# Service difficulty reports: N598FE

A list on [N598FE](https://openairdocs.org/aircraft/N598FE.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 · 281 reports

- [SDR FDEA202111232932](https://openairdocs.org/sdr/FDEA202111232932.md): None · none · Nov 23, 2021 · N598FE · Doug MD11F · Emergency Lighting
  > MDIS 598 33-50 4370 23NOV21 CRK FACT U DURING PRE FLIGHT CHECK FOUND EMER LIGHT BAT 1 LOW. MEL 23NOV21 04:24 CRK U RELEASED FOR SERVICE PER MEL: 33-50-04 CATEGORY: C EXPIRATION: 02DEC21 "MEL 33-50-04: EMER LIGHTS - INOP." CTR NO: 729
- [SDR FDEA202105251391](https://openairdocs.org/sdr/FDEA202105251391.md): Spar Cap · cracked · May 25, 2021 · N598FE · Doug MD11F · Vertical Stabilizer, Spar/Rib
  > DURING ULTRASONIC INSPECTION FOR VERTICAL CRACKS BEHIND SERVICE REPAIR SR10550013 PER DRAWING NO. SN10550000 REVISION C ON LEFT HAND SIDE LOWER VERTICAL STABILIZER FORWARD FLANGE OF UPPER REAR SPAR CAP, STATION 2164, EXISTING CRACK INDICATION FOUND FROM
- [SDR FDEA202105251389](https://openairdocs.org/sdr/FDEA202105251389.md): Frame · cracked · May 25, 2021 · N598FE · Doug MD11F · Fuselage Main, Frame
  > MAIN DECK CARGO COMPARTMENT-CABIN, DURING REMOVAL OF INSULATION BLANKET FOR SUPPORT BRACKET RECTIFICATION, FOUND FRAME AT STATION 5-32, LONGERON 12 LEFT CRACKED. MAIN DECK CARGO COMPARTMENT-CABIN AT LEFT HAND FRAME STATION 5-32, LONGERON 12 LEFT CRACKED
- [SDR FDEA202105251386](https://openairdocs.org/sdr/FDEA202105251386.md): Frame · dented · May 25, 2021 · N598FE · Doug MD11F · Fuselage Main, Frame
  > MAIN DECK CARGO COMPARTMENT-CABIN, FOUND FRAME AT STATION 1741, LONGERON 12 LEFT WITH DENT. MAIN DECK CARGO COMPARTMENT-CABIN AT LEFT HAND FRAME STATION 1741, LONGERON 12 LEFT DENT AREA REPAIRED AS PER SRM 53-00-07-2R FIGURE 201 REPAIR 2. REPETITIVE INSP
- [SDR FDEA202105251385](https://openairdocs.org/sdr/FDEA202105251385.md): Frame · dented · May 25, 2021 · N598FE · Doug MD11F · Fuselage Main, Frame
  > MAIN DECK CARGO COMPARTMENT-CABIN FOUND FRAME AT STATION 1761, LONGERON 12 LEFT WITH DENT MAIN DECK CARGO COMPARTMENT-CABIN AT LEFT HAND FRAME STATION 1761, LONGERON 12 LEFT DENT AREA REPAIRED AS PER SRM 53-00-07-2R FIGURE 201 REPAIR 2. REPETITIVE INSPEC
- [SDR FDEA202105251382](https://openairdocs.org/sdr/FDEA202105251382.md): Floor Panel · delaminated · May 25, 2021 · N598FE · Doug MD11F · Fuselage Floor Panel
  > FLIGHT DECK, FOUND FLOOR PANEL #216BF DELAMINATED. DELAMINATED FLOOR PANEL #216BF AT CABIN STATION 366 Ï¿½ STATION 386 REMOVED AS PER AMM 53-21-04. FLOOR PANEL #216BF FABRICATED AS PER FEDEX DRAWING SRZ-25-005 REVISION R. FLOOR PANEL #216BF INSTALLED AS PE
