skin
  > RIGHT HAND WING - OUTBOARD LEADING EDGE COMPARTMENT STATION XOS 613 BEADED DOUBLER CRACKED. DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R. REPAIR 15. FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA202208111956](https://openairdocs.org/sdr/FDEA202208111956.md): Doubler · cracked · Aug 11, 2022 · N588FE · Doug MD11F · Wing, Plate/Skin
  > RIGHT WING - OUTBOARD LEADING EDGE COMPARTMENT STATION XOS 880 BEADED DOUBLER CRACKED. DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA202208111955](https://openairdocs.org/sdr/FDEA202208111955.md): Doubler · cracked · Aug 11, 2022 · N588FE · Doug MD11F · Wing, Plate/Skin
  > RIGHT WING - OUTBOARD LEADING EDGE COMPARTMENT STATION XOS 758 BEADED DOUBLER CRACKED. DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA202208101952](https://openairdocs.org/sdr/FDEA202208101952.md): Longeron Splice · cracked · Aug 10, 2022 · N588FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > CENTRE CARGO COMPARTMENT, FOUND UNDERFLOOR LONGERON SPLICE SUSPECT CRACK BETWEEN STATION 1521 TO 1541, LONGERON 49 LEFT. LONGERON REMOVED AND REPLACED PER SRM 51-31-01-OG. LONGERON SPLICE FABRICATED BY MACHINING PER DOUGLAS DRAWING A5A7114 REVISION J.
- [SDR FDEA202208101951](https://openairdocs.org/sdr/FDEA202208101951.md): Longeron Splice · cracked · Aug 10, 2022 · N588FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > CENTRE CARGO COMPARTMENT, FOUND UNDERFLOOR LONGERON SPLICE SUSPECT CRACK BETWEEN STATION 1521 TO 1541, LONGERON 52. REMOVED AND REPLACED PER SRM 51-31-01- OG. LONGERON SPLICE FABRICATED BY MACHINING PER DOUGLAS DRAWING A5A7114 REVISION J. REPAIR CLASSIFI
- [SDR FDEA202208101950](https://openairdocs.org/sdr/FDEA202208101950.md): Longeron Splice · cracked · Aug 10, 2022 · N588FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > CENTRE CARGO COMPARTMENT, FOUND UNDERFLOOR LONGERON SPLICE SUSPECT CRACK BETWWEEN ATATION 1521 TO 1541, LONGERON 49 LEFT. REMOVED AND REPLACED PER SRM 51-31-01-OG. LONGERON SPLICE FABRICATED BY MACHINING PER DOUGLAS DRAWING A5A7114 REVISION J. REPAIR CL
- [SDR FDEA202208081922](https://openairdocs.org/sdr/FDEA202208081922.md): Frame · chafed · Aug 8, 2022 · N588FE · Doug MD11F · Fuselage Main, Frame
  > CABIN - LEFT HAND STATION 535 LONGERON 24 LEFT FRAME REPAIR OUTER ANGLE FOUND CHAFFING. BLENDED AND FOUND EXCEEDED LIMIT IN ACCORDANCE WITH SRM 53-00-00-2R FIGURE 202 SHEET 1. FRAME STATION 535 LONGERON 24 LEFT REPAIR CARRIED OUT IN ACCORDANCE WITH SRM
- [SDR FDEA202208081921](https://openairdocs.org/sdr/FDEA202208081921.md): Longeron · chafed · Aug 8, 2022 · N588FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > CABIN - LEFT HAND STATION 535 LONGERON 19 LEFT FRAME REPAIR OUTER ANGLE FOUND CHAFFING. BLENDED AND FOUND EXCEEDED LIMIT IN ACCORDANCE WITH SRM 53-00-00-2R FIGURE 202 SHEET 1.FRAME STATION 535 LONGERON 19 LEFT REPAIR CARRIED OUT IN ACCORDANCE WITH SR
