N614FE

Service difficulty reports · 388

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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'
  WHERE n_number = 'N614FE' AND registry_match = 'registration'
  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 FDEA2018091172411Hinge Bracket · corrodedRT WING O/B FLAP I/B FWD (WING SIDE) HINGE ACTUATOR I/B HOLE BORE CORROSION. HINGE ACTUATOR I/B HOLE BORE (HOLE 8) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE DIA 1.2806", FINAL HOLE DIA 1.284", MAXIMUM ALLOWABLE HOLE DIA 1.220". REPAIR BUSSep 7, 2018 · N614FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2018091172410Hinge Bracket · corrodedRT WING O/B FLAP I/B FWD (WING SIDE) HINGE ACTUATOR O/B HOLE BORE CORROSION. HINGE ACTUATOR O/B HOLE BORE (HOLE 8) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE DIA 1.220", FINAL HOLE DIA 1.223", MAXIMUM ALLOWABLE HOLE DIA 1.220". REPAIR BUSHSep 7, 2018 · N614FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2018091172409Hinge Bracket · corrodedRT WING O/B FLAP I/B FWD (WING SIDE) HINGE LOWER MOUNT I/B HOLE BORE CORROSION. HINGE LOWER MOUNT I/B HOLE BORE (NR 7) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE DIA 0.718". FINAL HOLE DIA 0.727", MAXIMUM HOLE DIA 0.709". REPAIR BUSHING FASep 7, 2018 · N614FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2018091172408Hinge Bracket · corrodedRT WING O/B FLAP I/B FWD (WING SIDE) HINGE LOWER MOUNT O/B HOLE BORE CORROSION. HINGE LOWER MOUNT O/B HOLE BORE (HOLE 7) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE DIA 0.705", FINAL HOLE DIA 0.722", MAXIMUM ALLOWABLE HOLE DIA 0.709". REPAISep 7, 2018 · N614FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2018091172407Hinge Bracket · corrodedRT WING O/B FLAP I/B FWD (WING SIDE) HINGE BARREL NUT HOLE SURFACE CORROSION. HINGE BARREL NUT HOLE SURFACE REWORKED PER CMM 57-44-08. EXISTING THK - UPPER 0.389", LOWER 0.373", MATERIAL REMOVED - UPPER & LOWER 0.005", REMAINING THK - UPPER 0.384", LOWER 0.368Sep 7, 2018 · N614FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2018091172406Hinge Bracket · corrodedLT WING O/B FLAP I/B FWD (WING SIDE) HINGE ACTUATOR O/B HOLE BORE CORROSION. HINGE ACTUATOR O/B HOLE BORE (HOLE 8) REWORKED & FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE DIA 1.222", FINAL HOLE DIA 1.252", MAXIMUM ALLOWABLE HOLE DIA 1.220". OVERSIZED BUSSep 7, 2018 · N614FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2018091172405Hinge Bracket · corrodedLT WING O/B FLAP I/B FWD (WING SIDE) HINGE ACTUATOR I/B HOLE BORE CORROSION. HINGE ACTUATOR I/B HOLE BORE (HOLE 8) REWORKED & FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE DIA 1.222", FINAL HOLE DIA 1.252", MAXIMUM ALLOWABLE HOLE DIA 1.220". OVERSIZED BUSSep 7, 2018 · N614FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2018091172404Hinge Bracket · corrodedLT WING O/B FLAP I/B FWD (WING SIDE) HINGE LOWER MOUNT O/B HOLE SURFACE CORROSION. HINGE LOWER MOUNT O/B HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING THK 0.400", MATERIAL REMOVED 0.004", REMAINING THK 0.396", MINIMUM ALLOWABLE