Boeing MD-11F

Service difficulty reports · 31,317

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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'
  WHERE aircraft_model_key = 'MD11F'
  ORDER BY difficulty_date DESC"

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SDR FDEA202507271325Doubler · not reportedCENTER LANDING GEAR WHEEL WELL - EXISTING REPAIR DOUBLER AT FORWARD RIGHT HAND CORNER STATION 1381 REQUIRES EVALUATION TO DETERMINE IF MAJOR OR MINOR AND IF THE REPAIR CONFORMS TO FAA APPROVED DATA. CENTER LANDING GEAR WHEEL WELL - EXISTING REPAIR DOUBLER Jul 27, 2025 · N613FE · Doug MD11F · Fuselage Structure (General)SDR 9WGA2025092354665Panel · corrodedCENTER UPPER PANEL CORRODED AT LH APPROX STA 1197, XCW 110 AT S-19. AFTER FURTHER EVALUATION BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT LH CENTER WING UPPER PANEL APPROX STA 1197, XCW 11Jul 25, 2025 · N546JN · Doug MD11F · Fuselage Miscellaneous StructureSDR 9WGA2025092354664Panel · corrodedDURING HEAVY MAINTENANCE CENTER UPPER PANEL CORRODED AT LH APPROX STA 1197, XCW 110 AT S-19.Jul 25, 2025 · N546JN · Doug MD11F · Fuselage Miscellaneous StructureSDR 9WGA2025092054664Panel · corrodedCENTER WING UPPER PANEL CORRODED AT LH APPROX STA 1173, XCW 112 AT S-22. AFTER FURTHER EVALUATION BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT LH CENTER WING UPPER PANEL APPROX. STA 1173, Jul 25, 2025 · N546JN · Doug MD11F · Fuselage Main, Plate/SkinSDR 9WGA2025092054663Panel · corrodedDURING HEAVY MAINTENANCE CENTER WING UPPER PANEL CORRODED AT LH APPROX STA 1226, XCW 22.5 AT S-15. AFTER FURTHER EVALUATION, BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT LH CENTER WING UPPJul 25, 2025 · N546JN · Doug MD11F · Fuselage Main, Plate/SkinSDR 9WGA2025092054662Panel · corrodedDURING HEAVY MAINTENANCE CENTER WING UPPER PANEL CORRODED AT FRONT SPAR BETWEEN CL AND XCW 8.0. AFTER FURTHER EVALUATION, BOEING CERTIFIED THE BLENDED UT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT FRONT SPAR BETWEEN CLJul 25, 2025 · N546JN · Doug MD11F · Fuselage Main, Plate/SkinSDR 9WGA2025092054661Panel · corrodedDURING HEAVY MAINTENANCE CHECK CENTER WING UPPER PANEL CORRODED AT RH APPROX STA 1172, XCW 6.5 AT S-22. AFTER FURTHER EVALUATION OF BLENDED OUT AREA AT RH APPROX STA 1172, XCW 6.5 AT S-22, BOEING FOUND BLENDED OUT LOCATION ACCEPTABLE AS A PERMANENT REPAIR IAWJul 25, 2025 · N546JN · Doug MD11F · Fuselage Main, Plate/SkinSDR 9WGA2025091954660Panel · corrodedDURING HEAVY MAINTENANCE CHECK CENTER WING UPPER PANEL CORRODED AT RH APPROX STA 1172, XCW 6.5 AT S-22. AFTER FURTHER EVALUATION OF BLENDED OUT AREA AT RH APPROX STA 1172, XCW 6.5 AT S-22, BOEING FOUND BLENDED OUT LOCATION ACCEPTABLE AS A PERMANENT REPAIR IAWJul 25, 2025 · N546JN · Doug MD11F · Fuselage Main, StructureSDR 9WGA2025091954659Panel · corrodedDURING HEAVY MAINTENANCE UPPER PANEL CORRODED AT LH APPROX STA 1196, XCW 5.0 AT S-19. AFTER FURTHER EVALUATION, BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT LH CENTER WING UPPER PANEL APPRJul 25, 2025 · N546JN · Doug MD11F · Fuselage Main, StructureSDR 9WGA2025091954658Panel · corrodedDURING HEAVY MAINTENANCE UPPER PANEL CORRODED AT RH