# Service difficulty reports: N620FE

A list on [N620FE](https://openairdocs.org/aircraft/N620FE.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 8 · 352 reports

- [SDR FDEA202608201184](https://openairdocs.org/sdr/FDEA202608201184.md): Indicator · false indication · Aug 20, 2026 · N620FE · Doug MD11F · Escape Slide
  > L1 ESCAPE SLIDE BOTTLE PRESSURE LIGHT DOES NOT ILLUMINATE WHEN PRESSED. RELEASED FOR SERVICE PER MEL: 25-61-02. L1 EVAC SLIDE REMOTE PRESS INDICATOR - INOP. PER MEL 25-61-02, VERIFYAND RECORD IN THE AML, EVAC SLIDE SYS PRESS ADEQAUTE ONCE EACH FLIGHT D
- [SDR FDEA202606190781](https://openairdocs.org/sdr/FDEA202606190781.md): Seat Track · worn · Jun 19, 2026 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 1279, X= -47.5" FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 1279, X = - 47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TR
- [SDR FDEA202606160754](https://openairdocs.org/sdr/FDEA202606160754.md): Seat Track · worn · Jun 16, 2026 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 755, X= -27.5" FOUND CROWN WORN. CABIN - MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 755, X = - 27.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CRO
- [SDR FDEA202606160753](https://openairdocs.org/sdr/FDEA202606160753.md): Longeron Splice · cracked · Jun 16, 2026 · N620FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > LOWER CENTER CARGO COMPARTMENT BILGE AREA LONGERON SPLICE FITTING FOUND CRACK BETWEEN STATION 1801-1821 LONGERON 46 RIGHT. CRACKED LONGERON SPLICE FITTING AT LOWER CENTER CARGO COMPARTMENT BILGE AREA BETWEEN STATION 1801-1821, LONGERON - 46 RIGHT REMOVED A
- [SDR FDEA202606160752](https://openairdocs.org/sdr/FDEA202606160752.md): Seat Track · worn · Jun 16, 2026 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 979, X= -27.5 FOUND CROWN WORN. CABIN - MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 979, X = - 27.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWA
- [SDR FDEA202606150745](https://openairdocs.org/sdr/FDEA202606150745.md): Seat Track · worn · Jun 15, 2026 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO SEAT TRACK AT STATION 1541, X= -47.5" FOUND CROWN WORN. THE SEAT TRACK WAS EVALUATED AND FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT AT BS 1571 TO EXISTING SPLI
- [SDR FDEA202606150744](https://openairdocs.org/sdr/FDEA202606150744.md): Seat Track · worn · Jun 15, 2026 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 1541, X= 27.5" FOUND CROWN WORN. THE SEAT TRACK WAS EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT IAW SRM 53-00-52-2R,
- [SDR FDEA202606150743](https://openairdocs.org/sdr/FDEA202606150743.md): Seat Track · worn · Jun 15, 2026 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 6-10, X= 8.5" FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 6-10, X = 8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAG
- [SDR FDEA202606150742](https://openairdocs.org/sdr/FDEA202606150742.md): Seat Track · worn · Jun 15, 2026 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 6-10, X= 27.5" FOUND CROWN WORN. THE SEAT TRACK WAS EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT IAW SRM 53-00-
- [SDR FDEA202606150741](https://openairdocs.org/sdr/FDEA202606150741.md): Seat Track · worn · Jun 15, 2026 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 6-10, X= 47.5" FOUND CROWN WORN. THE SEAT TRACK BS 6-10, X = 47.5 WAS EVALUATED & FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REP
- [SDR FDEA202606150740](https://openairdocs.org/sdr/FDEA202606150740.md): Seat Track · worn · Jun 15, 2026 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 1279, X= -27.5" FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT AT SEAT TRACK BS 1279, X = - 27.5 WORN CROWN EVALUATED & FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRA
- [SDR FDEA202606150739](https://openairdocs.org/sdr/FDEA202606150739.md): Seat Track · worn · Jun 15, 2026 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 5-10, X= -8.5" FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 5-10, X = - 8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TR
- [SDR FDEA202606150738](https://openairdocs.org/sdr/FDEA202606150738.md): Seat Track · worn · Jun 15, 2026 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 5-10, X= -27.5" FOUND CROWN WORN. THE SEAT TRACK WAS EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT AT BS 5-63 TO EXIS
