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 FDEA2018090502291Hinge Bracket · corrodedLT WING O/B FLAP ASSY O/B FWD HINGE (WING SIDE) BARREL NUT HOLE CORROSION. HINGE BARREL NUT HOLE (NR 10 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09. EXISTING HOLE DIA: 0.678", FINAL HOLE DIA: 0.707", MAXIMUM ALLOWABLE DIA: 0.667. OVERSIZE BUSHING FASDR FDEA2018083102290Hinge Bracket · corrodedLT WING O/B FLAP ASSY O/B FWD HINGE (WING SIDE) BARREL NUT HOLE SURFACE CORROSION. HINGE BARREL NUT HOLE SURFACE REWORKED AS PER CMM 57-44-09. EXISTING THICKNESS UPPER: 0.408"; LOWER: 0.408", MATERIAL REMOVED: UPPER: 0.012"; LOWER: 0.012", REMAINING THICKNESSDR FDEA2018083102289Hinge Bracket · corrodedLT WING O/B FLAP ASSY O/B FWD HINGE (WING SIDE) BARREL NUT LOWER BOLT HOLE CORROSION. HINGE BARREL NUT LOWER BOLT (NR 7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09, EXISTING HOLE DIA 0.390", FINAL HOLE DIA 0.410" MAXIMUM ALLOWABLE HOLE DIA 0.39SDR FDEA2018083102288Hinge Bracket · corrodedLT WING O/B FLAP ASSY O/B FWD HINGE (WING SIDE) BARREL NUT UPPER BOLT HOLE CORROSION. HINGE BARREL NUT UPPER BOLT HOLE (NR 7 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09. EXISTING HOLE DIA: 0.390", FINAL HOLE DIA: 0.410", MAXIMUM ALLOWABLE DIA: 0.391SDR FDEA2018083102287Hinge Bracket · corrodedLT WING O/B FLAP ASSY O/B FWD HINGE (WING SIDE) LOWER MOUNT O/B BORE CORROSION. HINGE LOWER MOUNT O/B BORE (NR 3 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09. EXISTING HOLE DIA: 0.595", FINAL HOLE DIA: 0.611", MAXIMUM ALLOWABLE DIA: 0.584. SHOULDER BSDR FDEA2018083102286Hinge Bracket · corrodedLT WING O/B FLAP ASSY O/B FWD HINGE (WING SIDE) LOWER MOUNT I/B BORE CORROSION. HINGE LOWER MOUNT I/B BORE (NR 3 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09. EXISTING HOLE DIA: 0.587", FINAL HOLE DIA: 0.611", MAXIMUM ALLOWABLE DIA: 0.584. SHOULDER BSDR FDEA2018083102280Hinge Bracket · corrodedLT WING I/B FLAP ASSY O/B FWD HINGE (WING SIDE) ACTUATOR ATTACH O/B BORE CORROSION. HINGE (WING SIDE) ACTUATOR ATTACH O/B BORE REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-07. EXISTING HOLE DIA: 1.064", FINAL HOLE DIA: 1.1065", MAXIMUM ALLOWABLE DIA: 1.0935SDR FDEA2018083102273Hinge Bracket · wornLT WING I/B FLAP ASSY O/B FWD HINGE (WING SIDE) PIVOT BUSHING WORN. WORN BUSHING AT FWD HINGE (WING SIDE) PIVOT BORE, REMOVED AND BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0332025 A PART 1 STEP 1F (1) AND STEP 1F (3). REPAIR CLASSIFIED AS MAJOR PER GSDR FDEA201808292261Hinge · wornRT WING I/B FLAP ASSY O/B FWD HINGE (WING SIDE) PIVOT BUSHING WORN. WORN BUSHING REMOVED AND BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-07 AND EA 1-5750-T0332026 A PART 1 STEP 1F(1) AND STEP 