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 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.SDR 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.SDR 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.SDR 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 SDR 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 6-2SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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 117SDR 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.SDR FDEA201308181933Hinge Fitting · corrodedLEFT WING OTBD FLAP, OTBD FORWARD (WING SIDE) HINGE BARREL NUT HOLE SURFACE CORROSION. REPAIRED IAW CMM.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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 1SDR 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 CLASDR 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.SDR 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.SDR FDEA201306301421Structure · corrodedRT WING OTBD FLAP INBD FWD (WING SIDE) HINGE BARREL NUT HOLE SURFACE CORROSION.SDR 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.SDR 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 ISDR FDEA201306151302Structure · corrodedRIGHT WING OTBD FLAP, INBD FWD (WING SIDE) HINGE ACTUATOR HOLE INBD BORE CORROSION.SDR FDEA201306151301Structure · corrodedRIGHT WING OTBD FLAP, INBD FWD (WING SIDE) HINGE PIVOT HOLE BORE CORROSION.SDR 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.SDR 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.SDR 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.SDR UALA2013052203548Trunnion · wornLEFT INBD FLAP TRUNNION WORN AT AREA D. BLENDED OUT DAMAGED AREA.SDR 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 02-093855-03ADSDR 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 CURRENTSDR 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".SDR 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".SDR 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.SDR 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.SDR 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.
Back to JASC 5744