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 FDEA201401060026Hinge Fitting · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE SIDE LOAD FITTING FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09 REVISION 78. REPAIRED IAW EA 1-5750-87641 REV C STEP 2, 3 AND 4. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 119.Jan 6, 2014 · N574FE · Doug MD11FSDR ASOA20131109271Fitting · wornDURING C-CHECK, THE LT WING AILERON PCA FITTING WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHINGS. MAINTENANCE R & R THE FITTING IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Nov 9, 2013 · N14143 · Emb EMB145XRSDR ASOA20131017254Bracket · wornDURING C-CHECK THE RT AILERON PCA ATTACH FITTING BRACKET WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHINGS. MAINTENANCE R & R THE BRACKET IAW EC5750-01177, REV C. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Oct 17, 2013 · N21129 · Emb EMB145XRSDR FDEA201309072153Hinge Fitting · corrodedRT WING INBD FLAP AFT HINGE BRACKET PIVOT INBD LUG BORE FOUND CORRODED. REWORKED AND FOUND EXCEED LIMITS IAW CMM 57-52-03 REVISION 76. BLEND OUT CARRIED OUT IAW SRM 57-00-00 REVISION 53. REPAIRED IAW EA 1-5750-T0302386 PART 1 STEP 1,3,4,5,7 AND 8. REPAIR Sep 7, 2013 · N643FE · Doug MD11FSDR FDEA201309072152Hinge Fitting · corrodedRT WING INBD FLAP AFT HINGE BRACKET PIVOT OTBD LUG BORE FOUND CORRODED. FOUND EXCEED LIMITS IAW CMM 57-52-03 REVISION 76. BLEND OUT CARRIED OUT IAW SRM 57-00-00 REVISION 53. REPAIRED IAW EA 1-5750- T0302386 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2Sep 7, 2013 · N643FE · Doug MD11FSDR FDEA201308221999Hinge Fitting · corrodedRIGHT WING INBD FLAP OTBD FWD (WING SIDE) HINGE PIVOT HOLE HAS SURFACE CORROSION. REPAIRED IAW EA 1-5750-104703C PART 2 STEPS 1,2, AND 4. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 117.Aug 22, 2013 · N522FE · Doug MD11FSDR FDEA201308222000Hinge Fitting · corrodedLEFT WING INBD FLAP, OTBD FWD (WING SIDE) HINGE PIVOT HOLE HAS SURFACE CORROSION. REPAIRED IAW EA 1-5750-104702C PART 2 STEPS 1,2 AND 4. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2- 100 REVISION 117.Aug 22, 2013 · N522FE · Doug MD11FSDR FDEA201308191958Hinge Fitting · corrodedLT WING INBD FLAP OTBD FWD (WING SIDE) HINGE PIVOT BORE HAS CORROSION. FOUND EXCEEDED LIMITS IAW CMM 57-44-07, REV 76. REPAIRED IAW EA 1-5750-104702C, PART 2, STEPS 1, 2 AND 3. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 117.Aug 19, 2013 · N522FE · Doug MD11FSDR FDEA201308191957Hinge Fitting · corrodedRT WING INBD FLAP OTBD FWD (WING SIDE) HINGE PIVOT CORROSION. FOUND EXCEEDED LIMIT IAW CMM 57-44-07, REV 76. REPAIRED IAW EA 1-5750-104703C, PART 2, STEPS 1, 2, AND 3. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 117.Aug 19, 2013 · N522FE · Doug MD11FSDR FDEA201308181942Hinge Fitting · corrodedRT WING OTBD FLAP, INBD FWD (WING SIDE) HINGE BARREL NUT HOLES SURFACE CORROSION. REPAIRED IAW EA 1-5750-T0302028A, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 117.Aug 18, 2013 · N522FE · Doug MD11FSDR FDEA201308181941Hinge Fitting · corrodedRT WING OTBD FLAP, INBOD FWD (WING SIDE) HINGE LOWER MOUNT INBD HOLE HAS SURFACE CORROSION. FOUND EXCEEDED LIMITS IAW CMM 57-44-08, REV 76. REPAIRED IAW EA 1-5750-T0302028A, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 117.Aug 18, 2013 · N522FE · Doug MD11FSDR FDEA201308181940Hinge Fitting · corrodedRT WING OTBD FLAP, OTBD FWD (WING SIDE) HINGE BARREL NUT HOLES SURFACE CORROSION. REPAIR SHIM FABRICATED AND INSTALLED IAW CMM 57-44-09, REV 76. REPAIR CLASSIFIED MINOR GMM 6-2-100, REV 117.Aug 18, 2013 · N522FE · Doug MD11FSDR FDEA201308181939Hinge Fitting · corrodedRT WING OTBD FLAP, OTBD FWD (WING SIDE) HINGE BARREL NUT LOWER BORE CORRODED. FOUND EXCEEDED LIMITS IAW CMM 57-44-09, REV 76. REPAIRED IAW EA 1- 5750-T0302072, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 117.Aug 18, 2013 · N522FE · Doug MD11FSDR FDEA201308181938Hinge Fitting · corrodedRT WING OTBD FLAP, OTBD FORWARD (WING SIDE) HINGE BARREL NUT UPPER BORE CORRODED. REPAIRHED IAW EA 1-5750-T0302072, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 117.Aug 18, 2013 · N522FE · Doug MD11FSDR FDEA201308181937Hinge Fitting · corrodedLT WING OTBD FLAP, INBD FORWARD (WING SIDE) HINGE BARREL NUT HOLE SURFACE CORRODED. REPAIRED IAW EA 1-5750-T0302026, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Aug 18, 2013 · N522FE · Doug MD11FSDR FDEA201308181936Structure · corrodedLT WING OTBD FLAP, OTBD FWD (WING SIDE) HINGE ACTUATOR HOLE OTBD BORE CORRODED. FOUND EXCEEDED LIMITS IAW CMM 57-44-09, REV 76. REPAIRED IAW EA 1-5750-T0302070A, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 117.Aug 18, 2013 · N522FE · Doug MD11FSDR FDEA201308181935Hinge · corrodedLT WING OTBD FLAP, OTBD FWD (WING SIDE) HINGE ACTUATOR HOLE OTBD BORE CORROSION. FOUND EXCEEDED LIMITS IAW CMM 57-44- 09, REV 76. REPAIRED IAW EA 1-5750-T0302070A, PART 1. CLASSIFIED MAJOR IAW GMM 6-2-100, REV 117Aug 18, 2013 · N522FE · Doug MD11FSDR FDEA201308181934Hinge · corrodedLT WING OTBD FLAP, INBD FWD( WING SIDE) HINGE PIVOT HOLE BORE CORROSION. FOUND EXCEEDED LIMITS. REPAIRED IAW EA 1-5750-T0302026. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Aug 18, 2013 · N522FE · Doug MD11FSDR FDEA201308181933Hinge Fitting · corrodedLEFT WING OTBD FLAP, OTBD FORWARD (WING SIDE) HINGE BARREL NUT HOLE SURFACE CORROSION. REPAIRED IAW CMM.Aug 18, 2013 · N522FE · Doug MD11FSDR 39LA2013072400164Bracket · corrodedFOUND CENTER WING RT OTBD FLAP BRACKET, INBD AND OTBD SKIN CORRODED BEYOND LIMITS. REPLACED WITH NEW SKINS PN'S 212-13202-05-1 AND 212-13202-05-2. REPAIR PREFORMED IAW EO2012032-309 AND EO2021032-424, AND DWG NR 2012032-2032.Jul 24, 2013 · N606AR · Casa C212CDSDR 39LA2013072400104Bracket · corrodedFOUND CENTER WING LT OTBD FLAP BRACKET, INBD SKIN CORRODED BEYOND LIMITS. REPLACED WITH NEW SKIN, PN 212-13202-05-2, IAW EO 2012032-309 AND EO 2012032-424, AND DWG NR 2012032-2032, SUPPORTED BY FAA FORM 8110-3 DATED 31 MAY 2013.Jul 24, 2013 · N606AR · Casa C212CDSDR FDEA201307221626Structure · corrodedLEFT WING OTBD FLAP, INBD FORWARD (WING SIDE) HINGE ACTUATOR INBD BORE CORRODED. BORE REWORKED AND FOUND EXCEEDED LIMITS IAW CMM 57-44-08, REV 76. REPAIR CARRIED OUT IAW EA 1-5750-166143, STEP 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 22, 2013 · N521FE · Doug MD11FSDR FDEA201307221625Structure · corrodedLEFT WING OTBD FLAP, INBD FORWARD (WING SIDE) HINGE UPPER MOUNT OTBD BORE CORRODED. BORE REWORKED AND FOUND EXCEEDED LIMITS IAW CMM 57-44-08, REV 76. REPAIR CARRIED OUT IAW EA 1-5750-166143, STEP 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 22, 2013 · N521FE · Doug MD11FSDR FDEA201307221624Structure · corrodedLEFT WING OTBD FLAP INBD FORWARD (WING SIDE) HINGE BARREL NUT HOLE SURFACE CORRODED. BARREL NUT BORE SURFACE REWORKED IAW CMM 20-10-6, REV 76. REPAIR SHIM FABRICATED AND INSTALLED IAW CMM 57-44-08, REV 76. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 22, 2013 · N521FE · Doug MD11FSDR FDEA201307221623Structure · corrodedRIGHT WING OTBD FLAP, INBD FORWARD (WING SIDE) HINGE UPPER MOUNT INBD BORE CORRODED. BORE REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08, REV 76, REPAIRED IAW EA 1-5750-T0301348, PART 1 STEP 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 22, 2013 · N521FE · Doug MD11FSDR FDEA201307221622Structure · corrodedRIGHT WING OTBD FLAP, INBD FWD (WING SIDE) HINGE UPPER MOUNT OTBD BORE CORRODED. BORE REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08, REV 76. REPAIRED IAW EA 1- 5750-T0301348, PART 1, STEP 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 22, 2013 · N521FE · Doug MD11FSDR FDEA201307221621Structure · corrodedRIGHT WING OTBD FLAP, INBD FWD (WING SIDE) HINGE ACTUATOR INBD BORE CORRODED. BORE REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08, REV 76. REPAIRED IAW EA 1-5750-T0301348, PART 1, STEP 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 22, 2013 · N521FE · Doug MD11FSDR FDEA201307221617Structure · corrodedRIGHT WING OTBD FLAP, OTBD FWD (WING SIDE) HINGE BARREL MOUNT LOWER BORE CORRODED. BORE NR 7 REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09, REV 76. REPAIRED IAW EA 1- 5750-T0301349, PART 1, STEP 2. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 22, 2013 · N521FE · Doug MD11FSDR FDEA201307221615Structure · corrodedRIGHT WING OTBD FLAP, OTBD FWD (WING SIDE) HINGE BARREL MOUNT UPPER BORE CORRODED. BORE NR 7 REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09, REV 76. REPAIRED IAW EA 1- 5750-T0301349, PART 1, STEP 2. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 22, 2013 · N521FE · Doug MD11FSDR FDEA201307221614Hinge Fitting · corrodedRT WING OTBD FLAP, OTBD FORWARD (WING) HINGE UPPER MOUNT INBD BORE CORRODED. REPAIRED IAW EA 1- 5750-T0301349 PART 1 STEP 1. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 116.Jul 22, 2013 · N521FE · Doug MD11FSDR FDEA201307221619Bushing · wornRT WING OTBD FLAP, OTBD FORWARD (WING) HINGE ACTUATOR, OUTBOARD BORE BUSHING WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 76. FOUND EXCEEDED LIMIT IAW CMM 57-44-09, REV 76. NEW BUSHING AND REPAIR WASHER FABRICATED AND INSTALLED IAW EA 1-5750-T0301349, PART 1Jul 22, 2013 · N521FE · Doug MD11FSDR FDEA201307221618Bushing · wornRT WING OTBD FLAP, OTBD FORWARD (WING) HINGE ACTUATOR INBD BORE BUSHING WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 76. FOUND EXCEEDED LIMITS IAW CMM 57-44-09, REV 76. NEW BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0301349, PART 1, STEP 3. REPAIR CLAJul 22, 2013 · N521FE · Doug MD11FSDR FDEA201307221616Hinge Fitting · corrodedRT WING OTBD FLAP, OTBD FORWARD (WING) HINGE BARREL MOUNT HAS SURFACE CORROSION. REWORKED IAW CMM 20-10-6, REV 76. FOUND WITHIN DWG NR ARC0503 AND CMM 57-44-09, REV 19, TABLE 601 LIMITS. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100, REV 116.Jul 22, 2013 · N521FE · Doug MD11FSDR FDEA201307191590Hinge Fitting · crackedRIGHT WING T/E OTBD FLAP INBD FORWARD HINGE BRACKET SIDE LOAD FITTING CRACKED. R & R IAW SRM 51-33-01, REV 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 19, 2013 · N521FE · Doug MD11FSDR FDEA201306301421Structure · corrodedRT WING OTBD FLAP INBD FWD (WING SIDE) HINGE BARREL NUT HOLE SURFACE CORROSION.Jun 30, 2013 · N525FE · Doug MD11FSDR FDEA201306181325Hinge Fitting · corrodedRIGHT WING OTBD FLAP AFT HINGE FWD MOUNT INBD (2A) FOUND WITH CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-04, REV 76. REPAIR ACCOMPLISHED IAW EA 1-5750-T0300851, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jun 18, 2013 · N525FE · Doug MD11FSDR FDEA201306161310Bracket · corrodedRT WING-OTBD FLAP ASSY INBD AFT HINGE INBD LUG PIVOT BORE CORROSION AFTER REMOVAL OF OTBD FLAP ASSY. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-04, REV.76. EXISTING HOLE DIAMETER 1.1525 INCH, FINAL HOLE DIAMETER 1.1605 INCH, MAXIMUM HOLE DIAMETER 1.15 IJun 16, 2013 · N572FE · Doug MD11FSDR FDEA201306151302Structure · corrodedRIGHT WING OTBD FLAP, INBD FWD (WING SIDE) HINGE ACTUATOR HOLE INBD BORE CORROSION.Jun 15, 2013 · N525FE · Doug MD11FSDR FDEA201306151301Structure · corrodedRIGHT WING OTBD FLAP, INBD FWD (WING SIDE) HINGE PIVOT HOLE BORE CORROSION.Jun 15, 2013 · N525FE · Doug MD11FSDR FDEA201306151300Hinge · corrodedRIGHT WING OTBD FLAP, OTBD FWD (WING SIDE) HINGE PIVOT HOLE CORRODED. REWORKED IAW CMM 57-44-09, REV 76. FOUND OUT OF LIMITS. REPAIRED IAW EA 1-5750-T0300831, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jun 15, 2013 · N525FE · Doug MD11FSDR FDEA201306151298Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD (WING SIDE) HINGE ACTUATOR HOLE OTBD BORE CORRODED. REWORKED AND FOUND EXCEEDED LIMITS IAW CMM 57-44-09, REV 76. REPAIR ACCOMPLISHED IAW EA 1-5750-T0300829, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jun 15, 2013 · N525FE · Doug MD11FSDR FDEA201306151297Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD (WING SIDE) HINGE ACTUATOR HOLE INBD BORE CORRODED. REWORKED AND FOUND EXCEEDED LIMITS IAW CMM 57-44-09 REV 76. REPAIR ACCOMPLISHED IAW EA 1-5750-T0300829, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jun 15, 2013 · N525FE · Doug MD11FSDR UALA2013052203548Trunnion · wornLEFT INBD FLAP TRUNNION WORN AT AREA D. BLENDED OUT DAMAGED AREA.May 21, 2013 · N816UA · Airbus A319131SDR DALA13012019233Support Fitting · inoperativeLEFT AND RT RETRACT ACTUATOR SUPPORT FITTINGS INSTALLATION CONFIGURATION DOES NOT MATCH EA 02-093855-03AD. REMOVED SEALANT AROUND NUT OF LT AND RT MLG ACTUATOR SUPPORT FITTINGS OTBD SIDES IN COMPLIANCE WITH EA 02-093855-03AD, STEP 12 AND EA JIC 02-093855-03ADMar 14, 2013 · N933DN · Doug MD9030SDR UALA2013031101416Structure · gougedUPPER RUDDER CONTROL MODULE MOUNT TRUNNION LOWER RIGHT ATTACH BORE IS GOUGED AND SCORED. CHIPPED AREA DIMENSIONS, .250 X .150 WITH A DEPTH OF .140. BLENDED GOUGED AREA FROM BOLT THREADS OUT TO .015" OVER FROM .312", DEPTH INTO BORE .312". NEEDS EDDY CURRENTMar 10, 2013 · N179UA · Boeing 747422SDR DALA13004953214Bolt · scoredDURING INSPECTION, FOUND RT AILERON, HINGE BOLT NR 2 SCORED. SCORED IS BEYOND LIMITS IAW AMM 27-14-41 PB 601. RECEIVED NEW BOLT TO BE INSTALLED ON JIC 5760-1010S-RT. DIMENSIONS L=.8750" X W=.7500".Jan 25, 2013 · N314US · Airbus A320211SDR DALA13004403214Bolt · scoredDURING INSPECTION, FOUND RT AILERON, HINGE BOLT NR 1 SCORED. SCORED IS BEYOND LIMITS IAW AMM 27-14-41, PB 601. RECEIVED NEW BOLT TO BE INSTALLED ON JIC 5760-1010S-RT. DIMENSION L=.8750"X W=.7500".Jan 23, 2013 · N314US · Airbus A320211SDR ASOA20130119057Bushing · migratedDURING C-CHECK RT AILERON INBD AND OTBD HAT BUSHINGS MIGRATED AT OTBD PCA ROD. MX PERFORMED REPAIR ON RT AILERON INBD AND OTBD HAT BUSHINGS IAW AMM 27-10-00-400-801-A. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Jan 19, 2013 · N34111 · Emb EMB145XRSDR ASOA20130119056Bushing · migratedDURING C-CHECK RT SPOILER CENTER INBD HAT BUSHING MIGRATED. MX PERFORMED REPAIR TO RT SPOILER CENTER INBD HAT BUSHING IAW EC5740-01152. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Jan 19, 2013 · N34111 · Emb EMB145XRSDR ASOA20130119054Bushing · migratedDURING C-CHECK, LT SPOILER INBD FITTING OTBD HAT BUSHING MIGRATED. MX PERFORMED REPAIR ON LT SPOILER INBD FITTING, OTBD HAT BUSHING IAW EC5740-01152. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Jan 19, 2013 · N34111 · Emb EMB145XR
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