JASC 5744

Service difficulty reports · 2,721

Reports filed under 5744 · Wing, Control Surface Attach Fittings, 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 jasc_code = '5744'
  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 FDEA201607132425Hinge · corrodedRT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, UPPER MOUNT OTBD BORE SURFACE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING THICKNESS: 0.709", MATERIAL REMOVED: 0.003", REMAINING THICKNESS: 0.706". MINIMUM ALLOWABLE THICKNESS:Jul 13, 2016 · N582FE · Doug MD11FSDR FDEA201607132424Hinge · corrodedRT WING, OTBD FLAP, OTBD FWD HINGE LOWER MOUNT INBD CORRODED. REWORKED AND FOUND, EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE: DIA 0.521", FINAL HOLE: DIA 0.613", MAXIMUM ALLOWABLE HOLE: DIA 0.584". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA NR 1-5750Jul 13, 2016 · N582FE · Doug MD11FSDR FDEA201607132423Hinge · corrodedRIGHT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE LOWER MOUNT OTBD BORE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE: DIA 0.581", FINAL HOLE: DIA 0.613", MAXIMUM ALLOWABLE HOLE: DIA 0.584". REPAIR BUSHING FABRICATED AND Jul 13, 2016 · N582FE · Doug MD11FSDR FDEA201607132422Hinge · corrodedRT WING, OTBD FLAP, OTBD FORWARD HINGE LOWER MOUNT INBD BORE SURFACE AREA CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING THICKNESS: 0.414", MATERIAL REMOVED: 0.008", REMAINING THICKNESS: 0.406", MINIMUM ALLOWABLE, THICKNESS: 0.408", RJul 13, 2016 · N582FE · Doug MD11FSDR FDEA201607132421Hinge · corrodedRT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD BORE SURFACE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING THICKNESS: 0.387", MATERIAL REMOVED: 0.008", REMAINING THICKNESS: 0.379", MINIMUM ALLOWABLE THICKNESS: Jul 13, 2016 · N582FE · Doug MD11FSDR FDEA201607132420Hinge · corrodedRIGHT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUT UPPER BOLT HOLE FOUND CORROSION. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 0.380", FINAL HOLE DIA: 0.407", MAXIMUM ALLOWABLE HOLE DIA: 0.391". REPAIR BUSHING FABRICATED Jul 13, 2016 · N582FE · Doug MD11FSDR FDEA201607132419Hinge · corrodedRIGHT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUT LOWER BOLT HOLE FOUND CORROSION. CORROSION AT RT WING, OTBD FLAP, OTBD FORWARD HINGE, WING SIDE, BARREL NUT LOWER BOLT HOLE, NR 7 HOLE, REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09. EXISTING HOJul 13, 2016 · N582FE · Doug MD11FSDR FDEA201607132418Hinge · corrodedRIGHT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUT HOLE FOUND CORROSION. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 0.662", FINAL HOLE DIA: 0.699", MAXIMUM ALLOWABLE HOLE DIA: 0.667". REPAIR BUSHING FABRICATED AND INSTALLJul 13, 2016 · N582FE · Doug MD11FSDR FDEA201607132417Hinge · corrodedRIGHT WING, OTBD FLAP, OTBD HINGE, WING SIDE, INBD ACTUATOR ATTACH BORE CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE: DIA 1.220", FINAL HOLE: DIA 1.224", MAXIMUM ALLOWABLE HOLE: DIA 1.220". REPAIR BUSHING FABRICATED AND INSTALJul 13, 2016 · N582FE · Doug MD11FSDR FDEA201607132416Hinge · corrodedRT WING, OTBD FLAP, OTBD HINGE, WING SIDE, OTBD ACTUATOR ATTACH BORE, CORRODED. REWORKED AND FOUND EXCEEDED LIMITS IAW CMM 57-44-09. EXISTING HOLE: DIA 1.220", FINAL HOLE: DIA 1.224", MAXIMUM ALLOWABLE HOLE: DIA 1.220". REPAIR BUSHING FABRICATED AND INSTALLJul 13, 2016 · N582FE · Doug MD11FSDR FDEA201607132411Hinge · corrodedLEFT WING, OTBD FLAP, INBD FORWARD HINGE, WING SIDE, ACTUATOR ATTACH OTBD BORE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 1.218", FINAL HOLE DIA: 1.224", MAXIMUM ALLOWABLE HOLE DIA: 1.220". REPAIR BUSHING FABRIJul 13, 2016 · N582FE · Doug MD11FSDR FDEA201607132409Hinge · corrodedLEFT WING, OTBD FLAP INBD FWD HINGE, WING SIDE, ACTUATOR ATTACH INBD BORE FOUND CORROSION. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-08 EXISTING HOLE DIA: 1.225", FINAL HOLE DIA: 1.231", MAXIMUM ALLOWABLE HOLE DIA: 1.220". REPAIR BUSHING FABRICATED AND Jul 13, 2016 · N582FE · Doug MD11FSDR FDEA201607132406Hinge · corrodedLT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, PIVOT BORE FOUND, CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 2.311", FINAL HOLE DIA: 2.316" AND MAXIMUM ALLOWABLE HOLE DIA: 2.3135". NEW REPAIR BUSHING FABRICATED AND INSTAJul 13, 2016 · N582FE · Doug MD11FSDR FDEA201607132403Hinge · corrodedLEFT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD BORE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 0.618", FINAL HOLE DIA: 0.645" AND MAXIMUM ALLOWABLE HOLE DIA: 0.584". NEW REPAIR BUSHING FABRICATJul 13, 2016 · N582FE · Doug MD11FSDR FDEA201607132401Hinge · corrodedLEFT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUT UPPER BOLT HOLE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 0.391", FINAL HOLE DIA: 0.407" AND MAXIMUM ALLOWABLE HOLE DIA: 0.391". NEW REPAIR BUSHING FAJul 13, 2016 · N582FE · Doug MD11FSDR FDEA201607132399Hinge · corrodedLEFT WING, OTBD FLAP OTBD FWD HINGE, WING SIDE, BARREL NUT LOWER BOLT HOLE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA, 0.390", FINAL HOLE DIA: 0.407" AND MAXIMUM ALLOWABLE HOLE DIA: 0.391". NEW REPAIR BUSHING FABRJul 13, 2016 · N582FE · Doug MD11FSDR FDEA201607132397Hinge · corrodedLEFT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUT HOLE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 0.674", FINAL HOLE DIA: 0.691" AND MAXIMUM ALLOWABLE HOLE DIA: 0.667". NEW REPAIR BUSHING, FABRICATED ANJul 13, 2016 · N582FE · Doug MD11FSDR FDEA201607132395Hinge · corrodedLEFT WING, OTBD FLAP OTBD FWD HINGE, WING SIDE, ACTUATOR ATTACH INBD BORE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 1.238", FINAL HOLE DIA: 1.244" AND MAXIMUM ALLOWABLE HOLE DIA: 1.220". NEW REPAIR BUSHING FABRIJul 13, 2016 · N582FE · Doug MD11FSDR FDEA201607132393Hinge · corrodedLEFT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, ACTUATOR ATTACH OTBD BORE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 1.247", FINAL HOLE DIA: 1.252" AND MAXIMUM ALLOWABLE HOLE DIA: 1.220". NEW REPAIR BUSHING FABRJul 13, 2016 · N582FE · Doug MD11FSDR FDEA201607012219Hinge · corrodedLEFT HAND WING OUTBOARD FLAP (WING SIDE) INBOARD FWD HINGE LOWER MOUNT OUTBOARD HOLE BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 0.706", FINAL HOLE DIA: 0.728", MAXIMUM ALLOWABLE HOLE DIA: 0.709". REPAIR BUSHING FABJul 1, 2016 · N602FE · Doug MD11FSDR FDEA201607012218Hinge · corrodedLEFT WING OUTBOARD FLAP (WING SIDE) INBOARD FWD HINGE LOWER MOUNT INBOARD HOLE BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-08. EXISTING HOLE: DIA 0.706", FINAL HOLE: DIA 0.728", MAXIMUM ALLOWABLE HOLE: DIA 0.709". REPAIR BUSHING FABRICATEDJul 1, 2016 · N602FE · Doug MD11FSDR FDEA201607012217Hinge · corrodedLEFT WING OUTBOARD FLAP (WING SIDE) INBOARD FWD HINGE UPPER MOUNT OUTBOARD HOLE BORE CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 0.942", FINAL HOLE DIA: 0.950", MAXIMUM ALLOWABLE HOLE DIA: 0.944". REPAIR BUSHING FABRICAJul 1, 2016 · N602FE · Doug MD11SDR FDEA201607012216Hinge · corrodedLEFT WING OUTBOARD FLAP (WING SIDE) INBOARD FWD HINGE UPPER MOUNT INBOARD HOLE BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 0.942", FINAL HOLE DIA: 0.950", MAXIMUM ALLOWABLE HOLE DIA: 0.944", REPAIR BUSHING FABRICATEDJul 1, 2016 · N602FE · Doug MD11SDR FDEA201607012215Hinge · corrodedLEFT WING OUTBOARD FLAP (WING SIDE) INBOARD FWD HINGE PIVOT HOLE BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 2.311", FINAL HOLE DIA: 2.317", MAXIMUM ALLOWABLE HOLE DIA: 2.3135". REPAIR BUSHING FABRICATED AND INSTAJul 1, 2016 · N602FE · Doug MD11SDR FDEA201606292189Hinge · corrodedLT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, ACTUATOR INBD HOLE BORE CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09, EXISTING HOLE DIA: 1.249", FINAL HOLE