THK 0.Sep 7, 2018 · N614FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2018091172402Hinge Bracket · corrodedLT WING O/B FLAP I/B FWD (WING SIDE) HINGE LOWER MOUNT I/B HOLE SURFACE CORROSION. HINGE LOWER MOUNT I/B HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING THK 0.436", MATERIAL REMOVED - FWD FACE 0.004", AFT FACE 0.013", REMAINING THK 0.41Sep 7, 2018 · N614FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2018091172401Hinge Bracket · corrodedLT WING O/B FLAP I/B FWD (WING SIDE) HINGE LOWER MOUNT O/B HOLE BORE CORROSION. HINGE LOWER MOUNT O/B HOLE BORE (NR 7 HOLE) REWORKED & FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE DIA 0.709", FINAL HOLE DIA 0.729", MAXIMUM ALLOWABLE HOLE DIA 0.709". OVERSep 7, 2018 · N614FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2018091172400Hinge Bracket · corrodedLT WING O/B FLAP I/B FWD (WING SIDE) HINGE LOWER MOUNT I/B HOLE BORE CORROSION. HINGE LOWER MOUNT I/B HOLE BORE (NR 7 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM57-44-08. EXISTING HOLE DIA 0.708", FINAL HOLE DIA 0.728", MAXIMUM ALLOWABLE HOLE DIA 0.709". OVESep 7, 2018 · N614FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2018091172399Hinge Bracket · corrodedLT WING O/B FLAP I/B FWD (WING SIDE) HINGE BARREL NUT HOLE SURFACE CORROSION. HINGE BARREL NUT HOLE SURFACE REWORKED AS PER CMM 57-44-08, EXISTING THK - UPPER 0.378", LOWER 0.348", MATERIAL REMOVED, UPPER & LOWER 0.005", REMAINING THK - UPPER 0.373", LOWER 0.3Sep 7, 2018 · N614FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2018091172397Hinge Bracket · corrodedLT WING O/B FLAP I/B FWD (WING SIDE) HINGE PIVOT HOLE BORE CORROSION. HINGE PIVOT HOLE BORE REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE DIA 2.312", FINAL HOLE DIA 2.317", MAXIMUM ALLOWABLE DIA 2.3135". OVERSIZED BUSHING FABRICATED & INSTALLSep 7, 2018 · N614FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2018091172396Hinge Bracket · corrodedLT WING O/B FLAP O/B FWD (WING SIDE) HINGE ACTUATOR O/B HOLE BORE CORROSION. HINGE ACTUATOR O/B HOLE BORE (NR 8 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09. EXISTING HOLE DIA 1.249", FINAL HOLE DIA 1.253", MAXIMUM ALLOWABLE HOLE DIA 1.220". REPAIRSep 7, 2018 · N614FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2018091172395Hinge Bracket · corrodedLT WING O/B FLAP O/B FWD (WING SIDE) HINGE ACTUATOR I/B HOLE BORE CORROSION. HINGE ACTUATOR I/B HOLE BORE (NR 8 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09. EXISTING HOLE DIA 1.249", FINAL HOLE DIA 1.253", MAXIMUM ALLOWABLE HOLE DIA 1.220". REPAIRSep 7, 2018 · N614FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2018091172394Hinge Bracket · corrodedLT WING O/B FLAP O/B FWD (WING SIDE) HINGE LOWER MOUNT O/B HOLE BORE CORROSION. HINGE LOWER MOUNT O/B HOLE BORE (NR 3 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09. EXISTING HOLE DIA 0.584", FINAL HOLE DIA 0.596", MAXIMUM ALLOWABLE HOLE DIA 0.584". SHSep 7, 2018 · N614FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2018091172393Hinge Bracket · corrodedLT WING O/B FLAP O/B FWD (WING SIDE) HINGE