APPROX STA 1205, XCW 4.0 AS S-18. AFTER FURTHER EVALUATION , BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT RH CENTER WING UPPER PANEL APPJul 25, 2025 · N546JN · Doug MD11F · Fuselage Main, StructureSDR 9WGA2025091954657Panel · corrodedDURING HEAVY MAINTENANCE CHECK CENTER WING UPPER PANEL CORRODED AT LH APPROX STA 1214, XCW 3.0 AT S-17. AFTER FURTHER EVALUATION OF BLENDED OUT AREA AT LH APPROX STA 1214, XCW 3.0 AT S-17, BOEING FOUND BLENDED OUT LOCATION ACCEPTABLE AS A PERMANENT REPAIR IAWJul 25, 2025 · N546JN · Doug MD11F · Fuselage Main, StructureSDR 9WGA2025091854656Panel · corrodedDURING HEAVY MAINTENANCE UPPER PANEL CORRODED AT RH APPROX STA 1229, XCW 17.5 AT S-15. AFTER FURTHER EVALUATION BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT RH CENTER WING UPPER PANEL APPRJul 25, 2025 · N546JN · Doug MD11F · Fuselage Main, StructureSDR 9WGA2025091854655Panel · corrodedDURING HEAVY MAINTENANCE UPPER PANEL CORRODED AT RH APPROX STA 1229, XCW 34.5 AT S-15. AFTER FURHTER EVALUATION, BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETE WITH ALL THE REQUESTED PROVISIONS AT RH CENTER WING UPPER PANEL APPRJul 25, 2025 · N546JN · Doug MD11F · Fuselage Main, StructureSDR 9WGA2025091854654Panel · corrodedDURING HEAVY MAINTENANCE UPPER PANEL CORRODED AT RH APPROX STA 1226, XCW 80.5 AT S-15. AFTER FURTHER EVALUATION, BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT RH CENTER WING UPPER PANEL APPJul 25, 2025 · N546JN · Doug MD11F · Fuselage Main, StructureSDR 9WGA2025090954647Panel · corrodedDURING HEAVY MAINTENANCE CHECK CENTER WING UPPER PANEL CORRODED AT LH APPROX STA 1197, XCW 110 AT S-19. AFTER FURHTER EVALUATION BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT LH CENTER WINGJul 25, 2025 · N546JN · Doug MD11F · Fuselage Main, StructureSDR 9WGA2025090954646Panel · corrodedDURING HEAVY MAINTENANCE CHECK CENTER WING UPPER PANEL CORRODED AT LH APPROX STA 1173, XCW 112 AT S-22. AFTER FURTHER EVALUATION BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT LH CENTER WINGJul 25, 2025 · N546JN · Doug MD11F · Fuselage Main, StructureSDR 9WGA2025082654645Panel · corrodedDURING HEAVY MAINTENANCE CHECK CENTER WING UPPER PANEL CORRODED AT LH APPROX STA 1226, XCW 22.5 AT S-15. AFTER FURTHER EVALUATION BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT LH CENTER WINJul 25, 2025 · N546JN · Doug MD11F · Fuselage Main, StructureSDR 9WGA2025082654644Panel · corrodedDURING HEAVY MAINTENANCE CHECK CENTER WING UPPER PANEL CORRODED AT FRONT SPAR BETWEEN CL AND XCW 8.0. AFTER FURTHER EVALUATION BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT FRONT SPAR BETWEJul 25, 2025 · N546JN · Doug MD11F · Fuselage Main, StructureSDR 9WGA2025082654643Panel · corrodedDURING HEAVY MAINTENANCE CENTER UPPER PANEL CORRODED AT RH APPROX STA 1172, XCW 0.5 AT 5-22. AFTER FURTHER EVALUATION OF BLENDED OUT AREA AT RH APPROX STA 1172, XCW 6.5 AT S-22 BOEING FOUND BLENDED OUT LOCATION ACCEPTABLE AS A PERMANENT REPAIR IAW MD-11, MESSJul 25, 2025 · N546JN · Doug MD11F · Fuselage Main, StructureSDR 9WGA2025082654642Panel · corrodedDURING HEAVY MAINTENANCE CENTER UPPER PANEL CORRODED AT RH APPROX STA. 1182, XCW 8.5 AT 5-21. AFTER