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 IPXA13B77019Skin · dentedHAIL DAMAGE 2 AT DENTS. 1ST DENT IS 1" DIA 24" FROM INBD EDGE AND 11.25 ROM AFT EDGE. 2ND DENT IS 1.5 IN DIA 23.5 FROM INBD EDGE AND 1.5 FROM A FT EDGE. REPAIR IAW EO B747-5750-49759-A.SDR IPXA13B77018Skin · dentedRT OTBD T/E MID FLAP 2 DENTS UPPER SIDE 1ST DENT 1.1" IN DIA 6.5 " FROM T/E AND 39.5 FROM INBD EDGE 2ND DENT IS 1.0" IN DIA. 2.5" FROM T/E A ND 58" FROM INBD EDGE. REPAIRED IAW EO B747-5750-49759-A.SDR REXA2013021100101Vane · chafedRIGHT INBOARD FLAP VANE CHAFED WHERE VANE HITS THE STOPS. REPAIRED IAW SRM 51-25-00/51-40-11/51-42-13.SDR IPXA13B76991Skin · damagedLT WING OTBD MIDFLAP UPPER SKIN DAMAGED. REPAIRED IAW EO B747-5750-49751-A.SDR A6WA201340218802Flap · dentedLEFT I/B FLAP DENTED AT TRAILING EDGE FO PANEL 583BB. REPAIRED IAW BOMBARDIER REO 601R-57-52-2011.SDR A6WA2013021804667Structure · damagedLEFT I/B FLAP I/B AFT HINGE BOX MOUNT LUG DAMAGED. BLENDED LEFT I/B FLAP I/B AFT HINGE BOX MOUNT LUG IAW REO 601R-57-21-1863.SDR QXEA2013020600349Flap Track · corrodedRT NR 4 FLAP TRACK MOUNTING FLANGES FOR CANOE FAIRING HAVE BARE METAL AND POSSIBLE CORROSION. MATCH DRILLED FRONT INBD BRACKET SRM 51-40-07-02-01. MATCH DRILLED COLLAR IAW SRM 51-40-07-02-01. INSTALLED FRONT INBD BRACKET IAW SRM 51-42-05-02-01 AND 51-41-00-00SDR SWAA2013020812454Flap · delaminatedLEFT WING O/B FORE FLAP IS DELAMINATED (I/B TRAILING EDGE). REMOVED AND REPLACED LT WING O/B FORE FLAP PER M/M. TAG NO: 619784 P/N ON: 65C35703-29 S/N ON: 2504 P/N OFF: SN OFF: 2547SDR FDEA201302050270Vane · chafedRT WING OTBD T/E FLAP VANE, OTBD LOWER EDGE FOUND CHAFED. REPAIRED AS PER EA 1-5750-165191. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 116.SDR ASAA2013020593899Skin · dentedRT INBD AFT FLAP HAS DENT 22" FROM OTBD EDGE AND 1" UP FROM T/E UPPER SKIN. REPAIRED RT INBD AFT FLAP DAMAGE 22 FROM OTBD EDGE IAW SRM 51 70 10, REP 2, PG 201. (PERMANENT REPAIR).SDR ASAA2013020593894Skin · chafedLT OTBD FOREFLAP INBD L/E CHAFING ON REAR SPAR ACCESS PANEL. REMOVED, FABRICATED AND INSTALLED NEW L/E SKIN SECTION IAW SRM 51-40-05 AND 51-40-02.SDR UIEA2013021900100Structure · chafedRT WING L/E NR 18 VC FLAP LOWER EDGE FOUND CHAFING. REPAIRED IAW R1 NR 57-40-10152, REV A.SDR QXEA2013020500299Flap Track · corrodedRT NR 5 FLAP TRACK MOUNTING FLANGES FOR CANOE FAIRING HAVE BARE METAL AND POSSIBLE CORROSION. REMOVED CORROSION IAW SRM 51-21-00-00-02. REMOVED NUTPLATE TO FOM IAW SRM 51-42-15-02-01. REMOVED CORRODED MOUNTING FLANGES IAW SRM 51-42-05-02-01 AND 51-41-00-00-SDR ASAA2013020593864Skin · chafedRT