- [SDR FDEA202208081920](https://openairdocs.org/sdr/FDEA202208081920.md): Skin · chafed · Aug 8, 2022 · N588FE · Doug MD11F · Wing, Plate/Skin
  > LEFT HAND WING - INBOARD FIXED LEADIING EDGE UPPER SURFACE STATION XIS 247 CHAFFING MARK. AREA SMOOTHED OUT AND FOUND WITHIN LIMIT AS PER SRM 57-40-02-2R REPAIR 8 FIGURE 201. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
- [SDR FDEA202208081919](https://openairdocs.org/sdr/FDEA202208081919.md): Skin · chafed · Aug 8, 2022 · N588FE · Doug MD11F · Wing, Plate/Skin
  > RIGHT HAND WING - INBOARD FIXED LEADING EDGE UPPER SURFACE STATION XIS 247 CHAFFING MARK. AREA SMOOTHED OUT AND FOUND WITHIIN LIMIT AS PER SRM 57-40-02-2R REPAIR 8 FIGURE 201. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
- [SDR FDEA202208081918](https://openairdocs.org/sdr/FDEA202208081918.md): Doubler · cracked · Aug 8, 2022 · N588FE · Doug MD11F · Wing, Plate/Skin
  > LEFT HAND WING - OUTBOARD LEADING EDGE COMPARTMENT STATION XOS 906 RIB DOUBLER CRACKED. DOUBLER REMOVED AND FABRICATED DOUBLER PER DOUGLAS DRAWING ARB 3954 REVISION K. FABRICATED DOUBLER INSTALLED AS PER SRM 51-33-01-0G. REPAIR CLASSIFED AS MAJOR PER
- [SDR FDEA202208081917](https://openairdocs.org/sdr/FDEA202208081917.md): Stringer · cracked · Aug 8, 2022 · N588FE · Doug MD11F · Wing, Longeron/Stringer
  > LEFT WING - OUTBOARD LEADING EDGE COMPARTMENT STATION XOS 666 STRINGER CRACKED. STRINGER REPAIR CARRIED OUT AT STRINGER AS PER SRM 57-40-03-2R REPAIR 2 FIGURE 202. REPAIR CLASSIFED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA202208081916](https://openairdocs.org/sdr/FDEA202208081916.md): Stringer · cracked · Aug 8, 2022 · N588FE · Doug MD11F · Wing, Longeron/Stringer
  > LEFT WING - OUTBOARD LEADING EDGE COMPARTMENT STATION XOS 791 STRINGER CRACKED. STRINGER REPAIR CARRIED OUT AT STRINGER AS PER SRM 57-40-03-2R REPAIR 2 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA202208081915](https://openairdocs.org/sdr/FDEA202208081915.md): Doubler · cracked · Aug 8, 2022 · N588FE · Doug MD11F · Wing, Plate/Skin
  > LEFT HAND WING - OUTBOARD LEADING EDGE COMPARTMENT STATION XOS 651 BEADED DOUBLER CRACKED. REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA202208081914](https://openairdocs.org/sdr/FDEA202208081914.md): Doubler · cracked · Aug 8, 2022 · N588FE · Doug MD11F · Wing, Plate/Skin
  > LEFT HAND WING - OUTBOARD LEADING EDGE COMPARTMENT STATION XOS 705 BEADED DOUBLER CRACKED. REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA202206211496](https://openairdocs.org/sdr/FDEA202206211496.md): Motor · leaking · Jun 21, 2022 · N588FE · Doug MD11F · Stabilizer Control System
  > ON CLIMB OUT. LVL 1 HYD 3 ELEV OFF. HYD 3 QTY INDICATED 4.7 AND DROPPING. FOLLOWED BY A LVL 1 HYD 3 OFF AND THEN A LVL 2 HYD 3 FAIL. QTY AT ZERO. COMPLIED WITH QRH. EMERGENCY DECLARED DIVERT TO INDY AT GOC REQUEST. REMOVED AND REPLACED #1 HORIZONTAL
- [SDR FDEA202205181255](https://openairdocs.org/sdr/FDEA202205181255.md): Cylinder · failed · May 18, 2022 · N588FE · Doug MD11F · Steering Unit