- [SDR FDEA202606150737](https://openairdocs.org/sdr/FDEA202606150737.md): Seat Track · worn · Jun 15, 2026 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 6-10, X= -8.5" FOUND CROWN WORN. THE SEAT TRACK BS 6-10, X = - 8.5 WAS EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL
- [SDR FDEA202606120729](https://openairdocs.org/sdr/FDEA202606120729.md): Seat Track · worn · Jun 12, 2026 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 1009, X= 27.5 FOUND CROWN WORN. THE SEAT TRACK STATION 1009, X = 27.5 WAS EVALUATED & FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPL
- [SDR FDEA202606120728](https://openairdocs.org/sdr/FDEA202606120728.md): Seat Track · worn · Jun 12, 2026 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 6-10, X= -47.5 FOUND CROWN WORN. THE SEAT TRACK WAS EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT IAW SRM 53-00-52-2
- [SDR FDEA202606120727](https://openairdocs.org/sdr/FDEA202606120727.md): Seat Track · worn · Jun 12, 2026 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 1079, X= -47.5 FOUND CROWN WORN. THE SEAT TRACK BS 1079, X = - 47.5 WAS EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMEN
- [SDR FDEA202606120726](https://openairdocs.org/sdr/FDEA202606120726.md): Seat Track · worn · Jun 12, 2026 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 1009, X= -47.5 FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT, AT SEAT TRACK STATION 1009, X = - 47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CRO
- [SDR FDEA202606120725](https://openairdocs.org/sdr/FDEA202606120725.md): Seat Track · worn · Jun 12, 2026 · N620FE · Doug MD11F · Fuselage Main, Structure
  > MAIN DECK CARGO SEAT TRACK AT STATION 879, X= 27.5 FOUND CROWN WORN. THE SEAT TRACK BS 879, X = 27.5 WAS EVALUATED AND FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT BS 869 TO 909
- [SDR FDEA202606110705](https://openairdocs.org/sdr/FDEA202606110705.md): Seat Track · worn · Jun 11, 2026 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 879, X= -27.5 FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 879, X = - 27.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN
- [SDR FDEA202606110704](https://openairdocs.org/sdr/FDEA202606110704.md): Seat Track · worn · Jun 11, 2026 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 839, X= -8.5 FOUND CROWN WORN. THE SEAT TRACK STATION 839, X = - 8.5 EVALUATED AND FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT
- [SDR FDEA202606110703](https://openairdocs.org/sdr/FDEA202606110703.md): Seat Track · worn · Jun 11, 2026 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 806, X= -8.5 FOUND CROWN WORN. SEAT TRACK STATION 810, X = - 8.5 CROWN EVALUATED AND FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACE
- [SDR FDEA202606110702](https://openairdocs.org/sdr/FDEA202606110702.md): Seat Track · worn · Jun 11, 2026 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 806, X= 8.5 FOUND CROWN WORN. EVALUATED AND FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A, FIGURE 101 ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT AT EXISTING SPLICES BS 745 TO 806,
- [SDR FDEA202502050174](https://openairdocs.org/sdr/FDEA202502050174.md): Gland Nut · leaking · Feb 5, 2025 · N620FE · Doug MD11F · Landing Gear Retraction/Extension System
  > UNABLE TO RAISE LANDING GEAR HANDLE ON TAKEOFF. COMPLIED WITH QRH. STILL COULD NOT RAISE GEAR. FOUND MLG TRIM INTERLOCK CYLINDER NOT MOVING WITH HYDS ON, STOPPING MOVEMENT OF GEAR SELECTOR QUADRANT & VALVE. R & R TRIM CYLINDER INTERLOCK FUSE IAW AMM 32-37-06
- [SDR FDEA202411201698](https://openairdocs.org/sdr/FDEA202411201698.md): Drain Line · leaking · Nov 20, 2024 · N620FE · Doug MD11F · Hydraulic System, Main
  > HYD 3 FAIL ON DESCENT. EMERGENCY DECLARED. SYSTEM 3 FOUND EMPTY AT COCKPIT INDICATION AT BLOCK IN. OPENED #3 ENGINE FOR POSSIBLE LEAKS AND WHILE DRY MOTORING PER JRH CHAPTER 5 SAW LARGE AMOUNT OF HYDRAULIC FLUID EXITING THE RIGHT FLUID DISCONNECT PANEL SCU
- [SDR FDEA202411151678](https://openairdocs.org/sdr/FDEA202411151678.md): Wheel · missing · Nov 15, 2024 · N620FE · Doug MD11F · Wheel/Ski/Float
  > PILOTS WERE INFORMED AT BLOCK IN THAT #9 WHEEL WAS MISSING. NO PHYSICAL INDICATION ON EITHER TO OR LANDING. INSTALLED NEW.
