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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
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 BUSSDR 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 BUSHSDR 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 FASDR 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". REPAISDR 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 0.368SDR 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 BUSSDR 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 BUSSDR 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.SDR 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 0.41SDR 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". OVERSDR 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". OVESDR 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 0.3SDR 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 & INSTALLSDR 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". REPAIRSDR 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". REPAIRSDR 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". SHSDR 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", SDR 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 BSDR 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 BUSSDR 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 BUSHSDR 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 0.376SDR 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". SDR 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". SDR 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 FABRICATSDR 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. REPAISDR 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 BSDR 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 BSDR 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 BUSSDR 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 EXCEEDESDR 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", SDR 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 0.0SDR 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 SDR 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.SDR 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 SSDR 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 57-40-02SDR 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 PESDR 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 PERSDR 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 TSDR 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 SDR 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 REPAIRSDR 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 ASDR 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 FABSDR 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 REPSDR 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 LIMISDR 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.SDR 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.SDR 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.SDR 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.SDR 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 REPAISDR 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 G
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