N605FE
Service difficulty reports · 508
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 = 'N605FE' 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 = 'N605FE' 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 FDEA201811273372Longeron · corrodedFOUND CORROSION ON LONGERON 49R AT STA 1681. COMPLIED WITH E.A. 1-5310-T0343744; PART 1; MAINFRAME AFT INTERMEDIATE FUSELAGE; BOTTOM; STA. 1671-1691; R/H LONGERONS L49 & L50 CORROSION REPAIR..SDR FDEA201802982213Controller · failedAT FL330, 1:30 MINUTES INTO FLIGHT, RECEIVED LVL3 LOWER CARGO FIRE AFT ALERT, DECLARED AN EMERGENCY, RAN QRH FOR LOWER CARGO FIRE AFT AND DIVERTED TO KPHL. ON LANDING, FIRE DEPT SCANNED AIRPLANE AND REPORTED NO HOT SPOTS. R&R NR 1 & 2 LOWER CARGO FIRE EXTINGUISDR FDEA201807211799Support · corrodedLT NR 1 SPOILER ACTUATOR LOWER HINGE I/B BUSHING HOLE SPOT FACE FOUND WITH CORROSION. CORROSION AT LT NR 1 SPOILER ACTUATOR LOWER HINGE I/B BUSHING HOLE SPOT FACE REWORKED AS PER SRM 51-21-01-0G. EXISTING THICKNESS: 0.406", MATERIAL REMOVED I/B FACE: 0.041" , SDR FDEA201807211798Support · excess playLT WING NR 1 SPOILER ACTUATOR FOUND LOWER HINGE FREE PLAY. LT NR 1 SPOILER ACTUATOR LOWER HINGE I/B AND O/B HOLES REWORKED AS PER SRM 51-21-01-0G. I/B HOLE EXISTING HOLE DIA 0.954"-0.970", FINAL HOLE DIA 1.069", O/B HOLE EXISTING HOLE DIA 1.500"-1.505", FINALSDR FDEA201807211797Support · corrodedRT NR 1 SPOILER ACTUATOR LOWER HINGE I/B BUSHING HOLE SPOT FACE FOUND WITH CORROSION. CORROSION AT RT NR 1 SPOILER ACTUATOR LOWER HINGE I/B BUSHING HOLE SPOT FACE REWORKED AS PER SRM 51-21-01-0G. EXISTING THICKNESS: 0.406", MATERIAL REMOVED I/B FACE: 0.035", OSDR FDEA201807211796Support · excess playRT NR 1 SPOILER LOWER HINGE FOUND FREE PLAY. RT NR 1 SPOILER LOWER HINGE HOLE REWORKED AS PER SRM 51-21-01-0G. EXISTING HOLE DIA 0.954"-0.964", FINAL HOLE DIA 1.069", REPAIR BUSHING 01 EA FABRICATED AND INSTALLED AS PER EA 1-5750-T0341116 PT 1 STEP 4 AND STEP SDR FDEA201807241788Hinge Bracket · corrodedRT O/B FLAP FWD HINGE (WING SIDE) ACTUATOR O/B HOLE BORE FOUND WITH CORROSION. HINGE ACTUATOR O/B HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 1.250", FINAL HOLE DIA 1.253", MAXIMUM ALLOWABLE HOLE DIA 1.220". OVERSIZED BUSHISDR FDEA201807171764Bracket · corrodedLT O/B FLAP O/B FWD (WING SIDE) PIVOT HOLE BORE FOUND WITH CORROSION. IDLER BRACKET ATTACH HOLE BORE REWORKED AS PER SRM 51-21-01-0G. EXISTING HOLE DIA 1.0", FINAL HOLE DIA 1.384", LOCAL BLEND POSITION 9 O'CLOCK POSITION, L=0.25" X W= 0.25", DEPTH=0.065". I/B SDR FDEA201807171763Hinge · corrodedRT O/B FLAP O/B AFT HINGE (FLAP SIDE) PIVOT I/B HOLE BORE FOUND WITH CORROSION. AFT HINGE (FLAP SIDE) PIVOT I/B HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-04. EXISTING HOLE DIA 1.148", FINAL HOLE DIA 1.182", MAXIMUM ALLOWABLE HOLE DIA 1.150". OSDR FDEA201807171762Hinge · corrodedRT O/B FLAP I/B AFT HINGE PIVOT I/B HOLE BORE FOUND WITH CORROSION. AFT HINGE PIVOT I/B HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-04. EXISTING