1F(3). REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201807241788Hinge Bracket · corrodedRT O/B FLAP FWD HINGE (WING SIDE) ACTUATOR O/B HOLE BORE FOUND WITH CORROSION. HINGE ACTUATOR O/B HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 1.250", FINAL HOLE DIA 1.253", MAXIMUM ALLOWABLE HOLE DIA 1.220". OVERSIZED BUSHISDR FDEA201807171760Hinge Bracket · corrodedRT O/B FLAP O/B FWD HINGE (WING SIDE) ACTUATOR I/B HOLE BORE FOUND WITH CORROSION. FWD HINGE (WING SIDE) ACTUATOR I/B HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 1.221", FINAL HOLE DIA 1.248", MAXIMUM ALLOWABLE HOLE DIA 1.2SDR FDEA201807171759Hinge Bracket · corrodedRT O/B FLAP O/B FWD HINGE (WING SIDE) BARREL NUT HOLE SURFACE FOUND WITH CORROSION. FWD HINGE (WING SIDE) BARREL NUT HOLE SURFACE REWORKED AS PER CMM 57-44-09. EXISTING THICKNESS UPPER: 0.409", LOWER: 0.399", MATERIAL REMOVED UPPER: 0.013", LOWER: 0.013", REMASDR FDEA201807171758Hinge Bracket · corrodedRT O/B FLAP O/B FWD HINGE (WING SIDE) LOWER BARREL NUT HOLE BORE FOUND WITH CORROSION. FWD HINGE (WING SIDE) LOWER BARREL NUT HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 0.389", FINAL HOLE DIA 0.406", MAXIMUM ALLOWABLE HOLESDR FDEA201807171757Hinge Bracket · corrodedRT O/B FLAP O/B FWD HINGE (WING SIDE) UPPER BARREL NUT HOLE BORE FOUND WITH CORROSION. FWD HINGE (WING SIDE) UPPER BARREL NUT BORE (7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 0.389", FINAL HOLE DIA 0.406", MAXIMUM ALLOWABLE SDR FDEA201807171756Hinge Bracket · corrodedRT O/B FLAP O/B FWD HINGE (WING SIDE) LOWER MOUNT O/B HOLE SURFACE FOUND WITH CORROSION. FWD HINGE (WING SIDE) LOWER MOUNT O/B HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING THICKNESS 0.430", MATERIAL REMOVED: 0.007", (FWD) AND 0.01SDR FDEA201807171755Hinge Bracket · corrodedRT O/B FLAP O/B FWD HINGE (WING SIDE) LOWER MOUNT I/B HOLE SURFACE FOUND WITH CORROSION. FWD HINGE (WING SIDE) LOWER MOUNT I/B HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING THICKNESS: 0.435". MATERIAL REMOVED: 0.007" (FWD), 0.024" SDR FDEA201807171754Hinge Bracket · corrodedRT O/B FLAP O/B FWD HINGE (WING SIDE) LOWER MOUNT O/B HOLE BORE FOUND WITH CORROSION. FWD HINGE (WING SIDE) LOWER MOUNT O/B HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 0.597", FINAL HOLE DIA 0.613", MAXIMUM ALLOWABLE HOLE DSDR FDEA201807171753Hinge Bracket · corrodedRT O/B FLAP O/B FWD HINGE (WING SIDE) LOWER MOUNT I/B HOLE BORE FOUND WITH CORROSION. FWD HINGE (WING SIDE) LOWER MOUNT I/B HOLE BORE (3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 0.596", FINAL HOLE DIA 0.613", MAXIMUM ALLOWSDR FDEA201807171752Hinge Bracket · corrodedRT O/B FLAP O/B FWD HINGE (WING SIDE) ACTUATOR O/B HOLE BORE FOUND WITH CORROSION. FWD HINGE (WING SIDE) UPPER MOUNT O/B HOLE BORE (2 