JASC 5753
Service difficulty reports · 31,515
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 USAA2010121593070Flap · delaminatedPIT - C3 - MAJOR REPAIR - DISBOND ON LEFT OUTBOARD FLAP TRAILING EDGE. REPAIRED LEFT OUTBOARD FLAP TRAILING EDGE IAW A320 SRM 57-53-00.SDR REXA201000295Plate · missingP/N 601R10929-155 PLATE ASSEMBLY WAS NOTED TO BE MISSING FROM THE RIGHT WING INBOARD FLAP HINGE BOX INSTALLATION AT WS = 80.50. NO WEAR OR OTHER TYPE OF DAMAGE WAS NOTED IN THE AREA OF THE MISSING PLATE ASSEMBLY AND ALL FASTENERS WERE SECURE (SAFTIED WITH LOCSDR DALA1035545521Skin · damagedREMOVED DAMAGED UPPER SKIN AND CORE, TAPER SANDED, FABRICATED NEW CORE SECTION, BONDED CORE SECTION AND REPAIR PLIES IAW SRM 51-70-07, PARA 4. FOUND MORE DELAMINATION ON UPPER SKIN. REMOVED DAMAGE, TAPER SANDED, BONDED REPAIR PLIES, AND APPLIED SEAL RESIN IAWSDR ABXA201012100170Skin · corrodedRT WING INBOARD TRAILING EDGE FWD FLAP UPPER SURFACE HAS 2 BULGES IN THE SKIN ABOUT 67 TO 82 INCHES FROM THE FLAP INBOARD EDGE AND 11 TO 13 INCHES FROM THE TRAILING EDGE. REMOVED AND REPLACED RT INBOARD MAIN FLAP IAW B767 MM 27-51-03-04.SDR FDEA201012074609Fitting · misalignedRT WING INBD FWD FLAP TRACK FAIRING BRACKET ATTACHMENT HOLES ON AFT LANDING GEAR TRUNNION HSG MISALIGNED. BRACKET FOR RT WING INBD FWD FLAP TRACK FAIRING REPAIRED IAW EA F-5740-142375. (WING ATTACH FITTINGS - 1 FASTENER HOLE MISALIGNED ON 113N1159-1 FITTING).SDR SWAA107651Flap · delaminatedDURING SCHEDULED MV2 CHECK, FOUND LT WING O/B MID FLAP DELAMINATED. REMOVED AND REPLACED MID FLAP PER MM.SDR FDEA201012064598Skin · wornLT WING OTBD MAIN FLAP L/E INBD SIDE HAS A WORN SECTION APPROX 10" LONG . EVALUATED LT WING OTBD MAIN FLAP AND FOUND TO BE OUT OF LIMITS IAW SRM 57-53-01, PG 106, DETAIL VI. R & R L/E SKIN IAW SRM 51-40-02. CLASSIFIED CATEGORY "A". MAJOR REPAIR.SDR IPXA10163793Skin · dentedRT INBD FLAP LOWER SKIN DENT 18" FROM FWD EDGE. THIS IS CLASSIFIED AS A MAJOR REPAIR. TRANSFERRED TO NR 355102. COMPLETED REPAIR IAW EO A300-5750-37685-B. THIS IS A PERMANENT REPAIR AND CLEARS D424774.SDR SWAA107676Flap · delaminatedDURING SCHEDULED MV1 CHECK, FOUND RT INBOARD FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.SDR SWAA107675Flap · delaminatedDURING SCHEDULED MV1 CHECK, FOUND LT INBOARD FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.SDR IPXA10163770Skin · dentedRR INBD FLAP HAS DAMAGE CONSISTING OF A DENT IN LWR MAIN SKIN ASSY WITH A GOUGE. REPAIRED REF EO-A300-5750-37685-B.SDR FDEA201012034562Flap Track · crackedRT INBD FLAP CUTOUT FOR AFT FLAP NR 2 TRACK CRACKED, WS 