FURTHER EVALUATION OF BLENDED OUT AREA AT RH APPROX. STA. 1182, XCW 8.5 AT S-21 BOEING FOUND BLENDED OUT LOCATION ACCEPTABLE AS A PERMANENT REPAIR IAW MD-11 MJul 25, 2025 · N546JN · Doug MD11F · Fuselage Main, StructureSDR 9WGA2025082354641Panel · corrodedDURING HEAVY MAINTENANCE CENTER WING UPPER PANEL CORRODED AT L/H APPROX STA 1196, XCW 5.0 AT S-19. AFTER FURTHER EVALUATION, BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT L/H CENTER WING UJul 25, 2025 · N546JN · Doug MD11F · Wing Miscellaneous StructureSDR 9WGA2025082354640Panel · corrodedDURING HEAVY MAINTENANCE CHECK CENTER WING UPPER PANEL CORRODED AT RH APPROX STA. 1205, XCW 4.0 AT S-18. AFTER FURTHER EVALUATION BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT RH CENTER WINJul 25, 2025 · N546JN · Doug MD11F · Fuselage Miscellaneous StructureSDR 9WGA2025082254630Panel · corrodedDURING HEAVY MAINTENANCE CENTER WING UPPER PANEL CORRODED AT LH APPROX STA 1214, XCW 3.0 AT S-17. AFTER FURTHER EVALUATION OF BLENDED AREA AT LH APPROX STA 1214, XCW 3.0 AT S-17, BOEING FOUND BLENDED OUT LOCATION ACCEPTABLE AS A PERMANENT REPAIR IAW MD-11, MEJul 25, 2025 · N546JN · Doug MD11F · Fuselage Main, StructureSDR 9WGA2025082254629Panel · corrodedDURING HEAVY MAINTENANCE CENTER WING UPPER PANEL CORRODED AT RH AAPROX STA. 1229, XCW 17.5 AT S-15. AFTER FURTHER EVALUATION BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT R/H CENTER WING UPJul 25, 2025 · N546JN · Doug MD11F · Fuselage Main, StructureSDR 9WGA2025082254628Panel · corrodedDURING HEAVY MAINTENANCE CENTER WING UPPER PANEL CORRODED AT RH APPROX STA. 1229, XCW 34.5 AT S-15. AFTER FURTHER EVALUATION, BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT R/H CENTER WING Jul 25, 2025 · N546JN · Doug MD11F · Fuselage Main, StructureSDR 9WGA2025082254627Panel · corrodedDURING HEAVY CHECK CENTER WING UPPER PANEL CORRODED AT RH APPROX STA. 1226 XCW 80.5 AT S-15. AFTER FURTHER EVALUATION BOING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT R/H CENTER WING UPPER PANELJul 25, 2025 · N546JN · Doug MD11F · Fuselage Main, StructureSDR FDEA202507251318Floorbeam · crackedHIGH FREQUENCY EDDY CURRENT INSPECTION ON RIGHT HAND OVERWING FLOOR BEAM UPPER FLANGE AT STATION 1275, X=103 FOUND CRACK INDICATION APPROXIMATELY 0.1 INCH. HIGH FREQUENCY EDDY CURRENT INSPECTION ON RIGHT HAND OVERWING FLOOR BEAM UPPER FLANGE AT STATION 127Jul 25, 2025 · N609FE · Doug MD11F · Fuselage Main, Floor BeamSDR FDEA202507251317Trunnion · crackedDURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON NOSE LANDING GEAR LEFT HAND TRUNNION FITTING AT STATION 595 EXISTING REPAIR SLOT OUT AREA FOUND LONGERON 49 LEFT HAND SIDE WITH CRACK APPROXIMATELY 0.125". (REFER TO SPECIAL/NONROUTINE MAINTENANCE FORM #N0Jul 25, 2025 · N613FE · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR FDEA202507241311Skin · corrodedLEFT WING TIP LOWER SKIN STATION XW 998 FOUND CORRODED. REPAIR CARRIED OUT IAW EA 1-5730-T0384251 PART 1 (P1). REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jul 24, 2025 · N609FE · Doug MD11F · Wing, Plate/SkinSDR FDEA202507241310Skin · crackedNR 1 AIR CON RAM AIR EXHAUST CUTOUT CORNER DOUBLER FOUND CRACKED AT BS 565. REMOVED AND REPLACED WITH FABRICATED DOUBLER PER MD-11 SRM 51-31-01-G. DOUBLER FABRICATED PER DOUGLAS DRAWING ACA3850 REVISION AA. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jul 24, 2025 · N613FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA202507231297Hinge Bracket · corrodedRIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE (#3HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-07. OVERSIZED REPAIR BUSHING FABRICATEJul 23, 2025 · N609FE · Doug MD11F · Trailing Edge FlapsSDR FDEA202507231296Hinge Bracket · corrodedLEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE (#3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-07. OVERSIZED REPAIR BUSHING FABRICATEDJul 23, 2025 · N609FE · Doug MD11F · Trailing Edge FlapsSDR FDEA202507221291Indicator · no testON POST FLIGHT, THE R1 DOOR RAFT PUSH LIGHT WAS POPPED OUT. LIGHT WOULD NOT TEST. REMOVED AND REPLACED R1 SLIDE REMOTE PRESSURE INDICATOR ASSY IAW AMM 25-61-04-4.Jul 22, 2025 · N607FE · Doug MD11F · Emergency EquipmentSDR FDEA202507221288Seat Track · chafedAGING AIRCRAFT - EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK BETWEEN STATION 745 TO STATION 801 X = 8.5 LEFT HAND SIDE EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK BETWEEN STATION 745 TO STATION 801 X = 8.5 LEFT HAND Jul 22, 2025 · N613FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202507221287Seat Track · chafedEXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK BETWEEN STATION 745 TO STATION 856 X = -8.5 RIGHT HAND SIDE. EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK BETWEEN STATION 745 TO STATION 856 X = -8.5 RIGHT HAND SIDE EVALUATJul 22, 2025 · N613FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202507211338Bulkhead · damagedDURING FUSELAGE DECAY CHECK FOUND A SIGNIFICANT LEAK IN THE R/H MLG BAY AT THE FWD INBD CORNER. UPON FURTHER INVESTIGATION FOUND A TRIANGLE PANEL HAS THE LOWER END MISSING "CRACKED OFF" ABOUT 2 INCHES UP FROM THE BOTTOM AND ABOUT AN INCH WIDE. ABOVE THAT Jul 21, 2025 · N642FE · Doug MD11F · Fuselage Main, BulkheadSDR FDEA202507211279Longeron Splice · crackedLOWER CENTER CARGO BAY RT TUNNEL AREA LONGERON SPLICE FOUND CRACKED BETWEEN BS 5-113 - 1541 L35R. LONGERON 35 RT REMOVED & REPLACED WITH FABRICATED SPLICE IAW SRM 51-33-01-0G. SPLICE FABRICATED IAW DRAWING A5A7114 REVISION J. REPAIR CLASSIFIED AS MAJOR IAWJul 21, 2025 · N613FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA202507201268Doubler · noneAGING AIRCRAFT - EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE LOWER STRINGER DOUBLER STATION XOS 906.5607 EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE LOWER STRINGER DOUBLER STATION XOS 906.5607 EVALUATED AND FOUND REPAIRED IAW MD11 SRM 57-Jul 20, 2025 · N613FE · Doug MD11F · Wing, Plate/SkinSDR IPXA2025071911037Door · handler errorL-1 DOOR WAS ACTIVATED TO THE EMERGENCY POSITION BY GROUND LOAD CREW SERVICED DOOR ASSIST BOTTLE FOR L-1 DOOR IAW AMM 12-25-04-600-801. OK FOR SERVICE PLACARD REMOVED THIS CLOSES T3F18E0072JY8Jul 19, 2025 · N275UP · Doug MD11F · Passenger/Crew DoorsSDR FDEA202507191265Stringer · crackedDURING ACCOMPLISHING W/C: 57.20.01.1, FOUND CRACK ON UPPER AUXILLIARY TANK LOWER