OTBD FOREFLAP INBD L/E IS CHAFED. REPAIRED RT OTBD FOREFLAP INBD L/E IAW SRM 57-53-01, REPAIR 1.SDR SWAA2013020812445Skin · delaminatedRT WING I/B FORE FLAP UPPER SURFACE IS DELAMINATED 35" I/B FROM O/B END AND 8" FWD FROM T/E. REPAIRED RT/WING FORE FLAP UPPER SURFACE DISBOND, 35" FROM O/B END, 8" FROM T/E, IAW SRM 51-70-10-2R-0SDR SWAA2013020812444Skin · delaminatedLT WING I/B FORE FLAP UPPER SURFACE IS DELAMINATED 47" O/B FROM I/B END AND 8" FWD FROM T/E. REPAIRED LT/WING I/B FOREFLAP UPPER SURFACE DISBOND 47" FROM I/B END, 8" FROM T/E IAW SRM 51-70-10-2R-0SDR AALA20130204003Skin · dentedFOUND A LARGE DENT TO THE LEFT AFT FLAP UPPER SKIN LOCATED 55 INCHES FROM THE INBOARD EDGE AND 3.5 INCHES FROM THE TRAILING EDGE. BONDED DOUBLER OVER REPAIR AREA. PREPARED SURFACES, SEALED AND REFINISHED REPAIR PER SRM 51-70-10-2R.SDR DXTR20130207001Rib · crackedRT WING INBD FLAP, INBD T/E RIB IS CRACKED AT WS 64.073. COMPLIED WITH WING T/E RIB CRACK REPAIR IAW SRM 57-60-00 FOR RT INBD FLAP WELL RIB T/E.SDR DXTR20130206002Rib · crackedLT INBD FLAP INBD RIB CRACKED AT WS 64.073. COMPLETED REPAIR OF WING T/E RIB CRACKS IAW SRM 57-60-00 FOR LT INBD FLAP WELL RIB T/E.SDR USAA2013020400012Bracket · crackedC2 CHECK - CRACK ON RIGHT WING OUTBOARD TRAILING EDGE FLAP, INBOARD END RIB, NR 2 STIFFENER BRACKET AT OTEF STA 3.75. REPLACED RIGHT WING OUTBOARD TRAILING EDGE FLAP, INBOARD END RIB, NR 2 STIFFENER BRACKET IAW EA 504963.SDR IPXA3676938Skin · crackedRT OTBD FLAP, OTBD END L/E SKIN PANEL CRACKED AND DEFLECTED. REPAIRED IAW EO B767-5750-49506-B.SDR UALA2013020400685Skin · dentedLEFT WING TRAILING EDGE FLAP, AFT FLAP SEGMENT LOWER SURFACE HAS TWO DENTS WITH DELAMINATION ONE INCH APART. COMPLIED WITH ECRA 5753-01479. DAMAGE WAS REPAIRED.SDR UALA2013020400636Skin · dentedRIGHT WING I/B FLAP LOWER SURFACE 25 INCH OF O/B EDGE AND 2. 5 FWD OF T/E HAS SMALL DENT. MAJOR REPAIR ACCOMPLISHED. EVALUATED DAMAGE ON RT WING I/B FLAP LWR SKIN & FOUND TO BE OUT OF LIMITS SRM 57-53-01, REMOVED DAMAGE VERIFIED MATERIAL & FABRICATED DOUBLERSDR REXA2013020300084Skin · dentedMAINTENANCE FOUND A DENT ON THE RIGHT INBOARD FLAP UPPER SURFACE AT WS 120.00. THE DENT MEASURES 3.2" LONG X 3.1" WIDE X .055" DEEP. REPAIRED IAW EA CRJ257-01259 AS APPROVED BY 8110-3 DATED JANUARY 30, 2013.SDR SPUY201302020007Flap Track · corrodedDURING ROUTINE C-CHECK INSPECTION, LT WING LOWER SURFACE INBD FLAP TRACK COUPLING SHOWS CORROSION WS 304.0, REF N/R 0250.SDR ASAA2013020193871Skin · dentedLEFT WING INBD FOREFLAP LOWER SURFACE IS DENTED AT CENTER OF FLAP REPAIRED LT WING INBD FOREFLAP LOWER