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 0.955", MAXIMUM ALLOWABLE HOLE DIA 0.944". OVERSISDR FDEA201807171751Hinge Bracket · corrodedRT O/B FLAP O/B FWD HINGE (WING SIDE) PIVOT HOLE BORE FOUND WITH CORROSION. FWD HINGE (WING SIDE) PIVOT HOLE BORE (4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 2.312", FINAL HOLE DIA 2.316", MAXIMUM ALLOWABLE HOLE DIA 2.3135SDR FDEA201807171750Hinge Bracket · corrodedRT O/B FLAP I/B FWD HINGE (WING SIDE) BARREL NUT HOLE SURFACE FOUND WITH CORROSION. FWD HINGE (WING SIDE) BARREL NUT HOLE SURFACE REWORKED AS PER CMM 57-44-08. EXISTING THICKNESS UPPER: 0.375", LOWER: 0.351", UPPER: 0.003", LOWER: 0.003", REMAINING THICKNESS USDR FDEA201807171749Hinge Bracket · corrodedRT O/B FLAP I/B FWD HINGE (WING SIDE) ACTUATOR O/B HOLE BORE FOUND WITH CORROSION. ACTUATOR O/B HOLE BORE (8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. EXISTING HOLE DIA 1.221", FINAL HOLE DIA 1.2245", MAXIMUM ALLOWABLE HOLE DIA 1.220". OVERSIZSDR FDEA201807171748Hinge Bracket · corrodedRT O/B FLAP I/B FWD HINGE (WING SIDE) ACTUATOR I/B HOLE BORE FOUND WITH CORROSION. ACTUATOR I/B HOLE BORE (8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. EXISTING HOLE DIA 1.224", FINAL HOLE DIA 1.227", MAXIMUM ALLOWABLE HOLE DIA 1.220". OVERSIZESDR FDEA201807171747Hinge Bracket · corrodedRT O/B FLAP I/B FWD HINGE (WING SIDE) LOWER MOUNT O/B HOLE SURFACE FOUND WITH CORROSION. LOWER MOUNT O/B HOLE SURFACE (7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. EXISTING THICKNESS: 0.434", MATERIAL REMOVED FWD FACE: 0.008", AFT FACE: 0.009",SDR FDEA201807171746Hinge Bracket · corrodedRT O/B FLAP I/B FWD HINGE (WING SIDE) LOWER MOUNT I/B HOLE SURFACE FOUND WITH CORROSION. LOWER MOUNT O/B HOLE SURFACE (7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. EXISTING THICKNESS 0.425", MATERIAL REMOVED: 0.008", REMAINING THICKNESS: 0.417"SDR FDEA201807171745Hinge Bracket · corrodedRT O/B FLAP I/B FWD HINGE (WING SIDE) LOWER MOUNT O/B HOLE BORE FOUND WITH CORROSION. FWD HINGE (WING SIDE) LOWER MOUNT O/B HOLE BORE (7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. EXISTING HOLE DIA 0.720", FINAL HOLE DIA 0.738", MAXIMUM ALLOWABSDR FDEA201807171744Hinge Bracket · corrodedRT O/B FLAP I/B FWD HINGE (WING SIDE) LOWER MOUNT I/B HOLE BORE FOUND WITH CORROSION. FWD HINGE (WING SIDE) LOWER MOUNT I/B HOLE BORE (7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. EXISTING HOLE DIA 0.709", FINAL HOLE DIA 0.738", MAXIMUM ALLOWABSDR FDEA201807171743Hinge Bracket · corrodedLT O/B FLAP I/B FWD (WING SIDE) HINGE BARREL NUT HOLE SURFACE FOUND WITH CORROSION. FWD HINGE (WING SIDE) BARREL NUT HOLE SURFACE REWORKED AS PER CMM 57-44-08. EXISTING THICKNESS UPPER: 0.376", LOWER: 0.373", MATERIAL REMOVED UPPER: 0.003", LOWER: 0.003", REMASDR