Service difficulty reports

1,769,551 reports of malfunctions and defects, newest first. Air carriers must report; general aviation reporting is voluntary.

Query with SQL
duckdb -csv -c "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'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR UIEA2026081200743Tee Fitting · crackedLOWER FUSELAGE: STA 250 TO STA 260 FWD BULKHEAD R/H SIDE T-CHORD FOUND CRACKED.(<P >AT R/H NOSE W/W FWD BULKHEAD STA 250 TO STA 260, CRACKED T-CHORD REMOVED AND INSTALLED WITH NEW FABRICATED T-CHORD AS PER EN 3565-26 REV.0. REPAIR CLASSIFIED AS "MAJOR" REPAIR Oct 9, 2026 · N419MC · Boeing 74748EF · Fuselage Main, StructureSDR UIEA2026081200744Structure · abnormalWHILE ACCOMPLISHING SB747-53A2562 R3, AT STA 260 WL 20 L/H, FOUND EXISTING HOLE SIZE 04 EA DEVIATED FROM DRAWING: 141U1192. EXISTING HOLE SIZE = 3/16, DWG HOLE = 1/4; FOUND SHORT EDGE MARGIN. FITTING COMMON TO SEAT TRACK AND CHORD P/N: 65B11784U507.(<P >L/H ANOct 9, 2026 · N419MC · Boeing 74748EF · Fuselage Structure (General)SDR UIEA2026081200745Structure · abnormalWHILE ACCOMPLISHING SB747-53A2562 R3, AT STA 260 WL 20 RH, FOUND EXISTING HOLE SIZE 04 EA DEVIATED FROM DRAWING 141U1192. EXISTING HOLE SIZE = 3/16, DWG HOLE = 1/4; FOUND SHORT EDGE MARGIN- FITTING COMMON TO SEAT TRACK AND CHORD P/N: 65B11784U508.(<P >R/H ANGLOct 9, 2026 · N419MC · Boeing 74748EF · Fuselage Structure (General)SDR UIEA2026081900778Angle · crackedWHILE C/O DVI INSPECTION PER SB 747-53A2562 R3 STEP 22, FOUND UPPER INNER SIDE ANGLE 65B07941-544 FOUND CRACKED AT NOSE W/W RT TOP PANEL BS 260 - 340, RBL 30. >NOSE W/W R/H UPPER INNER NEW SIDE ANGLE TOP PANEL STA 260 - STA 340 RBL 30 (05 EA) FASTENER HOLES EOct 9, 2026 · N419MC · Boeing 74748EF · Fuselage Miscellaneous StructureSDR UIEA2026081900781Tee Fitting · crackedLOWER FUSELAGE, BS 250 - 260, FWD BULKHEAD LT SIDE TEE FITTING FOUND CRACKED. A NEW TEE FITTING FABRICATED IAW EN 3564-26 REV. 0. R & R IAW SRM 51-40-02-0G-0, REV 107.Oct 9, 2026 · N419MC · Boeing 74748EF · Fuselage Main, StructureSDR UIEA2026082400792Doubler · crackedSUSPECTED CRACK ON MED L1 DOOR UPPER HINGE CUTOUT DOUBLER EDGE. DOUBLER FOR MED L1 DOOR UPPER HINGE CUTOUT, REMOVED AND A NEW DOUBLER FABRICATED & INSTALLED IAW EN 3413-26, REV 0.Oct 9, 2026 · N419MC · Boeing 74748EF · Fuselage Main, StructureSDR UIEA2026082500794Stiffener · abnormalWHILE ACCOMPLISHING SB747-53A2562 R3 AT BS 280, RBL 20, TWO EXISTING FASTENER HOLES DEVIATED FROM THE DRAWING. EXISTING HOLE SIZE = 1/4", STIFFENER, INCOMING OVERSIZED FASTENER HOLE CONDITION COMMON TO STIFFENER WAS REPAIRED IAW EN 3594-26, REV 0. REPAIR CLASOct 9, 2026 · N419MC · Boeing 74748EF · Fuselage Miscellaneous StructureSDR UIEA2026083100828Seat Track · crackedFOUND A CRACK ON MAIN DECK SEAT TRACK, BS 260, RBL 33. THE SEAT TRACK WAS TRIMMED OFF, & A SEAT TRACK SPLICE REPAIR CARRIED OUT IAW EN 3583-26, REV 0. REPAIR CLASSIFIED AS A MAJOR REPAIR & CATEGORIZED AS A CATEGORY A PERMANENT REPAIR.Oct 9, 2026 · N419MC · Boeing 74748EF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2026083100829Seat