STRINGER S-47 ALONG XCW -17 (RIGHT HAND SIDE). CRACK ON UPPER AUXILLIARY TANK LOWER STRINGER S-47 ALONG XCW -17 (RIGHT HAND SIDE) REPAIRED AS PER MD-11 SRM 57-10-03-2R FIGURE Jul 19, 2025 · N613FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA202507181253Longeron · misrepairedEXISTING REPAIR AT CENTER CARGO LONGERON BETWEEN STATION 1531 TO STATION 1551, LONGERON 50R RIGHT HAND SIDE. EXISTING REPAIR AT CENTER CARGO LONGERON BETWEEN BS 1531 - 1551, LONGERON 50 RIGHT RIGHT HAND SIDE EVALUATED AND FOUND WITH MISSING STEPS IN WORK Jul 18, 2025 · N613FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA202507181252Seat Track · wornCABIN - RIGHT HAND STATION 1452 X= -47.5 SEAT TRACK CROWN WORN. CABIN Ï¿½ RIGHT HAND AT SEAT TRACK STATION 1452 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 REPAIRJul 18, 2025 · N613FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202507181251Seat Track · wornCABIN FLOOR SEAT TRACK FOUND CRACK FOUND CRACK AT STATION 808 X= 27.50. CABIN FLOOR SEAT TRACK AT STATION 808, X = 27.5 CRACKED CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN CRACKED SEAT TRACK REJul 18, 2025 · N613FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202507181250Seat Track · wornCABIN - LEFT HAND STATION 5-83 X= 8.5 SEAT TRACK CROWN WORN. CABIN-LEFT HAND AT SEAT TRACK STATION 5-83, 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 SECTJul 18, 2025 · N613FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202507181248Doubler · crackedLEFT WING, FIXED LEADING EDGE LOWER DOUBLER FOUND CRACKED ABOUT 1 INCH AT XOS 487.5. CRACKED DOUBLER REMOVED IAW SRM 51-35-01-0G & SRM 51-33-01-0G. DOUBLER FABRICATED IAW DRAWING ARB2933, REV AJ & INSTALLED IAW SRM 51-33-01-0G & SRM 51-35-01-0G. REPAIR CLASJul 18, 2025 · N609FE · Doug MD11F · Wing, Plate/SkinSDR FDEA202507181247Seat Track · wornCABIN - LEFT HAND STATION 1551 X= 27.5 SEAT TRACK CROWN WORN. CABIN-LEFT HAND AT SEAT TRACK STATION 1551, 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 SEJul 18, 2025 · N613FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202507181246Seat Track · wornCABIN - LEFT HAND STATION 1169 X= 8.5 SEAT TRACK CROWN WORN. CABIN-LEFT HAND AT SEAT TRACK STATION 1169, 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 SECTJul 18, 2025 · N613FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202507181245Seat Track · wornCABIN - LEFT HAND STATION 1289 X= 47.5 SEAT TRACK CROWN WORN. CABIN-LEFT HAND AT SEAT TRACK STATION 1189, 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 SEJul 18, 2025 · N613FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202507181244Seat Track · wornCABIN - LEFT HAND STATION 1169 X= 47.5 SEAT TRACK CROWN WORN. CABIN-LEFT HAND AT SEAT TRACK STATION 1169, 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 SEJul 18, 2025 · N613FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202507181243Seat Track · wornCABIN - RIGHT HAND STATION 1169 X= -27.5 SEAT TRACK CROWN WORN. CABIN-RIGHT HAND AT SEAT TRACK STATION 1169, 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 BJul 18, 2025 · N613FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
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