- [SDR FDEA202407140999](https://openairdocs.org/sdr/FDEA202407140999.md): Lamp · failed · Jul 14, 2024 · N620FE · Doug MD11F · Landing Gear Position and Warning
  > NOSE GEAR INDICATOR LIGHT OUT. SECONDARY GEAR INDICATOR (CONFIG PAGE) INDICATED ALL DOWN AND LOCKED. EMERGENCY DECLARED. LANDED WITHOUT INCIDENT. EMERGENCY DECLARED AMM 33-11-17-2 AMM 32-61-00-5 PER CREW DEBRIEF PRIMARY LIGHTS WERE INOP BUT CONFIG SYNO
- [SDR FDEA202403220345](https://openairdocs.org/sdr/FDEA202403220345.md): Lamp · inoperative · Mar 22, 2024 · N620FE · Doug MD11F · Emergency Equipment
  > ON POST FLIGHT WALK AROUND FOUND R1 DOOR SLIDE TEST LIGHT INOP WITH RELAMP UNSUCCESSFUL. RELAMPED WITH 368 BLUBS OPS CKS GOOD.
- [SDR FDEA202403030240](https://openairdocs.org/sdr/FDEA202403030240.md): Bracket · corroded · Mar 3, 2024 · N620FE · Doug MD11F · Wing, Control Surface Attach Fittings
  > 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 REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM57-44-07. OVE
- [SDR FDEA202403030239](https://openairdocs.org/sdr/FDEA202403030239.md): Bracket · corroded · Mar 3, 2024 · N620FE · Doug MD11F · Wing, Control Surface Attach Fittings
  > RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE SURFACE FOUND CORROSION. CORROSION AT RIGHT WING-WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-07. REPAIR EVALUATED AND FOUND
- [SDR FDEA202403030238](https://openairdocs.org/sdr/FDEA202403030238.md): Bracket · corroded · Mar 3, 2024 · N620FE · Doug MD11F · Wing, Control Surface Attach Fittings
  > 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 REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM57-44-07. OVERS
- [SDR FDEA202403030237](https://openairdocs.org/sdr/FDEA202403030237.md): Bracket · corroded · Mar 3, 2024 · N620FE · Doug MD11F · Wing, Control Surface Attach Fittings
  > 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 REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM57-44-07. OVERSIZED REPAIR BUSHING FABRICAT
- [SDR FDEA202403030236](https://openairdocs.org/sdr/FDEA202403030236.md): Bracket · corroded · Mar 3, 2024 · N620FE · Doug MD11F · Wing, Control Surface Attach Fittings
  > 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 REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM57-44-07. OVERSIZED REPAIR BUSHING FABRICATED
- [SDR FDEA202403030235](https://openairdocs.org/sdr/FDEA202403030235.md): Bracket · corroded · Mar 3, 2024 · N620FE · Doug MD11F · Wing, Control Surface Attach Fittings
  > LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING-WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM57-44-07. OVERS
- [SDR FDEA202403030234](https://openairdocs.org/sdr/FDEA202403030234.md): Bracket · corroded · Mar 3, 2024 · N620FE · Doug MD11F · Wing, Control Surface Attach Fittings
  > LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING-WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM57-44-07. OVERSIZ
- [SDR FDEA202403030233](https://openairdocs.org/sdr/FDEA202403030233.md): Bracket · corroded · Mar 3, 2024 · N620FE · Doug MD11F · Wing, Control Surface Attach Fittings
  > RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING-FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-52-03. OVERSIZED
- [SDR FDEA202403030232](https://openairdocs.org/sdr/FDEA202403030232.md): Bracket · corroded · Mar 3, 2024 · N620FE · Doug MD11F · Wing, Control Surface Attach Fittings
  > RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE SURFACE FOUND CORROSION. CORROSION AT RIGHT WING-FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-52-03. REP
- [SDR FDEA202403030231](https://openairdocs.org/sdr/FDEA202403030231.md): Bracket · corroded · Mar 3, 2024 · N620FE · Doug MD11F · Wing, Control Surface Attach Fittings
  > RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING-FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-52-03. OVERSIZED
- [SDR FDEA202403030230](https://openairdocs.org/sdr/FDEA202403030230.md): Bracket · corroded · Mar 3, 2024 · N620FE · Doug MD11F · Wing, Control Surface Attach Fittings
  > LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE SURFACE FOUND CORROSION. CORROSION AT LEFT WING-FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-52-03. REPAIR