Track · crackedFOUND CRACK ON MAIN DECK SEAT TRACK, BS 260, LBL 33, IN FRONT OF NOSE WHEEL WELL BULKHEAD AREA. THE SEAT TRACK WAS TRIMMED OFF, & SEAT TRACK SPLICE REPAIR CARRIED OUT IAW EN 3583-26, REV 0. REPAIR CLASSIFIED AS "MAJOR" REPAIR AND CATEGORIZED AS "CATEGORY A" POct 9, 2026 · N419MC · Boeing 74748EF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2026091700881Door Frame · crackedMAIN DECK L5 DOOR CUTOUT AREA AT BS 2220, STRINGER 18L FOUND CRACKED. L5 DOOR CUTOUT AREA REPAIRED IAW EN 3574-26, REV 0, & SRM 53-00-03-2R-1, REPAIR 1, REV 107.Oct 9, 2026 · N419MC · Boeing 74748EF · Fuselage Main, StructureSDR UIEA2026092000887Door Frame · crackedDURING HFEC INSPECTION ON DOOR STOP SUPPORT FITTINGS AT S16L, BS 2231, FOUND ONE LOWEST FWD HOLE WITH A CRACK INDICATION AT STRAP SIDE 3 & 9 O'CLOCK POSITION LOOKING OTBD. CRACK ON BS 2231 S16L. FRAME STRAP TRIMMED OUT & REPAIR CARRIED OUT IAW EN 3430-26, REOct 9, 2026 · N419MC · Boeing 74748EF · Fuselage Main, StructureSDR UIEA2026092100889Doubler · no discrepancySECT 41 LAP JOINT INSP: EXISTING DOUBLERS (06 EA) ON S-14L STA 140-160, S-44L STA 240-260, S-44R STA 240-260, S39R STA 380-420, S45L STA 400-420 AND S45R STA 400-420 FOUND THE REPAIR NOT CONFIRMED TO SRM 53-00-01, REPAIR 10, 12 OR 16(<P >DOUBLERS AT STA 240 - Oct 9, 2026 · N419MC · Boeing 74748EF · Fuselage Main, Plate/SkinSDR UIEA2026092800919Spar · damagedNR 3 PYLON UPPER SPAR WEB SKIN SUSPECT CRACK AT NAC STA 300. CRACKED NR 3 PYLON UPPER SPAR WEB SKIN R & R IAW SRM 51-40-02-0G-0 REV. 107, DWG. 311U2130. SHT. 6, REV. B; REPAIR CARRIED OUT IAW EN 3684-26, REV. 0. REPAIR CLASSIFIED AS "MAJOR" CATEGORIZED AS "CAOct 9, 2026 · N419MC · Boeing 74748EF · Nacelle/Pylon, Frame/Spar/RibSDR UIEA2026093000925Spar · damagedDURING NDT LFEC INSPECTION ON LHW REAR SPAR LOWER CHORD AND SKIN AT LANDING GEAR BEAM ATTACHMENT FITTINGS AND TRUNNION FITTINGS (SSID), FOUND 02 EA FASTENERS AT WS 469.8. TRUNNION FITTING SHEAR CLIP AREA LARGER THAN NORMAL(<P >02 FASTENERS ON LHW REAR SPAR LOWOct 9, 2026 · N419MC · Boeing 74748EF · Wing SparSDR UIEA2026093000926Spar · damagedDURING NDT LFEC INSPECTION ON RHW REAR SPAR LOWER AND SKIN AT LANDING GEAR BEAM ATTACHMENT FITTINGS AND TRUNNION FITTINGS (SSID0), FOUND 02 EA FASTENERS AT WS 469.8. TRUNNION FITTING SHEAR CLIP AREA LARGER THAN NORMAL TWO FASTENERS ON RT W REAR SPAR LOWER CHOROct 9, 2026 · N419MC · Boeing 74748EF · Wing SparSDR UIEA2026093000927Frame · damagedPER DWG 624U0072 SHEET 13, 08 FASTENERS ARE SHOWN BETWEEN STR-7 AND STR-8, BUT AT STA 2598 BLKHD HORIZONTAL STABILIZER FWD SIDE, ONLY 04 EA FASTENERS ARE INSTALLED PER SIDE OF BOTH LHS AND RHS FRAME . REWORK CARRIED OUT AT STA 2598 BULKHEAD HORIZONTAL STABILIOct 9, 2026 · N419MC · Boeing 74748EF · Fuselage Main, FrameSDR UIEA2026093000929Frame · damagedUNABLE TO PERFORM HFEC INSPECTION FULLY AROUND 04 EA FASTENERS AND 01 EDGE PER SB747-53A2837 PART 7 R0 STEP 1 & 2 OF FIGURE 42 AND DWG 624U0072 SHEET 13 AT LHS STA 2598 BLKHD FWD AND AFT FRAME OUTER CHORD. REWORKS CARRIED OUT AT THE LT STA 2598 BULKHEAD FWD AOct 9, 