- [SDR FDEA202105251381](https://openairdocs.org/sdr/FDEA202105251381.md): Floor Panel · delaminated · May 25, 2021 · N598FE · Doug MD11F · Fuselage Floor Panel
  > FLIGHT DECK, FOUND FLOOR PANEL #215DF DELAMINATED. DELAMINATED FLOOR PANEL #215DF AT CABIN STATION 334 Ï¿½ STATION 366 REMOVED AS PER AMM 53-21-04. FLOOR PANEL #215DF FABRICATED AS PER FEDEX DRAWING SRZ-25-005 REVISION R. FLOOR PANEL #215DF INSTALLED AS PE
- [SDR FDEA202105251379](https://openairdocs.org/sdr/FDEA202105251379.md): Floor Panel · delaminated · May 25, 2021 · N598FE · Doug MD11F · Fuselage Floor Panel
  > FLIGHT DECK, FOUND FLOOR PANEL #217AF DELAMINATED. DELAMINATED FLOOR PANEL #217AF AT CABIN STATION 330 Ï¿½ STATION 352.5 REMOVED AS PER AMM 53-21-04. FLOOR PANEL #217AF FABRICATED AS PER FEDEX DRAWING SRZ-25-005 REVISION R. FLOOR PANEL #217AF INSTALLED AS
- [SDR FDEA202105241374](https://openairdocs.org/sdr/FDEA202105241374.md): Seat Track · worn · May 24, 2021 · N598FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT-CABIN, FOUND SEAT TRACK AT STATION 6-10, X = 8.5 CROWN AREA WORN MAIN DECK CARGO COMPARTMENT - CABIN AT SEAT TRACK STATION 6-10, X = 8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABL
- [SDR FDEA202105241373](https://openairdocs.org/sdr/FDEA202105241373.md): Seat Track · worn · May 24, 2021 · N598FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT-CABIN, FOUND SEAT TRACK AT STATION 6-10, X = -8.5 CROWN AREA WORN. MAIN DECK CARGO COMPARTMENT - CABIN AT SEAT TRACK STATION 6-10, X = -8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWA
- [SDR FDEA202105231362](https://openairdocs.org/sdr/FDEA202105231362.md): Skin · cracked · May 23, 2021 · N598FE · Doug MD11F · Wing, Plate/Skin
  > HIGH FREQUENCY EDDY CURRENT INSPECTION ON CORNER 13 OF LEFT HAND FIXED LEADING EDGE SKIN ADJACENT TO CUTOUT FOUND CRACK APPROXIMATELY 0.3 INCH AT STATION XOS 657.25 LEFT HAND FIXED LEADING EDGE SKIN ADJACENT TO CUTOUT CORNER 13 CRACK APPROXIMATELY 0.3 IN
- [SDR FDEA202105231361](https://openairdocs.org/sdr/FDEA202105231361.md): Skin · cracked · May 23, 2021 · N598FE · Doug MD11F · Wing, Plate/Skin
  > RIGHT HAND WING FIXED LEADING EDGE SKIN EXISTING REPAIR DOUBLER FOUND CRACK AT STATION XOS 906. RIGHT HAND WING FIXED LEADING EDGE SKIN CRACKED EXISTING REPAIR DOUBLER AT STATION XOS 906 REMOVED AS PER MD11 SRM 51-31-01-0G AND REPAIRED AS PER MD11 SRM 57
- [SDR FDEA202105231358](https://openairdocs.org/sdr/FDEA202105231358.md): Doubler · cracked · May 23, 2021 · N598FE · Doug MD11F · Wing, Plate/Skin
  > LEFT HAND WING FIXED LEADING EDGE BEADED DOUBLER FOUND CRACK AT STATION XOS 765. LEFT HAND WING FIXED LEADING EDGE DOUBLER CRACK AT STATION X0S 765 REPAIRED AS PER MD11 SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6- 2-100.