200. REMOVED R/H I/B MIDFLAP LOWER AFT CHORD IAW SRM 51-30-2 FABRICATED LOWER CHORD 3 SECTIONS FROM BAC1503-100046 7075 T6 47.5", 32.25" AND 96.75" LONG AND 2 SPLICES FROM BAC1503-100046 7075 T6SDR A6WA201140025Bracket · chafedRT FLAP STUB FAIRING FWD BRACKET CHAFED AND BUTTPLATE BROKEN. REMOVED UNSERVICEABLE FAIRING (STUB RT) REC SERVICEABLE STUB FAIRING ( RT) FROM STOCK INSTALLED.SDR A6WA201140015Fitting · chafedLT OTBD FLAP, FLAP ROLLER GUIDE FITTING CHAFED. BLENDED CHAFED AREA AT LT OTBD FLAP GUIDE FITTING, REMOVING .022 OF MATERIAL WITHIN LIMITS IAW REO 601R-57-51-143.SDR A6WA201140017Cam · deformedRT OTBD FLAP VANE CAM FOLLOWER BEHIND CTR HINGE HAS DISPLACED METAL. REPAIRED TR OTBD FLAP VANE CAM FOLLOWER BY FEATHERING THE MUSHROOMED EDGE OF CAM FOLLOWER IAW SRM 51-12-00 AND REO 601R-57-53-19, REV D.SDR A6WA201040961Fitting · chafedOTBD FLAP ROLLER GUIDE FITTING (RT SIDE) HAS CHAFING DAMAGE, BLENDED CHAFED AREA AT RT OTBD FLAP GUIDE FITTING, REMOVING .028 OF MATERIAL WITHIN LIMITS IAW REO 601R-57-51-1453.SDR A6WA201040884Skin · chafedLT INBD FLAP, FLAP VANE HAS (3 EA) AREAS ON L/E WITH CHAFE DAMAGE WHERE VANE CONTACTS STOPS. REPAIRED CHAFED AREAS IAW REO 601R-57-52-004.SDR REXA201000285Skin · dentedA SINGLE INDENTATION WAS FOUND ON THE LEFT WING INBOARD FLAP LOWER SURFACE FORWARD OF THE AFT SPAR AT WS = 136. THE DAMAGE IS RECORDED AS 3.0 INCHES LONG BY 2.85 INCHES WIDE WITH A MAXIMUM DEPTH OF 0.027 INCH. THE DISCREPANCY IS LOCATED 11 INCHES INBOARD FROSDR SWAA107420Flap · delaminatedDURING SCHEDULED 16Y CHECK, FOUND RT WING I/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.SDR SWAA107415Flap · delaminatedDURING SCHEDULED 16Y CHECK, FOUND LT WING I/B EDGE AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER SRM.SDR SWAA107388Flap · delaminatedDURING SCHEDULED 16Y CHECK, FOUND LT WING AFT FLAP I/B EDGE DELAMINATED. REPAIRED AFT FLAP PER SRM.SDR SWAA107358Skin · puncturedDURING SCHEDULED 16Y CHECK, FOUND LT WING I/B FORE FLAP PUNCTURED LOWER SURFACE. REPAIRED FORE FLAP PER SRM.SDR SWAA107357Skin · delaminatedDURING SCHEDULED 16Y CHECK, FOUND RT WING O/B FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FORE FLAP PER SRM.SDR CALA2010120100599Skin · wornSUPPORT TASK - RT OTBD MIDFLAP, INBD L/E WORN. MARKED, TRIMMED OUT DAMAGED AREA AND INSTALLED FILLER AND DOUBLER IAW E CRA 5752-01496.SDR SWAA107500Flap · delaminatedDURING SCHEDULED 2HC2 CHECK, FOUND RT WING O/B TRAILING EDGE FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.SDR SWAA107499Flap · delaminatedDURING SCHEDULED 2HC2 CHECK, FOUND RT WING