JASC 5753
Service difficulty reports · 31,513
Reports filed under 5753 · Trailing Edge Flaps, 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 = '5753' 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 = '5753' 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 WX0A2015070272703Flap · crackedLEFT INBD FLAP TE CRACKED. REPLACED LT INBD FLAP TE IAW SRM 51-30-02.SDR FDEA201506282108Hinge Bracket · corrodedRIGHT INBD FLAP, OTBD AFT HINGE, OTBD PIVOT HOLE BORE CORRODED. WORKED & FOUND OUT OF LIMITS IAW CMM 57-52-03. REPAIR ACCOMPLISHED IAW EA1-5750-T0318614 PART 1. CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201506282107Hinge Bracket · corrodedRIGHT INBD FLAP, OTBD AFT HINGE, INBD PIVOT HOLE BORE CORRODED. WORKED & FOUND OUT OF LIMITS IAW CMM 57-52-03. REPAIR ACCOMPLISHED IAW EA 1-5750-T0318614 PART 1. CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201506282106Hinge · corrodedLEFT INBD FLAP, OTBD AFT HINGE PIVOT, OTBD HOLE BORE CORROSION. CORROSION REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING DIAMETER, HALF HINGE LUG 1.281 INCH, STRAP 1.220 INCH, FINAL DIAMETER, HALF HINGE LUG 1.326 INCH, STRAP 1.326 INCH, MAXIMUM SDR FDEA201506282105Hinge · corrodedLEFT INBD FLAP, OTBD AFT HINGE PIVOT, INBD HOLE BORE CORROSION. CORROSION REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HALF HINGE LUG 1.252 INCH, STRAP 1.220 INCH, FINAL HALF HINGE LUG 1.284 INCH, STRAP 1.284 INCH & MAXIMUM ALLOWABLE 1.220 INCSDR FDEA201506282104Hinge · corrodedLEFT OTBD FLAP, OTBD AFT HINGE PIVOT, OTBD HOLE BORE CORROSION. CORROSION REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-52-04. EXISTING 1.141 INCH, FINAL 1.152 INCH & MAXIMUM ALLOWABLE 1.150 INCH. REPAIR ACCOMPLISHED IAW EA 1- 5750-T0318605 PART 1. REFER TO WSDR AALA201506309008Wedge · delaminatedLEFT WING OTBD FLAP INBD TE WEDGE DELAMINATED. REPLACED LT WING OTBD FLAP INBD TE WEDGE IAW EA 252409.SDR AALA201506309007Wedge · delaminatedLEFT WING OTBD TE FLAP REAR WEDGE DELAMINATED. REPLACED IAW EA 252411.SDR FDEA201506262085Hinge · corrodedRIGHT WING, OTBD FLAP INBD FWD HINGE LOWER MOUNT OTBD HOLE BORE CORROSION. CORROSION AT HOLE NR 7, REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING 0.0713 INCH, FINAL= 0.719 INCH & MAXIMUM ALLOWABLE= 0.709 INCH. SHOULDER BUSHING FABRICATED BY MACHSDR FDEA201506262084Hinge · corrodedRIGHT WING, OTBD LAP OTBD FWD HINGE LOWER MOUNT INBD HOLE BORE CORROSION. CORROSION AT HOLE NR 7 REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING 0.0711 INCH, FINAL= 0.715 INCH, MAXIMUM ALLOWABLE= 0.709 INCH. SHOULDER BUSHING FABRICATED BY MACHINISDR FDEA201506262082Bracket · corrodedRIGHT WING OTBD FLAP INBD FWD HINGE ACTUATOR OTBD HOLE BORE CORROSION. CORROSION AT HOLE NR 8 REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING DIAMETER = 1.210 INCH, FINAL DIAMETER = 1.247 INCH, MAXIMUM ALLOWABLE= 1.220 INCH. REPAIR BUSHING FABRISDR FDEA201506262081Bracket · corrodedRIGHT WING, OTBD FLAP INBD FWD HINGE ACTUATOR INBD HOLE BORE CORROSION. CORROSION AT HOLE NR 8 REWORKED & FOUND EXCEED LIMIT IAW CMM 57-44-08. EXISTING DIAMETER 1.218 INCH, FINAL DIAMETER = 1.247 INCH, MAXIMUM ALLOWABLE =1.220 INCH. REPAIR BUSHING FABRICATSDR FDEA201506262080Hinge · corrodedRIGHT WING, OTBD FLAP INBD FWD HINGE PIVOT HOLE BORE CORROSION. CORROSION AT HOLE NR 4 REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING DIAMETER 2.313 INCH, FINAL DIAMETER = 2.316 INCH & MAXIMUM ALLOWABLE DIAMETER = 2.3135 INCH. REPAIR BUSHING FABSDR FDEA201506262077Hinge · corrodedRIGHT WING, OTBD FLAP OTBD FWD HINGE LOWER BARREL NUT HOLE BORE CORROSION. CORROSION AT HOLE NR 7. REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING 0.387 INCH, FINAL 0.405 INCH, MAXIMUM ALLOWABLE IS 0.391 INCH. REPAIR BUSHING FABRICATED BY MACHINSDR FDEA201506262076Hinge · corrodedRIGHT WING, OTBD FLAP OTBD FWD HINGE UPPER BARREL NUT HOLE BORE CORROSION. CORROSION AT HOLE NR 7 REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING IS 0.387 INCH, FINAL IS 0.405 INCH, MAXIMUM ALLOWABLE IS 0.391 INCH. REPAIR BUSHING FABRICATED BY MASDR FDEA201506262074Hinge Bracket · corrodedRIGHT WING OTBD FLAP, OTBD FWD HINGE LOWER MOUNT OTBD HOLE HAS SURFACE CORROSION. WORKED & FOUND OUT OF LIMITS IAW CMM 57-44-09. REPAIR SHIM FABRICATED & INSTALLED IAW EA1-5750-T0318565 P1 STEP 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201506262073Hinge Bracket · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE LOWER MOUNT INBD HOLE CORRODED. WORKED & FOUND OUT OF LIMITS IAW CMM 57-44-09. REPAIR SHIM FABRICATED & INSTALLED IAW EA 1-5750-T0318565 P1 STEP 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201506262072Hinge Bracket · corrodedRIGHT WING FLAP OTBD FWD HINGE LOWER MOUNT OTBD HOLE BORE CORRODED. WORKED & FOUND OUT OF LIMITS IAW CMM 57-44-08. BUSHINGS FABRICATED & INSTALLED IAW EA 1-5750-T0318610 P1 STEP 1A. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201506262071Hinge Bracket · corrodedLEFT WING, OTBD FLAP INBD FWD HINGE BARREL NUT HOLE HAS CORROSION. WORKED IAW CMM 57-44-08 AND REPAIRED IAW EA 1-5750-T0318531 PART 1 STEP 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201506262066Hinge Bracket · corrodedLEFT WING, OTBD FLAP INBD FWD HINGE LOWER INBD HOLE BORE CORRODED. WORKED & FOUND OUT OF LIMITS IAW CMM 57-44-08. REPAIR BUSHING FABRICATED & INSTALLED IAW EA 1-5750-T0318531 PART 1 STEP 1B. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201506262065Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD FWD HINGE LOWER OTBD HOLE BORE CORRODED. WORKED & FOUND OUT OF LIMITS IAW CMM 57-44-08. REPAIR BUSHING FABRICATED & INSTALLED IAW EA 1-5750-T0318531 PART 1 STEP 1B. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201506262063Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD FWD HINGE ACTUATOR INBD HOLE BORE CORRODED. WORKED & FOUND OUT OF LIMITS IAW CMM 57-44-08. REPAIR BUSHING FABRICATED & INSTALLED IAW EA 1-5750-T0318531 PART 1 STEP 1C. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201506262062Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD FWD HINGE ACTUATOR OTBD HOLE BORE CORRODED. WORKED & FOUND OUT OF LIMITS IAW CMM 57-44-08. REPAIR BUSHING FABRICATED & INSTALLED IAW EA 1-5750-T0318531 PART 1 STEP 1C. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201506262060Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD FWD HINGE PIVOT HOLE BORE CORRODED. WORKED & FOUND OUT OF LIMITS IAW CMM 57-44-08. REPAIR BUSHING FABRICATED & INSTALLED IAW EA 1-5750-T0318531 PART 1 STEP 1A. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR A6WA201542909Skin · dentedRIGHT INBD FLAP LOWER SKIN FWD OF MAIN SPAR INBD OF THE OTBD HINGE HAS TWO DENTS.SDR FDEA201506252027Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE BARREL NUT LOWER HOLE BORE CORRODED. WORKED & FOUND OUT OF LIMITS IAW CMM 57-44-09. REPAIR BUSHING FABRICATED & INSTALLED IAW EA 1-5750-T0318563 PART 1 STEP 1B.SDR FDEA201506252026Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE BARREL NUT UPPER HOLE BORE CORRODED. WORKED & FOUND OUT OF LIMITS IAW CMM 57-44-09. REPAIR BUSHING FABRICATED & INSTALLED IAW EA 1-5750-T0318563 PART 1.SDR FDEA201506252025Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE BARREL NUT HOLE SURFACE CORROSION. WORKED AND FOUND WITHIN LIMITS IAW CMM 57-44-09 REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201506252024Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE LOWER MOUNT OTBD HOLE SURFACE CORRODED. FOUND WITHIN LIMITS IAW CMM 57-44-09. REPAIR BUSHING FABRICATED & INSTALLED IAW CMM 57-44-09. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201506252023Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE LOWER MOUNT INBD HOLE SURFACE CORRODED. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-09. REPAIRED IAW EA 1-5750-T0318563 PART 1 STEP 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201506252022Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE LOWER MOUNT OTBD HOLE BORE CORRODED. FOUND OUT OF LIMITS IAW CMM 57-44-09. SHOULDER BUSHING, FABRICATED IAW EA 1-5750-T0318563 PART 1 STEP 1A. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201506242001Skin · dentedRIGHT WING, FOUND A DENT ON RT INBD FLAP LOWER SKIN ON INBD END. REPAIRED IAW EA 1-5750-T0318573 PART 1. MAJOR IAW GMM 6-2-100.SDR SWAA2015070941641Angle · crackedLEFT WING INBD FLAP TRACK INBD ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.SDR SWAA2015071041715Skin · debondedRIGHT WING INBD FORE FLAP UPPER SURFACE DISBONDED 36" FROM OTBD END. REPAIRED FORE FLAP IAW SRM.SDR SWAA2015063041224Skin · delaminatedRIGHT WING INBD FORE FLAP UPPER SKIN DELAMINATED. REPAIRED SKIN IAW SRM.SDR FDEA201506191875Skin · damagedRIGHT INBD AFT FLAP UPPER SURFACE HAS HAIL DAMAGE. REPAIRED IAW EA F-5750-T0318277 PTSDR FDEA201506191877Strap · crackedLEFT WING OTBD FLAP INBD FWD HINGE TENSION STRAP FOUND CRACKED XW486. TENSION STRAP REMOVED IAW SRM 51-33-01-0G & REPLACED WITH NEW SUPPORT TENSION STRAP IAW SRM 51-33-01-0G. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201506191874Skin · damagedLEFT OTBD FLAP UPPER SURFACE HAS HAIL DAMAGE. REPAIRED LT OTBD AFT FLAP IAW EA F-5750-T0318240 PT 1 & SRM 51-70-17.SDR SWAA2015063041253Flap · delaminatedLEFT WING OTBD AFT FLAP DELAMINATED. REPAIRED FLAP IAW SRM.SDR SWAA2015062341093Flap · delaminatedRIGHT WING INBD FORE FLAP DELAMINATED. REPAIRED FORE FLAP IAW EA.SDR SWAA2015062241038Flap · delaminatedLEFT WING OTBD TE AFT FLAP INBD CORNER DELAMINATED. R & R AFT FLAP IAW AMM.SDR SWAA2015062241008Skin · delaminatedRIGHT WING INBD FORE FLAP DELAMINATED ON UPPER SURFACE. REPAIR FORE FLAP IAW EA.SDR FDEA201506181859Skin · delaminatedRIGHT OTBD AFT FLAP UPPER SURFACE CTR AREA EVIDENCE OF DELAMINATION. REPAIRED 8 EACH AREAS OF DELAMINATION IAW SRM 51-20-01, SRM 51-21-10-7 & EA F-5750-T0318133 A PT 1.SDR SWAA2015070841501Fairing · crackedRIGHT WING NR 6 FLAP TRACK FAIRING 642BB, AFT END, AT APPROX. 8 O CLOCK POSITION LOOKING FORWARD, CRACKED. REPAIRED FAIRING IAW EA.SDR DALA2015061803861Skin · damagedWORN REPAIR DOUBLER ON RT WING INBD FLAP INBD VANE. INBD FLAP INBRD VANE WAS REPAIRED.SDR SWAA2015061840876Flap · delaminatedLEFT WING OTBD FLAP DELAMINATED. R & R AFT FLAP IAW AMM.SDR SWAA2015061840875Flap · damagedRIGHT WING INBD FORE FLAP DAMAGED ON INBD END. R & R FORE FLAP IAW AMM.SDR FDEA201506171832Structure · crackedRIGHT WING CTR FLAP INTERNAL STRUCTURE CRACKED AT RIB 18. REPAIRED IAW EA 6-5750-T0318301. MAJOR REPAIR IAW GMM 6-2-100 REV 127.SDR IPXA2015063090691Vane · delaminatedINSPECTION TYPE:3C, LT INBD FLAP VANE LOWER SURFACE HAS AREAS OF DELAMINATION. ACCOMPLISHED PERMANENT REPAIR ON LT INBD FLAP VANE LOWER SURFACE 67" TO 69" FROM INBD EDGE 14" TO 25" FROM T/E IAW SRM 57-50-80, REPAIR 2.SDR IPXA2015063090675Vane · delaminatedINSPECTION TYPE:3C, RT INBD FLAP VANE LOWER SKIN DELAMINTED. ACCOMPLISHED PERMANENT REPAIR ON RT INBD FLAP VANE LOWER SURFACE 70.5" TO 77" FROM INBD EDGE 9.6" TO 20.7" FROM T/E IAW SRM 57-50-80, REPAIR 2.
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