# Service difficulty reports: N574FE

A list on [N574FE](https://openairdocs.org/aircraft/N574FE.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 13 · 611 reports

- [SDR FDEA202609291447](https://openairdocs.org/sdr/FDEA202609291447.md): Battery Pack · discharged · Sep 29, 2026 · N574FE · Doug MD11F · Emergency Lighting
  > DURING PRE-FLIGHT EMERGENCY LIGHTS TEST, EMERGENCY LIGHT BATTERY 1 LOW ILLUMINATED. RELEASED FOR SERVICE PER MEL: 33-50-04. REMOVED AND REPLACED BATTERY IAW AMM 33-51-01-4-0. OPS CHKD NORMAL.
- [SDR FDEA202609011257](https://openairdocs.org/sdr/FDEA202609011257.md): Pressure Switch · no test · Sep 1, 2026 · N574FE · Doug MD11F · Emergency Equipment
  > DOOR L1 PNEUMATIC BOTTLE CIRCUITRY TEST LIGHT DOES NOT ILLUMINATE WHEN PRESSED. REMOVED AND INSTALLED SERVICEABLE L1 DOOR REMOTE PERSSURE INDICATOR ASSEMBLY. OPS CHECK GOOD.
- [SDR FDEA202606100694](https://openairdocs.org/sdr/FDEA202606100694.md): Bearing · damaged · Jun 10, 2026 · N574FE · Doug MD11F · Nacelle/Pylon, Main Frame
  > NR 3 ENGINE PYLON AFT BULKHEAD LUG BORE HOLE FOUND WITH CORROSION AFTER SPHERICAL BEARING REMOVED. CORROSION AT 3 ENGINE PYLON AFT BULKHEAD LUG BORE HOLE CARRIED OUT REPAIR AS PER EA 1-5440-T0387710 PART 1. REPAIR CLASSIFED AS MAJOR IAW GMM 6-2-100.
- [SDR FDEA202606100693](https://openairdocs.org/sdr/FDEA202606100693.md): Bearing · damaged · Jun 10, 2026 · N574FE · Doug MD11F · Nacelle/Pylon, Main Frame
  > NR 1 ENGINE PYLON AFT BULKHEAD LUG BORE HOLE FOUND WITH EXISTING DAMAGE AND CORROSION AFTER SPHERICAL BEARING REMOVED. REPAIR CARRIED OUT AS PER EA# 1-5440-T0387712 PART1 AND PART 2 AND PART 3. NR 1 PYLON, REMOVAL AND REPLACEMENT OF AFT BULKHEAD THIS EA DE
- [SDR FDEA202511102154](https://openairdocs.org/sdr/FDEA202511102154.md): Skin · cracked · Nov 10, 2025 · N574FE · Doug MD11F · Nacelle/Pylon, Main Frame
  > TAIL ENGINE INTAKE DUCT LEADING EDGE FOUND MULTIPLE CRACKS. #2 ENGINE NOSE COWL REMOVED AND REPLACED AS PER AMM 54-22-01-04, CARRIED OUT NOSE COWL ANTI-ICE SYSTEM FUNCTIONAL TEST AS PER AMM 30-22-00-700-804, FOUND SATISFACTORY. REPAIR CLASSIFIED AS MINOR A
- [SDR FDEA202511062135](https://openairdocs.org/sdr/FDEA202511062135.md): Stiffener · corroded · Nov 6, 2025 · N574FE · Doug MD11F · Vertical Stabilizer
  > VERTICAL STABILIZER CENTER SPAR UPON TRIM OUT OF STIFFENER FOUND CORROSION AT STATION 2122 X= -18.65 5 O'CLOCK AREA (REFERENCE SPECIAL/NONROUTINE MAINTENANCE FORM N00474). CORROSION ON STIFFENER AT EMPENNAGE VERTICAL STABILIZER REAR CENTER SPAR AT BS 2122
- [SDR FDEA202511052124](https://openairdocs.org/sdr/FDEA202511052124.md): Frame · cracked · Nov 5, 2025 · N574FE · Doug MD11F · Vertical Stabilizer Miscellaneous Structure
  > VERTICAL STABILIZER REAR CENTER SPAR STIFFENER CRACKED AT STATION 2122 5 O' CLOCK AREA. CRACKED STIFFENER AT EMPENNAGE VERTICAL STABILIZER REAR CENTER SPAR AT STATION 2122 5 O' CLOCK AREA REPAIRED AS PER EA# 1-5530-T0385238 P1 TITLE: STABILIZERS - VERTICAL
- [SDR FDEA202510272094](https://openairdocs.org/sdr/FDEA202510272094.md): Beam · cracked · Oct 27, 2025 · N574FE · Doug MD11F · Cargo/Baggage Doors
  > UPON REMOVAL OF R3 DOOR UPPER FORWARD DOOR BEAM FOUND WITH CRACK APPROXIMATELY 1.0". AT R3 DOOR, CRACKED UPPER FORWARD DOOR BEAM REMOVED AND REPLACED AS PER MD-11 SRM 51-35-01-0G. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
