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 FY4Y20110315Splice · corrodedTHE EXFOLIATION CORROSION IS FOUND AT LT I/B MID FLAP CHORD SPLICE AT WBL 193 DURING 6C CHECK. THE ORIGINAL THICKNESS OF THE CHORD SPLICE IS 0.072”. AFTER BLENT OUT, THE DIMENSION OF THE CORROSION AREA IS 3" (LENGTH) X 1 (WIDTH) AND REMAINDER THICKNESS IS 0.SDR FOTR2102212539Skin · debondedRT INBD MID FLAP T/E UPPER OTBD END HAS AREA DISDOND. REMOVED DAMAGED AREA, SANDED, CLEANED AND PREPPED AREA IAW SRM 51-40-20, PARA NR 7, REPAIRED RT INBD MID-FLAP T/E WEDGE BY HOT BONDING REPAIR IAW SRM 51-40-20, PAR NR 20.SDR FOTR2102212487Wedge · debondedLT INBD FLAP T/E WEDGE, UPPER INBD END IS DISBONDED. REMOVED DAMAGED AREA, SANDED, CLEANED AND PREPPED AREA IAW SRM 51-40-20, PARA NR7, REPAIRED LT INBD MID FLAP T/E WEDGE BY OT BONDING DOUBLER IAW SRM 51-40-20, PARA NR 20.SDR FOTR2102212485Wedge · debondedRT INBD MID FLAP T/E WEDGE, LWR INBD NR 1 TRACK IS DISBONDED. REMOVED DAMAGED AREA, SANDED, CLEANED AND PREPPED AREA IAW SRM 51-40-20 PARA NR 7, REPAIRED RT INBD MIDFLAP T/E WEDGE LWR NR 1 TRACK AREA BY HOT BONDING REPAIR IAW SRM 51-40-20, PARA NR 20.SDR FOTR2102212339Skin · crackedLT WING OTBD FLAP, AFT FLAP HAS CRACK AT L/E, JUST INBD OF MOST OTBD TRACK. CUT OUT DAMAGED AREA DIM 1.2" X 1" ON LT WING OTBD FLAP L/E IAW SRM 57-50-4, FIG 9. FABRICATED REPAIR DOUBLER FROM 2024T3 .040 PO 90011142, DIM 7.1" X 7.3" AND FILLER DIM 1.2" X 1" FRSDR SWAA111806Flap · delaminatedDURING SCHEDULED 24Y CHECK, FOUND LT WING I/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA111782Flap · delaminatedDURING SCHEDULED 24Y CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA111743Skin · delaminatedDURING SCHEDULED 26Y CHECK, FOUND RT WING AFT FLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED AFT FLAP PER SRM.SDR SWAA111698Skin · delaminatedDURING SCHEDULED 20Y CHECK, FOUND RT WING O/B AFT FLAP O/B SKIN DELAMINATED. REPAIRED AFT FLAP PER SRM.SDR SWAA111697Skin · delaminatedDURING SCHEDULED 20Y CHECK, FOUND LT WING I/B AFT FLAP O/B SKIN DELAMINATED. REPAIRED AFT FLAP PER SRM.SDR SWAA111688Skin · delaminatedDURING SCHEDULED 20Y CHECK, FOUND RT WING FORE FLAP UPPER SKIN DELAMIINATED. REPAIRED FORE FLAP PER SRM.SDR SWAA111667Skin Panel · delaminatedDURING SCHEDULED 16Y CHECK, FOUND LT WING LOWER SKIN WEDGE PANEL I/B MID FLAP I/B END DELAMINATED. REPAIRED MID FLAP PER SRM.SDR SWAA111665Flap · delaminatedDURING SCHEDULED 16Y CHECK, FOUND LT WING I/B AFT FLAP O/B END DELAMINATED. REPAIRED AFT FLAP