HOLE DIA 1.149", FINAL HOLE DIA 1.182", MAXIMUM ALLOWABLE HOLE DIA 1.150". REPAIR BUSHING FABRICATEDSDR FDEA201807171761Hinge · corrodedLT O/B FLAP I/B AFT HINGE (FLAP SIDE) I/B PIVOT HOLE BORE FOUND WITH CORROSION. CORRODED PIVOT HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-04. EXISTING HOLE DIA 1.124". FINAL HOLE DIA 1.182", MAXIMUM ALLOWABLE HOLE DIA 1.150". OVERSIZED BUSHING SDR FDEA201807171760Hinge Bracket · corrodedRT O/B FLAP O/B FWD HINGE (WING SIDE) ACTUATOR I/B HOLE BORE FOUND WITH CORROSION. FWD HINGE (WING SIDE) ACTUATOR I/B HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 1.221", FINAL HOLE DIA 1.248", MAXIMUM ALLOWABLE HOLE DIA 1.2SDR FDEA201807171759Hinge Bracket · corrodedRT O/B FLAP O/B FWD HINGE (WING SIDE) BARREL NUT HOLE SURFACE FOUND WITH CORROSION. FWD HINGE (WING SIDE) BARREL NUT HOLE SURFACE REWORKED AS PER CMM 57-44-09. EXISTING THICKNESS UPPER: 0.409", LOWER: 0.399", MATERIAL REMOVED UPPER: 0.013", LOWER: 0.013", REMASDR FDEA201807171758Hinge Bracket · corrodedRT O/B FLAP O/B FWD HINGE (WING SIDE) LOWER BARREL NUT HOLE BORE FOUND WITH CORROSION. FWD HINGE (WING SIDE) LOWER BARREL NUT HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 0.389", FINAL HOLE DIA 0.406", MAXIMUM ALLOWABLE HOLESDR FDEA201807171757Hinge Bracket · corrodedRT O/B FLAP O/B FWD HINGE (WING SIDE) UPPER BARREL NUT HOLE BORE FOUND WITH CORROSION. FWD HINGE (WING SIDE) UPPER BARREL NUT BORE (7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 0.389", FINAL HOLE DIA 0.406", MAXIMUM ALLOWABLE SDR FDEA201807171756Hinge Bracket · corrodedRT O/B FLAP O/B FWD HINGE (WING SIDE) LOWER MOUNT O/B HOLE SURFACE FOUND WITH CORROSION. FWD HINGE (WING SIDE) LOWER MOUNT O/B HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING THICKNESS 0.430", MATERIAL REMOVED: 0.007", (FWD) AND 0.01SDR FDEA201807171755Hinge Bracket · corrodedRT O/B FLAP O/B FWD HINGE (WING SIDE) LOWER MOUNT I/B HOLE SURFACE FOUND WITH CORROSION. FWD HINGE (WING SIDE) LOWER MOUNT I/B HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING THICKNESS: 0.435". MATERIAL REMOVED: 0.007" (FWD), 0.024" SDR FDEA201807171754Hinge Bracket · corrodedRT O/B FLAP O/B FWD HINGE (WING SIDE) LOWER MOUNT O/B HOLE BORE FOUND WITH CORROSION. FWD HINGE (WING SIDE) LOWER MOUNT O/B HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 0.597", FINAL HOLE DIA 0.613", MAXIMUM ALLOWABLE HOLE DSDR FDEA201807171753Hinge Bracket · corrodedRT O/B FLAP O/B FWD HINGE (WING SIDE) LOWER MOUNT I/B HOLE BORE FOUND WITH CORROSION. FWD HINGE (WING SIDE) LOWER MOUNT I/B HOLE BORE (3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 0.596", FINAL HOLE DIA 0.613", MAXIMUM ALLOWSDR FDEA201807171752Hinge Bracket · corrodedRT O/B FLAP O/B FWD HINGE (WING SIDE) ACTUATOR O/B HOLE BORE FOUND WITH CORROSION. FWD HINGE (WING SIDE) UPPER MOUNT O/B HOLE BORE (2 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 0.955", MAXIMUM ALLOWABLE HOLE DIA 0.944". OVERSISDR