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 ASOA20130118025Hinge Bracket · wornDURING C-CHECK, RT GROUND SPOILER INBD HINGE OTBD HAT BUSHING MIGRATED. MX R & R RT GROUND SPOILER INBD HINGE BRACKET IAW EC5740-01288. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20130118024Bushing · migratedDURING C-CHECK RT WING SPEED BRAKE CENTER HINGE ATTACHMENT INBD LOBE HAS MIGRATED HAT BUSHING. MX R & R CENTER HINGE INBD HAT BUSHING IAW EC5740-01152, REV C. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20130118022Hinge · wornDURING C-CHECK LT WING GROUND SPOILER INBD HINGE ATTACHMENT OTBD LOBE HAT BUSHING MIGRATED. MX R & R LT GROUND SPOILER INBD HINGE ATTACHMENT BRACKET IAW EC5740-01288. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20130118021Hinge · wornDURING C-CHECK LT WING GROUND SPOILER CENTER HINGE ATTACHMENT INBD LOBE HAT BUSHING MIGRATED. MX R & R LT GROUND SPOILER CENTER HINGE ATTACHMENT IAW EC5740-01288. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20130118020Hinge · wornDURING C-CHECK LT WING GROUND SPOILER OTBD HINGE ATTACHMENT INBD LOBE HAT BUSHING MIGRATED. MX R & R LT WING GROUND SPOILER OTBD HINGE ATTACHMENT IAW EC5740-01288. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR DALA13002203213Hinge Pin · damagedDURING INSPECTION, FOUND LT AILERON, HINGE PIN NR 3 SCORED. NEW LT AILERON NR 3 HINGE INSTALLED. SCORED NR 3 HINGE PIN FOUND OUT OF LIMITS PER AMM 27-14-41, PB 601.SDR FDEA201301080039Hinge Fitting · crackedLT WING OTBD FLAP INBD FORWARD HINGE OTBD SIDE LOAD FITTING CRACKED.SDR FDEA201212074264Hinge Bracket · corrodedRT WING, OTBD FLAP, INBD FORWARD HINGE BRACKET, LOWER MOUNT INBD BORE FOUND CORRODED. REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-44-08 REVISION 74. EXISTING HOLE DIAMETER: 0.705", FINAL HOLE DIAMETER: 0.709", MAXIMUM HOLE: 0.709". REPAIR BUSHING FABRSDR FDEA201210253745Fitting · corrodedRT WING (WING SIDE) OTBD FLAP VANE FITTING 'E' MOUNTING SURFACE FOUND CORROSION. REPAIRED IAW EA 1-5750-162385. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.SDR FDEA201210183670Bushing · wornRIGHT WING SIDE OTBD FLAP HINGE ACTUATOR ATTACHED FITTING BUSHING WORN. REPAIR ACCOMPLISHED AS PER EA 1-5750-127715 REVISION B PART 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.SDR FDEA201210183669Attach Bracket · wornRIGHT WING SIDE FLAP, OTBD HINGE ACTUATOR ATTACHED FITTING WORN. REPAIR ACCOMPLISHED AS PER EA 1-5750-127715 REVISION B PART 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.SDR FDEA201210183668Hinge Fitting · corrodedRT WING SIDE OTBD FLAP, OTBD HINGE FITTING FOUND CORRODED. REPAIR ACCOMPLISHED PER EA 1-5750-162384 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.SDR FDEA201210183667Hinge Bracket · corrodedRIGHT WING SIDE OTBD FLAP, OTBD HINGE FITTING FOUND CORRODED. REPAIR ACCOMPLISHED PER EA 1-5750-162384 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.SDR FDEA201210183666Hinge Bracket · damagedRIGHT WING OTBD FLAP INBD HINGE LOWER MOUNT OTBD HOLE REPAIR BUSHING FOUND DAMAGED. REPAIRED IAW EA 1-5750-127716, REVISION B, PART 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.SDR FDEA201210183659Hinge Fitting · corrodedRIGHT WING TE FLAP, WING SIDE OTBD HINGE FITTING MATING SURFACE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-162384 PART 1, STEP 1, 2, 3, 4 AND 7. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.SDR FDEA201210173646Hinge Bracket · corrodedRIGHT WING OTBD FLAP INBD HINGE SIDE LOAD FITTING LOWER FASTENER HOLE FOUND CORRODED. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 REVISION 74. EXISTING HOLE DIAMETER = 0.641 INCH, FINAL HOLE DIAMETER = 0.6455 INCH. MAXIMUM HOLE DIAMETER = 0.621 INCHSDR FDEA201209243418Hinge · damagedDURING FPI ON RT INBD FLAP, OTBD HINGE (FLAP SIDE) PIVOT INBD HOLE FOUND DAMAGED. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03 REVISION 74. REPAIRED IAW EA 1-5750-162593 PART 1. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.SDR FDEA201209233407Hinge · corrodedLEFT OTBD FLAP, OTBD FORWARD (WING) HINGE ACTUATOR OTBD HOLE FOUND CORRODED. REPAIRED IAW EA 1-5750-162588. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.SDR FDEA201209233405Hinge · corrodedLEFT OTBD FLAP, OTBD FORWARD (WING) HINGE ACTUATOR INBD HOLE FOUND CORRODED. REPAIRED IAW EA 1-5750-162588. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.SDR FDEA201209233404Hinge Fitting · corrodedLEFT OTBD FLAP, INBD FORWARD (WING SIDE) HINGE ACTUATOR INBD HOLE FOUND CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-08, REV 74. EXISTING DIAMETER 1.228", FINAL DIAMETER 1.232", MAXIMUM ALLOWABLE DIAMETER 1.220". REPAIR ACCOMPLISHED IAW EA 1-575SDR FDEA201209213376Hinge Fitting · corrodedRT OTBD FLAP, OTBD FORWARD WING HINGE ACTUATOR INBD HOLE CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09 REV 74. EXISTING HOLE DIAMETER 1.249", FINAL DIAMETER 1.254", MAXIMUM ALLOWABLE DIAMETER 1.220". REPAIR ACCOMPLISHED IAW EA 1-5750-162586 PASDR KCSA201208071141Attach Fitting · corrodedNR 8 FLAP TRACK AFT ATTACH FITTING WING SIDE HAS EVIDENCE OF POSSIBLE CORROSION ON MATING SURFACE.SDR KCSA201208071140Attach Fitting · corrodedNR 7 FLAP TRACK AFT ATTACH FITTING WING SIDE HAS EVIDENCE OF POSSIBLE CORROSION ON MATING SURFACE.SDR KCSA201208071139Attach Fitting · corrodedNR 6 FLAP TRACK AFT ATTACH FITTING WING SIDE HAS EVIDENCE OF POSSIBLE CORROSION ON MATING SURFACE.SDR FDEA201207072514Hinge Fitting · corrodedRT WING FLAP, OUTBD HINGE FITTING, HAS PITTING CORROSION. REMOVED CORROSION IAW CMM 57-44-09. FOUND TO BE WITHIN LIMITS IAW CMM 57-44-09.SDR CALA2014040390761Mount Bracket · damagedLEFT WING INB FLAP, OTBD AFT FAIRING, FWD INBD MOUNT BRACKET HAS PULLED RIVETS & ELONGATED HOLE. ACCOMPLISHED A FREEZE PLUG STRAP REPAIR. ACFT WILL BECOME NON-AIRWORTHY ON OR BEFORE 20JUL14 UNLESS NEW 8100-9 RECEIVED.SDR FDEA201206082147Stop Fitting · crackedRT WING OTBD FLAP SECONDARY STOP FITTING CRACKED. R & R IAW SRM 51-31-01, REV 49. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201206082146Hinge Bracket · corrodedLEFT WING INBD FLAP, OTBD AFT HINGE BRACKET PIVOT OTBD LUG BORE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMIT AS IAW CMM 57-52-03, REV 73. REWORK CARRIED OUT IAW EA 1-5750-162328. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.SDR FDEA201206082145Hinge Bracket · corrodedLT WING INBD FLAP OTBD AFT HINGE BRACKET PIVOT INBD LUG BORE FOUND CORROSION. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 73. REWORKED CARRIED OUT IAW EA 1-5750-162328. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.SDR KCSA201205231088Attach Fitting · corrodedNR 1 FLAP TRACK AFT ATTACH FITTING, WING SIDE, HAS CORROSION ON MATING SURFACE.SDR KCSA201205231087Attach Fitting · corrodedNR 3 FLAP TRACK AFT ATTACH FITTING, WING SIDE, HAS CORROSION ON MATING SURFACE.SDR KCSA201205231086Attach Fitting · corrodedNR 2 FLAP TRACK AFT ATTACH FITTING, WING SIDE, HAS CORROSION ON MATING SURFACE.SDR FDEA201205181862Hinge Fitting · corrodedLEFT WING OTBD FLAP, INBD FORWARD HINGE SIDE LOAD FITTING ATTACHMENT LOWER BOLT HOLE FOUND WITH CORROSION. REWORK CARRIED OUT IAW EA 8-5750-160613, PART 1A STEP 1 TO 9. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201205181846Hinge Fitting · corrodedLEFT WING OTBD FLAP, OTBD FORWARD HINGE SIDE LOAD FITTING ATTACHMENT MATING SURFACE FOUND WITH CORROSION. REWORK CARRIED OUT IAW CMM 20-11-02 REV 55. FOUND WITHIN LIMIT IAW CMM 57-44-09, REV 55, DWG ARC0503 AND EA 8-5750-160616, PART 1 PAGE 8 OF 10 FIG 1. RSDR FDEA201205181845Hinge Fitting · corrodedLT WING OTBD FLAP, OTBD FORWARD HINGE SIDE LOAD FITTING ATTACHMENT LOWER BOLT HOLE FOUND WITH CORROSION. REWORK CARRIED OUT IAW EA 8-5750-160616, PART 1B, STEPS 1 TO 9. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 114.SDR FDEA201205181844Hinge Fitting · corrodedLEFT WING OTBD FLAP, OTBD FORWARD HINGE SIDE LOAD FITTING ATTACHMENT UPPER BOLT HOLE FOUND WITH CORROSION. REWORK CARRIED OUT IAW EA 8-5750-160616, PART 1B, STEPS 1 TO 9. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 114.SDR FDEA201205181843Hinge Fitting · corrodedLEFT WING OTBD FLAP, OTBD FORWARD HINGE LOWER ATTACHMENT, OTBD BORE FOUND WITH CORROSION. REWORK CARRIED OUT IAW EA 8-5750-160616, PART 1A, STEPS 1 TO 9. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201205181842Hinge Fitting · corrodedLEFT WING OTBD FLAP, OTBD FORWARD HINGE LOWER ATTACHMENT INBD BORE FOUND WITH CORROSION. REWORK CARRIED OUT IAW EA 8-5750-160616, PART 1A STEPS 1 TO 9. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201205181841Hinge Fitting · damagedAFTER REMOVAL OF BUSHING ON RT WING, OTBD FLAP, INBD HINGE PIVOT OTBD ATTACHMENT LUG HOLE FOUND OVERSIZED. REPAIR ACCOMPLISHED EA 8-5750-160618, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201205181840Hinge Fitting · wornRT WING OTBD FLAP, INBD AFT HINGE PIVOT HOLE OUTBOARD ATTACHMENT LUG FOUND BUSHING WORN. NEW BUSHING FABRICATED AND INSTALLED IAW EA 8-5750-160618, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201205181839Hinge Fitting · corrodedRT WING OTBD FLAP, INBD FORWARD HINGE LOWER ATTACHMENT OTBD BORE FOUND WITH CORROSION. REWORK CARRIED OUT IAW EA 8-5750-160615, PART 1 A STEPS 1, 2, 3, 5 AND 6. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201205181838Hinge Fitting · corrodedRT WING OTBD FLAP, INBD FORWARD HINGE LOWER ATTACHMENT INBD BORE FOUND WITH CORROSION. REWORK CARRIED OUT IAW EA 8-5750-160615 PART 1 A STEPS 1, 2, 3, 4, 5 AND 6. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201205181837Hinge Fitting · corrodedRT WING OTBD FLAP, INBD FORWARD HINGE SIDE LOAD FITTING ATTACHMENT FOUND MATING SURFACE WITH CORROSION. REWORK CARRIED OUT IAW CMM 20-11-02, REV 55. FOUND WITHIN CMM 57-44-08, REV 55 AND DWG ARC0502 LIMITS IAW EA 8-5750-160615, PART 1, PAGE 9 OF 11. REPAIRSDR FDEA201205181836Hinge Fitting · corrodedRT WING OTBD FLAP, INBD FORWARD HINGE SIDE LOAD FITTING ATTACHMENT UPPER BOLT HOLE FOUND WITH CORROSION. REWORK CARRIED OUT IAW EA 8- 5750-160615 PART 1 B STEPS 1, 2, 3, 4 AND 5. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201205181835Hinge Fitting · corrodedRT WING, OTBD FLAP, INBD FORWARD HINGE SIDE LOAD FITTING ATTACHMENT LOWER BOLT HOLE FOUND WITH CORROSION. REWORK CARRIED OUT IAW EA 8-5750-160615, PART 1B STEPS 1, 2, 3, 4 AND 5. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201205181834Hinge Fitting · corrodedRT WING OTBD FLAP, OTBD FORWARD HINGE SIDE LOAD FITTING. ATTACHMENT UPPER BOLT HOLE FOUND WITH CORROSION. REWORK CARRIED OUT IAW EA 8-5750-160614, PART 1B, STEPS 1 TO 9. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201205181833Hinge Fitting · corrodedRT WING OTBD FLAP, OTBD FORWARD HINGE SIDE LOAD FITTING. ATTACHMENT FOUND MATING SURFACE WITH CORROSION. REWORK CARRIED OUT IAW CMM 20-11-02, REV 55 FOUND WITHIN LIMIT IAW CMM 57-44-09, REV 55, DWG ARC0503 AND EA 8-5750-160614, PART 1 PAGE 9 OF 10. REPAIR CSDR FDEA201205181832Hinge Fitting · corrodedRT WING OTBD FLAP, OTBD FWD HINGE LOWER ATTACHMENT OTBD BORE FOUND WITH CORROSION. REWORKED CARRIED OUT IAW EA 8-5750-160614 PART 1A STEPS 1 TO 9. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201205181831Hinge Fitting · corrodedRT WING OTBD, FLAP OTBD, FORWARD HINGE LOWER ATTACHMENT INBD BORE FOUND WITH CORROSION. REWORKED CARRIED OUT IAW EA 8-5750-160614, PART 1A STEPS 1 TO 9. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201205111792Bushing · wornLEFT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET SIDE ATTACH UPPER BOLT HOLE BUSHING FOUND WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE MEASURED DIAMETER 0.405" AND FOUND EXCEED LIMIT IAW CMM 57-44-09, REV 72 MAXIMUM ALLOWABLE DIAMETER 0.391". REPAIR
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