PER SRM.SDR SWAA111642Skin · puncturedDURING SCHEDULED 24Y CHECK, FOUND LT WING I/B FORE FLAP LOWER SKIN PUNCTURED. REPAIRED FORE FLAP PER SRM.SDR SWAA111621Flap · delaminatedDURING SCHEDULED 16Y CHECK, FOUND RT WING O/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.SDR SWAA111846Skin · delaminatedDURING SCHEDULED 12Y CHECK, FOUND LT WING OUTBOARD FLAP, LWR SKIN DELAMINATED AT INBOARD AFT CORNER. REPAIRED PER SRM.SDR FY4Y201103151Spar · corrodedTHE EXFOLIATION CORROSION IS FOUND AT LT INBD MID FLAP AFT SPAR LOWER CHORD AT WBL 82, DURING 6C CHECK. THE ORIGINAL THICKNESS OF THE CHORD IS 0.125". AFTER BLENT OUT, THE DIMENSION OF THE CORROSION AREA IS 3" (LENGTH) X 1" (WIDTH) AND REMAINDER THICKNESS ISSDR FY4Y197M20110315Skin · corrodedHEAVY CORROSION ON RT WING INBD MIDFLAP UPPER EXTERNAL SURFACE, AT WBL128, FWD OF FLAP T/E ABOUT 22.5". ORIGINAL THICKNESS IS 0.054" AFTER CORROSION REMOVE, REMAIN THICKNESS IS 0" IAW SRM 57-50-1, PAGE 8, AREA ABOUT 1" X 1.3750". REPAIR METHOD SRM 57-50-4, FSDR CA110316005Bushing · failed(CAN) DURING PERFORMANCE OF TASK CARD TOM 27-144-00-01, LT INBD FLAP, OTBD BALL SCREW & GIMBAL LUBRICATION & TOM 27-144-00-02, RT INBD FLAP, OTBD BALL SCREW & GIMBAL LUBRICATION. FOUND THAT THE LOWER GIMBAL BUSHING ASSEMBLIES ON BOTH LT & RT INBD FLAPS, WERE SDR USAA2011033191303Skin · debondedCLT - Q5/QX6 - DISBONDING ON RIGHT INBOARD FOREFLAP UPPER SKIN APPROX. 33.5 INCHES INBOARD FROM THE OUTBOARD END & 9 INCHES FORWARD OF THE AFT TRAILING EDGE. REPAIRED RIGHT INBOARD FOREFLAP UPPER SKIN IAW B737 SRM 51-70-10.SDR SWAA111908Skin · debondedDURING SCHEDULED 24Y CHECK, FOUND LEFT I/B FORE FLAP UPPER SKIN DISBONDED. REPAIRED FORE FLAP SKIN PER SRM.SDR SWAA111871Skin · delaminatedDURING SCHEDULED 16Y CHECK, FOUND DELAMINATION ON UPPER SKIN, OUTBOARD FORE FLAP. REPAIRED FLAP PER SRM.SDR SWAA111865Skin · crackedDURING SCHEDULED 16Y CHECK, FOUND CRACK ON RT WING LWR SURFACE OF INBOARD FORE FLAP. REPLACED FLAP PER MM.SDR UALA2011031001164Fairing · puncturedRIGHT OTBD FLAP, INBD FLAP CANOE AFT SECTION INBD SIDE HAS PUNCTURE. APPROX 6IN FROM FWD EDGE AND 1" IN LENGTH. ONLY THRU OUTER SKIN. CANOE IS HONEYCOMB STRUCTURE. TAP TEST AND VISUAL INSPECTION OF CRACK-PUNCTURE NR 5 CANOE FAIRING. WITHIN LIMITS PER SRM. TO BSDR MASA2011031102126Vane · damagedLEFT OTBD FLAP VANE DAMAGED. FERRY FLIGHT TO OKC, MX R2 FLAP VANE.SDR EE4Y20110138Vane · bulgedLT WING FLAP CTR FIXED VANE LOWER SKIN BULGED AT INBD AREA.SDR DALA1122631200Flap · delaminatedADF 008-ON WALK