  > TAXI OUT WAS FINE. ON TAXI IN, FIRST RIGHT HAND TURN NOTICED ABOUT HALF WAY THROUGH THE RIGHT TURN, TILLER BECAME IN EFFECTIVE AND USED DIFFERENTIAL BRAKING TO STRAITENED UP. TRIED NEXT RIGHT TURN AT GATE VERY SLOW, AGAIN NO AUTHORITY. STOPPED THE AIRPLAN
- [SDR FDEA201811153224](https://openairdocs.org/sdr/FDEA201811153224.md): Battery Pack · unknown · Nov 15, 2020 · N588FE · Doug MD11F · Emergency Lighting
  > EMER LT BAT 1 LO LEVEL ALERT 1 WHEN TESTING EMER LIGHTS. PERFORMED EMER LT TEST IAW AMM 33-50-00-5 OPS CHECKS NORMAL. A/C OK FOR SERVCE
- [SDR FDEA202009242305](https://openairdocs.org/sdr/FDEA202009242305.md): Skin · damaged · Sep 24, 2020 · N588FE · Doug MD11F · Horizontal Stabilizer, Plate/Skin
  > EMPENNAGE LEFT HAND HORIZONTAL STABILIZER OUTBOARD LEADING EDGE 331FT FOUND WITH EXISTING BLIND RIVET REPAIR AT XFS=322.131 TO XFS 333.764. EMPENNAGE LEFT HAND HORIZONTAL STABILIZER OUTBOARD LEADING EDGE 331FT, WITH EXISTING BLIND RIVET REPAIR BETWEEN XFS=322
- [SDR FDEA202009212284](https://openairdocs.org/sdr/FDEA202009212284.md): Beam · cracked · Sep 21, 2020 · N588FE · Doug MD11F · Passenger/Crew Doors
  > CABIN - L3 PLUG DOOR LOWER STOP BEAM FOUND CRACK. CABIN - AT L3 PLUG DOOR, CRACKED LOWER STOP BEAM REMOVED AND REPLACED WITH NEW LOWER STOP BEAM AS PER SRM 51-31-01-0G. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
- [SDR FDEA202009182241](https://openairdocs.org/sdr/FDEA202009182241.md): Frame · cracked · Sep 18, 2020 · N588FE · Doug MD11F · Horizontal Stabilizer Structure
  > CRACK FOUND APPROXIMATELY 0.4 INCH IN LENGTH AT PYLON CARRY THROUGH STRUCTURE WEBS AT 364QR ACCESS PANEL FRAME CUTOUT AT STATION 2164. CRACKED AT PYLON CARRY THROUGH STRUCTURE WEBS AT 364QR ACCESS PANEL FRAME CUTOUT AT STATION 2164. REMOVED AS PER SRM 51-33-
- [SDR FDEA202009182243](https://openairdocs.org/sdr/FDEA202009182243.md): Intercostal · cracked · Sep 18, 2020 · N588FE · Doug MD11F · Empennage Structure
  > EMPENNAGE,UPON REMOVAL FOR BANJO FITTING REPAIR ACCESS,RIGHT HAND SIDE LOWER WEB PANEL FOUND WITH A CRACKLINE FROM CORNER EDGE AT STATION Y=2164. RIGHT HAND SIDE LOWER WEB INTERCOSTAL REAR CENTER SPAR TO REAR SPAR CRACK AT STATION Y=2164 REPAIR CARRIED OUT, A
- [SDR FDEA202009182242](https://openairdocs.org/sdr/FDEA202009182242.md): Intercostal · cracked · Sep 18, 2020 · N588FE · Doug MD11F · Empennage Structure
  > EMPENNAGE, UPON REMOVAL FOR BANJO FITTING REPAIR ACCESS, LEFT HAND SIDE LOWER WEB PANEL FOUND WITH A CRACKLINE FROM CORNER EDGE AT STATION Y=2164. LEFT HAND SIDE LOWER WEB INTERCOSTAL REAR CENTER SPAR TO REAR SPAR CRACK AT STATION Y=2164 REPAIR CARRIED OUT, A
- [SDR FDEA202009182247](https://openairdocs.org/sdr/FDEA202009182247.md): Bulkhead Web · dented · Sep 18, 2020 · N588FE · Doug MD11F · Fuselage Main, Bulkhead