LOWER MOUNT I/B HOLE BORE CORROSION. HINGE LOWER MOUNT I/B HOLE BORE (NR 3 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09. EXISTING HOLE DIA 0.584", FINAL HOLE DIA 0.596", MAXIMUM ALLOWABLE HOLE DIA 0.584", Sep 7, 2018 · N614FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2018091172392Hinge Bracket · corrodedLT WING O/B FLAP O/B FWD (WING SIDE) HINGE UPPER MOUNT O/B HOLE BORE CORROSION. HINGE UPPER MOUNT O/B HOLE BORE (NR 2 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM57-44-09. EXISTING HOLE DIA 0.880", FINAL HOLE DIA 0.948", MAXIMUM ALLOWABLE DIA 0.944". REPAIR BSep 7, 2018 · N614FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2018091172391Hinge Bracket · corrodedRT WING O/B FLAP O/B FWD (WING SIDE) HINGE ACTUATOR O/B HOLE BORE CORROSION. HINGE ACTUATOR O/B HOLE BORE (HOLE 8) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09. EXISTING HOLE DIA 1.280", FINAL HOLE DIA 1.1287", MAXIMUM ALLOWABLE HOLE DIA 1.220". REPAIR BUSSep 7, 2018 · N614FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2018091172390Hinge Bracket · corrodedRT WING O/B FLAP O/B FWD (WING SIDE) HINGE ACTUATOR I/B HOLE BORE CORROSION. HINGE ACTUATOR I/B HOLE BORE (HOLE 8) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09, EXISTING HOLE DIA 1.220", FINAL HOLE DIA 1.248", MAXIMUM ALLOWABLE HOLE DIA 1.220". REPAIR BUSHSep 7, 2018 · N614FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2018091172389Hinge Bracket · corrodedRT WING O/B FLAP O/B FWD (WING SIDE) HINGE BARREL NUT HOLE SURFACE CORROSION. HINGE BARREL NUT HOLE SURFACE REWORKED PER CMM 57-44-09. EXISTING THK - UPPER 0.381", LOWER 0.386", MATERIAL REMOVED - UPPER & LOWER 0.010", REMAINING THK - UPPER 0.371", LOWER 0.376Sep 7, 2018 · N614FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2018091172385Hinge Bracket · corrodedRT WING O/B FLAP O/B FWD (WING SIDE) HINGE UPPER MOUNT O/B HOLE SURFACE CORROSION. HINGE UPPER MOUNT HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT PER CMM57-44-09. EXISTING THK 0.715", MATERIAL REMOVED 0.004", REMAINING THK 0.711", MINIMUM ALLOWABLE THK 0.72". Sep 7, 2018 · N614FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2018091172384Hinge Bracket · corrodedRT WING O/B FLAP O/B FWD (WING SIDE) HINGE UPPER MOUNT HOLE SURFACE CORROSION. HINGE UPPER MOUNT O/B HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT PER CMM57-44-09. EXISTING THK 0.715", MATERIAL REMOVED 0.004", REMAINING THK 0.711", MINIMUM ALLOWABLE THK 0.72". Sep 7, 2018 · N614FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2018091172383Hinge Bracket · corrodedRT WING O/B FLAP O/B FWD (WING SIDE) HINGE PIVOT HOLE BORE CORROSION. HINGE PIVOT HOLE BORE (HOLE 4) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09. EXISTING HOLE DIA 2.300", FINAL HOLE DIA 2.3185", MAXIMUM ALLOWABLE HOLE DIA 2.3135". REPAIR BUSHING FABRICATSep 7, 2018 · N614FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2018091172378Hinge · corrodedRT WING I/B FLAP O/B AFT (FLAP SIDE) HINGE PIVOT O/B HOLE BORE CORROSION. HINGE PIVOT O/B HOLE BORE (HOLE A AND B) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. EXISTING