AROUND FOUND FOD ON LEFT WING O/B FLAP ASSY I/B SIDE. LEFT WING O/B FLAP I/B SIDE DELAMINATED AREA COMPOSITE REPAIR CARRIED OUT AS PER SRM 57-53-01, REPAIR 1, FIG 201 AND SRM 51-70-06 FIG 9.SDR IPXA11B65466Fairing · delaminatedINSPECTION TYPE:D, LT WING OTBD MID FLAP OTBD L/E DELAMINATION. COMPOSITE FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A, FIG 5, REV 17.SDR IPXA1565431Skin · delaminatedINSPECTION TYPE:C3, RT WING INBD MAIN FLAP HAS DELAMINATION ON UPPER SURFACE AT 11" FROM T/E, 103.5" FROM INBD END. REPAIRED DELAMINATED SKIN AND REPLACED CORE TO FULL DEPTH IAW SRM 51-70-07-0G.SDR SWAA111469Skin · delaminatedDURING SCHEDULED 26Y CHECK, FOUND LT WING I/B FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED SKIN PER SRM.SDR SWAA111468Skin · delaminatedDURING SCHEDULED 26Y CHECK, FOUND RT WING I/B FORE FLAP UPPER SKIN DELAMINATED. REPAIRED SKIN PER SRM.SDR A6WA201140248Panel · damaged(2) SCREW HOLES ON RT INBD FLAP L/E UNDER PANEL 684 JB ARE ELONGATED. REPAIR HOLES (2EA) ON RT INBD FLAP L/E UNDER PANEL NR 684 JB IAW REO 601R-57-52-1685.SDR DALA1122641200Skin · dentedLT WING I/B TRAILING EDGE AFT FLAP LOWER SURFACE FOUND DENT MARK. METAL HOT BOND REPAIR PERFORMED ON DENTED AREA AS PER SRM 57-53-01 REPAIR 1 FIG 201 AND SRM 51-70-10 REPAIR 4 FIG 201.SDR FDEA201103070902Skin · gougedRT WING INBD T/E FORE FLAP GOUGED, L/E LOWER SKIN NEAR OTBD END, APPROX WBL 240. REMOVED DAMAGED AREA, FABRICATED REPAIR DOUBLER, AND INSTALLED REPAIR DOUBLER AT RT WING I/B T/E FORE FLAP L/E LOWER SKIN NEAR O/B END IAW SRM 57-50-4 FIG 1, 51- 10-1, AND 51-SDR REXA201100169Vane · chafedLEFT INBOARD FLAP VANE HAS CHAFE DAMAGE AT THREE AREAS ON LEADING EDGE AT STOP CONTACT AREAS. REMOVED DAMAGE BY BLENDING (MATERIAL REMOVED APPROX 0.010"). REPAIRED IAW BOMBARDIER REO 601R-57-52-004 REV C.SDR REXA201100168Vane · chafedRT INBOARD FLAP VANE HAS CHAFE DAMAGE AT THREE AREAS ON LEADING EDGE AT STOP CONTACT AREAS. REMOVED CHAFE DAMAGE BY BLENDING AREAS (MATERIAL REMOVED APPROX .010"). REPAIRED IAW BOMBARDIER REO 601R-57-52-004 REV C.SDR REXA201100163AVane · chafedLEFT INBOARD FLAP VANE HAS CHAFE DAMAGE AT THREE AREAS ON LEADING EDGE AT STOP CONTACT AREAS. REMOVED DAMAGE BY BLENDING (MATERIAL REMOVED APPROX 0.010"). REPAIRED IAW BOMBARDIER REO 601R-57-52-004 REV C.SDR REXA201100162Vane · chafedRT INBOARD FLAP VANE HAS CHAFE DAMAGE AT THREE AREAS ON LEADING EDGE AT STOP CONTACT AREAS. REMOVED CHAFE DAMAGE BY BLENDING AREAS (MATERIAL REMOVED APPROX .010"). REPAIRED IAW BOMBARDIER