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.

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..Nov 27, 2018 · N605FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR 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 EXTINGUIAug 28, 2018 · N605FE · Doug MD11F · Fire DetectionSDR 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" , Jul 21, 2018 · N605FE · Doug MD11F · SpoilersSDR 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", FINALJul 21, 2018 · N605FE · Doug MD11F · SpoilersSDR 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", OJul 21, 2018 · N605FE · Doug MD11F · SpoilersSDR 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 Jul 21, 2018 · N605FE · Doug MD11F · SpoilersSDR 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 BUSHIJul 20, 2018 · N605FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR 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 Jul 17, 2018 · N605FE · Doug MD11F · Trailing Edge FlapsSDR 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". OJul 17, 2018 · N605FE · Doug MD11F · Trailing Edge FlapsSDR 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 FABRICATEDJul 17, 2018 · N605FE · Doug MD11F · Trailing Edge FlapsSDR 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 Jul 17, 2018 · N605FE · Doug MD11F · Trailing Edge FlapsSDR 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 1.2Jul 17, 2018 · N605FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR 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", REMAJul 17, 2018 · N605FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR 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 HOLEJul 17, 2018 · N605FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR 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 Jul 17, 2018 · N605FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR 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 0.01Jul 17, 2018 · N605FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR 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" Jul 17, 2018 · N605FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR 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 DJul 17, 2018 · N605FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR 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 ALLOWJul 17, 2018 · N605FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR 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". OVERSIJul 17, 2018 · N605FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR 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 2.3135Jul 17, 2018 · N605FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR 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 UJul 17, 2018 · N605FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR 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". OVERSIZJul 17, 2018 · N605FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR 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". OVERSIZEJul 17, 2018 · N605FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR 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",Jul 17, 2018 · N605FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR 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"Jul 17, 2018 · N605FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR 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 ALLOWABJul 17, 2018 · N605FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR 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 ALLOWABJul 17, 2018 · N605FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR 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", REMAJul 17, 2018 · N605FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR 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 HOLJul 17, 2018 · N605FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR 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 1.2Jul 17, 2018 · N605FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR 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 Jul 17, 2018 · N605FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR 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 BUJul 17, 2018 · N605FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR 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 1.220Jul 17, 2018 · N605FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR 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" . OVERJul 17, 2018 · N605FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR 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". OVERSIZJul 17, 2018 · N605FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR 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: 0.3Jul 17, 2018 · N605FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR 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: 0.5Jul 17, 2018 · N605FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR 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:Jul 17, 2018 · N605FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR 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 Jul 17, 2018 · N605FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR 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". MAXIMUJul 17, 2018 · N605FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR 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 CJul 17, 2018 · N605FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR 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 CJul 17, 2018 · N605FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR 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". OVERSJul 14, 2018 · N605FE · Doug MD11F · Trailing Edge FlapsSDR 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". OVERJul 14, 2018 · N605FE · Doug MD11F · Trailing Edge FlapsSDR 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". OVEJul 14, 2018 · N605FE · Doug MD11F · Trailing Edge FlapsSDR 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". OVJul 14, 2018 · N605FE · Doug MD11F · Trailing Edge FlapsSDR 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". CARRIEDJul 14, 2018 · N605FE · Doug MD11F · Rudder, Plate/SkinSDR 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-Jul 9, 2018 · N605FE · Doug MD11F · Wing, Plate/SkinSDR 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 REPAJul 9, 2018 · N605FE · Doug MD11F · Wing, Plate/Skin
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