O/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.SDR SWAA107498Flap · delaminatedDURING SCHEDULED 2HC2 CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR QXEA2010120200834Skin · chafedC2 CHECK - LT OTBD FLAP UPPER SKIN IS CHAFED BETWEEN WING STA Y209.00 AND Y281.00. BLENDED AREA IAW SRM 57-52-30-02-01. MIN THICKNESS REMAINING .029" REF NTM 51-00-02-250-801. CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-01-250-801. FOUND TO BE WITHIN SDR QXEA2010120100832Flap Track · chippedC2 CHECK - RT WING NR3 LOWER FLAP TRACK HAS AN AREA OF CHIPPED/MISSING TUNGSTEN COATING. REMOVED ALL LOOSE MATERIAL FROM MARKED LOCATION (ON TOP SURFACE, AFT END) AND POLISHED AREA TO REMOVE ALL SHARP EDGES IAW RD 8/4-57-1468. CONFIRMED CRACK FREE CONDITION SDR FDEA201011304524Skin · crackedLT WING INBD AFT FLAP HAS CRACK ON LOWER SKIN AT FASTENER, WBL 203. REMOVED 6 EA FASTENERS AT AREA LT WING INBD AFT FLAP LOWER SKIN IAW SRM 51-30-2. FABRICATED REPAIR PLATE IAW SRM 57-50-4, FIG 5 AND INSTALLED REPAIR PLATE IAW SRM 51-30-2 AND 57-50-4, FIG 5SDR SWAA107316Flap · delaminatedDURING SCHEDULED HC2 CHECK, FOUND LT WING OVERHEAD AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA107313Flap · delaminatedDURING SCHEDULED MV1 CHECK, FOUND LT WING O/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.SDR DALA1034451701Skin · damagedUPPER SKIN DAMAGE LT WING AFT MAIN FLAP 8 " FROM INBD SIDE. REPAIRED IAW SRM 57-53- 01 REPAIR 1 AND SRM 51-70-10.SDR QXEA2010113000824Flap Track · chippedC2 CHECK - LT WING NR3 LOWER FLAP TRACK HAS AREAS OF CHIPPED/MISSING TUNGSTEN CARBIDE COATING. REMOVED ALL LOOSE MATERIAL FROM MARKED LOCATIONS (ON TOP SURFACE, AFT END) AND POLISHED AREA TO REMOVE ALL SHARP EDGES IAW RD 8/4-57-1468. CONFIRMED AFFECTED AREA SDR YENA20101129163Rod · brokenFLT 435 BOS-MCO, CREW REPORTED IN LEVEL FLIGHT A/C BANKED 5-10 DEGREES WITH AUTO PILOT ENGAGED. ON FLIGHT CONTROL PAGE LEFT OUTER AILERON INDICATES UP AND RIGHT OUTER AILERON DOWN. TRIM ROLL AND YAW CENTERED TRIM BALL CENTERED. THRUST ON BOTH ENGINES SYMMETSDR A6WA201040875Skin · gougedLT INBD FLAP L/E PANELS 584AB AND 584BB ARE GOUGED, BLENDED OUT GOUGES ON FLAP PANELS IAW SRM 51-21-00.SDR A6WA201040874Skin · chafedL/E OF FLAP FAIRING 697BB IS CHAFED. BLENDED AREA IAW SRM 51-12-00.SDR CNMA20100033Skin · dentedBIRD STRIKE ON RT WING OTBD FLAP LOWER SURFACE OTBD OF INBD FLAP VORTELON BY 42" AND 10" FROM T/E WITH SURFACE CRACK 9" PARALEL TO SEAM. DENT AREA 5" RND. R & R RT OTBD FLAP IAW MM 27-11 & SB 767-27A0155.SDR IPXA0B63695Skin · puncturedRT INBD MID FLAP LOWER SKIN HAS 2 PUNCTURES. FIRST PUNCTURE