- [SDR FDEA202105231360](https://openairdocs.org/sdr/FDEA202105231360.md): Doubler · cracked · May 23, 2021 · N598FE · Doug MD11F · Wing, Plate/Skin
  > LEFT HAND WING FIXED LEADING EDGE RIB DOUBLER FOUND CRACK AT STATION XOS 789. LEFT HAND WING FIXED LEADING EDGE RIB DOUBLER CRACK AT XOS 789 REMOVED AS PER MD11 SRM 51-33-01-0G. RIB DOUBLER FABRICATED AS PER DOUGLAS DRAWING ARB3954 REVISION: K AND INSTA
- [SDR FDEA202105231359](https://openairdocs.org/sdr/FDEA202105231359.md): Doubler · cracked · May 23, 2021 · N598FE · Doug MD11F · Wing, Plate/Skin
  > LEFT HAND WING FIXED LEADING EDGE SKIN SUPPORT BEADED DOUBLER FOUND CRACK AT STATION XOS 545. LEFT HAND WING FIXED LEADING EDGE SKIN SUPPORT BEADED DOUBLER AT STATION XOS 545 REPAIRED AS PER MD11 SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS
- [SDR FDEA202101030005](https://openairdocs.org/sdr/FDEA202101030005.md): Indicator · inoperative · Jan 3, 2021 · N598FE · Doug MD11F · Emergency Equipment
  > L-1 ENTRY DOOR EVAC SLIDE REMOTE PRESS INDICATOR DOES NOT TEST. L-1 ENTRY DOOR EVAC SLIDE REMOTE PRESS INDICATOR INOP. REMOVED AND REPLACED REMOTE PRESSURE INDICATOR ASSEMBLY PER MD11 AMM 25-61-04-4 AND MD11 IPC 25-61-05-01 ITEM 160. PERFORMED OPERAT
- [SDR FDEA202011012751](https://openairdocs.org/sdr/FDEA202011012751.md): Skin · damaged · Nov 1, 2020 · N598FE · Doug MD11F · Fuselage Main, Plate/Skin
  > NR 3 PACK DOOR CUT OUT UPPER AFT CORNER SKIN LOOKS TO BE CRACKED. PERFORMED HFEC OF SUSPECTED DAMAGED AREA, REF BOEING NTSPM 06-10-.01 PROCEDURE 11. CONFIRMED CRACK DEFECT INDICATION AND MARKED LENGTH. SHGN 02NOV20 06:31 MEM U. DUCT IN PACK 3 BAY REMOVED T
- [SDR FDEA202005080913](https://openairdocs.org/sdr/FDEA202005080913.md): Light · inoperative · May 8, 2020 · N598FE · Doug MD11F · Escape Slide
  > L1 EVACUATION SLIDE REMOTE PRESSURE PRESS TO TEST LIGHT INOP. RELEASED FOR SERVICE PER MEL: 25-61-02 CATEGORY: C EXPIRATION: 18MAY20 MEL 25-61-02: L1 EVAC SLIDE REMOTE PRESS INDICATOR - INOP. PER MEL 25-61-02, VERIFY AND RECORD IN THE AML, EVAC SLIDE SY
- [SDR FDEA2019100752444](https://openairdocs.org/sdr/FDEA2019100752444.md): Cable · failed · Oct 5, 2019 · N598FE · Doug MD11F · Landing Gear Brake System
  > UNABLE TO SET PARK BRAKE.PARK BRAKE KEEPS SPRINGING BACK. PARKING BRAKE CABLE AND ROD END REPLACED IAW AMM 32-44-00-5. OPS CHECKED GOOD. ACFT OK FOR SERVICE.