SURFACE.SDR ASAA2013020193835Structure · chafedRT W6 OTBD FOREFLAP INBD L/E IS CHAFED. REMOVED, FABRICATED AND INSTALLED NEW L/E SECTION IAW SRM 51-40-05 AND 51-40-02.SDR SWAA2013020812468Attach Angle · cracked(RIGHT WING) TRANSVERSE WEB ATTACH ANGLE CRACKED AT MAIN FLAP PROGRAM ROLLER SUPPORT ARM ATTACH POINT. REMOVED AND REPLACED CRACKED ATTACH ANGLE AT TRANSVERSE WEB AT MAIN FLAP PROGRAM ROLLER SUPPORT ARM PER SRM 51-10-02-0G-0 & SRM 51-40-02-0G-SDR SWAA2013020412308Spindle · corrodedNR 7 FLAP CARRIAGE SPINDLE HAS EVIDENCE OF CORROSION & FLAKED OUT OF THEMAL COATING. REMOVED AND REPLACED NR 7 FLAP CARRIAGE PER MT 327-51-08 NR 7 P/N OFF:65C34483-6SWA, S/N OFF:B6576 PN ON:65-46481-154WN, S/N ON:B5561.SDR DALA1302601610Skin · delaminatedLT WING INBD MAIN FLAP IS DELAMINATED AND REPAIRED IAW SRM 57-53-01, FIG 201 AND SRM 51-70-05, PAR 5A.SDR DALA1302591610Skin · delaminatedRT WING INBD MAIN FLAP L/E OTBD FAIRING IS DELAMINATED. REPAIRED IAW SRM 57-53-01, FIG 201 AND SRM 51-70-07, PAR 5A.SDR DALA1302581610Skin · dentedRT WING OTBD FLAP LWR SURFACE T/E INBD AREA IS DENTED. REPAIRED IAW SRM 57-53-01, FIG 201 AND SRM 51-70-07, PAR 5A.SDR R61A201301300095Bearing Support · corrodedWHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE RIGHT WING F6 TORQUE TUBE BEARING SUPPORT CORRODED. MAINTENANCE REMOVED AND REPLACED THE RIGHT WING F6 BEARING SUPPORT IAW EMB 170 AMM 27-51-03. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.SDR IPXA13177040Skin · damagedINSPECTION TYPE:1C, RT WING CENTER FLAP NOSE SKIN DAMAGED. ACCOMPLISHED REPAIR ON RT WING CENTER FLAP NOSE SKIN IAW SRM 57-50-00, FIG 208.SDR BJNA2013002050001Skin · damagedDURING A SCHEDULED A-18 CHECK, MECHANICS FOUND THE LT INBD FORE FLAP CONTAINING A LARGE HOLE WITH MISSING CORE HONEYCOMB STRUCTURE. THE DAMAGE DID NOT PROTRUDE THROUGH THE OTHER SIDE OF THE SKIN.SDR QXEA2013012900186Skin · chafedRT OTBD FLAP IS CHAFED BY THE SHROUD. BLENDED CHAFE DAMAGE IAW SRM 57-52-30-02-02. ULTRASONIC TESTING OF DAMAGED AREAS A, B, & C WITHIN LIMITS. TREATED AREAS IAW SRM 51-25-10-02-01.SDR QXEA2012012900188Flap Track · gougedRT NR 4 FLAP TRACK IS GOUGED ON THE INBD AND OTBD SIDES. BLENDED TRACK IAW SRM 57-50-50-02-01. ULTRASONIC THICKNESS TESTS GOOD. EDDY CURRENT INSP FOUND NO CRACKS.SDR QXEA2013012900191Flap Track · gougedLT NR 4 FLAP TRACK GOUGED ON INBD AND OTBD SIDES. BLENDED TRACK IAW SRM 57-50-50-02-01. PERFORMED ULTRASONIC THICKNESS TEST IAW SRM 57-50-50. ALL WITHIN LIMITS. EDDY CURRENT FOUND NO DEFECTS.SDR QXEA2013012900192Flap Track · gougedRT 3 LOWER FLAP TRACK IS GOUGED. POLISHED DAMAGED AREA