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 FDEA201605201685Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, ACTUATOR ATTACH OTBD LUG BORE FOUND CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 1.248", FINAL HOLE DIA: 1.252" AND MAXIMUM ALLOWABLE HOLE DIA: 1.220". NEMay 20, 2016 · N615FE · Doug MD11FSDR FDEA201605201684Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, ACTUATOR ATTACH INBD LUG BORE FOUND CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 1.249", FINAL HOLE DIA: 1.252" AND MAXIMUM ALLOWABLE HOLE DIA: 1.220". NEMay 20, 2016 · N615FE · Doug MD11FSDR FDEA201605201683Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, LOWER OTBD STUD ATTACH BORE FOUND CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM57-44-08. EXISTING HOLE DIA: 0.709", FINAL HOLE DIA: 0.727" AND MAXIMUM ALLOWABLE HOLE DIA: 0.709". NEW SMay 20, 2016 · N615FE · Doug MD11FSDR FDEA201605201682Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, LOWER INBD STUD ATTACH BORE FOUND CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 0.709", FINAL HOLE DIA: 0.727" AND MAXIMUM ALLOWABLE HOLE DIA: 0.709". NEW May 20, 2016 · N615FE · Doug MD11FSDR FDEA201605201680Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, PIVOT BORE FOUND CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM57-44-08. EXISTING HOLE DIA: 2.311", FINAL HOLE DIA: 2.316" AND MAXIMUM ALLOWABLE HOLE DIA: 2.3135". NEW REPAIR BUSHING FAMay 20, 2016 · N615FE · Doug MD11FSDR FDEA201605201679Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET, WING SIDE, ACTUATOR ATTACH OTBD LUG BORE FOUND CORROSION. NR 8 HOLE CORROSION REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER 1.219", FINAL HOLE DIAMETER 1.224" & MAXIMUM ALLOWABLE HOLE DIMay 20, 2016 · N615FE · Doug MD11FSDR FDEA201605201678Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET, WING SIDE, ACTUATOR ATTACH INBD LUG BORE FOUND CORROSION. NR 8 HOLE CORROSION REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER 1.218", FINAL HOLE DIAMETER 1.224" & MAXIMUM ALLOWABLE HOLE DIMay 20, 2016 · N615FE · Doug MD11FSDR FDEA201605201677Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET, WING SIDE, LOWER OTBD STUD ATTACH SPOT FACE FOUND CORROSION. REWORKED & FOUND EXCEEDED LIMIT IAW MM 57-44-09. EXISTING THICKNESS 0.421", MATERIAL REMOVED, FWD FACE 0.009" & AFT FACE 0.009", REMAINING THICKNESS 0.4May 20, 2016 · N615FE · Doug MD11FSDR FDEA201605201676Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET, WING SIDE, LOWER INBD STUD ATTACH SPOT FACE FOUND CORROSION. REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING THICKNESS 0.399", MATERIAL REMOVED 0.009", REMAINING THICKNESS 0.390" & MINIMUM ALLOWABLE THIMay 20, 2016 · N615FE · Doug MD11FSDR FDEA201605201675Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET, WING SIDE, LOWER OTBD STUD ATTACH BORE FOUND CORROSION. NR 3 HOLE CORROSION REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER 0.581", FINAL HOLE DIAMETER 0.589" & MAXIMUM ALLOWABLE HOLE DIAMMay 20, 2016 · N615FE · Doug MD11FSDR FDEA201605201674Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET, WING SIDE, LOWER INBD STUD ATTACH BORE FOUND CORROSION. HOLE 3 CORROSION REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER 0.596", FINAL HOLE DIAMETER 0.598" & MAXIMUM ALLOWABLE HOLE DIAMETEMay 20, 2016 · N615FE · Doug MD11FSDR FDEA201605171635Hinge · corrodedRIGHT WING, OTBD FLAP INBD FWD HINGE, WING SIDE, ACTUATOR OTBD HOLE BORE CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING DIA: 1.282", FINAL DIA: 1.288", MAXIMUM ALLOWABLE DIA: 1.220". REPAIR BUSHING FABRICATED AND INSTALLEDMay 17, 2016 · N595FE · Doug MD11FSDR FDEA201605171634Hinge · corrodedRIGHT WING, OTBD FLAP INBD FWD HINGE, WING SIDE, ACTUATOR INBD HOLE BORE CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING DIA: 1.250", FINAL DIA: 1.254", MAXIMUM ALLOWABLE DIA: 1.220". REPAIR BUSHING FABRICATED BY MACHINING AMay 17, 2016 · N595FE · Doug MD11FSDR FDEA201605171633Hinge · corrodedRIGHT WING, OTBD FLAP INBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE BORE CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING DIA: 0.708", FINAL DIA: 0.722". MAXIMUM ALLOWABLE DIA: 0.709". SHOULDER BUSHING FABRICATED BY MACHIMay 17, 2016 · N595FE · Doug MD11FSDR FDEA201605171632Hinge · corrodedRIGHT WING, OTBD FLAP INBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE BORE CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING DIA: 0.708", FINAL DIA: 0.722". MAXIMUM ALLOWABLE DIA : 0.709". SHOULDER BUSHING FABRICATED BY MACHMay 17, 2016 · N595FE · Doug MD11FSDR FDEA201605171631Hinge · corrodedRIGHT WING, OTBD FLAP INBD FWD HINGE, WING SIDE, UPPER MOUNT OTBD HOLE BORE CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING DIA: 0.943", FINAL DIA: 0.953". MAXIMUM ALLOWABLE DIA: 0.944". REPAIRED BUSHING, FABRICATED BY MACMay 17, 2016 · N595FE · Doug MD11FSDR FDEA201605171630Hinge · corrodedRIGHT WING, OTBD FLAP OTBD FWD HINGE, WING SIDE, ACTUATOR OTBD HOLE BORE CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 1.251 INCH, FINAL DIAMETER 1.254 INCH & MAX ALLOWABLE DIAMETER 1.220 INCH;. REPAIRED BUSHING, FAMay 17, 2016 · N595FE · Doug MD11FSDR FDEA201605171629Hinge · corrodedRIGHT WING, OTBD FLAP OTBD FWD HINGE, WING SIDE, BARREL NUT LOWER HOLE BORE CORROSION. CORROSION AT HOLE NR 7 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 0.382 INCH, FINAL DIAMETER 0.410 INCH & MAXIMUM ALLOWABLE DIAMETER 0.391 INCH. RMay 17, 2016 · N595FE · Doug MD11FSDR FDEA201605171628Hinge · corrodedRIGHT WING, OTBD FLAP OTBD FWD HINGE, WING SIDE, BARREL NUT UPPER HOLE BORE CORROSION. CORROSION HOLE NR 7 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 0.382 INCH, FINAL DIAMETER 0.410 INCH & MAX ALLOWABLE DIAMETER 0.391 INCH. REPAIREDMay 17, 2016 · N595FE · Doug MD11FSDR FDEA201605171627Hinge · corrodedRIGHT WING, OTBD FLAP OTBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE BORE CORROSION. CORROSION AT HOLE 3 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 0.598 INCHES, FINAL DIAMETER 0.604 INCHES, MAX ALLOWABLE DIAMETER 0.584 INCHES. REPMay 17, 2016 · N595FE · Doug MD11FSDR FDEA201605171626Hinge · corrodedRIGHT WING, OTBD FLAP OTBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE BORE CORROSION. CORROSION AT HOLE 3 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 0.598 INCHES, FINAL DIAMETER 0.604 INCHES, MAX ALLOWABLE DIAMETER 0.584 INCHES. REPMay 17, 2016 · N595FE · Doug MD11FSDR FDEA201605171625Hinge · corrodedRIGHT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, UPPER MOUNT INBD HOLE BORE CORROSION. CORROSION HOLE NR 2 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 0.944 INCHES, FINAL DIAMETER 0.951 INCHES, MAX ALLOWABLE DIAMETER 0.944 INCHES. REPMay 17, 2016 · N595FE · Doug MD11FSDR FDEA201605171622Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, ACTUATOR OTBD HOLE BORE CORROSION. CORROSION AT HOLE NR 8 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING DIAMETER 1.218 INCH, FINAL DIAMETER 1.226 INCH & MAXIMUM ALLOWABLE DIAMETER 1.220 INCH. REPAIMay 17, 2016 · N595FE · Doug MD11FSDR FDEA201605171621Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, ACTUATOR INBD HOLE. BORE CORROSION. CORROSION AT HOLE NR 8 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING DIAMETER 1.252 INCH, FINAL DIAMETER 1.255 INCH & MAXIMUM ALLOWABLE DIAMETER 1.220 INCH. REPMay 17, 2016 · N595FE · Doug MD11FSDR FDEA201605171620Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE SURFACE CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING THICKNESS 0.437 INCHES, MATERIAL