FDEA201807171742Hinge Bracket · corrodedLT O/B FLAP I/B FWD (WING SIDE) HINGE ACTUATOR O/B HOLE BORE FOUND WITH CORROSION. FWD HINGE (WING SIDE) ACTUATOR O/B HOLE BORE (8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. EXISTING HOLE DIA 1.249", FINAL HOLE DIA 1.280", MAXIMUM ALLOWABLE HOLSDR FDEA201807171741Hinge Bracket · corrodedLT O/B FLAP I/B FWD (WING SIDE) HINGE ACTUATOR I/B HOLE BORE FOUND WITH CORROSION. FWD HINGE ACTUATOR I/B HOLE BORE (NR 8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. EXISTING HOLE DIA 1.224", FINAL HOLE DIA 1.280", MAXIMUM ALLOWABLE HOLE DIA 1.2SDR FDEA201807171740Hinge Bracket · corrodedLT O/B FLAP I/B FWD (WING SIDE) HINGE LOWER MOUNT I/B HOLE BORE FOUND WITH CORROSION. FWD HINGE LOWER MOUNT I/B HOLE BORE (NR 7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. EXISTING HOLE DIA 0.650", FINAL HOLE DIA 0.713", MAXIMUM ALLOWABLE HOLE SDR FDEA201807171739Hinge Bracket · corrodedLT O/B FLAP O/B FWD (WING SIDE) PIVOT HOLE BORE FOUND WITH CORROSION. FWD HINGE PIVOT HOLE BORE (NR 4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. EXISTING HOLE DIA 2.3159", FINAL HOLE DIA 2.321", MAXIMUM ALLOWABLE HOLE DIA 2.3135". OVERSIZED BUSDR FDEA201807171738Hinge Bracket · corrodedLT O/B FLAP O/B FWD (WING SIDE) HINGE ACTUATOR O/B HOLE BORE FOUND WITH CORROSION. HINGE ACTUATOR O/B HOLE BORE (NR 8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 1.220", FINAL HOLE DIA 1.251", MAXIMUM ALLOWABLE HOLE DIA 1.220SDR FDEA201807171737Hinge Bracket · corrodedLT O/B FLAP O/B FWD (WING SIDE) HINGE ACTUATOR I/B HOLE BORE FOUND WITH CORROSION. ACTUATOR I/B HOLE BORE (NR 8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 1.220", FINAL HOLE DIA 1.251", MAXIMUM ALLOWABLE HOLE DIA 1.220" . OVERSDR FDEA201807171736Hinge Bracket · corrodedLT O/B FLAP O/B FWD (WING SIDE) HINGE LOWER BARREL NUT HOLE FOUND WITH CORROSION. LOWER BARREL NUT HOLE (NR 7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 0.384", FINAL HOLE DIA 0.409", MAXIMUM ALLOWABLE HOLE DIA 0.391". OVERSIZSDR FDEA201807171735Hinge Bracket · corrodedLT O/B FLAP O/B FWD (WING SIDE) PIVOT HOLE BORE FOUND WITH CORROSION. HINGE UPPER BARREL NUT HOLE (NR 7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE: DIAMETER 0.384", FINAL HOLE DIAMETER: 0.409", MAXIMUM ALLOWABLE HOLE DIAMETER: 0.3SDR FDEA201807171734Pivot · corrodedLT O/B FLAP O/B FWD (WING SIDE) PIVOT HOLE BORE FOUND WITH CORROSION. HINGE LOWER MOUNT O/B HOLE BORE (3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE: DIAMETER 0.582", FINAL HOLE DIAMETER: 0.630" MAXIMUM ALLOWABLE HOLE DIAMETER: 0.5SDR FDEA201807171733Bracket · corrodedLT O/B FLAP O/B FWD (WING SIDE) PIVOT HOLE BORE FOUND WITH CORROSION. HINGE LOWER MOUNT O/B HOLE BORE (NR 3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE: DIAMETER 0.582", FINAL HOLE DIAMETER: 0.630" MAXIMUM ALLOWABLE HOLE DIAMETER:SDR FDEA201807171732Hinge Bracket · corrodedLT O/B FLAP O/B FWD (WING SIDE) HINGE LOWER MOUNT I/B HOLE BORE FOUND WITH CORROSION. HINGE LOWER MOUNT I/B HOLE BORE (3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE: DIAMETER 0.582", FINAL HOLE DIAMETER: 0.627" MAXIMUM ALLOWABLE SDR FDEA201807171731Pivot · corrodedLT O/B FLAP O/B FWD (WING SIDE) PIVOT HOLE BORE FOUND WITH CORROSION. CORROSION AT LT O/B FLAP O/B FWD (WING SIDE) PIVOT HOLE BORE (4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE: DIAMETER 2.310". FINAL HOLE DIAMETER: 2.354". MAXIMUSDR FDEA201807171730Hinge Bracket · wornRT INBOARD FLAP OUTBOARD FWD HINGE (WING SIDE) PIVOT BUSHING WORN. RT I/B FLAP O/B FWD HINGE (WING SIDE) PIVOT BORE MEASURED DIA 2.500" AND FOUND WITHIN LIMIT AS PER CMM 57-44-07. MAXIMUM ALLOWABLE HOLE DIA 2.531". NEW BUSHING FABRICATED AND INSTALLED AS PER CSDR FDEA201807171729Hinge Bracket · wornLT INBOARD FLAP OUTBOARD FWD HINGE (WING SIDE) PIVOT BUSHING WORN. LT I/B FLAP O/B FWD HINGE (WING SIDE) PIVOT BORE MEASURED DIA 2.526" AND FOUND WITHIN LIMIT AS PER CMM 57-44-07. MAXIMUM ALLOWABLE HOLE DIA 2.531". NEW BUSHING FABRICATED AND INSTALLED AS PER CSDR CA180529015Bracket · corroded(CAN) DURING THE INSPECTION OF CPCP CARD NR C57-530-02-01 (48 MONTH) LEVEL 3 CORROSION. EXFOLIATION WAS FOUND ON THE LOWER CORNER BRACKET OF THE RT AILERON 1/B HINGE RIB AT THE RIB 20 LOCATION. P/N: HC572H0761-003. ONCE THE RT AILERON 1/B HINGE RIB WAS REMOSDR SCNA201805176088Skin · crackedNR 5 SLAT HAS A SMALL CRACK ON THE LOWER SKIN WHERE ACTUATOR BRACKET IS LOCATED. R & R THE NR 5 LE SLAT.SDR KCSA201805151111Support Fitting · crackedPOSSIBLE CRACK ON LOWER O/B SIDE OF NR 6 SPOILER SUPPORT FITTING.SDR SIMA20180217004Bushing · migratedRIGHT AILERON OUTBOARD HINGE FITTING, INBOARD BUSHING MIGRATED. REMOVED AND REPLACED THE RT AILERON OTBD FITTING IAW EO EM-27MR-112.SDR AALA20180228005Hinge · corrodedRIGHT WING FLAP CENTER HINGE UPPER AND LOWER STUDS AND FITTING CORRODED. INSTALLED A NEW CENTER HINGE STUDS AND FITTING IAW AMM 57-40-01.SDR AALA20180223004Hinge Fitting · corrodedTHE AIRCRAFT IS IN BASE MAINTENANCE. LEFT HAND WING ONBOARD FLAP CENTER HINGE UPPER AND LOWER STUDS AND FITTING CORRODED. INSTALLED NEW STUDS AND FITTING PER AMM 57-40-01.SDR AALA201712059006Hinge Fitting · wornAIRCRAFT IN BASE MAINTENANCE. RIGHT AILERON FAILED BACKLASH FUNCTIONAL TEST. REPLACED AILERON HINGE FITTING NR 4. PER AMM 57-61-00-000-801.SDR AALA201712059005Hinge Fitting · wornAIRCRAFT IN BASE MAINTENANCE. RIGHT AILERON FAILED BACKLASH FUNCTIONAL TEST. REPLACED AILERON HINGE FITTING NR 3 PER AMM 57-61-00-000-801.
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