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 SCNA20161120316Skin · delaminatedLEFT OUTBOARD AFT FLAP, INBOARD TRAILING EDGE DELAMINATED. REPAIRED THE FLAP.SDR 7C7A2016112000260Flap Track · corrodedCORROSION LT FLAP TRACK ATTACHMENT. REPAIRED IAW ECO 008.57-16.16.SDR 7C7A2016112000258Flap Track · corrodedCORROSION ON RT FLAP TRACK NR 5 AT ATTACHMENT. REPAIRED IAW ECO 008.57-16.15.SDR ASMF201612012Skin · dentedDURING TRANSIT CHECK, TECHNICAL PERSONNEL DETECTED THE INBOARD TRAILING EDGE FLAP AND INBOARD AFT FLAP WITH DAMAGES BY FOD. MAINTENANCE PERSONNEL PERFORMED REVISION DETECTING A DENT OF 25.0” LENGTH, 55.0” WIDTH, 0.625” DEPTH BETWEEN ITEF 112.55 AND ITEF 138.05SDR FDEA201611184087Bracket · corrodedRIGHT WING INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT OUTBOARD HOLE BORE FOUND CORRODED. FOUND OUT OF LIMITS IAW CMM 57-52-03. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-72651C PART 5 STEP 2A & 2B. REPAIR CLASSIFIED AS MAJOR IAW GMM 6SDR FDEA201611184086Bracket · corrodedRIGHT WING INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT INBOARD HOLE BORE FOUND WITH CORROSION. FOUND OUT OF LIMITS IAW CMM 57-52-03. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-72651C PART 5 STEP 2A & 2B. REPAIR CLASSIFIED AS MAJOR ISDR FDEA201611184085Vane · corrodedLEFT WING OUTBOARD FLAP VANE FITTING, BUSHING HOLE CORRODED. FOUND OUT OF LIMITS IAW SRM 57-50-02 REPAIR 5 FIG 201. OVERSIZED BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-100680A PART 2 STEP 1E. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201611184084Vane · corrodedLEFT WING OUTBOARD FLAP VANE FITTING BUSHING HOLE CORRODED. FOUND OUT OF LIMITS IAW SRM 57-50-02 REPAIR 5 FIG 201. A NEW BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-100680A PART 2 STEP 1E. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201611184083Vane · corrodedLEFT WING OUTBOARD FLAP VANE FITTING BUSHING HOLE CORRODED. FOUND OUT OF LIMITS IAW SRM 57-50-02 REPAIR 5 FIG 201. A NEW BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-100680A PART 2 STEP 1E. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201611184089Bracket · corrodedLEFT WING INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT OUTBOARD HOLE BORE FOUND CORRODED. FOUND OUT OF LIMITS CMM 57-52-03. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-72646B PART 5 STEP 2A & 2B. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2SDR FDEA201611184088Bracket · corrodedLEFT WING INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT INBOARD HOLE BORE FOUND CORRODED. FOUND OUT OF LIMITS IAW CMM 57-52-03. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-72646B PART 5 STEP 2A & 2B. REPAIR CLASSIFIED AS MAJOR IAW GMM6-SDR DALA2016111908992Vane · wornLEFT WING HAS A WORN DOUBLER ON THE LT GUIDE VANE, OUTBOARD FLAP. VANE WAS REPAIRED IAW SRM 57-03D PAR.11.SDR DALA2016111808919Vane · wornLEFT WING WORN DOUBLER ON GUIDE VANE, OUTBOARD FLAP REPAIRED IAW SRM 57-03D PAR. 11.SDR SWAA2016120910333Fairing · crackedLT WING FLAP TRACK FAIRING 543BB INTERNAL CAVITY CRACKED. REPAIRED FAIRING IAW SRM AND EA.SDR REXA2016111602290Guide Plate · crackedRIGHT OUTBOARD FLAP, MID HINGE, OUTBOARD FAIRING GUIDE PLATE IS CRACKED. REMOVED AND REPLACED RIGHT OUTBOARD FLAP MID HINGE OUTBOARD FAIRING GUIDE PLATE IAW SRM 51-42-06 APPLIED TOP COAT IAW SRM 51-25-16.SDR FDEA201611164042Skin · dentedRIGHT WING TE FLAP LOWER SKIN AT APPROX XIFH 253 HAD TWO DENTS. REPAIRED IAW SRM 57-10-00 FIG 85, SHT 1, VOL 1.SDR FDEA201611164041Skin · dentedRIGHT INBD FLAP LOWER SURFACE DENTED. REPAIRED IAW SRM 57-10-00. FIG 85, SHT 1, VOL 1SDR FDEA201611164037Skin · crackedLEFT OTBD FLAP UPPER INBD SKIN IS CRACKED. REPAIRED IAW SRM 57-00-01, FIG 4, SHT 2, VOL 1.SDR FDEA201611164036Skin · crackedLEFT OTBD FLAP UPPER L/E SKIN CRACKED. REPAIRED IAW SRM 57-00-01, FIG 4, SHT 2, VOL 1.SDR FDEA201611164035Skin · crackedLEFT OTBD FLAP UPPER T/E SKIN FOUND CRACKED. REPAIRED IAW SRM 57-00-01 FIG 4 SHT 2 VOL 1.SDR SWIA2016120642891Vane · corrodedRIGHT INBD FLAP CENTER FLAP VANE CAP HAD OUT OF LIMITS CORROSION. REMOVED AND REPLACED THE FLAP VANE CAP IAW SRM.SDR FDEA201611144254Skin · dentedTHE RT INBOARD MAIN FLAP DENTED 20 INCHES FROM OUTBOARD EDGE OF FLAP AND 23 INCHES FROM AFT EDGE OF FLAP. REPAIRED IAW SRM 57-53-01, 57-53-01 AND SRM 51-70-10.SDR SWAA2016111709783Flap · delaminatedLT WING OUTBOARD AFT FLAP DELAMINATED. R&R AFT FLAP PER AMM.SDR AALA20161113006Fitting · damagedNR 3 FLAP JACK SCREW AFT CARRIAGE LOWER MOUNT FITTING IS DAMAGED. REMOVED AND REPLACED THE FITTING IAW SRM 51-40-02-0G AND 51-00-05-1.SDR DALA2016111808923Vane · corrodedCORROSION ON RIGHT WING TE FLAP GUIDE VANE. THE VANE WAS REPLACED IAW SRM 57-03D PAR 11.SDR A6WA2016111544577Rib · damagedRIGHT INBD FLAP DAMAGED AT OB LOWER EDGE.SDR DALA2016111208742Vane · dentedSEVERAL DENTS ON AFT MOVABLE FLAP VANE ON THE LT WING. THE FLAP VANE WAS REPAIRED IAW SRM 57-53-01 REP.1 PARAGRAPH 4.SDR AALA201611169028Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING OUT BOARD FLAP 4 TRACK PIVOT BOLT. REPLACED BOLT PER AMM 27-54-62-000-001-A AND 27-54-62-400-001-A.SDR FQAR20161110054Bracket · crackedDURING A ROUTINE INSPECTION, AN ANGLE IN THE LEFT WING THAT IS CO-LOCATED WITH THE OUTBOARD FLAP MOUNTING BRACKET WAS FOUND TO BE CRACKED THROUGH THE RIVETS.SDR DALA2016111408773Bearing · migratedRIGHT WING NR 7 FLAP MOVABLE FARING AFT LINK LOWER BEARING MIGRATED. THE BEARING WAS REMOVED IAW SOPM 20-50-03, REV 107. MEASURED AND FOUND ELONGATED IAW CMM 57-26-60, RERAIR 9-2, REV 23. MACHINED AND FOUND WITHIN LIMITS IAW CMM 57-26-60, REPAIR 9-2, REV 23SDR DALA2016111108690Skin · delaminatedDELAMINATED UPPER SKIN XV2= 257 ON LT WING OUTBOARD FLAP CENTER VANE. THE FLAP VANE WAS REPAIRED IAW SRM 57-03D PAR.11.SDR DALA2016111008432Vane · delaminatedDELAMINATED UPPER SKIN APPROX XV2= 257 AT LT WING OUTBOARD FLAP CENTER VANE. THE FLAP VANE WAS REPAIRED IAW SRM 57-03D PAR. 1.SDR SWAA2016110909533Fairing · delaminatedRIGHT WING INBOARD