REMOVED FWD SIDE 0.006 INCHES, AFT SIDE 0.016 INCHES, REMAINING THICMay 17, 2016 · N595FE · Doug MD11FSDR FDEA201605171619Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE BORE CORROSION. CORROSION AT HOLE NR 7 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-48-08. EXISTING DIAMETER 0.708 INCHES, FINAL DIAMETER 0.731 INCHES, MAX ALLOWABLE DIAMETER 0.709 INCHES. RMay 17, 2016 · N595FE · Doug MD11FSDR FDEA201605171618Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE BORE CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING DIAMETER 0.727 INCHES, FINAL DIAMETER 0.731 INCHES & MAX ALLOWABLE DIAMETER 0.709 INCHES. REPAIR BUSHINMay 17, 2016 · N595FE · Doug MD11FSDR FDEA201605171617Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, UPPER MOUNT HOLE OTBD BORE CORROSION. REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING DIAMETER 0.942 INCHES, FINAL DIAMETER 0.950 INCHES & MAX ALLOWABLE DIAMETER 0.944 INCHES. REPAIR BUSHING FABRICATMay 17, 2016 · N595FE · Doug MD11FSDR FDEA201605171616Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, BARREL NUT LOWER HOLE BORE CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08, EXISTING DIAMETER 0.627 INCHES, FINAL DIAMETER 0.629 INCHES & MAX ALLOWABLE DIAMETER 0.621 INCHES. REPAIR BUSHINGMay 17, 2016 · N595FE · Doug MD11FSDR FDEA201605171615Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, FWD MOUNT INBD HOLE BORE CORROSION. CORROSION AT HOLE NR 6 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 1.2805 INCH, FINAL DIAMETER 1.284 INCH & MAX ALLOWABLE DIAMETER 1.254 INCH. REPAIREMay 17, 2016 · N595FE · Doug MD11FSDR FDEA201605171614Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, ACTUATOR OTBD HOLE BORE CORROSION. CORROSION AT HOLE NR 8 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 1.256 INCH, FINAL DIAMETER 1.259 INCH, MAX ALLOWABLE DIAMETER 1.220 INCH. REPAIRED BMay 17, 2016 · N595FE · Doug MD11FSDR FDEA201605171613Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, ACTUATOR INBOARD HOLE BORE CORROSION. CORROSION AT HOLE NR 8 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 1.252 INCH, FINAL DIAMETER 01.259 INCH, MAX ALLOWABLE DIAMETER 1.220 INCH. REPAIRMay 17, 2016 · N595FE · Doug MD11FSDR FDEA201605171612Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUTS HOLE BORE CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 0.665 INCHES, FINAL DIAMETER 0.677 INCHES & MAX ALLOWABLE DIAMETER 0.667 INCHES. REPAIR BUSHING FABMay 17, 2016 · N595FE · Doug MD11FSDR FDEA201605171611Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUT LOWER HOLE BORE CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 0.390 INCHES, FINAL DIAMETER 0.407 INCHES, MAX ALLOWABLE DIAMETER 0.391 INCHES. REPAIR BUSHINMay 17, 2016 · N595FE · Doug MD11FSDR FDEA201605171610Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUT UPPER HOLE BORE FOUND CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 0.390 INCHES, FINAL DIAMETER 0.407 INCHES, MAX ALLOWABLE DIAMETER 0.391 INCHES. REPAIREDMay 17, 2016 · N595FE · Doug MD11FSDR FDEA201605171609Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE BORE FOUND CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 0.582 INCH, FINAL DIAMETER 0.597 INCHES. MAX ALLOWABLE DIAMETER 0.584 INCHES. SHOULDER May 17, 2016 · N595FE · Doug MD11FSDR 2016FA0000220Hinge Bracket · corrodedRT INBD AILERON HINGE BRACKET FOUND TO HAVE EXFOLIATION CORROSION AT AIRFRAME ATTACH POINT, REQUIRING REPLACEMENT OF PART. OTHER CONTROL SURFACE HINGES/ATTACH BRACKETS INSPECTED WITH NO DEFECTS.May 10, 2016 · N217BH · Casa C212CDSDR FDEA201604191278Hinge Bracket · corrodedRIGHT WING OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, LOWER INBD STUD ATTACH SURFACE FOUND CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING THICKNESS: 0.404", MATERIAL REMOVED 0.010", REMAINING THICKNESS 0.394", MINIMUM ALLOApr 19, 2016 · N613FE · Doug MD11FSDR FDEA201604191277Hinge Bracket · corrodedRIGHT WING OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, LOWER OTBD STUD ATTACH BORE FOUND CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER 0.705", FINAL HOLE DIAMETER 0.723", MAX ALLOWABLE HOLE DIAMETER 0.709". Apr 19, 2016 · N613FE · Doug MD11FSDR FDEA201604191276Hinge Bracket · corrodedRIGHT WING OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, LOWER INBD STUD ATTACH BORE FOUND CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER 0.705", FINAL HOLE DIAMETER 0.723", MAX ALLOWABLE HOLE DIAMETER 0.709". Apr 19, 2016 · N613FE · Doug MD11FSDR FDEA201604191275Hinge Bracket · corrodedRIGHT WING OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, PIVOT BORE FOUND CORROSION. CORROSION REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER 2.310". FINAL HOLE DIAMETER 2.317", MAX ALLOWABLE HOLE DIAMETER 2.3135". REPAIRED BUSHINApr 19, 2016 · N613FE · Doug MD11FSDR FDEA201604191274Hinge Bracket · corrodedRIGHT WING OTBD FLAP, OTBD FWD HINGE BRACKET, WING SIDE, ACTUATOR ATTACH OTBD LUG BORE FOUND CORROSION. NR 8 HOLE REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER 1.217 INCHES, FINAL HOLE DIAMETER 1.247 INCHES & MAXIMUM ALLOWABLE DIAMApr 19, 2016 · N613FE · Doug MD11FSDR FDEA201604191273Hinge Bracket · corrodedRIGHT WING OTBD FLAP, OTBD FWD HINGE BRACKET, WING SIDE, ACTUATOR ATTACH INBD LUG BORE FOUND CORROSION. NR 8 HOLE REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER 1.218 INCHES, FINAL HOLE DIAMETER 1.245 INCHES & MAXIMUM ALLOWABLE DIAMApr 19, 2016 · N613FE · Doug MD11FSDR FDEA201604191272Hinge Bracket · corrodedRIGHT WING OTBD FLAP, OTBD FWD HINGE BRACKET, WING SIDE, ATTACH UPPER BORE FOUND CORROSION. NR 7 HOLE REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER 0.323 INCHES, FINAL HOLE DIAMETER 0.406 INCHES & MAXIMUM ALLOWABLE DIAMETER 0.391 IApr 19, 2016 · N613FE · Doug MD11FSDR FDEA201604191271Hinge Bracket · corrodedRIGHT WING OTBD FLAP, OTBD FWD HINGE BRACKET, WING SIDE, LOWER OTBD STUD ATTACH BORE FOUND CORROSION. NUMBER 3 HOLE REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER 0.580 INCHES, FINAL HOLE DIAMETER 0.614 INCHES & MAXIMUM ALLOWABLE DIApr 19, 2016 · N613FE · Doug MD11FSDR FDEA201604191270Hinge Bracket · corrodedRIGHT WING OTBD FLAP, OTBD FWD HINGE BRACKET, WING SIDE, LOWER INBD STUD ATTACH BORE FOUND CORROSION. HOLE NR 3 REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER 0.580 INCHES, FINAL HOLE DIAMETER 0.621 INCHES, MAXIMUM ALLOWABLE DIAMETApr 19, 2016 · N613FE · Doug MD11FSDR FDEA201604191269Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, LOWER INBD STUD ATTACH SURFACE FOUND CORROSION. REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING THICKNESS 0440 INCHES, MATERIAL REMOVED, FWD FACE, 0.016 INCHES, AFT FACE, 0.037 INCHES & REMAIApr 19, 2016 · N613FE · Doug MD11FSDR FDEA201604191268Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, LOWER OTBD STUD ATTACH BORE FOUND CORROSION. CORROSION EXCEEDED LIMIT AS PER MD-11 CMM 57-44-09. EXISTING HOLE DIAMATER 0.706 INCH ; FINAL HOLE DIAMATER 0.725 INCH ; MAXIMUM ALLOWABLE DIAMATER 0.7Apr 19, 2016 · N613FE · Doug MD11FSDR FDEA201604191267Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, LOWER INBD STUD ATTACH BORE FOUND CORROSION.Apr 19, 2016 · N613FE · Doug MD11FSDR FDEA201604191266Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET, WING SIDE, FWD ATTACH OTBD LUG BORE FOUND CORROSION. CORROSION AT NR 6 HOLE REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER 1.254 INCHES, FINAL HOLE DIAMETER 1.259 INCHES & MAXIMUM ALLOWABApr 19, 2016 · N613FE · Doug MD11F
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