2026 · N419MC · Boeing 74748EF · Fuselage Main, FrameSDR UIEA2026093000930Frame · damagedUNABLE TO PERFORM HFEC INSPECTION FULLY AROUND 06 EA FASTENERS AND 01 EDGE PER SB747-53A2837 PART 8 R0 STEP 1 & 2 OF FIGURE 42 AND DWG 624U0072 SHEET 13 AT RHS STA 2598 BLKHD FWD AND AFT FRAME OUTER CHORD. REWORK CARRIED OUT AT RHS STA 2598 BULKHEAD FWD AND AOct 9, 2026 · N419MC · Boeing 74748EF · Fuselage Main, FrameSDR UIEA2026093000933Door Sill · corrodedAFT CARGO DOOR LOWER SILL FOUND CORRODED. CORRODED DOOR SILL ON AFT CARGO DOOR AREA REMOVED AND REPLACED, AND REPAIR CARRIED OUT AS PER SRM 51-40-2-0G-0 REV. 107 AND EN 3557-26, REV. 0. REPAIR CLASSIFIED AS "MAJOR" AND CATEGORIZED AS "CATEGORY A" PERMANENT REOct 9, 2026 · N419MC · Boeing 74748EF · Fuselage Main, StructureSDR UIEA2026100300940Door Frame · crackedDURING HFEC INSPECTION ON LOWER LOBE AFT CARGO DOOR CUTOUT FORWARD UPPER CORNERS, FOUND CRACK APPROX 0.3" IN LENGTH AS MARKED(<P>DOUBLER REPAIR CARRIED OUT ON THE LOWER LOBE AFT CARGO DOOR CUTOUT FWD UPPER CORNER CRACKED AREA AS PER SRM 53-60-01-2R-3 REPAIR 3,Oct 9, 2026 · N419MC · Boeing 74748EF · Fuselage Main, StructureSDR UIEA2026100300941Frame · crackedDURING HFEC OPEN HOLE INSPECTION ON RHS STA 940 TENSION TIE AND FRAME, FOUND 02 EA FASTENER HOLE ON FRAME AND CHORD WITH CRACK(<P >FRAME SPLICE REPAIR CARRIED OUT ON RHS STA 940 TENSION TIE AND FRAME CRACK 02 FASTENER HOLES AREAS AS PER SRM 53-20-07-2R-8 FIGUROct 9, 2026 · N419MC · Boeing 74748EF · Fuselage Main, FrameSDR UIEA2026100500952Doubler · misinstalledSEC 42 LAP JOINT INSP OF EXISTING DOUBLERS (02 EA) ON S39L, STA 940-960 AND S39R, STA 920-960; FOUND THE REPAIR NOT CONFIRMED TO SRM 53-00-01, REPAIR 10,12 OR 16. BODY FAIRING PANEL REMOVED & REINSTALLED IAW AMM 53-51-01-004-001, REV 117 & AMM 53-51-01-404-00Oct 9, 2026 · N419MC · Boeing 74748EF · Fuselage Main, Plate/SkinSDR UIEA2026100600964Doubler · misinstalledSECT 46 LAP JOINT INSP OF EXISITNG DOUBLERS (05 EA), STRINGER 14L, BS 1980-2020, S12L, BS 1720-1740, S12L, STA 2140-2160, S34L, STA 1640-1960 AND S40L, STA 1640-1820; FOUND THE REPAIR NOT CONFORMED TO SRM 53-00-01, REPAIR 10, 12 OR 16. REPAIRED IAW EN 3737-Oct 9, 2026 · N419MC · Boeing 74748EF · Fuselage Main, Plate/SkinSDR UIEA2026100600965Tension Tie · crackedDURING HFEC OPEN HOLE INSPECTION ON LHS STA 920 TENSION TIE AND FRAME, FOUND 01 EA FASTENER HOLE ON AFT CHANNEL WITH CRACK. TENSION TIE AFT CHANNEL TRIMMED OUT AND SPLICE REPAIR CARRIED OUT IAW SRM 53-20-30-2R-1, REPAIR 1, FIGURE 201, REV. 107. REPAIR CLASSIFOct 9, 2026 · N419MC · Boeing 74748EF · Fuselage Main, StructureSDR UIEA2026100700966Support Frame · damagedHFEC OPEN HOLE INSPECTION CARRIED OUT ON 02 EA FASTENER HOLES AT STA 2598 BLKHD FRAME SUPPORT STA 2598 BELOW S-11L AND FOUND 02 EA HOLES DAMAGED ON THE 2ND LAYER, VIEW I/B AND FITTING HOLES. DAMAGED AREAS ON BS 2598 BULKHEAD FRAME SUPPORT AREAS REPAIRED IAW EOct 9, 2026 · N419MC · Boeing 74748EF · Fuselage Main, StructureSDR DALA2026100905576Frame · damagedFOUND TOOLING DAMAGE ON FUSELAGE FRAME Y908, STR 2R-3R, COMPLIED WITH ER/A 