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.
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 FDEA201709122502Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD HINGE (WING SIDE) ACTUATOR OTBD LUG HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO335291A, PART 1, STEP 1D.SDR FDEA201709122501Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD HINGE (WING SIDE) ACTUATOR INBD LUG HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO335291A, PART 1, STEP 1D.SDR FDEA201709122500Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD HINGE (WING SIDE) LOWER MOUNT OUTBD HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO335291A, PART 1, STEP 1C, AND STEP 1.SDR FDEA201709122499Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD HINGE (WING SIDE) LOWER MOUNT INBD HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO335291A, PART 1, STEP 1C AND STEP 1.SDR FDEA201709122498Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD HINGE (WING SIDE) UPPER MOUNT OUTBD HOLE SPOT SURFACE FOUND CORRODED. THE SPOT SURFACE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. REPAIRED THE AREA IAW EA 1-5750-T0335291A, PART 1, STEP 1.SDR FDEA201709122497Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD HINGE (WING SIDE) UPPER MOUNT INBD HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. A REPAIR BUSHING WAS FABRICATED, AND INSTALLED IAW EA 1-5750-TO335291A, PART 1, STEP 1A.SDR FDEA201709122496Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD HINGE (WING SIDE) PIVOT HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO335291A, PART 1, STEP 1B.SDR FDEA201709122495Hinge Bracket · corrodedRIGHT WING OTBD FLAP OTBD HINGE (WING SIDE) ACTUATOR OUTBD LUG HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO335331, PART 1, STEP 2D.SDR FDEA201709122494Hinge Bracket · corrodedRIGHT WING OTBD FLAP OTBD HINGE (WING SIDE) ACTUATOR INBD LUG HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44- 09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO335331, PART 1, STEP 2D.SDR FDEA201709122493Hinge Bracket · corrodedRIGHT WING OTBD FLAP OTBD HINGE (WING SIDE) BARREL NUT LOWER HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO335331, PART 1, STEP 2C.SDR FDEA201709122492Hinge Bracket · corrodedRIGHT WING OTBD FLAP OUTBD HINGE (WING SIDE) BARREL NUT UPPER HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO335331, PART 1, STEP 2C.SDR FDEA201709122491Hinge Bracket · corrodedRIGHT WING OTBD FLAP OUTBD HINGE (WING SIDE) LOWER MOUNT OTBD HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO335331, PART 1, STEP 2B, AND STEP 2.SDR FDEA201709122490Hinge Bracket · corrodedRIGHT WING OUTBD FLAP OUTBD HINGE (WING SIDE) LOWER MOUNT INBD HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO335331, PART 1, STEP 2B, AND STEP 2.SDR FDEA201709122489Hinge Bracket · corrodedRIGHT WING OTBD FLAP OUTBD HINGE (WING SIDE) UPPER MOUNT OTBD HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO335331, PART 1, STEP 2A.SDR FDEA201709122488Hinge Bracket · corrodedLEFT WING OUTBD FLAP OUTBD HINGE (WING SIDE) ACTUATOR OUTBD LUG HOLE BORE FOUND CORRODED. THE HOLE BORE WAS REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335322, PART 1, STEP 2D.SDR FDEA201709122487Hinge Bracket · corrodedLEFT WING OUTBD FLAP OUTBD HINGE (WING SIDE) BARREL NUT HOLE SPOT SURFACE FOUND CORRODED. SURFACE REWORKED IAW CMM 57-44-09. A REPAIR SHIM FABRICATED AND INSTALLED IAW CMM 57-44-09.SDR FDEA201709122486Hinge Bracket · corrodedLEFT WING OUTBD FLAP OUTBD HINGE (WING SIDE) ACTUATOR INBD LUG HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335322, PART 1, STEP 2D.SDR FDEA201709122485Hinge Bracket · corrodedLEFT WING OUTBD FLAP OUTBD HINGE (WING SIDE) BARREL NUT LOWER HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND TO BE OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335322, PART 1, STEP 2C.SDR FDEA201709122484Hinge Bracket · corrodedLEFT WING OUTBD FLAP OUTBD HINGE (WING SIDE) BARREL NUT UPPER HOLE BORE FOUND CORRODED. BORE REWORKED AND FOUND TO BE OUT OF LIMITS IAW CMM 57-44-09. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335322, PART 1, STEP 2C.SDR FDEA201709122483Hinge Bracket · corrodedLEFT WING OUTBD FLAP OTBD HINGE (WING SIDE) LOWER MOUNT OTBD HOLE FWD AND AFT SURFACE FOUND CORRODED. MOUNT BORE, FWD AND AFT SURFACE REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335322, PART 1SDR FDEA201709122482Hinge Bracket · corrodedLEFT WING OUTBD FLAP OUTBD HINGE (WING SIDE) LOWER MOUNT INBD HOLE FWD AND AFT SURFACE FOUND CORRODED. BORE FWD AND AFT SURFACE REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335322, PART 1, STEPSDR FDEA201709122481Hinge Bracket · corrodedLEFT WING OUTBD FLAP OUTBD HINGE (WING SIDE) LOWER MOUNT OUTBD HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND TO BE OUT OF LIMITS IAW CMM 57-44-09. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335322, PART 1, STEP 2 AND 2A.SDR FDEA201709122480Hinge Bracket · corrodedLEFT WING OUTBD FLAP OUTBD HINGE ( WING SIDE ) LOWER MOUNT INBD HOLE BORE FOUND CORRODED., THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335322, PART 1, STEP 2 AND 2A.SDR FDEA201709122479Hinge Bracket · corrodedLEFT WING OUTBD FLAP OTBD HINGE ( WING SIDE ) UPPER MOUNT OTBD HOLE BORE FOUND CORRODED. BORE REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335322, PART 1, STEP 2B.SDR FDEA201709022447Hinge Bracket · corrodedRIGHT WING INBOARD FLAP OUTBOARD HINGE (WING SIDE) PIVOT HOLE BORE FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-07. A NEW REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0330927 A, PART 1, STEP 1F. REPAIR CLASSIFIED AS MAJOR IASDR FDEA201709022446Hinge Bracket · corrodedLEFT WING INBOARD FLAP OUTBOARD HINGE (WING SIDE) PIVOT HOLE BORE FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-07. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0330926 B, PART 1, STEP 1F. REPAIR CLASSIFIED AS MAJOR IAW GMSDR FDEA201708162235Hinge · corrodedLEFT WING, INBD FLAP, OTBD FWD HINGE (WING SIDE) PIVOT LUG SPOTFACE FOUND CORRODED. THE CORROSION WAS REWORKED AND FOUND WITHIN LIMITS IAW CMM 57-44-07. REPAIRED IAW EA 1-5750-T0331118, B, PART 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201708162233Hinge · corrodedLEFT WING, INBD FLAP OTBD FWD HINGE (WING SIDE) PIVOT BORE FOUND CORROSION. CORROSION REWORKED AND FOUND WITHIN LIMIT IAW CMM 57-44-07. REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0331118 B, PART 1, STEPS F 1 AND F 3. THE REPAIR WAS CLASSIFIEDSDR FDEA201708102169Hinge Bracket · corrodedRIGHT WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) ACTUATOR ATTACH OUTBOARD BORE FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-07. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331120 B, PART 1, STEPS F1 AND F 3. THESDR FDEA201708102168Hinge Bracket · corrodedRIGHT WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) ACTUATOR ATTACH INBOARD BORE FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-07. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331120 B, PART 1, STEP F 1 AND F 3, THESDR AALA201707039019Fitting · damagedAIRCRAFT WAS GROUNDED. WHILE ACCOMPLISHING JOB CARD 26T60057066 FOUND RIGHT INBD FLAP INBD TRUNNION FITTING DAMAGED BEYOND ALLOWABLE LIMITS. REMOVED AND REPLACED RIGHT INBD FLAP INBD TRUNNION IAW JOB CARD 26L00027003. OPERATIONAL CHECK GOOD.SDR AALA20170512003Stud · corrodedCORROSION ON RT WING OUTBOARD FLAP INBOARD HINGE UPPER AND LOWER MOUNTING STUDS AT WING STATION XW 154.584. REMOVED AND REPLACED THE STUDS IAW AMM 57-40-01.SDR IPXA2017050916928Stud · corrodedINSPECTION TYPE: 3C, RT OTBD AILERON ACTUATOR MOUNT STUD IS RUSTED, HALF SHEARED. REMOVED AND REPLACED ALL THE OTBD AILERON ACTUATOR MOUNT STUDS IAW DWG.ARB7411.SDR FDEA201703170945Fitting · crackedLEFT WING OTBD FLAP, INBD FWD HINGE SIDE LOAD FITTING CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201703070803Hinge Bracket · corrodedRT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) ACTUATOR ATTACH INBOARD BORE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09 EXISTING HOLE DIA 1.218", FINAL HOLE DIA 1.226", MAXIMUM ALLOWABLE HOLE DIA 1.220". OVERSIZED BUSHINGSDR FDEA201703070802Hinge Bracket · corrodedRT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) ACTUATOR ATTACH OUTBOARD