# Service difficulty reports: N586FE

A list on [N586FE](https://openairdocs.org/aircraft/N586FE.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 10 · 500 reports

- [SDR FDEA202312111931](https://openairdocs.org/sdr/FDEA202312111931.md): Wire · loose · Dec 11, 2023 · N586FE · Doug MD11F · Light System Wiring
  > 1R ENTRY DOOR EMERGENCY EXIT LIGHT SIGN INOP. RELAMPED NO HELP. ROUBLE SHOT WIRING TO EMER LIGHT, TIGHTENED LOOSE WIRE IAW WDM 33-52-01. OPS CHECK NORMAL IAW AMM 33-52-04-2.
- [SDR FDEA202311181862](https://openairdocs.org/sdr/FDEA202311181862.md): Tire · damaged · Nov 18, 2023 · N586FE · Doug MD11F · Brake Anti-Skid Section
  > UPON TOUCHDOWN PDX RWY10R, RECEIVED LVL2 ANTI-SKID R FAIL, IMMEDIATELY FOLLOWED BY LVL2 TIRE FAIL. #7 TIRE FAIL INDICATION. SAME TIRE AS ANTI SKID SYSTEM MEL FOR THIS AIRCRAFT 32-45-01-01. REMOVED AND REPLACED #7 MAIN WHEEL/TIRE ASSEMBLY. IAW MD-11 AMM 3
- [SDR FDEA202311151853](https://openairdocs.org/sdr/FDEA202311151853.md): Anti-Skid Sys · failed · Nov 15, 2023 · N586FE · Doug MD11F · Brake Anti-Skid Section
  > UPON TOUCHDOWN PDX RWY10R, RECEIVED LVL2 ANTI-SKID R FAIL, IMMEDIATELY FOLLOWED BY LVL2 TIRE FAIL. #7 TIRE FAIL INDICATION. SAME TIRE AS ANTI SKID SYSTEM MEL FOR THIS AIRCRAFT 32-45-01-01. REINSTALLED AUX STRUCTURE AFT SPAR CLOSE OUT PANEL RT MLG OUTBD PER
- [SDR FDEA202303140429](https://openairdocs.org/sdr/FDEA202303140429.md): Cowling · cracked · Mar 14, 2023 · N586FE · Doug MD11F · Powerplant System
  > #1 ENG I/B FAN COWL CRACKED AT OIL ACCESS DOOR. COMPLIED EA 1-7110-T0371830 PT3 AND MD11 SRM 54-22-02-2R REPAIR 3 PG 13
- [SDR FDEA202208192002](https://openairdocs.org/sdr/FDEA202208192002.md): Battery Pack · no test · Aug 19, 2022 · N586FE · Doug MD11F · Emergency Lighting
  > DURING EMERGENCY LIGHT PREFLIGHT TEST, LEVEL ONE EMER LT BAT 1 LO MEL 19AUG22 03:20 MEM U RELEASED FOR SERVICE PER MEL: 33-50-04 CATEGORY: C EXPIRATION: 29AUG22 "MEL 33-50-04: EMER LIGHTS - INOP.". C/7329674
- [SDR FDEA202206241544](https://openairdocs.org/sdr/FDEA202206241544.md): Bolt · worn · Jun 24, 2022 · N586FE · Doug MD11F · Main Landing Gear
  > AFTER TAKEOFF THE LEFT MAIN GEAR INDICATOR WAS RED. WE CHECKED THE CONFIG PAGE WHICH SHOWED RED AS WELL. WE FOLLOWED THE QRH PROCEDURE BUT THE GEAR STILL SHOWED RED ON BOTH INDICATIONS. SHORTLY AFTERWARDS THE GEAR SUDDENLY SHOWED ALL SAFE AND WE CONTINUED
- [SDR FDEA202202040227](https://openairdocs.org/sdr/FDEA202202040227.md): Fire Detector · broken · Feb 4, 2022 · N586FE · Doug MD11F · Fire Detection
  > 1:30 INTO FLIGHT RECEIVED LEVEL 1 FIRE DET 3 FAIL. REMOVED AND REPLACED #3 ENG FDCU, NO HELP ORIGINAL UNIT REINSTALLED. IAW AMM 26-11-02-4. TROIUBLESHOT PER MD11 FIM 26-11-00-2 AND WDM 71-51-11 FOUND LOWER TURBINE 'A' AND 'B' LOOPS RESISTANCE OUT OF L
- [SDR FDEA202201190095](https://openairdocs.org/sdr/FDEA202201190095.md): None · failed · Jan 19, 2022 · N586FE · Doug MD11F · Engine Thrust Reverser