FDEA201807171751Hinge Bracket · corrodedRT O/B FLAP O/B FWD HINGE (WING SIDE) PIVOT HOLE BORE FOUND WITH CORROSION. FWD HINGE (WING SIDE) PIVOT HOLE BORE (4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 2.312", FINAL HOLE DIA 2.316", MAXIMUM ALLOWABLE HOLE DIA 2.3135SDR FDEA201807171750Hinge Bracket · corrodedRT O/B FLAP I/B FWD HINGE (WING SIDE) BARREL NUT HOLE SURFACE FOUND WITH CORROSION. FWD HINGE (WING SIDE) BARREL NUT HOLE SURFACE REWORKED AS PER CMM 57-44-08. EXISTING THICKNESS UPPER: 0.375", LOWER: 0.351", UPPER: 0.003", LOWER: 0.003", REMAINING THICKNESS USDR FDEA201807171749Hinge Bracket · corrodedRT O/B FLAP I/B FWD HINGE (WING SIDE) ACTUATOR O/B HOLE BORE FOUND WITH CORROSION. ACTUATOR O/B HOLE BORE (8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. EXISTING HOLE DIA 1.221", FINAL HOLE DIA 1.2245", MAXIMUM ALLOWABLE HOLE DIA 1.220". OVERSIZSDR FDEA201807171748Hinge Bracket · corrodedRT O/B FLAP I/B FWD HINGE (WING SIDE) ACTUATOR I/B HOLE BORE FOUND WITH CORROSION. ACTUATOR I/B HOLE BORE (8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. EXISTING HOLE DIA 1.224", FINAL HOLE DIA 1.227", MAXIMUM ALLOWABLE HOLE DIA 1.220". OVERSIZESDR FDEA201807171747Hinge Bracket · corrodedRT O/B FLAP I/B FWD HINGE (WING SIDE) LOWER MOUNT O/B HOLE SURFACE FOUND WITH CORROSION. LOWER MOUNT O/B HOLE SURFACE (7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. EXISTING THICKNESS: 0.434", MATERIAL REMOVED FWD FACE: 0.008", AFT FACE: 0.009",SDR FDEA201807171746Hinge Bracket · corrodedRT O/B FLAP I/B FWD HINGE (WING SIDE) LOWER MOUNT I/B HOLE SURFACE FOUND WITH CORROSION. LOWER MOUNT O/B HOLE SURFACE (7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. EXISTING THICKNESS 0.425", MATERIAL REMOVED: 0.008", REMAINING THICKNESS: 0.417"SDR FDEA201807171745Hinge Bracket · corrodedRT O/B FLAP I/B FWD HINGE (WING SIDE) LOWER MOUNT O/B HOLE BORE FOUND WITH CORROSION. FWD HINGE (WING SIDE) LOWER MOUNT O/B HOLE BORE (7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. EXISTING HOLE DIA 0.720", FINAL HOLE DIA 0.738", MAXIMUM ALLOWABSDR FDEA201807171744Hinge Bracket · corrodedRT O/B FLAP I/B FWD HINGE (WING SIDE) LOWER MOUNT I/B HOLE BORE FOUND WITH CORROSION. FWD HINGE (WING SIDE) LOWER MOUNT I/B HOLE BORE (7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. EXISTING HOLE DIA 0.709", FINAL HOLE DIA 0.738", MAXIMUM ALLOWABSDR FDEA201807171743Hinge Bracket · corrodedLT O/B FLAP I/B FWD (WING SIDE) HINGE BARREL NUT HOLE SURFACE FOUND WITH CORROSION. FWD HINGE (WING SIDE) BARREL NUT HOLE SURFACE REWORKED AS PER CMM 57-44-08. EXISTING THICKNESS UPPER: 0.376", LOWER: 0.373", MATERIAL REMOVED UPPER: 0.003", LOWER: 0.003", REMASDR FDEA201807171742Hinge Bracket · corrodedLT O/B FLAP I/B FWD (WING SIDE) HINGE ACTUATOR O/B HOLE BORE FOUND WITH CORROSION. FWD HINGE (WING SIDE) ACTUATOR O/B HOLE BORE (8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. EXISTING HOLE DIA 1.249", FINAL HOLE DIA 1.280", MAXIMUM ALLOWABLE