FLAP OUTBOARD TRACK FAIRING DELAMINATED. REPAIRED THE FAIRING IAW SRM.SDR WVER2016110850813Vane · chafedRIGHT INBD FLAP VANE HAS CHAFE DAMAGE AT W.S. 90.00.SDR FDEA201611073878Skin · crackedLEFT WING CENTER FLAP UPPER SKIN AT RIB 26 FOUND CRACKED. CUT OUT LOWER SKIN FOR ACCESS IAW SRM 57-50-00 FIG.205 CUT OUT AWAY THE DAMAGE FLANGE OF THE RIB IAW SRM 57-50-00 FIG.201 INSTALLED AREPAIR ANGLE IAW SRM 57-50-00.SDR ASAA2016110718675Fitting · corrodedAFTER REMOVAL OF INBD FOREFLAP INBD TORQUE TUBE, FOUND ATTACH FITTING FOR TORQUE TUBE CORRODED. ACFT GROUNDED. REMOVED AND REPLACED THE FITTING IAW AMM 20-50-11-912-602 PG 6.SDR WVER2016110700011Bracket · crackedCRACKED ATTACH BRACKET FOR SLAT TRACK BOX INSIDE RIGHT WING FUEL TANK INSIDE FUEL ACCESS PANEL 651AB.SDR ASOA201611076127Skin · dentedRIGHT INBD FLAP DENTED. REPAIRED IAW SRM 57-52-01-201-001-A01 REPAIR IV. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR DALA2016110708291Vane · wornWEAR ON TRAILING EDGE AREA STA XV1=211 AT RT WING OUTBOARD FLAP INBOARD VANE. TRAILING EDGE AREA STA XV1=211 AT RT WING OUTBOARD FLAP INBOARD VANE WAS REPAIRED SRM 57-03 D.SDR DALA2016111008689Vane · crackedWEAR ON PREVIOUS REPAIR DOUBLER ON LEADING EDGE XV1=161 ON LT WING OUTBOARD FLAP INBOARD VANE. THE FLAP INBOARD VANE WAS REPLACED IAW SRM 57-03 D PAR. 11.SDR FDEA201611043826Skin · nickedLEFT WING INBD FLAP LOWER SURFACE NICKED. REPAIRED LOWER FLAP SKIN IAW SRM 57-10-00 FIG 85. MAJOR REPAIR.SDR SWAA2016110709434Fairing · delaminatedRT WING NR 6 INBOARD FLAP FAIRING, AFT FAIRING FORWARD SECTION DELAMINATED. R&R FAIRING PER EA.SDR SWAA2016110409368Flap · delaminatedLT WING TRAILING EDGE AFT FLAP DELAMINATED LOWER AFT CORNER APPROX 9X8 INCHES. R&R AFT FLAP ASSEMBLY IAW AMM.SDR SWAA2016110409367Flap · delaminatedRT WING OUTBOARD AFT FLAP DELAMINATED. R&R AFT FLAP PER AMM.SDR SWAA2016110409340Fairing · delaminatedRIGHT WING INBOARD FLAP OUTBOARD NR 6 TRACK FAIRING FORWARD SECTION DELAMINATED. R & R THE FAIRING IAW EA.SDR SWAA2016110309326Flap · delaminatedLT WING OUTBOARD AFT FLAP DELAMINATED. R&R AFT FLAP PER AMM.SDR DALA2016110308192Vane · wornWEAR ON TRAILING EDGE AREA STA XV2= 297 AT LT WING OUTBOARD FLAP OUTBOARD VANE. TRAILING EDGE AREA STA XV2= 297 AT LT WING OUTBOARD FLAP OUTBOARD VANE WAS REPAIRED PER SRM 57-03D PAR 11 AND ERA 492663-14MA REV ORIGINAL.SDR DALA2016110308187Skin · wornWEAR ON TRAILING EDGE AREA LOWER SURFACE STA XV2=297 AT LT WING OUTBOARD FLAP OUTBOARD VANE. TRAILING EDGE AREA LOWER SURFACE STA XV2=297 AT LT WING OUTBOARD FLAP OUTBOARD VANE WAS REPAIRED PER SRM 57- 03D PAR 11.SDR EBVR20161101001Skin · debondedRIGHT INBD FLAP LOWER SURFACE HAS AN AREA OF DE LAMINATION CAUSED BY IMPACT DAMAGE LOCATED DIRECTLY BEHIND THE MAIN TIRE. COMPLIED WITH ERO-868488 REV IR.SDR IPXA2016103110104Skin · dentedRIGHT INBD AFT FLAP LOWER SKIN DENTED, 64.5 INCHES FROM INBD EDGE AND 7.75 INCHES FROM T/E OF FLAP. REPAIRED IAW EO B767-5750-62331-A.
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