DIA: 1.252" MAXIMUM ALLOWABLE HOLE DIA: 1.220". REPAIR BUSHING FABRICATED AND INSTALLEDJun 29, 2016 · N602FE · Doug MD11FSDR FDEA201606292188Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUT LOWER HOLE BORE CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09. EXISTING HOLE D: 0.420", FINAL HOLE D: 0.423", MAXIMUM ALLOWABLE HOLE D: 0.391". REPAIR BUSHING FABRICATED AND INSTALLED IJun 29, 2016 · N602FE · Doug MD11FSDR FDEA201606292187Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUT UPPER HOLE BORE CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE: DIA 0.420", FINAL HOLE: DIA 0.423", MAXIMUM ALLOWABLE HOLE: DIA 0.391". REPAIR BUSHING FABRICATED AND INJun 29, 2016 · N602FE · Doug MD11FSDR FDEA201606292186Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE SURFACE CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING THICKNESS: 0.400", MATERIAL REMOVED: 0.006", FWD FACE; 0.023", AFT FACE, REMAINING THICKNESS: 0.371". MINIMUJun 29, 2016 · N602FE · Doug MD11FSDR FDEA201606292185Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE SURFACE CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09. EXISTING THICKNESS: 0.419", MATERIAL REMOVED: 0.006", FWD FACE; 0.006", AFT FACE, REMAINING THICKNESS: 0.389". MINIMUM Jun 29, 2016 · N602FE · Doug MD11FSDR FDEA201606292184Hinge · corrodedLT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE BORE CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 0.614", FINAL HOLE DIA: 0.620", MAXIMUM ALLOWABLE HOLE DIA: 0.584". REPAIR BUSHING FABRICATED IAW EA: 1Jun 29, 2016 · N602FE · Doug MD11FSDR FDEA201606292183Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE BORE CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 0.614", FINAL HOLE DIA: 0.620", MAXIMUM ALLOWABLE HOLE DIA: 0.584". REPAIR BUSHING FABRICATED IAW EAJun 29, 2016 · N602FE · Doug MD11FSDR FDEA201606292182Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, UPPER MOUNT OTBD HOLE BORE CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 0.942", FINAL HOLE DIA: 0.946". MAXIMUM ALLOWABLE HOLE DIA: 0.944". REPAIR BUSHING FABRICATED AND INSTAJun 29, 2016 · N602FE · Doug MD11FSDR FDEA201606292181Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, UPPER MOUNT INBD HOLE BORE CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 0.942", FINAL HOLE DIA: 0.946". MAXIMUM ALLOWABLE HOLE DIA: 0.944". REPAIR BUSHING FABRICATED BY MACHJun 29, 2016 · N602FE · Doug MD11FSDR FDEA201606292180Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE PIVOT HOLE BORE CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 2.311". FINAL HOLE DIA: 2.316". MAXIMUM ALLOWABLE HOLE DIA: 2.3135". REPAIR BUSHING FABRICATED AND INSTALLED IAWJun 29, 2016 · N602FE · Doug MD11FSDR FDEA201606101927Hinge · corrodedRT WING OTBD FLAP INBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE BORE CORROSION. CORROSION FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA 0.644", FINAL HOLE DIA 0.713", MAXIMUM ALLOWABLE DIA 0.709". REPAIR BUSHING FABRICATED AND INSTALLED IAW EAJun 10, 2016 · N620FE · Doug MD11FSDR FDEA201606101926Hinge · corrodedRT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUTS HOLE BORE CORROSION. CORROSION FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA 0.594", FINAL HOLE DIA 0.705", MAXIMUM ALLOWABLE DIA: 0.667". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-Jun 10, 2016 · N620FE · Doug MD11FSDR FDEA201606101925Hinge · corrodedLT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, ACTUATOR INBD HOLE BORE CORROSION. CORROSION FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING DIA 1.214", FINAL DIA 1.224", MAX ALLOWABLE DIA 1.220". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0325892Jun 10, 2016 · N620FE · Doug MD11FSDR FDEA201606101924Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE BORE CORROSION. CORROSION FOUND EXCEED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 0.643", FINAL HOLE DIA: 0.716", MAXIMUM ALLOWABLE DIA: 0.709". REPAIR BUSHING FABRICATED AND INSTALLED IJun 10, 2016 · N620FE · Doug MD11FSDR FDEA201606101923Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, PIVOT HOLE BORE CORROSION. CORROSION REWORKED AND FOUND EXCEEDING LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 2.306", FINAL HOLE DIA: 2.3290", MAXIMUM ALLOWABLE DIA: 2.3135". REPAIR BUSHING FABRICATED AND INSTAJun 10, 2016 · N620FE · Doug MD11FSDR FDEA201606101922Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUT LOWER HOLE BORE CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA, 0.325" FINAL HOLE DIA: 0.406" MAXIMUM ALLOWABLE DIA: 0.391". REPAIR BUSHING FABRICATED ANDJun 10, 2016 · N620FE · Doug MD11FSDR FDEA201606101921Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUT UPPER HOLE BORE CORROSION. HINGE REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 0.324" FINAL HOLE DIA: 0.406" MAXIMUM ALLOWABLE DIA: 0.391". REPAIR BUSHING FABRICATED AND INSTAJun 10, 2016 · N620FE · Doug MD11FSDR FDEA201606101920Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE LOWER MOUNT OTBD HOLE BORE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE, DIA: 0.582" FINAL HOLE, DIA: 0.598" MAXIMUM ALLOWABLE DIA: 0.584". REPAIR BUSHING FABRICATED AND INSJun 10, 2016 · N620FE · Doug MD11FSDR FDEA201606101919Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE BORE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE, DIA: 0.579" FINAL HOLE DIA: 0.598" MAXIMUM ALLOWABLE DIA: 0.584". REPAIR BUSHING FABRICATED AND INJun 10, 2016 · N620FE · Doug MD11FSDR FDEA201605241727Hinge · corrodedRIGHT WING, OTBD FLAP, INBD FWD HINGE, WING SIDE, BARREL NUTS HOLE SURFACE CORROSION. CORROSION AT RT WING, OTBD FLAP, INBD FWD HINGE, WING SIDE, BARREL NUT HOLE SURFACE REWORKED IAW CMM 57-44-08. EXISTING THICKNESS: UPPER 0.368", LOWER 0.365". MATERIAL REMOVMay 24, 2016 · N595FE · Doug MD11FSDR FDEA201605241726Hinge · corrodedLEFT WING, OTBD FLAP, INBD FWD HINGE, WING SIDE, BARREL NUTS, HOLE SURFACE CORROSION. CORROSION AT LT WING, OTBD FLAP 11B, FWD HINGE, WING SIDE, BARREL NUT, HOLE SURFACE REWORKED IAW CMM 57-44-08. EXISTING THICKNESS: UPPER 0.371", LOWER: 0.3955", MATERIALMay 24, 2016 · N595FE · Doug MD11FSDR FDEA201605231720Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD FWD HINGE BRACKET, WING SIDE, SIDE ATTACH SURFACE FOUND CORROSION. REWORKED IAW CMM 57-44-08. EXISTING THICKNESS: UPPER 0.402", LOWER 0.378", MATERIAL REMOVED: UPPER 0.010", LOWER 0.010" AND REMAINING THICKNESS: UPPER 0.392", LOWER 0May 23, 2016 · N615FE · Doug MD11FSDR FDEA201605231719Hinge Bracket · corrodedRIGHT WING OTBD FLAP INBD FWD HINGE BRACKET, WING SIDE, SIDE ATTACH SURFACE FOUND CORROSION. REWORKED IAW CMM 57-44-08. EXISTING THICKNESS: UPPER 0.392", LOWER 0.353", MATERIAL REMOVED: UPPER 0.010", LOWER 0.010" AND REMAINING THICKNESS: UPPER 0.382", LOWER May 23, 2016 · N615FE · Doug MD11FSDR FDEA201605221709Hinge Bracket · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE BRACKET, WING SIDE, LOWER OTBD STUD ATTACH SPOT FACE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING THICKNESS: 0.408", MATERIAL REMOVED: FWD 0.008", AFT 0.025", REMAINING THICKNESS: 0.375" ANMay 22, 2016 · N615FE · Doug MD11FSDR FDEA201605221708Hinge Bracket · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE BRACKET, WING SIDE, LOWER OTBD STUD ATTACH BORE FOUND CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 0.584", FINAL HOLE DIA: 0.613" AND MAXIMUM ALLOWABLE HOLE DIA: 0.584". NEW May 22, 2016 · N615FE · Doug MD11FSDR FDEA201605221707Hinge Bracket · corrodedRIGHT WING, OTBD FLAP OTBD FWD HINGE BRACKET, WING SIDE, LOWER INBD STUD ATTACH BORE FOUND CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 0.584", FINAL HOLE DIA: 0.612" AND MAXIMUM ALLOWABLE HOLE DIA: 0.584". NEWMay 22, 2016 · N615FE · Doug MD11F
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