HOLSDR FDEA201807171741Hinge Bracket · corrodedLT O/B FLAP I/B FWD (WING SIDE) HINGE ACTUATOR I/B HOLE BORE FOUND WITH CORROSION. FWD HINGE ACTUATOR I/B HOLE BORE (NR 8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. EXISTING HOLE DIA 1.224", FINAL HOLE DIA 1.280", MAXIMUM ALLOWABLE HOLE DIA 1.2SDR FDEA201807171740Hinge Bracket · corrodedLT O/B FLAP I/B FWD (WING SIDE) HINGE LOWER MOUNT I/B HOLE BORE FOUND WITH CORROSION. FWD HINGE LOWER MOUNT I/B HOLE BORE (NR 7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. EXISTING HOLE DIA 0.650", FINAL HOLE DIA 0.713", MAXIMUM ALLOWABLE HOLE SDR FDEA201807171739Hinge Bracket · corrodedLT O/B FLAP O/B FWD (WING SIDE) PIVOT HOLE BORE FOUND WITH CORROSION. FWD HINGE PIVOT HOLE BORE (NR 4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. EXISTING HOLE DIA 2.3159", FINAL HOLE DIA 2.321", MAXIMUM ALLOWABLE HOLE DIA 2.3135". OVERSIZED BUSDR FDEA201807171738Hinge Bracket · corrodedLT O/B FLAP O/B FWD (WING SIDE) HINGE ACTUATOR O/B HOLE BORE FOUND WITH CORROSION. HINGE ACTUATOR O/B HOLE BORE (NR 8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 1.220", FINAL HOLE DIA 1.251", MAXIMUM ALLOWABLE HOLE DIA 1.220SDR FDEA201807171737Hinge Bracket · corrodedLT O/B FLAP O/B FWD (WING SIDE) HINGE ACTUATOR I/B HOLE BORE FOUND WITH CORROSION. ACTUATOR I/B HOLE BORE (NR 8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 1.220", FINAL HOLE DIA 1.251", MAXIMUM ALLOWABLE HOLE DIA 1.220" . OVERSDR FDEA201807171736Hinge Bracket · corrodedLT O/B FLAP O/B FWD (WING SIDE) HINGE LOWER BARREL NUT HOLE FOUND WITH CORROSION. LOWER BARREL NUT HOLE (NR 7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 0.384", FINAL HOLE DIA 0.409", MAXIMUM ALLOWABLE HOLE DIA 0.391". OVERSIZSDR FDEA201807171735Hinge Bracket · corrodedLT O/B FLAP O/B FWD (WING SIDE) PIVOT HOLE BORE FOUND WITH CORROSION. HINGE UPPER BARREL NUT HOLE (NR 7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE: DIAMETER 0.384", FINAL HOLE DIAMETER: 0.409", MAXIMUM ALLOWABLE HOLE DIAMETER: 0.3SDR FDEA201807171734Pivot · corrodedLT O/B FLAP O/B FWD (WING SIDE) PIVOT HOLE BORE FOUND WITH CORROSION. HINGE LOWER MOUNT O/B HOLE BORE (3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE: DIAMETER 0.582", FINAL HOLE DIAMETER: 0.630" MAXIMUM ALLOWABLE HOLE DIAMETER: 0.5SDR FDEA201807171733Bracket · corrodedLT O/B FLAP O/B FWD (WING SIDE) PIVOT HOLE BORE FOUND WITH CORROSION. HINGE LOWER MOUNT O/B HOLE BORE (NR 3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE: DIAMETER 0.582", FINAL HOLE DIAMETER: 0.630" MAXIMUM ALLOWABLE HOLE DIAMETER:SDR FDEA201807171732Hinge Bracket · corrodedLT O/B FLAP O/B FWD (WING SIDE) HINGE LOWER MOUNT I/B HOLE BORE FOUND WITH CORROSION. HINGE LOWER MOUNT I/B HOLE BORE (3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE: DIAMETER 0.582", FINAL HOLE DIAMETER: 0.627" MAXIMUM ALLOWABLE SDR FDEA201807171731Pivot · corrodedLT O/B FLAP O/B FWD (WING SIDE) PIVOT HOLE BORE FOUND WITH CORROSION. CORROSION