TO BREAK SHARP EDGES IAW SRM 57-50-50. DAMAGE FOUND TO BE IN SACRIFICAL COATING ONLY IAW SRM 57-50-50-02-03.SDR SWAA2013020412260Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED FLAP TRACK FAIRING NR 3 OUTBOARD SIDE LEFT WING. REPLACED SUPPORT ANGLE LOCATED FLAP TRACK FAIRING NR 3 OUTBOARD SIDE LEFT WING IAW B737-300 SRM 51-10- 02 IAW B737-300 SRM 51-40-02 AND DRAWING 65C26309.SDR USAA2013021900021Strut · corroded3S CHECK - CORROSION ON RIGHT WING AFT FLAP INTERCONNECTING STRUT AT WS 181, RIB 8. REPLACED RIGHT WING AFT FLAP INTERCONNECTING STRUT AT WS 181, RIB 8 IAW A320 AMM 27-51-44.SDR ASAA2013012893893Skin · crackedLEFT WING OTBD FLAP L/E VORTEX GENERATOR INBD OF NR 2 FLAP TRACK, SKIN IS CRACKED AROUND PERIMETER. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW REO G15938, REV B AND EA CMPT-57EA-09791. PERFORMED HFEC OF CUTOUT IAW NTM 51-00-00 PG 6. NO CRACKS FOUNDSDR SWAA2013021112503Flap · delaminatedRIGHT I/B FORE FLAP LWR I/B SIDE HAS DELAMINATION. ACCOMPLISHED PERMANENT REPAIR 6"X6" ON RIGHT I/B FORE FLAP LWR I/B SIDE IAW B737 SRM 51-70-10 PAR 7 ,8, 9, 20, 22. APPLIED TOP COAT IAW B737 SRM 51-21-39.SDR SWAA2013021112502Skin · delaminatedRIGHT O/B TRAILING EDGE FLAP HAS DELAMINATION ON LWR TRAILING EDGE. ACCOMPLISHED PERMANENT REPAIR 4" DIA ON RIGHT O/B AFT FLAP LWR SKIN TRAILING EDGE IAW B737 SRM 57-53-01, SRM 51-70- 10 REPAIR 2.SDR SWAA2013020712363Fitting · corrodedLEFT O/B FLAP INBOARD TRACK INSPAR ATTACH POINT HAS CORROSION IN BOLT HOLE AND CORRODED HARDWARE. REMOVED AND REPLACED: LEFT WING O/B FLAP, INBOARD TRACK, ATTACH FITTING IAW B737 SRM 51-40-02, 51-40-05, B737 AMM 28-11-00 AND B SOPM 20-50-03.SDR A6WA2013020500670Beam · gougedLEFT I/B FLAP VANE SLIDING BEAMS ARE GOUGED UNDER UPPER AD LOWER ROLLERS. REPAIRED PER REO 601R-57-52-1979.SDR A6WA2013020504668Bracket · chafedLEFT WING TE FLAP VANE MOUNTING BRACKET IS CHAFED AND ON IN FRONT THE I/B EDGE. REMOVED CHAFED DAMAGE BY EDGE BLENDING.SDR UIEA2013013100049Flap Track · damagedNR 12 FLAP TRACK DAMAGED RT OTBD MID FLAP. NEW TRACK INSTALLED WITH INSTALLATION OF SERVICE MID FLAP ASSY, REF ITEM NR 7 IAW AMM 27-51-04-401.SDR UIEA2013013100053Flap · damagedREMOVE RT OTBD MID FLAP DUE TO DAMAGE. REMOVED RT OTBD MID FLAP IAW AMM 27-51-04. INSTALLED SERVICEABLE RT OTBD MID FLAP IAW AMM 27-51-04. OPS CHECK NORMAL IAW MM 27-51-04.SDR UIEA2013013100058Carriage · lack of lubeRT WING OTBD FLAP, LUBE BOTH INBD AND OTBD MID FLAP CARRIAGES. (LUBED BOTH INBD AND OTBD CARRIAGES OF OTBD FLAP RT WING IAW AMM 12-21-20-643-001.)
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