- [SDR FDEA201907021460](https://openairdocs.org/sdr/FDEA201907021460.md): Spring · broken · Jul 2, 2019 · N598FE · Doug MD11F · Passenger/Crew Doors
  > MDIS 598 52-10 1538 02JUL19 IND OPEN U WHEN AIRCRAFT BLOCKED IN THE L1 MAIN CABIN DOOR EMERGENCY EXIT SIGN MOVABLE CEILING PANEL WOULD NOT GO UP WITH DOOR INTO CEILING. SEEMS THE DRIVE CABLE IS BROKEN MEL 02JUL19 06:52 IND U RELEASED FOR SERV
- [SDR FDEA201906071252](https://openairdocs.org/sdr/FDEA201906071252.md): Bracket · corroded · Jun 7, 2019 · N598FE · Doug MD11F · Trailing Edge Flaps
  > RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM
- [SDR FDEA201906071251](https://openairdocs.org/sdr/FDEA201906071251.md): Bracket · corroded · Jun 7, 2019 · N598FE · Doug MD11F · Trailing Edge Flaps
  > RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57
- [SDR FDEA201906071249](https://openairdocs.org/sdr/FDEA201906071249.md): Bracket · corroded · Jun 7, 2019 · N598FE · Doug MD11F · Trailing Edge Flaps
  > LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION.
- [SDR FDEA2019060641210](https://openairdocs.org/sdr/FDEA2019060641210.md): Floor Support · corroded · Jun 4, 2019 · N598FE · Doug MD11F · Fuselage Miscellaneous Structure
  > MAIN DECK AFT FLOOR SUPPORT AT STATION 1887 - 2007 X = - 57 FOUND CORROSION. MAIN DECK AFT FLOOR SUPPORT AT STATION 1887 TO STATION 2007 X = - 57, CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-00-2R FIGURE 206. CORRODED FLOOR SUPPORT R
- [SDR FDEA2019060321206](https://openairdocs.org/sdr/FDEA2019060321206.md): Skin · corroded · Jun 2, 2019 · N598FE · Doug MD11F · Wing, Plate/Skin
  > RIGHT WING UPPER WING SURFACE TRAILING EDGE FOUND CORROSION AT XORS 1070. REPAIR CARRIED OUT AT RIGHT WING - UPPER WING SURFACE TRAILING EDGE AT XORS 1070 AS PER ENGINEERING AUTHORIZATION: 1-5730-T0347222 P1 TITLE: WING - PLATES AND SKINS - RIGHT WING -
- [SDR FDEA2019060311196](https://openairdocs.org/sdr/FDEA2019060311196.md): Bracket · corroded · May 31, 2019 · N598FE · Doug MD11F · Wing, Attach Fittings
  > RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT HOLE SURFACE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT HOLE SURFACE REWORKED AS PER MD-11 CMM 57-44-08 AND FOUND LOWER BARREL NUT FACE EXCEED L
- [SDR FDEA2019060311195](https://openairdocs.org/sdr/FDEA2019060311195.md): Bracket · corroded · May 31, 2019 · N598FE · Doug MD11F · Wing, Attach Fittings
  > LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT HOLE SURFACE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT HOLE SURFACE REWORKED AS PER MD-11 CMM 57-44-08 AND FOUND LOWER AND UPPER BARREL NUT FACE
- [SDR FDEA201905301185](https://openairdocs.org/sdr/FDEA201905301185.md): Skin · dented · May 30, 2019 · N598FE · Doug MD11F · Cargo/Baggage Doors
  > AFT CARGO DOOR FORWARD EDGE APPROXIMATELY10 INCHES BELOW FORWARD UPPER CORNER FOUND DENT 5.5" LENGTH X 1.5" WIDTH X 0.086"DEPTH AT STATION Y = 1942 DENT AT AFT CARGO DOOR FORWARD EDGE APPROXIMATELY 10 INCHES BELOW FORWARD UPPER CORNER CARRIED OUT REPAIRED
- [SDR FDEA201905301184](https://openairdocs.org/sdr/FDEA201905301184.md): Seat Track · corroded · May 30, 2019 · N598FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK RIGHT HAND OUTBOARD FLOOR CURVE SEAT TRACK AT STATION 421 X = -107.25 FOUND CORROSION. MAIN DECK RIGHT HAND OUTBOARD FLOOR AT CURVE SEAT TRACK STATION 421 X = - 107.25, CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE
- [SDR FDEA2019052861169](https://openairdocs.org/sdr/FDEA2019052861169.md): Bracket · corroded · May 26, 2019 · N598FE · Doug MD11F · Trailing Edge Flaps
  > RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (#3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-07. OVERSIZED BUSHING FABR
- [SDR FDEA2019052861168](https://openairdocs.org/sdr/FDEA2019052861168.md): Bracket · corroded · May 26, 2019 · N598FE · Doug MD11F · Trailing Edge Flaps
  > LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (#3 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. REPAIR BUSHING FABRICATE
- [SDR FDEA2019052861167](https://openairdocs.org/sdr/FDEA2019052861167.md): Skin · cracked · May 26, 2019 · N598FE · Doug MD11F · Wing, Plate/Skin
  > HFEC INSPECTION CARRY OUT AND FOUND CRACK APPROXIMATELY 1/4" IN LENGTH AT LEFT HAND SIDE CORNER NUMBER 11 FUEL ACCESS DOOR FORWARD INBOARD CORNER. REPAIR CARRIED OUT AT LEFT HAND SIDE CORNER NO.11 FUEL ACCESS DOOR FORWARD INBOARD CORNER AT XOS 586 AS PER S
- [SDR FDEA2019052861166](https://openairdocs.org/sdr/FDEA2019052861166.md): Former · cracked · May 26, 2019 · N598FE · Doug MD11F · Wing Spar
  > LEFT HAND WING FIXED LEADING EDGE COMPARTMENT STATION XOS 939 FORMER FOUND CRACKED. CRACKED FORMER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED FORMER AS PER DOUGLAS DRAWING ARB1292 REVISION G. INSTALLED FORMER AT LEFT HAND WING FIXED LEADING EDGE COMPA
- [SDR FDEA201905261165](https://openairdocs.org/sdr/FDEA201905261165.md): Doubler · cracked · May 26, 2019 · N598FE · Doug MD11F · Wing Main, Frame Structure
  > RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT STATION XOS 605 LOWER STRINGER DOUBLER FOUND CRACKED. CRACKED DOUBLER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED DOUBLER AS PER DOUGLAS DRAWING ARB2933 REVISION AJ. INSTALLED DOUBLER AT RIGHT HAND WING FIXE
- [SDR FDEA2019052861164](https://openairdocs.org/sdr/FDEA2019052861164.md): Doubler · cracked · May 26, 2019 · N598FE · Doug MD11F · Wing Main, Frame Structure
  > LEFT HAND WING FIXED LEADING EDGE COMPARTMENT LOWER STATION XOS 546 STRINGER DOUBLER FOUND CRACKED. CRACKED DOUBLER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED DOUBLER AS PER DOUGLAS DRAWING ARB2933 REVISION AJ. INSTALLED FABRICATED DOUBLER AT LEFT HAND
- [SDR FDEA201905241151](https://openairdocs.org/sdr/FDEA201905241151.md): Hinge Bracket · corroded · May 24, 2019 · N598FE · Doug MD11F · Trailing Edge Flaps
  > RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE OUTBOARD LUG HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE OUTBOARD LUG HOLE BORE (A AND B HOLES) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57
- [SDR FDEA201905241150](https://openairdocs.org/sdr/FDEA201905241150.md): Hinge Bracket · corroded · May 24, 2019 · N598FE · Doug MD11F · Trailing Edge Flaps
  > RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE INBOARD LUG HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE INBOARD LUG HOLE BORE (G AND F HOLES) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-5
- [SDR FDEA201905241149](https://openairdocs.org/sdr/FDEA201905241149.md): Hinge Bracket · corroded · May 24, 2019 · N598FE · Doug MD11F · Trailing Edge Flaps
  > LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE OUTBOARD LUG HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE OUTBOARD LUG HOLE BORE (A AND B HOLES) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-5
- [SDR FDEA201905241148](https://openairdocs.org/sdr/FDEA201905241148.md): Hinge Bracket · corroded · May 24, 2019 · N598FE · Doug MD11F · Trailing Edge Flaps
  > LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE INBOARD LUG HOLE BORE (G AND F HOLES) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52
- [SDR FDEA201905241147](https://openairdocs.org/sdr/FDEA201905241147.md): Bracket · corroded · May 24, 2019 · N598FE · Doug MD11F · Trailing Edge Flaps
  > RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD HOLE SURFACE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-
- [SDR FDEA201905241146](https://openairdocs.org/sdr/FDEA201905241146.md): Bracket · corroded · May 24, 2019 · N598FE · Doug MD11F · Trailing Edge Flaps
  > RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INBOARD HOLE SURFACE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INBOARD HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44- 08
- [SDR FDEA201905241144](https://openairdocs.org/sdr/FDEA201905241144.md): Bracket · corroded · May 24, 2019 · N598FE · Doug MD11F · Trailing Edge Flaps
  > RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57
- [SDR FDEA201905241142](https://openairdocs.org/sdr/FDEA201905241142.md): Bracket · corroded · May 24, 2019 · N598FE · Doug MD11F · Trailing Edge Flaps
  > RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM
- [SDR FDEA201905241140](https://openairdocs.org/sdr/FDEA201905241140.md): Bracket · corroded · May 24, 2019 · N598FE · Doug MD11F · Trailing Edge Flaps
  > RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57
- [SDR FDEA201905241152](https://openairdocs.org/sdr/FDEA201905241152.md): Frame · chafed · May 24, 2019 · N598FE · Doug MD11F · Fuselage Main, Frame
  > MAIN DECK LEFT HAND FRAME AT STATION 535 LONGERON 24 LEFT FOUND EXISTING REPAIR OUTER ANGLE CHAFFED. MAIN DECK LEFT HAND FRAME AT STATION 535 LONGERON 24 LEFT, CHAFFED MARK AT EXISTING OUTER REPAIR ANGLE REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00
- [SDR FDEA2019052431131](https://openairdocs.org/sdr/FDEA2019052431131.md): Bracket · corroded · May 23, 2019 · N598FE · Doug MD11F · Trailing Edge Flaps
  > RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE FORWARD MOUNT OUTBOARD LUG HOLE SURFACE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE FORWARD MOUNT OUTBOARD LUG HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-1
- [SDR FDEA2019052431130](https://openairdocs.org/sdr/FDEA2019052431130.md): Bracket · corroded · May 23, 2019 · N598FE · Doug MD11F · Trailing Edge Flaps
  > RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CM
- [SDR FDEA2019052431129](https://openairdocs.org/sdr/FDEA2019052431129.md): Bracket · corroded · May 23, 2019 · N598FE · Doug MD11F · Trailing Edge Flaps
  > RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM
- [SDR FDEA2019052431128](https://openairdocs.org/sdr/FDEA2019052431128.md): Bracket · corroded · May 23, 2019 · N598FE · Doug MD11F · Trailing Edge Flaps
  > RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE (#3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM
- [SDR FDEA2019052431127](https://openairdocs.org/sdr/FDEA2019052431127.md): Bracket · corroded · May 23, 2019 · N598FE · Doug MD11F · Trailing Edge Flaps
  > RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT INBOARD HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT INBOARD HOLE BORE (#3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-

Next page: https://openairdocs.org/aircraft/N598FE/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 = 'N598FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N598FE/reports

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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.