AT LT O/B FLAP O/B FWD (WING SIDE) PIVOT HOLE BORE (4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE: DIAMETER 2.310". FINAL HOLE DIAMETER: 2.354". MAXIMUSDR FDEA201807171730Hinge Bracket · wornRT INBOARD FLAP OUTBOARD FWD HINGE (WING SIDE) PIVOT BUSHING WORN. RT I/B FLAP O/B FWD HINGE (WING SIDE) PIVOT BORE MEASURED DIA 2.500" AND FOUND WITHIN LIMIT AS PER CMM 57-44-07. MAXIMUM ALLOWABLE HOLE DIA 2.531". NEW BUSHING FABRICATED AND INSTALLED AS PER CSDR FDEA201807171729Hinge Bracket · wornLT INBOARD FLAP OUTBOARD FWD HINGE (WING SIDE) PIVOT BUSHING WORN. LT I/B FLAP O/B FWD HINGE (WING SIDE) PIVOT BORE MEASURED DIA 2.526" AND FOUND WITHIN LIMIT AS PER CMM 57-44-07. MAXIMUM ALLOWABLE HOLE DIA 2.531". NEW BUSHING FABRICATED AND INSTALLED AS PER CSDR FDEA2018071641711Hinge Bracket · corrodedRT INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) INBOARD PIVOT HOLE BORE FOUND WITH CORROSION. CORROSION (HOLE G AND F) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03. EXISTING HOLE DIA 1.255", FINAL HOLE DIA 1.284", MAXIMUM ALLOWABLE HOLE DIA 1.220". OVERSSDR FDEA2018071641710Hinge Bracket · corrodedRT INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) OUTBOARD PIVOT HOLE BORE FOUND WITH CORROSION. CORROSION (HOLE A AND B) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03. EXISTING HOLE DIA 1.290", FINAL HOLE DIA 1.326", MAXIMUM ALLOWABLE HOLE DIA 1.220". OVERSDR FDEA2018071641709Hinge Bracket · corrodedLT INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT OUTBOARD HOLE BORE FOUND WITH CORROSION. CORROSION (HOLE A AND B) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03. EXISTING HOLE DIA 1.254", FINAL HOLE DIA 1.2835", MAXIMUM ALLOWABLE HOLE DIA 1.220". OVESDR FDEA2018071641708Hinge Bracket · corrodedLT INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT INBOARD HOLE BORE FOUND WITH CORROSION. CORROSION (HOLE G AND F) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03. EXISTING HOLE DIA 1.1885", FINAL HOLE DIA 1.222", MAXIMUM ALLOWABLE HOLE DIA 1.220". OVSDR FDEA2018071641707Skin · corrodedUPPER AFT RUDDER ASSEMBLY LT UPPER SKIN FOUND WITH CORROSION AT APPROX ZAR 554.920. CORROSION REMOVED PER SRM 51-21-01-0G AND FOUND EXCEEDED ALLOWABLE LIMITS AS PER SRM 55-00-00-2R FIG 202. ORIGINAL THK 0.016", THK REMOVED 0.015", THK REMAINED 0.001". CARRIEDSDR FDEA201807091652Skin · crackedDURING HFEC INSPECTION, 01 EA CRACK FOUND APPROX 1/8 INCH IN LENGTH AT RT WING CORNER NR 5 SLAT ACTUATOR ACCESS DOOR, FORWARD INBOARD CORNER. REPAIR CARRIED OUT AT RT WING CORNER NR 5 SLAT ACTUATOR ACCESS DOOR FWD INBOARD CORNER AT XOS 490 AS PER SRM 57-40-01-SDR FDEA201807091651Skin · crackedDURING HFEC INSPECTION, 01 EA CRACK FOUND APPROX 1/2 INCH IN LENGTH AS MARKED AT LT WING CORNER NR 13 SLAT TRACK NR 10 CUTOUT, AFT INBOARD CORNER. REPAIR CARRIED OUT AT LT WING CORNER NR 13 SLAT TRACK NR 10 CUTOUT AT XOS 659 AS PER SRM 57-40-02-2R FIG 201 REPA
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