REO 601R-57-52-004 REV C.SDR SWAA111383Skin · delaminatedDURING SCHEDULED 16Y CHECK, FOUND LT WING O/B AFT FLAP UPPER SURFACE DELAMINATED. REPAIRED AFT FLAP PER SRM.SDR IPXA1565827Support Bracket · damagedINSPECTION TYPE:C3, RT WING T/E - INBD MAIN FLAP - LOWER SURFACE - JUST INBD OF OTBD FLAP TRACK - FAIRING SUPPORT BRACKET HAS FRETTING DAMAGE. R & R BRACKET IAW ATS ER 11-01898.SDR USAA2011031191030Skin · debondedCLT - C3 - MAJOR REPAIR - DISBONDING ON LEFT WING OUTBOARD AFT FLAP AT INBOARD LOWER SURFACE. REPLACED LEFT WING OUTBOARD AFT FLAP IAW B737 AMM 27-51-39.SDR AALA20110305TUL07Skin · damagedRIGHT INBOARD MAIN UPPER SKIN HAS COUNTER BORED HOLES IN INNER SKIN AND CORE 11 INCHES OUTBOARD FROM INBOARD END OF FLAP. INSTALLED HOT BONDED DOUBLER REPAIR OVER COUNTER BORED HOLES PER SRM 51-70-10-2R2, ON INNER SKIN.SDR AALA20110305TUL06Skin · damagedRIGHT INBOARD MAIN FLAP UPPER SKIN HAS COUNTER BORED HOLES IN INNER SKIN AND CORE 134 INCHES OUTBOARD FROM INBOARD END OF FLAP. INSTALLED HOT BONDED DOUBLER REPAIR OVER POTTED COUNTER BORED HOLES PER SRM 51-70-10-2R2, ON INNER SKIN.SDR DALA1115869873Vane · delaminatedLEFT WING CENTER FIXED FLAP VANE DELAMINATED 0N IB END. REMOVED L/WING FLAP CENTER FIXED VANE IAW DC-9 MM 27-51-03. REPLACED FLAP FIXED VANE DUE TO DELAMINATION OUT OF LIMITS PER TRAVELER 2477NO1195. INSTALLED NEW SERVICEABLE VANE IAW DC9 MM 27-51-03. OPSSDR IPXA11566031Panel · gougedINSPECTION TYPE:C3, PANEL NR 666BR IS GOUGED ON INTERNAL SIDE (MARKED). REPAIRED IAW ATS ER 11-01823 DATED 4-8-11, EO B757-5750-42137, A DATED 4-11-11, DWG 113N3500, SRM 51-30-01, SRM 51-40-08.SDR A6WA201140191Plate · chafedLT INBD FLAP INBD HINGE LUG PLATE CHAFED. REPAIRED IAW REO 601R-57-15-3, TYPE 1, ZONE A.SDR IPXA11B65470Skin · delaminatedINSPECTION TYPE:D, LT WING INBD FORE FLAP L/E DELAMINATION. COMPOSITE FIBREGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A, FIG 5, REV 17.SDR IPXA11B65469Wedge · delaminatedINSPECTION TYPE:D, RT WING OTBD FORE FLAP UPPER T/E DELAMINATION. COMPOSITE FIBREGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A, FIG 5, REV 17.SDR IPXA11B65468Wedge · delaminatedINSPECTION TYPE:D, RT WING INBD AFT LOWER T/E DELAMINATION. COMPOSITE FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A, FIG 5, REV 17.SDR IPXA11B65467Fairing · delaminatedINSPECTION TYPE:D, LT WING OTBD MID FLAP L/E DELAMINATION. COMPOSITE FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A, FIG 5, REV. 17.
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