  > ABOVE 10 K FEET. RECEIVED A RED U/L REVERSER LIGHT NR 1 ENG. ACCOMPANIED BY SIGNIFICANT VIBRATIONS. SHUTDOWN ENG IAW QRH. ON LANDING, LIGHT TURNED TO AMBER. EMERGENCY DECLARED RTB ON INSPECTION OF # 1 THRUST REVERSER, FOUND O/B CENTER DRIVER UNIT BRAKE
- [SDR FDEA202201060021](https://openairdocs.org/sdr/FDEA202201060021.md): None · delaminated · Jan 6, 2022 · N586FE · Doug MD11F · Fuselage Main, Structure
  > REWORK N00508; CORRECTIVE ACTION REQUIRES REPORTABLE DISCREPANCY REPORT (RDR) PER ITEMS 3,5,6 (RDR REVISED 8-23-21) AND SERVICE DIFFICULTY REPORT ITEM 13,14 (GMM REVISION 177) REMOVED AND REPLACED LOWER AFT RUDDER REF AMM 27-20-20-4.
- [SDR FDEA202201060020](https://openairdocs.org/sdr/FDEA202201060020.md): None · delaminated · Jan 6, 2022 · N586FE · Doug MD11F · Fuselage Main, Structure
  > REWORK N00507; CORRECTIVE ACTION REQUIRES REPORTABLE DISCREPANCY REPORT (RDR) PER ITEMS 3,5,6 (RDR REVISED 8-23-21) AND SERVICE DIFFICULTY REPORT ITEM 13,14 (GMM REVISION 177) REMOVED AND REPLACED LOWER AFT RUDDER REF AMM 27-20-20-4.
- [SDR FDEA202111302988](https://openairdocs.org/sdr/FDEA202111302988.md): Channel · corroded · Nov 30, 2021 · N586FE · Doug MD11F · Standard Practices/Structures
  > CTR CARGO, L/H SIDE ROLLER TRAY EXFOLIATED AT APPROX STA. 1600 APPROX LBL 48. REMOVED AND REPLACED CENTER CARGO LEFT HAND ROLLER TRAY STA. 1600, LBL 48. REF MD11 SRM 51-30-01-0G, DWG AFJ7065.
- [SDR FDEA202111302950](https://openairdocs.org/sdr/FDEA202111302950.md): Seat Track · corroded · Nov 30, 2021 · N586FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO COMPARTMENT, CORRODED SEAT TRACK LOBES AT STATION 1801 RBL70 REMOVED AND INSTALLED NEW SEAT TRACK AND SPLICE AT STA 1801 RBL70 MAIN DECK REF SRM 51-41-01-0G FIG.7, SRM 53-00-52-2R FIG. 201, SRM 51-33-01-0G, AND SRM 51-31-01-0G "MAJOR REPAI
- [SDR FDEA202111293084](https://openairdocs.org/sdr/FDEA202111293084.md): Seat Track · corroded · Nov 29, 2021 · N586FE · Doug MD11F · Cabin Equipment/Furnishings
  > MAIN CARGO - STA 1781, RBL 107 - SEAT TRACK HAS 2 FLOOR BOARD ATTACH LOBES CORRODED. (VIEWED FROM CENTER CARGO ABOVE CEILING, MARKED) 0005202340: LEMUS, JOSE H - 14-DEC-2021 17:00 REPAIRED SEAT TRACK PER SRM 53-00-52-2R REPAIR 1 FIG. 201 SHEETS 1-3, SRM 51
- [SDR FDEA202111293083](https://openairdocs.org/sdr/FDEA202111293083.md): None · corroded · Nov 29, 2021 · N586FE · Doug MD11F · Fuselage Main, Structure
  > AFT CARGO - STA 1902 R/H SIDE - SIDEWALL PANEL VERTICAL STANCHION HAS CORROSION ON LOWER SECTION I/B SIDE (MARKED) REMOVED AND REPLACE SIDE WALL PANEL VERTICAL STANCHION AT STA 1902 REF SRM 51-31- 01-OG
- [SDR FDEA202111243052](https://openairdocs.org/sdr/FDEA202111243052.md): Shear Tie · corroded · Nov 24, 2021 · N586FE · Doug MD11F · Fuselage Main, Structure
  > AFT CARGO - R/H SIDE - SHEAR TIE HAS CORROSION AT STA 1902 BETWEEN LONGERON 42 & 43 REMOVED, FABRICATED AND INSTALLED SHEAR TIE (P/N: AGA7009-7) AT STA 1902 BTWN L-42 AND L-43 RHS REF, DOUGLAS DWG AGA7009 AND MD11 SRM 51-31-01-0G.