HOLE DIA: 1.188" - 1.283, FINAL HOLE DIA: 1.3785", MAXIMUM ALLOWABLE DIA: 1.220. REPAISep 7, 2018 · N614FE · Doug MD11F · Trailing Edge FlapsSDR FDEA2018091172377Hinge · corrodedRT WING I/B FLAP O/B AFT (FLAP SIDE) HINGE PIVOT I/B HOLE BORE CORROSION. HINGE PIVOT I/B HOLE BORE (HOLE G AND F) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. EXISTING HOLE DIA: 1.188"-1.290, FINAL HOLE DIA: 1.328", MAXIMUM ALLOWABLE DIA: 1.220. REPAIR BSep 7, 2018 · N614FE · Doug MD11F · Trailing Edge FlapsSDR FDEA2018091172376Hinge · corrodedLT WING I/B FLAP O/B AFT (FLAP SIDE) HINGE PIVOT O/B HOLE BORE CORROSION. HINGE PIVOT O/B HOLE BORE (HOLE A AND B) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. EXISTING HOLE DIA: 1.188"-1.256, FINAL HOLE DIA: 1.282", MAXIMUM ALLOWABLE DIA: 1.220. REPAIR BSep 7, 2018 · N614FE · Doug MD11F · Trailing Edge FlapsSDR FDEA2018091172375Hinge · corrodedLT WING I/B FLAP O/B AFT (FLAP SIDE) HINGE PIVOT I/B HOLE BORE CORROSION. HINGE PIVOT I/B HOLE BORE (HOLE G AND F) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. EXISTING HOLE DIA 1.188"-1.220, FINAL HOLE DIA: 1.250", MAXIMUM ALLOWABLE DIA 1.220. REPAIR BUSSep 7, 2018 · N614FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201809052352Seat Track · corrodedMAIN DECK CARGO COMPT FLOOR PANEL OPEN UP FOR SUPRORT REPAIR FOUND SEAT TRACK FLANGE CORROSION AT STA 1681, X= 8.5. CORROSION REMOVED 0.066", REMAIN 0.014", MATERIAL THK 0.080" AND FOUND EXCEEDED LIMIT PER SRM 53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1 AND EXCEEDESep 5, 2018 · N614FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA2018090512335Floor Support · corrodedUPON REMOVAL OF FLOOR PANEL FOR ACCESS, SEAT TRACK REPAIR FOUND CORROSION ON FLOOR SUPPORT AT RT STA 1761, X=- 8.5 TO X=-27.5. FLOOR SUPPORT CORROSION REMOVED AS PER SRM 51-21-01-0G AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-00-2R FIG 202. MATERIAL THK 0.70", Aug 31, 2018 · N614FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA2018090512334Floor Support · corrodedUPON REMOVAL OF FLOOR PANEL FOR ACCESS OF SEAT TRACK REPAIR FOUND CORROSION ON FLOOR SUPPORT AT RT STA 1821, X=- 8.5 TO X=- 27.5. FLOOR SUPPORT CORROSION REMOVED AS PER SRM 51- 21-01-0G AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-00-2R FIG 202. MATERIAL THK 0.0Aug 31, 2018 · N614FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA2018090512333Doubler · crackedRIGHT WING LEADING EDGE COMPARTMENT OUTBOARD OF SLAT TRACK NR 10 CUTOUT BETWEEN 5TH AND 6TH RIBS, XOS 696 FOUND L/E PLATING BEADED DOUBLER CRACK. CRACKED BEADED DOUBLER AT XOS 696 TRIMMED AND REPAIR CARRIED OUT AS PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR Aug 31, 2018 · N614FE · Doug MD11F · Wing, Plate/SkinSDR FDEA2018090512332Doubler · crackedRIGHT WING LEADING EDGE COMPARTMENT INBOARD OF ACCESS PANEL 626FB CUTOUT FOUND L/E PLATING BEADED DOUBLER CRACK. CRACKED BEADED DOUBLER TRIMMED AND REPAIR CARRIED OUT AS PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.Aug 31, 2018 · N614FE · Doug MD11F · Wing, Plate/SkinSDR FDEA2018090512331Doubler · crackedRIGHT WING LEADING EDGE COMPARTMENT OUTBOARD OF SLAT TRACK NR 10 CUTOUT BETWEEN 4TH AND 5TH RIBS (COUNT OUTBOARD FROM SLAT TRACK NR 10) AT XOS 687 FOUND L/E PLATING BEADED DOUBLER CRACK. CRACKED BEADED DOUBLER AT XOS 687 TRIMMED AND REPAIR CARRIED OUT AS PER SAug 31, 2018 · N614FE · Doug MD11F · Wing, Plate/SkinSDR FDEA2018090512330Doubler · crackedRIGHT WING LEADING EDGE COMPARTMENT OUTBOARD OF SLAT TRACK NR 10 CUTOUT BETWEEN 2ND AND 3RD RIBS (COUNT OUTBOARD FROM SLAT TRACK NR 10) AT XOS 677 FOUND L/E PLATING BEADED DOUBLER CRACK. CRACKED BEADED DOUBLER TRIMMED AND REPAIR CARRIED OUT AS PER SRM 57-40-02Aug 31, 2018 · N614FE · Doug MD11F · Wing, Plate/SkinSDR FDEA2018090512329Doubler · crackedRIGHT WING LEADING EDGE COMPARTMENT OUTBOARD OF SLAT TRACK NR 10 AT XOS 665 CUTOUT FOUND L/E PLATING BEADED DOUBLER CRACK . CRACKED BEADED DOUBLER AT XOS 665 TRIMMED AND REPAIR CARRIED OUT AS PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PEAug 31, 2018 · N614FE · Doug MD11F · Wing, Plate/SkinSDR FDEA2018090512328Seat Track · corrodedMDCC CORROSIONS ON SEAT TRACK FLANGE AT RT STA 1830, X=-107. SEAT TRACK CORROSION REMOVED 0.048" REMAIN 0.032", REMAIN 0.032", MATERIAL THK 0.080" AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A ALLOWABLE DAMAGE 1 AND EXCEEDED LIMIT. SEAT TRACK REPAIRED AS PERAug 31, 2018 · N614FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA2018090512327Floor Support · corrodedMAIN DECK CARGO AFT FLOOR PANEL SUPPORT FOUND WITH CORROSION AT STA 1887 - STA 2007 X=-25. FLOOR PANEL SUPPORT CORROSION REMOVED PER SRM 51-21-01-0G AND FOUND EXCEEDED LIMIT PER SRM 53-00-00-2R FIG 202. ORIGINAL THK 0.080", MATERIAL REMOVED 0.060", REMAINING TAug 31, 2018 · N614FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA2018090512326Floor Support · corrodedMDC AFT FLOOR SUPPORT ASSY FOUND WITH CORROSION AT STA 1887 TO STA 2007 X=0. FLOOR SUPPORT CORROSION REMOVED PER SRM 51- 21-01-0G ORIGINAL THK 0.080", MATERIAL REMOVED 0.060", REMAINING THK 0.020" AND FOUND EXCEEDED LIMIT PER SRM 53-00-00-2R FIG 202. SUPPORT Aug 31, 2018 · N614FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA2018090512323Seat Track · corrodedMAIN DECK CARGO COMPT CORROSION ON SEAT TRACK FLANGE AT RT STA 1037, X =-75.25. SEAT TRACK CORROSION REMOVED 0.046", REMAIN 0.025", MATERIAL THK 0.071" AND FOUND EXCEEDED LIMIT PER SRM 53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1 AND EXCEEDED LIMIT SEAT TRACK REPAIRAug 31, 2018 · N614FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA2018090512322Seat Track · corrodedMAIN DECK CARGO COMPT CORROSION ON SEAT TRACK FLANGE AT RT STA 975, X=-75.25. SEAT TRACK CORROSION REMOVED 0.056" REMAIN 0.015" MATERIAL THICKNESS 0.071" AND FOUND EXCEEDED LIMT AS PER SRM 53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1 AND EXCEEDED LIMIT. SEAT TRACK AAug 31, 2018 · N614FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA2018090512325Longeron Splice · crackedCRACK LINE IMAGE FOUND ON X-RAY FILM AT FWD TRANSVERSE SKIN SPLICE ASSY AT STA 6-100, LT LONGERON 4, NR 5 HOLE TO NR 6 HOLE (FROM CENTER OF SPLICE