  > AFT CARGO, STATION 1841 BULKHEAD WEB X=2" TO 18" FOUND DENTS. AFT CARGO STATION 1841 BULKHEAD WEB X=2 TO 18 REMOVED, AS PER SRM 51-33-01-0G AT STATION 1841 X=0 TO X=60. WEB FABRICATED, AS PER DOUGLAS DRAWING AGA 7170 REVISION R. WEB INSTALLED AT STATION
- [SDR FDEA202009182246](https://openairdocs.org/sdr/FDEA202009182246.md): Web · cracked · Sep 18, 2020 · N588FE · Doug MD11F · Fuselage Miscellaneous Structure
  > AFT CARGO-STATION 1841 X= -44" WEB CRACK ON EXISTING DOUBLER REPAIR. AFT CARGO STATION 1841 BULKHEAD WEB X= -44" REMOVED, AS PER SRM 51-33-01-0G AT STATION 1841, X=0 TO X= -62. WEB FABRICATED, AS PER DOUGLAS DRAWING AGA 7170 REVISION R. WEB INSTALLED, A
- [SDR FDEA202009162225](https://openairdocs.org/sdr/FDEA202009162225.md): Floor Panel · delaminated · Sep 16, 2020 · N588FE · Doug MD11F · Fuselage Floor Panel
  > CABIN, MAIN DECK CARGO COMPARTMENT FLOOR PANEL NUMBER 272EF AT STATION 1361 TO STATION 1481, FOUND ACCESS DOOR HOLE EDGE DELAMINATED. DELAMINATED FLOOR PANEL 272EF AT CABIN STATION 1361 TO STATION 1481 REMOVED, AS PER AMM 53-21-04. FLOOR PANEL 272EF FABRICAT
- [SDR FDEA202009142209](https://openairdocs.org/sdr/FDEA202009142209.md): Rib · cracked · Sep 14, 2020 · N588FE · Doug MD11F · Leading Edge Devices
  > RIGHT HAND WING NUMBER 1 SLAT CRUISE PERFORMANCE FILLET RIB AT XIS 150.7474 ALIGNMENT PIN AREA FOUND CRACK. RIGHT HAND WING NUMBER 1 SLAT ASSEMBLY (INCLUDES SLAT AND CRUISE PERFORMANCE FILLET). REMOVED AND REPLACED, AS PER AMM 27-80-20-4. REFERENCE TO WRI
- [SDR FDEA202009142208](https://openairdocs.org/sdr/FDEA202009142208.md): Skin · cracked · Sep 14, 2020 · N588FE · Doug MD11F · Wing, Plate/Skin
  > HIGH FREQUENCY EDDY CURRENT INSPECTION ON RIGHT HAND WING FIXED LEADING EDGE SKIN ADJACENT TO ACCESS DOOR CORNER 5 FOUND CRACK APPROXIMATELY 2.2 INCHES AT XOS 490. RIGHT HAND WING FIXED LEADING EDGE SKIN ADJACENT TO ACCESS DOOR CORNER 5 AT XOS 490 REPAIR CARR
- [SDR FDEA202009142195](https://openairdocs.org/sdr/FDEA202009142195.md): Spar · cracked · Sep 14, 2020 · N588FE · Doug MD11F · Vertical Stabilizer, Plate/Skin
  > DURING ULTRASONIC INSPECTION FOR VERTICAL CRACKS BEHIND SERVICE REPAIR SR10550013, PER DRAWING NUMBER SN10550000 ON LEFT HAND SIDE OF THE LOWER VERTICAL STABILIZER FORWARD FLANGE OF UPPER REAR SPAR CAP, STATION Y=2164, CRACK INDICATION FOUND ON THIRD FAST
- [SDR FDEA202009142197](https://openairdocs.org/sdr/FDEA202009142197.md): Spar Cap · cracked · Sep 14, 2020 · N588FE · Doug MD11F · Vertical Stabilizer, Spar/Rib
  > DURING ULTRASONIC INSPECTION FOR VERTICAL CRACKS BEHIND SERVICE REPAIR SR10550013, PER DRAWING NUMBER SN10550000 ON LEFT HAND SIDE OF THE LOWER VERTICAL STABILIZER FORWARD FLANGE OF UPPER REAR SPAR CAP, STATION Y=2164, CRACK INDICATION FOUND ON THIRD FAS

Next page: https://openairdocs.org/aircraft/N588FE/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 = 'N588FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N588FE/reports

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