- [SDR FDEA202111222919](https://openairdocs.org/sdr/FDEA202111222919.md): Vane · damaged · Nov 22, 2021 · N586FE · Doug MD11F · Trailing Edge Flaps
  > RH WING INBD FLAP VANE LOWER SURFACE BETWEEN CTR AND OUTBD TRACK HAS IMPACT DAMAGE REPAIRED R/H WING INBD FLAP VANE LOWER SURFACE, IMPACT DAMAGE REF. SRM 57-50-80-2R REPAIR 2, PER SRM 51-62-01-0G PAR. 10F.
- [SDR FDEA202111182898](https://openairdocs.org/sdr/FDEA202111182898.md): Longeron · corroded · Nov 18, 2021 · N586FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > AFT CARGO PIT AT STA.1887 RHS LONGERON 40 IS CORRODED BEYOND LIMITS (MARKED) REMOVED CORRODED LONGERON AT STA 1887 RHS L-40 AND REPAIR PER MD11 SRM 53-00-05- 2R 201. AND MD11 SRM 53-00-01-2R FIG 201 SHEET 10. SEE JPF FOR DETAILS. "MAJOR REPAIR"
- [SDR FDEA202111162867](https://openairdocs.org/sdr/FDEA202111162867.md): Seat Track · corroded · Nov 16, 2021 · N586FE · Doug MD11F · Fuselage Main, Structure
  > AFT CGO COMPARTMENT, STA 1841-STA 1967, RBL20, SEAT TRACK CORROSION ON MULTIPLE AREAS. AFT CARGO STA. 1841-1967 RH REMOVED AND REPLACED SEAT TRACK IAW DOUGLAS DWG. AGA3855.
- [SDR FDEA202111162868](https://openairdocs.org/sdr/FDEA202111162868.md): Floorboard · damaged · Nov 16, 2021 · N586FE · Doug MD11F · Fuselage Floor Panel
  > UPPER MAIN DECK FLOOR BOARD PANEL (271BF)STA. 1321 LBL-50 REQUIRES FABRICATION. REMOVED AND REPLACED MAIN DECK FLOOR BOARD PANEL (271BF) STATION 1321 LBL50 REF FEDEX DWG SRZ-25-005.