ASSY) OF CENTER FASTENER ROW. CRACK LONGERON SPLICE AT STA 6-100, LT LONGERON 4 REMOVED AND REPLACED WITH NEW FABAug 31, 2018 · N614FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA2018090512324Seat Track · corrodedMAIN DECK CARGO COMPT SEAT TRACK CORROSIONS AT RT STA 485, X= - 27.5. CORROSION REMOVED 0.070", REMAINING THK: 0.020", ORIGINAL MATERIAL THK: 0.090" AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A ALLOWABLE DAMAGE 1 FIGURE 101 AND EXCEEDED LIMIT SEAT TRACK REPAug 31, 2018 · N614FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA2018090512321Seat Track · corrodedLOWER CTR CARGO COMPT CEILING FOUND CABIN FLOOR SEAT TRACK WITH CORROSION AT STA 5-73 TO 5-113 X =-75. CORROSION REMOVED 0.044", REMAINING THK 0.027", ORIGINAL THK 0.071" AND FOUND EXCEEDED LIMIT PER SRM 53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1 AND EXCEEDED LIMIAug 31, 2018 · N614FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA2018090502294Seat Track · crackedMAIN DECK CARGO COMPT FLOOR SEAT TRACK FOUND CRACK AT STA 695 X =27.5. SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R REPAIR 1 FIG 201 AT STA 685 TO STA 705 X=27.5 SEAT TRACK. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Aug 30, 2018 · N614FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA2018090502295Seat Track · crackedMAIN DECK CARGO COMPT FLOOR SEAT TRACK FOUND CRACK AT STA 755 X = 47.5. SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R FIG 201 REPAIR 1 AT CABIN STA 725 TO 765 X= 47.5. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Aug 30, 2018 · N614FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201808292239Seat Track · crackedMAIN DECK CARGO COMPT FLOOR SEAT TRACK FOUND CRACK AT STA 635 X = 47.5. SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R REPAIR 1 FIG 201 AT CABIN STA 605 TO STA 655 X=47.5. SEAT TRACK REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Aug 29, 2018 · N614FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201808292237Seat Track · crackedMAIN DECK CARGO COMPT FLOOR SEAT TRACK FOUND CRACK AT STA 635 X= 8.5. CRACKED SEAT TRACKED REPAIRED PER SRM 53-00-52-2R REPAIR 1 FIG 201 AT CABIN STA 625 TO STA 705 X= 8.5. SEAT TRACK REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Aug 29, 2018 · N614FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201808292236Seat Track · corrodedMDC FLOOR SEAT TRACK FOUND WITH CORROSION AT STA 1821, X=- 8.5. SEAT TRACK CORROSION MATERIAL REMOVED 0.055", MATERIAL REMAIN 0.016", MATERIAL THK 0.071" FOUND EXCEED LIMIT AS PER SRM 53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1 AND EXCEEDED LIMIT. SEAT TRACK REPAIAug 29, 2018 · N614FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201808292235Doubler · crackedLEFT WING LEADING EDGE COMPARTMENT AT XOS 528 ABOVE OUTBOARD SLAT DRIVE CYLINDER FOUND L/E PLATING BEADED DOUBLER CRACK. CRACKED BEADED DOUBLER AT XOS 528 TRIMMED AND REPAIR CARRIED OUT AS PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED MAJOR AS PER GAug 29, 2018 · N614FE · Doug MD11F · Wing, Plate/Skin
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