- [SDR FDEA202510272092](https://openairdocs.org/sdr/FDEA202510272092.md): Skin · cracked · Oct 27, 2025 · N574FE · Doug MD11F · Fuselage Main, Plate/Skin
  > DURING HIGH FREQUENCY EDDY CURRENT INSPECTION CARRY OUT ON THE FUSELAGE SKIN EDGE AT THE SECOND COAX PENETRATION HOLES OF INMARSAT SATCOM, BETWEEN STATION 939 AND STATION 959, FOUND CRACK INDICATION ON THE EDGE OF THE SKIN. CRACK ON THE FUSELAGE SKIN EDGE
- [SDR FDEA202510162014](https://openairdocs.org/sdr/FDEA202510162014.md): Longeron Splice · corroded · Oct 16, 2025 · N574FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > LOWER CENTER CARGO BAY BILGE AREA LONGERON 52 EXISTING REPAIR SPLICE FITTING FOUND WITH CORROSION AT BS 1691. CORROSION ON LONGERON 52, BS 1701 AND EXISTING REPAIR SPLICE FITTING AT BS 1691, LONGERON-52 AT LOWER CENTER CARGO COMPARTMENT BILGE AREA EVALUATED
- [SDR FDEA202510141997](https://openairdocs.org/sdr/FDEA202510141997.md): Longeron · corroded · Oct 14, 2025 · N574FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > LOWER CENTER CARGO COMPARTMENT BILGE AREA LONGERON 50RIGHT EXISTING REPAIR SPLICE FITTING FOUND WITH CORROSION AT STATION 1691. CORROSION ON LONGERON 50RIGHT STATION 1701 AND SPLICE FITTING AT STATION 1691, LONGERON - 50RIGHT AT LOWER CENTER CARGO COMPARTM
- [SDR FDEA202510111963](https://openairdocs.org/sdr/FDEA202510111963.md): Seat Track · worn · Oct 11, 2025 · N574FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 5-06, X = - 47.5" CROWN FOUND WORN. SEAT TRACK STATION 5-06, 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 TRACK REP
- [SDR FDEA202510111961](https://openairdocs.org/sdr/FDEA202510111961.md): Floorbeam · cracked · Oct 11, 2025 · N574FE · Doug MD11F · Fuselage Main, Floor Beam
  > HIGH FREQUENCY EDDY CURRENT INSPECTION ON RIGHT HAND SIDE OVERWING FLOORBEAM UPPER FLANGE AT STATION Y = 1275.25. X = - 104.25 FOUND CRACK INDICATION APPROX X 0.8". CABIN - CRACK AT RIGHT HAND OVERWING FLOOR BEAM UPPER FLANGE STATION Y = 1275.25, X= - 104.25
- [SDR FDEA202510101938](https://openairdocs.org/sdr/FDEA202510101938.md): Doubler · cracked · Oct 10, 2025 · N574FE · Doug MD11F · Fuselage Main, Structure
  > LEFT HAND AIR-CONDITION COMPARTMENT AFT BULKHEAD APPROXIMATE STATION 595 LONGERON 46LEFT X= 42, DOUBLER FOUND CRACKED. CRACKED DOUBLER AT LEFT HAND AIR-CONDITION COMPARTMENT AFT BULKHEAD APPROXIMATE STATION 595 LONGERON 46LEFT X= 42 AREA REPAIRED AS PER EA
- [SDR FDEA202510021871](https://openairdocs.org/sdr/FDEA202510021871.md): Longeron Splice · cracked · Oct 2, 2025 · N574FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > CAC COMPARTMENT APPROXIMATE BS 1159, LONGERON 47LT SPLICE, SUSPECT CRACK. CRACKED SPLICE AT BS 1159 TO BS 1129/6-100, L47L REMOVED IAW SRM 51-31-01-0G. SPLICE FABRICATED IAW DRAWING A6A7115 REVISION J. FABRICATED SPLICE INSTALLED IAW SRM 51-31-01-0G. REPAIR C
- [SDR FDEA202510021870](https://openairdocs.org/sdr/FDEA202510021870.md): Longeron Splice · cracked · Oct 2, 2025 · N574FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > CAC COMPARTMENT APPROXIMATE BS 1159, LONGERON 46LEFT, SPLICE SUSPECT CRACK. CRACKED SPLICE AT BS 1159 TO STATION 1129/6-100, LONGERON 46L REMOVED IAW SRM 51-31-01-0G. SPLICE FABRICATED IAW DRAWING A6A7115 REVISION J. FABRICATED SPLICE INSTALLED IAW SRM 51-3
- [SDR FDEA202510021869](https://openairdocs.org/sdr/FDEA202510021869.md): Longeron · damaged · Oct 2, 2025 · N574FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > LOWER CENTER CARGO COMPARTMENT BILGE AREA AFTER REMOVAL OF LONGERON SPLICE FITTING FOUND LONGERON 52 FASTENER HOLE ELONGATED AT STATION 1691. DAMAGED LONGERON 52 SECTION STATION 1691 AT LOWER CENTER CARGO BILGE AREA REPAIRED AS PER MD-11 SRM 53-00-0-2R, REP
- [SDR FDEA2025100911865](https://openairdocs.org/sdr/FDEA2025100911865.md): Skin · dented · Oct 1, 2025 · N574FE · Doug MD11F · Fuselage Main, Plate/Skin
  > FUSELAGE: RAMP REPORTED DENT 24 INCH FORWARD OF BULK CARGO DOOR AT AFT FUSELAGE ON SKIN BETWEEN STATION 1887 - STATION 1902 LONGERON 40LEFT - LONGERON 41LEFT, REQUIRED TO PERFORM TERMINATING REPAIR, (REFERANCE: WRI: 53304011). DENT AT 24 INCH FORWARD OF BU
- [SDR FDEA202509261834](https://openairdocs.org/sdr/FDEA202509261834.md): Skin · cracked · Sep 26, 2025 · N574FE · Doug MD11F · Fuselage Main, Structure
  > UPON REMOVAL OF R3 DOOR AFT DOOR JAMB LOWER WEB BOX CUT OUT FOUND CRACKED AT BS 1310. R3 DOOR AFT DOOR JAMB, CRACK AT BS 1310 LOWER WEB BOX CUTOUT REPAIRED IAW SRM 53-40-15-2R, FIGURE 201, REPAIR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
- [SDR FDEA202509251830](https://openairdocs.org/sdr/FDEA202509251830.md): Seat Track · worn · Sep 25, 2025 · N574FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1009, X = - 8.5" CROWN FOUND WORN. SEAT TRACK BS 1009, X = - 8.5 CROWN EVALUATED & FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. WORN SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT A
- [SDR FDEA202509251829](https://openairdocs.org/sdr/FDEA202509251829.md): Seat Track · worn · Sep 25, 2025 · N574FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1199, X = - 8.5" CROWN FOUND WORN. SEAT TRACK STATION 1199, X = - 8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. WORN SEAT TRACK REPAIRED BY SE
- [SDR FDEA202509251828](https://openairdocs.org/sdr/FDEA202509251828.md): Seat Track · worn · Sep 25, 2025 · N574FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 1685, X = - 27.5" CROWN FOUND WORN. CABIN - AT SEAT TRACK BS 1685, X = - 27.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SE
- [SDR FDEA202509251826](https://openairdocs.org/sdr/FDEA202509251826.md): Stringer · cracked · Sep 25, 2025 · N574FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > DURING ACCOMPLISHING W/C: 57.20.0.1, FOUND CRACK ON UPPER AUXILLIARY TANK LOWER STRINGER 47, ALONG XCW -46.5 (RIGHT SIDE). CRACKED STRINGER S-47 ALONG XCW -46.5 (RIGHT SIDE) ON UPPER AUXILLIARY TANK LOWER AREA REPAIRED AS PER MD-11 SRM 57-10-03-2R FIGURE 201 R
- [SDR FDEA202509251825](https://openairdocs.org/sdr/FDEA202509251825.md): Stringer · cracked · Sep 25, 2025 · N574FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > DURING ACCOMPLISHING W/C: 57.20.0.1, FOUND CRACK ON UPPER AUXILLIARY TANK LOWER STRINGER 47, ALONG XCW 17 (LEFT SIDE). CRACKED STRINGER S-47 ALONG XCW 17 (LEFT SIDE) ON UPPER AUXILLIARY TANK LOWER AREA REPAIRED AS PER MD-11 SRM 57-10-03-2R FIGURE 201 REPAIR 1.
- [SDR FDEA202509251824](https://openairdocs.org/sdr/FDEA202509251824.md): Stringer · cracked · Sep 25, 2025 · N574FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > DURING ACCOMPLISHING W/C: 57.20.0.1, FOUND CRACK ON UPPER AUXILLIARY TANK LOWER STRINGER 48, ALONG XCW -46.5 (RIGHT SIDE). CRACKED STRINGER S-48 ALONG XCW -46.5 (RIGHT SIDE) ON UPPER AUXILLIARY TANK LOWER AREA REPAIRED AS PER MD-11 SRM 57-10-03-2R FIGURE 201 R
- [SDR FDEA202509251823](https://openairdocs.org/sdr/FDEA202509251823.md): Longeron · corroded · Sep 25, 2025 · N574FE · Doug MD11F · Fuselage Main, Longeron/Stringer
  > LOWER CENTER CARGO COMPARTMENT BILGE AREA LONGERON 51RIGHT STATION 1701 FOUND WITH CORROSION. CORROSION ON LONGERON 51RIGHT, STATION 1701 AT LOWER CENTER CARGO COMPARTMENT BILGE AREA EVALUATED AND FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-
- [SDR FDEA202509251822](https://openairdocs.org/sdr/FDEA202509251822.md): Trunnion · cracked · Sep 25, 2025 · N574FE · Doug MD11F · Fuselage, Landing Gear Attach Fittings
  > DURING HIGH FREQUENCY EDDY CURRENT INSPETION ON THE LEFT HAND NOSE LANDING GEAR TRUNNION FITTING AFT OF NOSE LANDING GEAR DOOR AFT HINGE FITTING SLOT OUT AREA FOUND 01 EACH CRACKS WITH LENGTH APPROXIMATE 0.3" AT STATION 590. REPAIRED IAW EA 1-5310-T0385087
- [SDR FDEA202509251821](https://openairdocs.org/sdr/FDEA202509251821.md): Skin · cracked · Sep 25, 2025 · N574FE · Doug MD11F · Wing, Plate/Skin
  > 01 EACH FASTENER HOLE #15 FOUND CRACK INDICATION DURING OPEN-HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT LEFT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS= 683.4 AND STATION XORS= 713.6. REPAIR CARRIED OUT AT LEFT HAND WING LOWER SKIN AC
- [SDR FDEA202509251820](https://openairdocs.org/sdr/FDEA202509251820.md): Seat Track · worn · Sep 25, 2025 · N574FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 6-65. X = - 8.5" CROWN FOUND WORN. CABIN - AT SEAT TRACK STATION 6-65, 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 FDEA202509251819](https://openairdocs.org/sdr/FDEA202509251819.md): Seat Track · worn · Sep 25, 2025 · N574FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1545, X = - 8.5" CROWN FOUND WORN. SEAT TRACK STATION 1545, X= -8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. SEAT TRACK REPAIRED BY SECTIONAL REPLACEME
- [SDR FDEA202509251818](https://openairdocs.org/sdr/FDEA202509251818.md): Seat Track · worn · Sep 25, 2025 · N574FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1601. X = 8.5" CROWN FOUND WORN. CABIN - AT SEAT TRACK STATION 1601, X = 8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY
- [SDR FDEA202509251817](https://openairdocs.org/sdr/FDEA202509251817.md): Seat Track · worn · Sep 25, 2025 · N574FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1470. X = 8.5" CROWN FOUND WORN. THE SEAT TRACK CROWN 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
- [SDR FDEA202509251816](https://openairdocs.org/sdr/FDEA202509251816.md): Seat Track · worn · Sep 25, 2025 · N574FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 5-10, X = - 27.5" CROWN FOUND WORN. SEAT TRACK STATION 5-10, 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 TRACK REPAI
- [SDR FDEA202509251815](https://openairdocs.org/sdr/FDEA202509251815.md): Seat Track · worn · Sep 25, 2025 · N574FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1299. X = - 47.5" CROWN FOUND WORN. SEAT TRACK STATION 1299, 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 TRACK REPAIRE
- [SDR FDEA202509251814](https://openairdocs.org/sdr/FDEA202509251814.md): Seat Track · worn · Sep 25, 2025 · N574FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 960. X = 27.5" CROWN FOUND WORN. SEAT TRACK STATION 960, 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 TRACK REPAIRED BY
- [SDR FDEA202509251813](https://openairdocs.org/sdr/FDEA202509251813.md): Seat Track · worn · Sep 25, 2025 · N574FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 775, X = - 47.5" CROWN FOUND WORN. SEAT TRACK STATION 775, X = - 47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIR
- [SDR FDEA202509251812](https://openairdocs.org/sdr/FDEA202509251812.md): Seat Track · worn · Sep 25, 2025 · N574FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 630. X = - 27.5" CROWN FOUND WORN. SEAT TRACK STATION 630, 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 TRACK REPA
- [SDR FDEA202509251811](https://openairdocs.org/sdr/FDEA202509251811.md): Seat Track · worn · Sep 25, 2025 · N574FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1130. X = 75.25" CROWN FOUND WORN. SEAT TRACK STATION 1130, 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 SEAT TRACK REPAIRE
- [SDR FDEA202509251810](https://openairdocs.org/sdr/FDEA202509251810.md): Seat Track · worn · Sep 25, 2025 · N574FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 5-10, X = - 8.5" CROWN FOUND WORN. SEAT TRACK STATION 5-10, 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 REPAIRED
- [SDR FDEA202509251809](https://openairdocs.org/sdr/FDEA202509251809.md): Seat Track · worn · Sep 25, 2025 · N574FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 5-33, X = - 8.5" CROWN FOUND WORN. SEAT TRACK STATION 5-33, 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 REPAIR
- [SDR FDEA202509251808](https://openairdocs.org/sdr/FDEA202509251808.md): Seat Track · worn · Sep 25, 2025 · N574FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1045. X = - 8.5" CROWN FOUND WORN. SEAT TRACK STATION 1045, 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 REPAI
- [SDR FDEA202509251807](https://openairdocs.org/sdr/FDEA202509251807.md): Seat Track · worn · Sep 25, 2025 · N574FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1019. X = 8.5" CROWN FOUND WORN. CABIN - AT SEAT TRACK STATION 1019, 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 RE
- [SDR FDEA202509251806](https://openairdocs.org/sdr/FDEA202509251806.md): Seat Track · worn · Sep 25, 2025 · N574FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1045. X = 8.5" CROWN FOUND WORN. CABIN - AT SEAT TRACK STATION 1045, X = 8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMITS IAW MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REP
- [SDR FDEA202509251805](https://openairdocs.org/sdr/FDEA202509251805.md): Seat Track · worn · Sep 25, 2025 · N574FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1009. X = - 27.5" CROWN FOUND WORN. CABIN - 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 FDEA202509251804](https://openairdocs.org/sdr/FDEA202509251804.md): Seat Track · worn · Sep 25, 2025 · N574FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1019. X = - 27.5" CROWN FOUND WORN. CABIN - AT SEAT TRACK STATION 1019, 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 FDEA202509251803](https://openairdocs.org/sdr/FDEA202509251803.md): Seat Track · worn · Sep 25, 2025 · N574FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1299. X = 47.5" CROWN FOUND WORN. SEAT TRACK STATION 1299, 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 TRACK REPAIRED BY
- [SDR FDEA202509251802](https://openairdocs.org/sdr/FDEA202509251802.md): Seat Track · worn · Sep 25, 2025 · N574FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 5-10. X = 47.5" CROWN FOUND WORN. SEAT TRACK CROWN 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 FDEA202509251801](https://openairdocs.org/sdr/FDEA202509251801.md): Seat Track · worn · Sep 25, 2025 · N574FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 5-15, X = 27.5" CROWN FOUND WORN. SEAT TRACK CROWN EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT AT EXISTING SPLICES BS
- [SDR FDEA202509251800](https://openairdocs.org/sdr/FDEA202509251800.md): Seat Track · worn · Sep 25, 2025 · N574FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1481. X = 27.5" CROWN FOUND WORN. SEAT TRACK CROWN EVALUATED AND FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT AT BS 1471 TO EXISTING S
- [SDR FDEA202509241794](https://openairdocs.org/sdr/FDEA202509241794.md): Seat Track · worn · Sep 24, 2025 · N574FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1210, X = 8.5" CROWN FOUND WORN. SEAT TRACK STATION 1210, 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 REPAIRED BY

Next page: https://openairdocs.org/aircraft/N574FE/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 = 'N574FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N574FE/reports

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