- [SDR FDEA202403030229](https://openairdocs.org/sdr/FDEA202403030229.md): Bracket · corroded · Mar 3, 2024 · N620FE · Doug MD11F · Wing, Control Surface Attach Fittings
  > LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING-FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-52-03. OVERSIZED
- [SDR FDEA202403030228](https://openairdocs.org/sdr/FDEA202403030228.md): Bracket · corroded · Mar 3, 2024 · N620FE · Doug MD11F · Wing, Control Surface Attach Fittings
  > LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING-FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-52-03. OVERSIZED B
- [SDR FDEA202402280220](https://openairdocs.org/sdr/FDEA202402280220.md): Floor Panel · damaged · Feb 28, 2024 · N620FE · Doug MD11F · Fuselage Floor Panel
  > CABIN - RIGHT HAND FLOOR PANEL #272EF VIEW PORT CUTOUT HOLE FOUND DAMAGE AT STATION 1381, X = - 50. CABIN - DAMAGED RIGHT HAND FLOOR PANEL #272EF AT STATION 1381, X = - 50 REMOVED AND REPLACED AS PER MD-11 AMM 53-21-04-4. RIGHT HAND FLOOR PANEL #272EF FABR
- [SDR FDEA202402280219](https://openairdocs.org/sdr/FDEA202402280219.md): Floor Panel · damaged · Feb 28, 2024 · N620FE · Doug MD11F · Fuselage Floor Panel
  > CABIN - LEFT HAND FLOOR PANEL #271EF VIEW PORT CUTOUT HOLE FOUND DAMAGE AT STATION 1381, X = 50. CABIN - DAMAGED LEFT HAND FLOOR PANEL #271EF AT STATION 1381, X = 50 REMOVED AND REPLACED AS PER MD-11 AMM 53-21-04-4. LEFT HAND FLOOR PANEL #271EF FABRICATED
- [SDR FDEA202402140159](https://openairdocs.org/sdr/FDEA202402140159.md): Stringer · cracked · Feb 14, 2024 · N620FE · Doug MD11F · Wing, Longeron/Stringer
  > UPPER AUX TANK STRINGER 47 AT STATION XCW 17 FOUND CRACK. UPPER AUXILLARY TANK STRINGER 47 AT STATION XCW 17 CRACKED AREA REPAIR CARRIED OUT AS PER MD-11 SRM 57-10-03-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6- 2-100.
- [SDR FDEA202402140158](https://openairdocs.org/sdr/FDEA202402140158.md): Stringer · cracked · Feb 14, 2024 · N620FE · Doug MD11F · Wing, Longeron/Stringer
  > UPPER AUX TANK STRINGER 47 AT STATION XCW -46.5 FOUND CRACK. UPPER AUXILLARY TANK STRINGER 47 AT STAION XCW - 46.5 CRACKED AREA REPAIR CARRIED OUT AS PER MD-11 SRM 57-10-03-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA202402120151](https://openairdocs.org/sdr/FDEA202402120151.md): Seat Track · damaged · Feb 12, 2024 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK RIGHT HAND STATION 1541, X = -8.5 FOUND CROWN DAMAGE. AT RIGHT HAND SEAT TRACK STATION 1541, X = - 8.5 DAMAGED CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK
- [SDR FDEA202402120150](https://openairdocs.org/sdr/FDEA202402120150.md): Seat Track · damaged · Feb 12, 2024 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK RIGHT HAND STATION 1421, X = -8.5 FOUND CROWN DAMAGE. AT RIGHT HAND SEAT TRACK STATION 1421, X = - 8.5 DAMAGED CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK
- [SDR FDEA202402120149](https://openairdocs.org/sdr/FDEA202402120149.md): Seat Track · damaged · Feb 12, 2024 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK LEFT HAND STATION 1381, X = 8.5 FOUND CROWN DAMAGE. AT LEFT HAND SEAT TRACK STATION 1381, X = 8.5 DAMAGED CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REPA
- [SDR FDEA202402120148](https://openairdocs.org/sdr/FDEA202402120148.md): Seat Track · damaged · Feb 12, 2024 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK RIGHT HAND STATION 1341, X = -8.5 FOUND CROWN DAMAGE. AT RIGHT HAND SEAT TRACK STATION 1341, X = - 8.5 DAMAGED CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK
- [SDR FDEA202402120147](https://openairdocs.org/sdr/FDEA202402120147.md): Seat Track · damaged · Feb 12, 2024 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK LEFT HAND STATION 1219, X = 8.5 FOUND CROWN DAMAGE. AT LEFT HAND SEAT TRACK STATION 1219, X = 8.5 DAMAGED CROWN EVALUATED AND FOUND EXCEED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REPAIR

Next page: https://openairdocs.org/aircraft/N620FE/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 = 'N620FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N620FE/reports

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