- [SDR FDEA202111152915](https://openairdocs.org/sdr/FDEA202111152915.md): Support · corroded · Nov 15, 2021 · N586FE · Doug MD11F · Fuselage Main, Structure
  > AFT CARGO RH STA. 1954 BELOW FLOOR PANEL 187HF OUTBOARD RAIL (REF. AGA3857-508) HAS EXFOLATION CORROSION EXISTS IN 2 LOCATION APROX. 2.00 X 1.00 AND 1.50 X 1.25. REMOVED AND REPLACED FLOOR SUPPORT RAILPER DWG. AGA3857-508
- [SDR FDEA202111152916](https://openairdocs.org/sdr/FDEA202111152916.md): Support · corroded · Nov 15, 2021 · N586FE · Doug MD11F · Fuselage Main, Structure
  > AFT CARGO RH STA. 1954 BELOW FLOOR PANEL 187HF OUTBOARD RAIL (REF. AGA3857-508) HAS EXFOLATION CORROSION EXISTS IN 2 LOCATION APROX. 2.00 X 1.00 AND 1.50 X 1.25. REMOVED AND REPLACED FLOOR SUPORT PER DWG AGA 3857
- [SDR FDEA202111152858](https://openairdocs.org/sdr/FDEA202111152858.md): None · delaminated · Nov 15, 2021 · N586FE · Doug MD11F · Wing Structure
  > R/H WING, UPPER SURFACE, PANEL ARC7163 JUST FWD OF SPOILERS #4  APPEARS TO BE DELAMINATED. BULGING AND SEVERAL FASTENERS PULLING THROUGH PANEL. PERFORMED REPAIR ON ARC7163 FWD OUTBOARD CORNER DELAM AREA PER SRM 51-62-01- 0G PAR 10A, 10F. AND SRM 57-50-80
- [SDR FDEA202111132869](https://openairdocs.org/sdr/FDEA202111132869.md): Seat Track · corroded · Nov 13, 2021 · N586FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO COMPARTMENT, APPROX. STATION 1675, RBL-48 SEAT TRACK FLANGE EXFOLIATING AROUND THE HOLE FOR CLIP-NUT. REPAIR DAMAGED SEAT TRACK REF SRM 53-00-52-2R FIG. 201 REPAIR 5.
- [SDR FDEA202111132839](https://openairdocs.org/sdr/FDEA202111132839.md): Floorbeam · corroded · Nov 13, 2021 · N586FE · Doug MD11F · Fuselage Main, Floor Beam
  > MAIN DECK FLOOR SUPPORT CORRODED AT STATION 1741, RBL-49 TO RBL-71. REMOVED AND REPLACED SUPPORT AFA3853-20 REF DAC DWG NFA6398 AND SRM 51-31-01-OG. "MAJOR REPAIR"
- [SDR FDEA202111122841](https://openairdocs.org/sdr/FDEA202111122841.md): Floorbeam · corroded · Nov 12, 2021 · N586FE · Doug MD11F · Fuselage Main, Floor Beam
  > MAIN DECK FLOOR SUPPORT CORRODED AT STATION 1256, RBL-77 TO RBL-86.5 REMOVED AND REPLACED SUPPORT AEA0410-2 REF DAC DWG NEA6398 AND SRM 51-31-01-OG. "MAJOR REPAIR"
- [SDR FDEA202111122840](https://openairdocs.org/sdr/FDEA202111122840.md): Floorbeam · corroded · Nov 12, 2021 · N586FE · Doug MD11F · Fuselage Main, Floor Beam
  > MAIN DECK FLOOR SUPPORT CORRODED AT STATION 1256, RBL-90 TO RBL-106. REMOVED AND REPLACED SUPPORT AEA0395-2 REF DAC DWG NEA6398 AND SRM 51-31-01-OG. "MAJOR REPAIR"
- [SDR FDEA202111122837](https://openairdocs.org/sdr/FDEA202111122837.md): Support · corroded · Nov 12, 2021 · N586FE · Doug MD11F · Wing Main, Frame Structure
  > R/H WING REAR SPAR SUPPORT-UPPER O/B IDLER, ARB0042-2 IS CORRODED REMOVED AND REPLACED ARB0042-2 SUPPORT PER DAC DWG ARB0042.
- [SDR FDEA202111102815](https://openairdocs.org/sdr/FDEA202111102815.md): Support · corroded · Nov 10, 2021 · N586FE · Doug MD11F · Fuselage Main, Structure
  > MAIN CARGO DECK, FLOOR PANEL SUPPORT CORRODED AT STA. 979 BETWEEN RBL 75-107 REMOVED AND REPLACED FLOOR SUPPORT P/N ADA 3615-73 AT STA 979 RBL 90 REF SRM 51- 33-01-OG, DAC DWG ADA 3615
- [SDR FDEA202111092803](https://openairdocs.org/sdr/FDEA202111092803.md): Seat Track · corroded · Nov 9, 2021 · N586FE · Doug MD11F · Standard Practices/Structures
  > MAIN CABIN STA. 939 LBL "8.00 REFERENCE FLOOR BOARD 245FF, EXFOLIATION CORRISION EXIST APPROX. DIMENSIONS "2.00 X '1.00 ON SEAT TRACK. REMOVED AND INSTALLED SEAT TRACK AND SPLICES PER SRM 51-41-01-0G, FIG 7 SRM 53-00- 52-2R,FIG 201, SRM 51-33-01-0G.
- [SDR FDEA202111062825](https://openairdocs.org/sdr/FDEA202111062825.md): Support · corroded · Nov 6, 2021 · N586FE · Doug MD11F · Cargo Compartments
  > MAIN CARGO DECK, STA 1661 RBL 48-72 FLOOR SUPPORT CORRODED REMOVED AND REPLACED FLOOR SUPPORT AFA3853-24 REF DAC DWG NFA6018 AND SRM 51- 31-01-OG.
- [SDR FDEA202111062788](https://openairdocs.org/sdr/FDEA202111062788.md): Floor Panel · damaged · Nov 6, 2021 · N586FE · Doug MD11F · Fuselage Floor Panel
  > MAIN CABIN APPORX. STA 1480-1600, RBL 92 FLOOR BOARD FASTNER GROMMETS CORRODED. FABRICATED NEW MAIN DECK FLOOR PANEL AT STA 1480 - STA 1600 RBL 92 PER FEDEX DRAWING SRZ-25-005.
- [SDR FDEA202111022763](https://openairdocs.org/sdr/FDEA202111022763.md): Support · cracked · Nov 2, 2021 · N586FE · Doug MD11F · Fuselage Miscellaneous Structure
  > RH WING FILLET FAIRING SUPPORT RIB (PANELS 152LT/152KT) - CRACK AT INBD ANGLE STA. 5- 113 BETWEEN L36-L37. CRACK CONFIRMED WITH NDT HFEC. FABRICATED AND INSTALLED NEW ANGLE REF DWG A5A7064.
- [SDR FDEA202111022758](https://openairdocs.org/sdr/FDEA202111022758.md): Angle · cracked · Nov 2, 2021 · N586FE · Doug MD11F · Fuselage Main, Attach Fittings
  > RH WING FILLET FAIRING FRAME (BETWEEN PANELS 152LT/152KT) - CRACK STA. 5-113 BTW L28-L29 FABRICATED AND INSTALLED NEW ANGLE REF DWG# A5A7064.
- [SDR FDEA202110242790](https://openairdocs.org/sdr/FDEA202110242790.md): Skin · corroded · Oct 24, 2021 · N586FE · Doug MD11F · Standard Practices/Structures
  > LHS AFT FUSE CANT SKIN AT APPROX STA2128-STA2164, L32L TO L35L HAS EXFOLIATED CORROSION. REPAIRED LHS AFT FUSE CANT SKIN STA 2128-ST A2164 L33L TO L35L PER SRM 53-70-01-2R FIG.202. SHEET 1,2,AND 5
- [SDR FDEA202110192720](https://openairdocs.org/sdr/FDEA202110192720.md): Intercostal · cracked · Oct 19, 2021 · N586FE · Doug MD11F · Cargo/Baggage Doors
  > AFT CARGO AFT DOOR JAMB - STA 1959, STR 40 - INTERCOSTAL CARCKED P/N AGA7211-21 (REMOVAL AND INSTALLATION ON N1196)
- [SDR FDEA202110142634](https://openairdocs.org/sdr/FDEA202110142634.md): Door Frame · corroded · Oct 14, 2021 · N586FE · Doug MD11F · Fuselage Main, Structure
  > AFT CARGO DOOR JAMB - AFT SIDE STA 1959, BETWEEN L40 - L45 HAS INTEGRANULAR CORROSION IN SEVERAL PLACES ON FWD SIDE OF FRAME INSTALLED NEW FRAME P/N: AGA7202-501 REF MD-11 SRM 51-33-01-0G, SRM 51-35-01-0G, AND DRAWING AGA7202, NGA6084. MAJOR REPAIR.
- [SDR FDEA202110132827](https://openairdocs.org/sdr/FDEA202110132827.md): Support · damaged · Oct 13, 2021 · N586FE · Doug MD11F · Cargo Compartments
  > MAIN DECK AT STA 1911 RBL 85-60 FLOOR PANEL SUPPORT BRACKET DAMAGED (MARKED) REMOVED AND REPLACED FLOOR SUPPORT AGA7079-1 REF DAC DWG AGA7127 AND SRM 51-31- 01-OG. "MAJOR REPAIR"
- [SDR FDEA202110122546](https://openairdocs.org/sdr/FDEA202110122546.md): Support · corroded · Oct 12, 2021 · N586FE · Doug MD11F · Fuselage Floor Panel
  > MAIN CABIN STA 1501 RBL 12 FLOOR SUPPORT HAS CORROSION.(REF NR 572 FOR FABRICATION OF SUPPORT). REMOVED AND REPLACED FLOOR SUPPORT AEA0409-1 REF DAC DWG NEA6018 AND SRM 51-38- 01-OG PARAGRAPH 5B.
- [SDR FDEA202110112516](https://openairdocs.org/sdr/FDEA202110112516.md): Skin · unknown · Oct 11, 2021 · N586FE · Doug MD11F · Wing, Plate/Skin
  > REPAIR ASSESSMENT: L/H WING, FIXED LEADING EDGE UPPER SURFACE AT STA. XIS 247 HAS AN EXISTING EXTERNAL REPAIR DOUBLER, APPROX. 9"X 11". DOT 52 REPAIR WAS PREVIOUSLY INSTALLED PER SRM 57-40-02 NFIG. 201 REPAIR 8. REFERNCE E.A. 1- 5100-T0363904 "STRUCTURES-R
- [SDR FDEA202110092786](https://openairdocs.org/sdr/FDEA202110092786.md): Shear Tie · corroded · Oct 9, 2021 · N586FE · Doug MD11F · Fuselage Main, Structure
  > AFT CARGO - CENTER SHEAR-TIE AFT SIDE OF FRAME STA 1967 SHOWS SIGN OF EXFOLIATED CORROSION.(MARKED) REMOVED AND REPLACED SHEAR TIE PER DWG AGA7134 AND SRM51-33-01-OG.
- [SDR FDEA202110082564](https://openairdocs.org/sdr/FDEA202110082564.md): Stiffener · cracked · Oct 8, 2021 · N586FE · Doug MD11F · Fuselage Main, Attach Fittings
  > AFT FUSELAGE (TAIL CONE) BULKHEAD, STA Y 2163, LOWEST STIFFENER CRACKED AT RHS OUTBD EDGE. 0004002951: RODRIGUEZ, HECTOR - 08-NOV-2021 06:52 INSTALLED STIFFENER AND SUPPORT -19 ON LOWER R/H SIDE OUTBOARD EDGE OF AFT FUSELAGE BULKHEAD (TAIL CONE) AT STA
- [SDR FDEA202110082789](https://openairdocs.org/sdr/FDEA202110082789.md): Longeron · corroded · Oct 8, 2021 · N586FE · Doug MD11F · Standard Practices/Structures
  > CAC COMPARTMENT LONGERON L51 (PART # AAA7086-1) CORRODED. REMOVE AND REPLACE LONGERON AAA7086-1 REF DWG NAA6754 AND SRM 51-31-01-OG.
- [SDR FDEA202110082487](https://openairdocs.org/sdr/FDEA202110082487.md): Floor Panel · damaged · Oct 8, 2021 · N586FE · Doug MD11F · Cargo Compartments
  > MAIN CARGO FLOOR PANEL AT STA 759 LBL75-759 IS DAMAGED (MARKED) FABRICATED NEW MAIN CARGO DECK FLOOR PANEL AT STA 759 LBL 75-759 PER FEDEX DRAWING SRZ-25-005
- [SDR FDEA202110050028](https://openairdocs.org/sdr/FDEA202110050028.md): Rudder · corroded · Oct 5, 2021 · N586FE · Doug MD11F · Rudder Control System
  > REMOVE UPPER FWD RUDDER F.O.M. 0000575467: WRAY, BASIL P. B. - 05-JAN-2022 22:23 REMOVED AND INSTALLED SERVICEABLE UPPER FWD RUDDER MPN: NMC6017-529 S/N: 239644 PER AMM 27-20-30-4, 4A-4E, 5A-5H. 0000383059: FAROOQUI, MOHAMMAD Z - 06-JAN-2022 14:48 VARIF
- [SDR FDEA2021102752617](https://openairdocs.org/sdr/FDEA2021102752617.md): Skin · corroded · Oct 5, 2021 · N586FE · Doug MD11F · Fuselage Main, Plate/Skin
  > AFT FUSELAGE - ZONE 312 - UPPER AFT R/H FUSELAGE APROXIMATE STA 2163 TO 2092, STRINGER 11R TO 13R CORROSION PRESENT. AFT FUSELAGE ZONE 312 UPPER AFT R/H FUSELAGE STA 2163.685 TO 2069.440, STRINGER 11R TO 13R CORROSION REPAIR PERFORMED IAW EA 1-5330-T036513
- [SDR FDEA202110052719](https://openairdocs.org/sdr/FDEA202110052719.md): Skin · unknown · Oct 5, 2021 · N586FE · Doug MD11F · Nacelle/Pylon Structure
  > REPAIR ASSESSMENT: REPAIR DOUBLER FOUND ON RH SIDE UPPER SKIN PANEL OF #2 ENGINE NACELLE. DOT 151 REPAIR WAS PREVIOUSLY INSTALLED PER E.A. 1-5480-T0300648 C "NACELLE /PYLON- FILLET/FAIRINGS-LOWER VERTICAL STAB PANEL" REF. E.A. 1-5100-T0363904 'STRUCTURES-
- [SDR FDEA202110030014](https://openairdocs.org/sdr/FDEA202110030014.md): Rudder · corroded · Oct 3, 2021 · N586FE · Doug MD11F · Rudder Control System
  > NEED TO REMOVE UPPER AFT RUDDER FOM. 0000575467: WRAY, BASIL P. B. - 05-JAN-2022 21:21 REMOVED AND INSTALLED SERVICEABLE UPPER AFT RUDDER MPN: NMC6019-505, S/N: 48406 PER AMM 27-20-30-4 1.A.-3.H.
- [SDR FDEA202110013027](https://openairdocs.org/sdr/FDEA202110013027.md): Frame · corroded · Oct 1, 2021 · N586FE · Doug MD11F · Fuselage Main, Structure
  > AFT CARGO - DURING PERFORMING CORROSION REMOVAL OF LWR CLOSE OUT WEB FITTING ABOVE LATCH SPOOLS, FOUND ZEE FRAME P/N AGA7195-3Z HEAVILY CORRODED, REQUIRES NEW ZEE FRAME TO BE FABRICATED FABRICATED NEW ZEE FRAME AGA7195-3 PER DOUGLAS DRAWING AGA7195, MD11 S
- [SDR FDEA202110012441](https://openairdocs.org/sdr/FDEA202110012441.md): Paint · deteriorated · Oct 1, 2021 · N586FE · Doug MD11F · Elevator, Plate/Skin
  > RIGHT OUTBOARD ELEVATOR; UPPER SURFACE PAINT DETERIORATED. PREPPED AND PAINTED R/H O/B ELEVATOR PER SRM 51-21-02-0G
- [SDR FDEA202110012440](https://openairdocs.org/sdr/FDEA202110012440.md): Skin · damaged · Oct 1, 2021 · N586FE · Doug MD11F · Elevator, Plate/Skin
  > R/H OUTBOARD ELEVATOR SKIN FOUND TO HAVE DAMAGED/MISSING STATIC MESH AND LAMINATIONS REPAIRED R/H ELEVATOR I.A.W. SRM 51-21-05-2R REPAIR#1 FIG.201 STEPS 1-7.

Next page: https://openairdocs.org/aircraft/N586FE/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 = 'N586FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N586FE/reports

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