IS .2500" DIA AND 2.2500" FROM T/E, 69.5" FROM INBD EDGE. SECOND PUNCTURE IS .2500" DIA 4.2500" FROM T/E AND 69.5" FROM INBD EDGE. REMOVED DAMAGE AND REPAIRED IAW EO B747-5750-40625-A.SDR IPXA0B63694Structure · damagedRT OTBD FORE FLAP DAMAGED. REPAIRED IAW EO B747-5750-40626-A.SDR IPXA0B63693Structure · damagedRT INBD MID FLAP HAS .3750 HOLE LOCATED 11.3750 FROM T/E AND 19.2500 FROM INBD EDGE. REMOVED DAMAGE AND REPAIRED IAW B747-5750-40625-A.SDR UALA2010112904377Skin · delaminatedRT WING OTBD FLAP LOWER SKIN DELAMINATED AND SEPARATED FROM FWD SPAR AT RIB 10. DAMAGE IS APPROX 7 AND 1-2 INCHES LONG AND 3 INCHES WIDE. LOCATION IS FROM 1 AND 1-2 INCHES INBD OF RIB 10, EXTENDING 6 INCHES OTBD OF RIB 10 AND IS 3 INCHES FROM LOWER SKIN FWDSDR CALA2011031500140Support Fitting · corrodedSUPPORT TASK LT WING NR 2 FLAP TRACK MOUNT HOLES SPOT FACE HAS SURFACE CORROSION UPPER SIDE. REMOVED AND REPLACED FLAP TRACK SUPPORT FITTING REF BOEING DWG 65C80736, SOPM 20-50-19, AND SRM 51-40-02.SDR FOTR2019813376Skin · corrodedCORROSION ON RT OTBD FWD FLAP. REMOVED DAMAGE, SANDED, CLEANED PREPPED AREA IAW SRM 51-40-20. FABBED DOUBLES FROM 2024-T3 .020" PO 9009917, APPROX 12" X 3". HOT BONDED DOUBLER TO PREPPED AREA IAW SRM 51-40-20. CLEANED, SEALED AND FINISHED REPAIR IAW SRM 51-40SDR IPXA0M63666Skin · damagedRT INBD FLAP DAMAGED ON LOWER SKIN. REPAIRED RT INBD FLAP IAW EOMD11-5750-40592-A.SDR FDEA201011224454Fairing · crackedRT WING FLAP FAIRING NR 672HB FWD EDGE ALUMINIUM HAS CRACK AT 5.00 POS CRACKED RT WING FLAP FAIRING NR 672HB R & R IAW SRM 51-40-02, REV 101. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR A6WA201040866Vane · chafedLT INBD FLAP VANE HAS CHAFING DAMAGE IN 3 PLACES ON L/E. R & R NEW SERVICEABLE TITANIUM CAPS ON LT INBD FLAP VANE L/E IAW SB 601R-57-022, REV B.SDR A6WA201040865Vane · chafedRT INBD FLAP ON L/E HAS CHAFING DAMAGE IN 3 PLACES. REMOVED AND INSTALLED NEW SERVICEABLE TITANIUM CAPS ON RT INBD FLAP VANE L/E IAW SB 601R-57-022, REV B.SDR DALA1033439853Hinge Fitting · crackedDURING M-CHECK FOUND RIGHT WING FLAP IN SIDE ACCESS HOLE O/B SIDE OF NR 4 FLAP HINGE SUPPORT ANGLE IS CRACKED AT UPPER ATTACH BOLT. REMOVED PER DC-9 SRM 51-30-02. REMOVED & INSTALLED FLAP HINGE IAW DC-9 SRM 51-30-01.SDR REXA201000268Skin · dentedLEFT INBOARD FLAP OUTER LOWER SKIN HAS TWO DENTS - GOUGE 0.500" X 1.500" X 0.030". PERFORMED A MAJOR REPAIR TO THE LEFT INBOARD FLAP OUTER LOWER SKIN IAW CRJ 200 SRM 57-52-00, INBOARD FLAP AND VANE - REPAIR 3 - NON-FLUSH REPAIR TO INBOARD FLAP SKIN.
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