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 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.Jan 18, 2013 · N16951 · Emb EMB145LRSDR 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.Jan 18, 2013 · N16951 · Emb EMB145LRSDR 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.Jan 18, 2013 · N16951 · Emb EMB145LRSDR 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.Jan 18, 2013 · N16951 · Emb EMB145LRSDR 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.Jan 18, 2013 · N16951 · Emb EMB145LRSDR 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.Jan 14, 2013 · N313US · Airbus A320211SDR FDEA201301080039Hinge Fitting · crackedLT WING OTBD FLAP INBD FORWARD HINGE OTBD SIDE LOAD FITTING CRACKED.Jan 8, 2013 · N614FE · Doug MD11FSDR 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 FABRDec 7, 2012 · N579FE · Doug MD11FSDR 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.Oct 25, 2012 · N602FE · Doug MD11FSDR 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.Oct 18, 2012 · N602FE · Doug MD11FSDR 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.Oct 18, 2012 · N602FE · Doug MD11FSDR 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.Oct 18, 2012 · N602FE · Doug MD11FSDR 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.Oct 18, 2012 · N602FE · Doug MD11FSDR 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.Oct 18, 2012 · N602FE · Doug MD11FSDR 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.Oct 18, 2012 · N602FE · Doug MD11FSDR 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 INCHOct 17, 2012 · N602FE · Doug MD11FSDR 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.Sep 24, 2012 · N585FE · Doug MD11FSDR 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.Sep 23, 2012 · N585FE · Doug MD11FSDR 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.Sep 23, 2012 · N585FE · Doug MD11FSDR 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 1-575Sep 23, 2012 · N585FE · Doug MD11FSDR 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 PASep 21, 2012 · N585FE · Doug MD11FSDR KCSA201208071141Attach Fitting · corrodedNR 8 FLAP TRACK AFT ATTACH FITTING WING SIDE HAS EVIDENCE OF POSSIBLE CORROSION ON MATING SURFACE.Aug 7, 2012 · N715CK · Boeing 747209BSDR KCSA201208071140Attach Fitting · corrodedNR 7 FLAP TRACK AFT ATTACH FITTING WING SIDE HAS EVIDENCE OF POSSIBLE CORROSION ON MATING SURFACE.Aug 7, 2012 · N715CK · Boeing 747209BSDR KCSA201208071139Attach Fitting · corrodedNR 6 FLAP TRACK AFT ATTACH FITTING WING SIDE HAS EVIDENCE OF POSSIBLE CORROSION ON MATING SURFACE.Aug 7, 2012 · N715CK · Boeing 747209BSDR 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.Jul 7, 2012 · N396FE · Doug MD1010FSDR 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.Jul 6, 2012 · N548UA · Boeing 757222SDR 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.Jun 8, 2012 · N623FE · Doug MD11FSDR 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.Jun 8, 2012 · N623FE · Doug MD11FSDR 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.Jun 8, 2012 · N623FE · Doug MD11FSDR KCSA201205231088Attach Fitting · corrodedNR 1 FLAP TRACK AFT ATTACH FITTING, WING SIDE, HAS CORROSION ON MATING SURFACE.May 23, 2012 · N715CK · Boeing 747209BSDR KCSA201205231087Attach Fitting · corrodedNR 3 FLAP TRACK AFT ATTACH FITTING, WING SIDE, HAS CORROSION ON MATING SURFACE.May 23, 2012 · N715CK · Boeing 747209BSDR KCSA201205231086Attach Fitting · corrodedNR 2 FLAP TRACK AFT ATTACH FITTING, WING SIDE, HAS CORROSION ON MATING SURFACE.May 23, 2012 · N715CK · Boeing 747209BSDR 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.May 18, 2012 · N368FE · Doug MD1010FSDR 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. RMay 18, 2012 · N368FE · Doug MD1010FSDR 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.May 18, 2012 · N368FE · Doug MD1010FSDR 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.May 18, 2012 · N368FE · Doug MD1010FSDR 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.May 18, 2012 · N368FE · Doug MD1010FSDR 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.May 18, 2012 · N368FE · Doug MD1010FSDR 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.May 18, 2012 · N368FE · Doug MD1010FSDR 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.May 18, 2012 · N368FE · Doug MD1010FSDR 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.May 18, 2012 · N368FE · Doug MD1010FSDR 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.May 18, 2012 · N368FE · Doug MD1010FSDR 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. REPAIRMay 18, 2012 · N368FE · Doug MD1010FSDR 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.May 18, 2012 · N368FE · Doug MD1010FSDR 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.May 18, 2012 · N368FE · Doug MD1010FSDR 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.May 18, 2012 · N368FE · Doug MD1010FSDR 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 CMay 18, 2012 · N368FE · Doug MD1010FSDR 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.May 18, 2012 · N368FE · Doug MD1010FSDR 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.May 18, 2012 · N368FE · Doug MD1010FSDR 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". REPAIRMay 11, 2012 · N606FE · Doug MD11F
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