BORE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 1.218", FINAL HOLE DIA 1.226" MAXIMUM ALLOWABLE HOLE DIA 1.220", OVERSIZED BUSHING SDR FDEA201703070801Hinge Bracket · corrodedRT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT OUTBOARD BORE SURFACE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09. EXISTING THICKNESS 0.402" , MATERIAL REMOVED 0.008", REMAINING THICKNESS 0.394". MINIMUM ALLOWABLSDR FDEA201703070800Hinge Bracket · corrodedRT WING OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE) ACTUATOR ATTACH INBOARD BORE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08. EXISTING HOLE DIAMETER 1.220 INCH; FINAL HOLE DIAMETER 1.234 INCH; MAXIMUM ALLOWABLE DIAMETER 1.220 INCSDR FDEA201703070799Hinge Bracket · corrodedRT WING OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE) ACTUATOR ATTACH OUTBOARD BORE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08. EXISTING HOLE DIAMETER 1.220 INCH; FINAL HOLE DIAMETER 1.234 INCH; MAXIMUM ALLOWABLE DIAMETER 1.220 INSDR FDEA201703070798Hinge Bracket · corrodedLT WING OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE) ACTUATOR ATTACH OUTBOARD BORE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08. EXISTING HOLE DIAMETER 1.219 INCH; FINAL HOLE DIAMETER 1.226 INCH; MAXIMUM ALLOWABLE DIAMETER 1.220 INSDR FDEA201703070797Hinge Bracket · corrodedLT WING OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE) ACTUATOR ATTACHED INBOARD BORE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08. EXISTING HOLE DIAMETER 1.219 INCH; FINAL HOLE DIAMETER 1.226 INCH; MAXIMUM ALLOWABLE DIAMETER 1.220 ISDR FDEA201703070796Hinge Bracket · corrodedLT WING OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE) FORWARD MOUNT OUTBOARD LUG SURFACE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08. EXISTING THICKNESS: 0.380" MATERIAL REMOVED: 0.003" REMAINING THICKNESS: 0.377" MINIMUM ALLOWABLESDR FDEA201703070795Hinge Bracket · corrodedLT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) ACTUATOR ATTACH OUTBOARD BORE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 1.218", FINAL HOLE DIA 1.222", MAXIMUM ALLOWABLE HOLE DIA 1.220". OVERSIZED BUSHINGSDR FDEA201703070794Hinge Bracket · corrodedLT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) ACTUATOR ATTACH INBOARD BORE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44--09 EXISTING HOLE DIA 1.281", FINAL HOLE DIA 1.285", MAXIMUM ALLOWABLE HOLE DIA 1.220". OVERSIZED BUSHING SDR FDEA201703070793Hinge Bracket · corrodedLT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) BARREL NUT LOWER BOLT H0LE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIAMETER 0.406 INCH; FINAL HOLE DIAMETER 0.422 INCH; MAXIMUM ALLOWABLE DIAMETER 0.391 INCHSDR FDEA201703070792Hinge Bracket · corrodedLT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) BARREL NUT UPPER BOLT HOLE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44--09 EXISTING HOLE DIA 0.405", FINAL HOLE DIA 0.422", MAXIMUM ALLOWABLE HOLE DIA 0.391". OVERSIZED BUSHING FASDR FDEA201703070791Hinge Bracket · corrodedLT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT INBOARD BORE SURFACE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09. EXISTING THICKNESS 0.410", MATERIAL REMOVED 0.005", REMAINING THICKNESS 0.405". MINIMUM ALLOWABLE SDR FDEA201703070790Hinge Bracket · corrodedLT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT BORE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 2.316", FINAL HOLE DIA 2.320", MAXIMUM ALLOWABLE HOLE DIA 2.3135". OVERSIZED BUSHING FABRICATED AND ISDR FDEA201703060782Hinge Bracket · corrodedLT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT OUTBOARD BORE SURFACE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09. EXISTING THICKNESS 0.405", MATERIAL REMOVED 0.005", REMAINING THICKNESS 0.400". MINIMUM ALLOWABLESDR NACA2017022700013Attach Fitting · corrodedRIGHT OUTBOARD FLAP, NR 8 TRACK FORWARD ATTACH FITTING (ON WING) HAS EVIDENCE OF CORROSION BETWEEN TRACK ATTACH BUSHINGS. REPLACED THE FWD ATTACH FITTING IAW BAC5047, AMM 20-50-11 REV 123, & DWG 65-45455 REV E.
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