637401-14. (1855981) (AICRAFT GROUNDED).Oct 9, 2026 · N920AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2026100905575Frame · damagedFOUND TOOLING DAMAGE ON FUSELAGE FRAME Y927 BETWEEN STRG L3R TO L4R, ADDITIONAL ENGINEERING AUTHORIZATION ER/A REVISION IS REQUIRED. (1855903) (AICRAFT GROUNDED).Oct 9, 2026 · N920AT · Boeing 717200 · Fuselage Main, FrameSDR FDEA202610091536Floorbeam · corrodedMAIN CARGO COMPARTMENT FLOORBEAM BS 1200 BETWEEN 24LBL TO 0BL SOME AREAS WITH CORROSION. AREA OUT OF LIMITS WAS REPAIRED AT MAIN CARGO COMPARTMENT FLOORBEAM BS 1200 BETWEEN 26LBL TO 13LBL IAW SRM 53-00-51-2R, REPAIR.1.Oct 9, 2026 · N943FD · Boeing 7572G5 · Fuselage Main, Floor BeamSDR FDEA202610091533Seat Track · wornMAIN DECK CARGO BAY SEAT TRACK AT BS 1671, X= -8.5" FOUND CROWN WORN. THE SEAT TRACK WAS EVALUATED & FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT BTWN BS 1651- 1691, X= -8.5 IAOct 9, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202610091532Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1671, X= 8.5" 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 BTWN BS 1651 TO Oct 9, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202610091531Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1551, X= 27.5" FOUND THE CROWN WORN. THE SEAT TRACK WAS EVALUATED AND FOUND EXCEEDED LIMITS SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT BTWN BS 1571 TOct 9, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202610091530Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1551, X= 47.5" FOUND THE 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 BTWN BS 157Oct 9, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202610091529Seat Track · wornCABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 5-11, 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 AT SOct 9, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202610091528Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 5-11, X= 27.5, FOUND THE CROWN WORN. THE SEAT TRACK WAS EVALUATED & FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT BTWN BS 5-43 TO EOct 9, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202610091527Seat Track · wornCABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 5-11, X= 8.5" 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 STOct 9, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202610091526Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 1421, X= 8.5", FOUND THE 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 BTWN BS 1391 AOct 9, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202610091525Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1421, X= -8.5" 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 STATION 1Oct 9, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202610091524Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 1421, X= -27.5" FOUND THE 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 BTWN BS 1391 TOct 9, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202610091523Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1421, 