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.
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
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 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 SDR 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 1-575SDR 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 1-5SDR 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"SDR 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". SDR 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 1SDR 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 0.667SDR 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.SDR 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 SDR 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 ASDR 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 1-57SDR 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 1-57SDR 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, PARSDR 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 1-5SDR 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 SDR 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, PARSDR 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 SDR 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 SDR 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.SDR 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.SDR 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.SDR 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.SDR 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 .SDR 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 .SDR 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 SSDR 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 STEPSDR 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 SDR 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 :0SDR 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 SDR 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 STESDR 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.SDR A6WA201240333Hinge Fitting · crackedNDT INDICATED A CRACK AT THE AFT HOLE OF THE AFT HINGE FITTING LOCATION. REPAIRED IAW REO 601R-57-21-1608.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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 FABRICATESDR 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 FABRICATESDR 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 6-2-100SDR 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, RSDR 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 6-2SDR 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, RESDR 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 GMSDR 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, STESDR 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, STEPSDR 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.SDR 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-SDR 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.SDR SWAA2012022001566Trunnion · corrodedLT MLG FWD TRUNNION LUG FACE FITTING CORRODED. REPAIRED FITTING PER EA.SDR SWAA2012022001565Trunnion · corrodedRT MLG FWD TRUNNION LUG FACE FITTING CORRODED. REPAIRED FITTING PER EA.
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