JASC 5744

Service difficulty reports · 2,730

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 FDEA201203191016Hinge Bracket · corrodedRIGHT WING OTBD FLAP, INBD FORWARD HINGE BRACKET ACTUATOR ATTACH OTBD LUG BORE FOUND CORRODED. BORE REWORKED AND FOUND EXCEED LIMITS IAW CMM 57-44-08, REV 72. EXISTING DIAMETER 1.251", FINAL DIAMETER 1.256", MAXIMUM ALLOWABLE DIAMETER 1.220". REPAIR CARRIED Mar 19, 2012 · N576FE · Doug MD11FSDR FDEA201203191015Hinge Bracket · corrodedRIGHT WING OTBD FLAP INBD FORWARD HINGE BRACKET PIVOT BORE FOUND CORRODED. BORE REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-08, REV 72. EXISTING DIAMETER 2.3115", FINAL DIAMETER 2.316", MAXIMUM ALLOWABLE DIAMETER 2.3135". REPAIR ACCOMPLISHED IAW EA 1-575Mar 19, 2012 · N576FE · Doug MD11FSDR FDEA201203191014Hinge Bracket · corrodedRIGHT WING OTBD FLAP, INBD FORWARD HINGE BRACKET LOWER INBD STUD HOLE FOUND CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-08, REV 72. EXISTING DIAMETER 0.708", FINAL DIAMETER 0.721", MAXIMUM ALLOWABLE DIAMETER 0.709". REPAIR CARRIED OUT IAW EA 1-5Mar 19, 2012 · N576FE · Doug MD11FSDR FDEA201203191013Hinge Bracket · corrodedRIGHT WING OTBD FLAP, INBD FORWARD HINGE BRACKET SIDE LOAD FITTING ATTACH SURFACE FOUND CORRODED. REWORKED IAW CMM 57-44-08, REV 72. EXISTING THICKNESS UPPER 0.393", LOWER 0.392", REMAINING THICKNESS UPPER 0.390", LOWER 0.389. MATERIAL REMOVED: UPPER 0.003"Mar 19, 2012 · N576FE · Doug MD11FSDR FDEA201203170991Bushing · wornRIGHT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET ACTUATOR ATTACH OTBD LUG BUSHING FOUND WORN. WORN BUSHING REMOVED IAW CMM 20-20-07, REV 72 AND FOUND EXCEED LIMITS IAW CMM 57-44-09, REV 72. BORE MEASURED DIAMETER 1.222", MAXIMUM ALLOWABLE DIAMETER 1.220". Mar 17, 2012 · N576FE · Doug MD11FSDR FDEA201203170989Hinge Fitting · corrodedRIGHT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET, LOWER OTBD STUD HOLE, FOUND CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09, REV 72. EXISTING HOLE DIAMETER 0.585", FINAL HOLE DIAMETER 0.610", MAXIMUM ALLOWABLE DIAMETER 0.584". REPAIRED IAW EA 1Mar 17, 2012 · N576FE · Doug MD11FSDR FDEA201203170987Hinge Fitting · corrodedRIGHT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET WING SIDE LOAD FITTING ATTACH BARREL NUT HOLE FOUND CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09 REV 72. EXISTING HOLE DIAMETER 0.660", FINAL HOLE DIAMETER 0.669", ALLOWABLE HOLE DIAMETER 0.667Mar 17, 2012 · N576FE · Doug MD11FSDR FDEA201203140933Hinge Fitting · corrodedRT WING (WING SIDE) OTBD FLAP HINGE, CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09, REV 72. REPAIR CARRIED OUT IAW STEP 1, 2, 9, 10, 11 AND 12 OF EA 1-5750-150447, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.Mar 14, 2012 · N610FE · Doug MD11FSDR FDEA201203140934Bushing · wornRT WING (WING SIDE) OTBD FLAP, OTBD HINGE, OTBD ACTUATOR HOLE BUSHING WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE MEASURED DIA 1.224" AND FOUND EXCEEDED LIMIT IAW CMM 57-44-04, REV 72 , MAX ALLOWABLE DIA 1.220", BUSHING FABRICATED AND INSTALLED IAW Mar 14, 2012 · N610FE · Doug MD11FSDR FDEA201203140932Hinge Fitting · corrodedRT WING (WING SIDE) OTBD FLAP, OTBD HINGE, INBD ACTUATOR HOLE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09, REV 72. EXISTING HOLE DIA 1.223", FINAL HOLE DIA. 1.249" , MAX ALLOWABLA DIA 1.220" REPAIR CARRIED OUT IAW STEP 1,2,9,10,11 AMar 14, 2012 · N610FE · Doug MD11FSDR FDEA201203120888Hinge · damagedRT WING OTBD FLAP, OTBD HINGE BUSHING ON PIVOT HOLE REMOVED IAW CMM 20-20-07, REV 72 . BORE MEASURED DIA 2.315" AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09, REV 72 MAX ALLOWABLE, DIA 2.3135". NEW BUSHING FABRICATED AND INSTALLED IAW STEP 10 AND 11 OF EA 1-57Mar 12, 2012 · N610FE · Doug MD11FSDR FDEA201203120885Hinge Fitting · corrodedRT WING (WING SIDE) OTBD FLAP, OTBD HINGE PIVOT HOLE FOUND EXCEEDED CMM LIMITS AFTER BUSHING REMOVAL FOR NDT ACCESS. MEASURED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09, REV 72 EXISTING HOLE DIA 2.315" MAX ALLOWABLE DIA 2.3135'. REPAIR CARRIED OUT IAW EA 1-57Mar 12, 2012 · N610FE · Doug MD11FSDR FDEA201203120883Hinge Fitting · corrodedRT WING (WING SIDE) OTBD FLAP OTBD HINGE LOWER MOUNT INBD HOLE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09, REV 72 EXISTING HOLE DIA 0.582', FINAL HOLE DIA 0.598", MAX. ALLOWABLE DIA 0.584' REPAIR CARRIED OUT IAW EA 1-5750-150447, PARMar 12, 2012 · N610FE · Doug MD11FSDR FDEA201203120882Hinge Fitting · corrodedRT WING (WING SIDE) OTBD FLAP OTBD HINGE LOWER MOUNT OTBD HOLE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09, REV 72 . EXISTING HOLE DIA 0.585", FINAL HOLE DIA. 0.598", MAX ALLOWABLE HOLE DIA.0.584" REPAIR CARRIED OUT IAW STEP 3 OF EA 1-5Mar 12, 2012 · N610FE · Doug MD11FSDR FDEA201203120881Hinge Fitting · corrodedRT WING (WING SIDE) OTB FLAP INBD HINGE SIDE LOAD FITTING SURFACE FOUND CORRODED. REWORKED IAW CMM 57-44-09, REV 72. EXISTING THK UPPER:0.412", LOWER:0.408". REMAINING THK UPPER:0.407", LOWER:0.403'. MATERIAL REMOVED: UPPER: 0.005", LOWER:0.005" IAW STEP Mar 12, 2012 · N610FE · Doug MD11FSDR FDEA201203120880Bushing · wornRT WING (WING SIDE) OTBD FLAP INBD HINGE INBD ACTUATOR HOLE BUSHING WORN. BUSHING REMOVED CMM 20-20-07, REV 72. BORE MEASURED DIA 1.223", AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08, REV 72. MAX ALLOWABLE DIA 1.220", WASHER INSTALLED IAW EA 1-5750-160003, PARMar 12, 2012 · N610FE · Doug MD11FSDR FDEA201203120879Hinge Fitting · wornRT WING (WING SIDE) OTBD FLAP INBD HINGE OTBD ACTUATOR HOLE BUSHING WORN. BUSHING REMOVED CMM 20-20-07, REV 72 BORE MEASURED DIA 1.222", AND FOUND EXCEEDED LIMIT IAW 1 CMM 57-44-08 REV 72. MAX ALLOWABLE DIA.1.220" .BUSHING FABRICATED AND INSTALLED IAW STEP 5 Mar 12, 2012 · N610FE · Doug MD11FSDR FDEA201203120878Hinge Fitting · corrodedRIGHT WING (WING SIDE) OTBD FLAP INBD HINGE SIDE LOAD FITTING SURFACE FOUND CORRODED. REWORKED IAW CMM 57-44-08, REV 72. EXISTING THICKNESS UPPER: 0.375", LOWER: 0.355", REMAINING THICKNESS UPPER: 0.365", LOWER: 0.345", MATERIAL REMOVED UPPER: 0.010", LOWER Mar 12, 2012 · N610FE · Doug MD11FSDR FDEA201203090843Bushing · migratedLEFT WING (WING SIDE) OTBD FLAP INBD HINGE PIVOT HOLE REPAIR BUSHING FOUND MIGRATED. REPAIRED IAW EA 1-5750-160002 STEP 3, 7, 8 AND 9 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.Mar 9, 2012 · N610FE · Doug MD11FSDR FDEA201203090842Hinge Fitting · corrodedLEFT WING (WING SIDE) OTBD FLAP INBD HINGE SIDE LOAD FITTING SURFACE FOUND CORRODED. REPAIRED IAW EA 1-5750-160002, STEP 4 AND 5 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.Mar 9, 2012 · N610FE · Doug MD11FSDR FDEA201203090841Hinge Fitting · corrodedLEFT WING (WING SIDE) OTBD FLAP INBD HINGE LOWER MOUNT INBD HOLE FOUND CORRODED. REPAIRED IAW EA 1-5750-160002, PART 1, STEP 2,7,8,9 AND 10. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Mar 9, 2012 · N610FE · Doug MD11FSDR FDEA201203090840Hinge Fitting · corrodedLEFT WING (WING SIDE) OTBD FLAP INBD HINGE LOWER MOUNT OTBD HOLE FOUND CORRODED. REPAIRED IAW EA 1-5750-160002, PART 1, STEP 2.Mar 9, 2012 · N610FE · Doug MD11FSDR FDEA201203090839Bushing · wornLEFT WING (WING SIDE) OTBD FLAP INBD HINGE, INBD ACTUATOR, HOLE BUSHING WORN. REPAIRED IAW EA 1-5750-160002, PART 1, STEP 1, 7, 8 AND 9 .Mar 9, 2012 · N610FE · Doug MD11FSDR FDEA201203090838Bushing · wornLEFT WING (WING SIDE) OTBD FLAP INBD HINGE OTBD ACTUATOR HOLE BUSHING WORN. REPAIRED IAW EA1-5750-160002, PART 1 STEP 1, 7, 8 AND 9 .Mar 9, 2012 · N610FE · Doug MD11FSDR FDEA201203090837Bushing · wornLEFT WING (WING SIDE) OTBD FLAP OTBD HINGE INBD ACTUATOR HOLE BUSHING WORN. MEASURED AND FOUND OUT OF LIMITS IAW CMM 57-44-09, REV 72. EXISTING HOLE DIA 1.254", MAX HOLE DIA 1.220", BUSHING FABRICATED AND INSTALLED IAW STEP 9 AND 10. WASHER FABRICATED IAW SMar 9, 2012 · N610FE · Doug MD11FSDR FDEA201203090836Hinge Fitting · corrodedLEFT WING (WING SIDE) OTBD FLAP OTBD HINGE SIDE LOAD FITTING UPPER HOLE FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09, REV 72 . EXISTING HOLE DIA. 0.398", FINAL HOLE 0.4095", MAX HOLE DIA. 0.391", BUSHING FABRICATED AND INSTALLED PER STEPMar 9, 2012 · N610FE · Doug MD11FSDR FDEA201203090835Hinge Fitting · corrodedLEFT WING (WING SIDE) OTBD FLAP OTBD HINGE SIDE LOAD FITTING LOWER HOLE FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09, REV 72 EXISTING HOLE DIA. 0.398", FINAL HOLE DIA. 0.4095", MAX HOLE DIA. 0.391", BUSHING FABRICATED AND INSTALLED IAW Mar 9, 2012 · N610FE · Doug MD11FSDR FDEA201203090834Hinge Fitting · corrodedLEFT WING (WING SIDE) OTBD FLAP OTBD HINGE SIDE LOAD FITTING SURFACE FOUND CORRODED. REWORKED IAW REV 72 UPPER FACE EXISTING THICKNESS: 0.413", MATERIAL REMOVED :0.003", REMAINING THICKNESS :0.410", LOWER FACE EXISTING THICKNESS: 0.410", MATERIAL REMOVED :0Mar 9, 2012 · N610FE · Doug MD11FSDR FDEA201203090833Hinge Fitting · corrodedLEFT WING (WING SIDE) OTBD FLAP OTBD HINGE LOWER MOUNT INBD HOLE FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09, REV 72. MAX ALLOWABLE DIA.0.584", EXISTING HOLE DIA 0.538", FINAL HOLE DIA 0.595", BUSHING FABRICATED AND INSTALLED IAW STEP Mar 9, 2012 · N610FE · Doug MD11FSDR FDEA201203090832Hinge Fitting · corrodedLEFT WING (WING SIDE) OTBD FLAP, OTBD HINGE LOWER MOUNT OTBD HOLE FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09, REV 72. EXISTING HOLE DIA 0.585", FINAL HOLE DIA.0.597", MAX HOLE DIA 0.584". BUSHING FABRICATED AND INSTALLED AS IAW STEMar 9, 2012 · N610FE · Doug MD11FSDR A6WA201240437Hinge · brokenLEFT STUB FAIRING IS GOUGED AND HAS BROKEN HINGE. REPLACED UNSERVICEABLE LT STUB FAIRING WITH SERVICEABLE STUB FAIRING IAW SRM 51-42-06 AND SRM 51-40-11.Mar 7, 2012 · N430AW · Cndair CL6002B19SDR A6WA201240333Hinge Fitting · crackedNDT INDICATED A CRACK AT THE AFT HOLE OF THE AFT HINGE FITTING LOCATION. REPAIRED IAW REO 601R-57-21-1608.Mar 1, 2012 · N404AW · Cndair CL6002B19SDR FDEA201202240677Hinge Fitting · corrodedCORROSION FOUND DURING FPI ON LT WING SIDE OTBD FLAP, OTND HINGE PIVOT BORE HOLE. REPAIRED IAW EA 1-5750-156843 PART 1. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REV.114.Feb 24, 2012 · N587FE · Doug MD11FSDR FDEA201202230657Bushing · wornRIGHT WING OTBD FLAP INBD FORWARD HINGE BRACKET ACTUATOR ATTACH OTBD LUG BUSHING FOUND WORN. NEW BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-156842 PART 1 STEP 4 AND STEP 5. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 114.Feb 23, 2012 · N587FE · Doug MD11FSDR FDEA201202230656Bushing · wornRT WING OTBD FLAP, INBD FORWARD HINGE BRACKET ACTUATOR ATTACH INBD LUG BUSHING FOUND WORN. REPAIRED IAW EA 1-5750-156842 PART 1. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 114.Feb 23, 2012 · N587FE · Doug MD11FSDR FDEA201202230650Hinge Fitting · corrodedRT WING OTBD FLAP INBD FORWARD HINGE BRACKET LOWER OTBD STUD HOLE FOUND CORRODED. REPAIRED IAW EA 1-5750-156842 PART 1. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 114.Feb 23, 2012 · N587FE · Doug MD11FSDR FDEA201202230664Bushing · wornLT WING INBD FLAP, OTBD AFT HINGE BRACKET PIVOT OTBD LUG BUSHING FOUND WORN. REWORKED IAW CMM 20-20-07, REV 72. BORE MEASURED DIAMETER 1.329 AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 72. MAXIMUM ALLOWABLE DIAMETER 1.220". REWORK CARRIED OUT AND FABRICATEFeb 23, 2012 · N587FE · Doug MD11FSDR FDEA201202230663Bushing · wornLT WING INBD FLAP, OTBD AFT HINGE BRACKET PIVOT INBD LUG BUSHING FOUND WORN. REMOVED IAW CMM 20-20-07, REV 72 BORE MEASURED DIAMETER 1.256" AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 72. MAXIMUM ALLOWABLE DIAMETER 1.220". REWORKED CARRIED OUT AND FABRICATEFeb 23, 2012 · N587FE · Doug MD11FSDR FDEA201202230662Bushing · wornLT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET ACTUATOR ATTACH OTBD LUG BUSHING FOUND WORN. REPAIRED IAW EA 1-5750-156843, PART 1, NEW BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-156843 PART 1, STEP 4 AND STEP 5. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100Feb 23, 2012 · N587FE · Doug MD11FSDR FDEA201202230661Bushing · wornLT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET ACTUATOR ATTACH INBD LUG BUSHING FOUND WORN. REPAIRED IAW EA 1-5750-156843 PART 1, NEW BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-156843 PART 1 STEP 4 AND STEP 5. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, RFeb 23, 2012 · N587FE · Doug MD11FSDR FDEA201202230660Bushing · wornLT WING OTBD FLAP, INBD FORWARD HINGE BRACKET ACTUATOR ATTACH OTBD LUG BUSHING FOUND WORN. REPAIRED IAW EA 1-5750-156841 PART 1, REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1- 5750-156841, PART 1 STEP 4 AND STEP 5. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2Feb 23, 2012 · N587FE · Doug MD11FSDR FDEA201202230659Bushing · wornLT WING OTBD FLAP, INBD FORWARD HINGE BRACKET ACTUATOR ATTACH INBD LUG BUSHING FOUND WORN. REPAIRED IAW EA 1-5750-156841 PART 1, NEW BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-156841 PART 1, STEP 4 AND STEP 5. REPAIR CLASSIFIED AS MINOR GMM 6-2-100, REFeb 23, 2012 · N587FE · Doug MD11FSDR FDEA201202230658Bushing · wornRT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET ACTUATOR ATTACH OTBD LUG BUSHING FOUND WORN. BUSHING REPAIRED IAW EA 1-5750-156844 PART 1, REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-156844 PART 1, STEP 4 AND STEP 5. REPAIR CLASSIFIED AS MINOR IAW GMFeb 23, 2012 · N587FE · Doug MD11FSDR FDEA201202230655Hinge Bracket · damagedRIGHT WING INBD FLAP OTBD HINGE BRACKET PIVOT OTBD BORE FOUND SCRATCHED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 72 EXISTING DIAMETER 1.256", FINAL DIAMETER 1.2825", MAXIMUM DIAMETER 1.220". FABRICATED BUSHING INSTALLED IAW EA.1-5750-156846, STEFeb 23, 2012 · N587FE · Doug MD11FSDR FDEA201202230653Hinge Bracket · damagedRT WING INBD FLAP, OTBD AFT HINGE BRACKET PIVOT BORE FOUND SCRATCHES. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 72 EXISTING DIAMETER 1.3275", FINAL DIAMETER 1.3355", MAXIMUM DIAMETER 1.220". FABRICATED BUSHING INSTALLED IAW EA 1-5750-156846, STEPFeb 23, 2012 · N587FE · Doug MD11FSDR FDEA201202230652Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD FORWARD HINGE BRACKET SIDE LOAD FITTING CONTACT SURFACE FOUND CORRODED. REPAIRED IAW EA 1-5750-156841 PART 1, REPAIR SHIM FABRICATED AND INSTALLED IAW EA 1-5750-156841, PART 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 114.Feb 23, 2012 · N587FE · Doug MD11FSDR FDEA201202230651Hinge Bracket · corrodedRT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET ACTUATOR ATTACH INBD LUG BORE FOUND CORRODED. REPAIRED IAW EA 1-5750-156844, PART 1, REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-156844 PART 1, STEP 4 AND STEP 5. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-Feb 23, 2012 · N587FE · Doug MD11FSDR FDEA201202230649Hinge Bracket · corrodedLT WING OTBD FLAP INBD HINGE BRACKET LOWER OTBD STUD HOLE FOUND CORRODED. REPAIRED IAW EA 1-5750-156841, PART 1, REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-156841, PART 1, STEP 4 AND STEP 5. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 114.Feb 23, 2012 · N587FE · Doug MD11FSDR SWAA2012022001566Trunnion · corrodedLT MLG FWD TRUNNION LUG FACE FITTING CORRODED. REPAIRED FITTING PER EA.Feb 18, 2012 · N438WN · Boeing 7377H4SDR SWAA2012022001565Trunnion · corrodedRT MLG FWD TRUNNION LUG FACE FITTING CORRODED. REPAIRED FITTING PER EA.Feb 18, 2012 · N438WN · Boeing 7377H4
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