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 STATION 14Oct 9, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202610091521Seat Track · wornMAIN DECK CARGO BAY SEAT TRACK AT BS 1296, X= -47.5, CROWN WORN. THE SEAT TRACK WAS EVALUATED & FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT BTWN BS 1311 TO EXISTING SPLICE BOct 9, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202610091520Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 1296, X= -27.5" FOUND THE 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 BTWN BS 1311 TOOct 9, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202610091519Seat Track · wornMAIN DECK CARGO BAY SEAT TRACK AT BS 1296, X= -8.5, CROWN WORN. THE SEAT TRACK WAS EVALUATED & FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT BTWN BS 1311 TO EXISTING SPLICE BS 1Oct 9, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202610091518Seat Track · wornMAIN DECK CARGO BAY SEAT TRACK AT BS 1296, X= 8.5", CROWN WORN. THE SEAT TRACK WAS EVALUATED & FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT BTWN BS 1269 - 1311 IAW SRM 53-00-5Oct 9, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202610091517Seat Track · wornMAIN DECK CARGO BAY SEAT TRACK AT BS 1296, X= 27.5" CROWN WORN. THE SEAT TRACK WAS EVALUATED & FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT BTWN BS 1249 - 1311 IAW SRM 53-00-52-2ROct 9, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202610091516Seat Track · wornMAIN DECK CARGO BAY SEAT TRACK AT BS 1159, X= 47.5" CROWN WORN. THE SEAT TRACK WAS EVALUATED & FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT BTWN EXISTING SPLICES BS 1129/6-100Oct 9, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202610091515Seat Track · wornMAIN DECK CARGO BAY SEAT TRACK AT BS 1139, X= -8.5" 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 BTWN EXISTING SPLICES BS 1129/6-1Oct 9, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202610091514Seat Track · wornMAIN DECK CARGO BAY SEAT TRACK AT BS 1159, X=8.5" CROWN WORN. THE SEAT TRACK WAS EVALUATED & FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT BTWN EXISTING SPLICES BS 1129/6-100 -Oct 9, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202610091512Seat Track · wornMAIN DECK CARGO BAY SEAT TRACK AT BS 1149, X=-47.5" CROWN WORN. THE SEAT TRACK WAS EVALUATED & FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT AT EXISTING SPLICES BS 1129/6-100 TOOct 9, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202610091511Seat Track · wornMAIN DECK CARGO BAY SEAT TRACK AT BS 879, X=47.5" CROWN WORN. THE SEAT TRACK WAS EVALUATED & FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT BTWN BS 869 TO EXISTING SPLICE BS 929 Oct 9, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202610091510Seat Track · wornMAIN DECK CARGO BAY SEAT TRACK AT BS 806, X=-27.5" CROWN WAS WORN. THE SEAT TRACK WAS EVALUATED & FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT BTWN BS 816 TO EXISTING SPLICE BSOct 9, 2026 · N610FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings