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 FOTR201201282013Skin · debondedLWR INBD T/E OF RT WING OTBD AFT FLAP DISBONDED. REPAIRED ON FAS WO 21143, NR 36435.SDR FOTR0209201236446Skin · delaminatedLEFT WING INBD FLAP OTBD T/E DELAMINATED. REPAIRED ON FAS WO21143, NR 36446.SDR ZZDA2012122Skin · damagedRT WING INBOARD MAIN FLAP LOWER SURFACE, STA WS180, DENTED & GOUGED. ACCOMPLISHED MAIN FLAP LOWER SURFACE DOUBLER REPAIR PER B737 SRM 57-53-01, 51-20-01 AND 51-40-08, 51-40-02.SDR SWAA2012021701515Skin · delaminatedLT WING INBOARD FORE FLAP DELAMINATED. REPAIRED FORE FLAP IAW SRM.SDR IPXA2171654Skin · corrodedINSPECTION TYPE:10YR, LT WING OTBD FLAP UPPER SKIN UNDER THE STATIC WICK. RETAINER NEAR RIB 27A IS CORRODED. REPAIRED LT WING OTBD FLAP UPPER SKIN UNDER THE STATIC WICK RETAINER NEAR RIB 27A IAW STA-SA, EA 300-5750-01-A3679 AND EO A300-5750-45984-A.SDR FOTR0201201276387Skin · debondedLEFT WING T/E INBD FLAP ON THE UPPER SURFACE HAS 1 EA. REPAIR, REQUIRES EVALUATION. REPAIRED ON FAS WO 21143, NR 36387.SDR SWAA1201154Skin · delaminatedRT WING I/B FORE FLAP IS DELAMINATED AT O/B END UPPER SURFACE. REPAIRED FORE FLAP PER SRM.SDR REXA2012000160Skin · chafedLEFT INBOARD FLAP VANE LEADING EDGE CHAFED 3 PLACES: FLPS55, 103, 142. REPAIRED IAW BOMBARDIER REO 601R-57-52-004 REV C.SDR FDEA201201270356Skin · gougedLEFT INBD FLAP LOWER SURFACE OF L/E HAS A 3" LONG X .250" WIDE X .015" DEEP GOUGE BETWEEN THE 4TH AND 5TH RUB STRIP. SMOOTHED AND BLENDED GOUGE ON LT INBD FLAP IAW SRM 51-73-10. CHECKED LIMITS. OUT OF LIMITS IAW SRM 57-50-00 FIG 101. CUT OUT DAMAGE ON LT INSDR A6WA201240299Fitting · chafedCHAFING AT LEFT OTBD FLAP ROLLER FITTING. OPENSDR UALA2012012600552Wedge · dentedLT WING LT O/B FLAP T/E HAS LARGE DENT OTBD OF ENGINE. WEDGE IS REMOVED AND ROUTED TO SHOP 273, UNDER R29994. DAMAGE PRECISE LOCATION IS APPROX 20" OUTBOARD OF GAP SEAL ON TRAILING EDGE OF OUTBOARD FLAP, IN ZONE 2 AS IDENTIFIED IN FIGURE 101 OF SRM 57-53-00 SDR SWIA201229431Roller · brokenFLAP DISAGREEMENT. (FLT 5339) REPLACED BROKEN ROLLER ASSEMBLY FOR RIGHT OUTBOARD FLAPS.SDR SWAA120675Skin · delaminatedDURING SCHEDULED 16Y CHECK, FOUND RT WING I/B FORE FLAP UPPER SKIN DELAMINATED AT I/B END. REPAIRED FORE FLAP IAW MM.SDR SWAA120674Skin · delaminatedDURING SCHEDULED 16Y CHECK, FOUND RT WING I/B FORE FLAP SKIN DELAMINATED. REPAIRED FORE FLAP PER SRM.SDR SWAA120618Flap · delaminatedDURING SCHEDULED SPV CHECK, FOUND LT WING T/E I/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP IAW MM.SDR USAA2012020900002Skin · delaminatedC1 CHECK - AREA OF DELAMINATION ON RIGHT OUTBOARD FLAP UPPER SURFACE 4.5 INCHES FROM AFT EDGE & 161 INCHES FROM INBOARD END. REPAIRED RIGHT OUTBOARD FLAP UPPER SURFACE IAW B757 SRM 51-70-17.SDR SWAA120698Flap · delaminatedDURING SCHEDULED 2HC2 CHECK, FOUND RIGHT O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR IPXA12171523Skin · chafedINSPECTION TYPE:4C, LT WING CENTER FLAP UPPER SKIN REPAIR DOUBLER IS DAMAGED BETWEEN STR 2.6 AND STR 2.7 AND RIBS 21-23. ACCOMPLISHED REPAIR ON LT WING CENTER FLAP UPPER SKIN BETWEEN STR 2.6 AND STR 2.7 AND RIBS 21-23 IAW EO A300-5750-45820-A, PARA 6A.SDR IPXA12171522Skin · damagedINSPECTION TYPE:4C, LT CENTER FLAP UPPER SKIN PREVIOUS REPAIR DOUBLER IS DAMAGED BETWEEN STR 2.6 AND STR 2.8 AT RIBS 13 -15. ACCOMPLISHED REPAIR ON LT CENTER FLAP UPPER SKIN BETWEEN STR 2.6 AND STR 2.8 AT RIBS 13-15 IAW EO A300-5750-45815-A, PARA 6A.SDR IPXA12171521Skin · chafedINSPECTION TYPE:4C, RT WING CENTER FLAP UPPER SURFACE SKIN IS CHAFED IN 2 PLACES BETWEEN RIB 13 AND RIB 15 STR 2.6-2.8. ACCOMPLISHED REPAIR ON RT WING CENTER FLAP UPPER SURFACE SKIN BETWEEN RIB 13 AND RIB 15 AT STR 2.6-2.8 IAW EO A300-5750-45869-A, PARA 6A.SDR IPXA12171520Bullnose · chafedINSPECTION TYPE:4C, RT WING MID FLAP OTBD BULLNOSE IS CHAFED. ACCOMPLISHED REPAIIR ON RT WING MID FLAP OTBD BULLNOSE IAW SRM 57-50-00, PARA 4H, FIG 208.SDR IPXA12171519Bullnose · chafedINSPECTION TYPE:4C, RT WING OTBD FLAP INBD BULLNOSE IS CHAFED. ACCOMPLISHED REPAIR ON RT WING OTBD FLAP INBD BULLNOSE IAW SRM 57-50-00, PARA 4H, FIG 208.SDR NSVA2011414Repair · debondedLT FLAP UPPER SURFACE HAS PREVIOUS REPAIR, LOCATED IN T/E. COMPOSITE HONEY COMB UP TO AFT SPAR APROX STA 222.4 AREA IS 6" WIDE BY 5" IN LENGTH. CENTER OF REPAIR FAILS TAP AND DISBOND TESTS. REFERENCE CA-M6 #137723 SEQ 396 CONTROL #343-34.SDR QXEA2012012600101Flap Track · wornLEFT NR 3 LOWER FLAP TRACK, HORIZONTAL SURFACE HAS CARBIDE COATING WEAR. ACFT IS DOWN FOR C-CHECK. POLISHED LEFT NR 3 LOWER FLAP TRACK AND MEASURED REMAINING THICKNESS IAW RD 8/4-57-1511. MATERIAL LOSS WITHIN LIMITS, CONFIRMED AREA CRACK FREE REF RD 8/4-57SDR A6WA201240290Vane · chafedRIGHT INBD FLAP VANE HAS CHAFING ON L/E NEAR INBD, CTR & OTBD ACTUATOR SIDE BEAM HINGE FITTINGS. RIVET FOD UNDER L/E FROM PREVIOUS SHEET METAL WORK. BLENDED CHAFED AREA ON RT INBD FLAP VANE INBD, CTR OTBD ACTUATOR SLIDE BEAM HINGE FITTINGS FOUND TO BE WITHINSDR VNAA2012012300012Flap · dentedDURING SCHEDULED MAINTENANCE THE RIGHT INBOARD FLAP WAS FOUND DENTED. THE RIGHT INBOARD FLAP WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.SDR SWAA2012020901285Skin · puncturedLT WING I/B FORE FLAP LOWER SKIN PUNCTURED AT O/B OF I/B TRACK. REMOVED AND REPLACED FORE FLAP PER MM.SDR SWAA120538Flap · puncturedDURING SCHEDULED MV2 CHECK, FOUND RT WING I/B FORE FLAP PUNCTURED. REMOVED AND REPLACED FORE FLAP PER MM.SDR IPXA12571219Skin · puncturedRT OTBD FLAP LWR SKIN HAS 2 PUNCTURES. REPAIRED IAW EO B757-5750-45778-A.SDR IPXA12571209Skin · puncturedRIGHT OB T/E FLAP LWR SKIN PUNCTURE. REPAIRED IAW EO B757-5750-45779-A.SDR SWAA2012021601496Flap · delaminatedLEFT WING O/B TRAILING EDGE FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.SDR FDEA201201210290Skin · dentedLT WING INBD FLAP LOWER SURFACE DENT 1EA BETWEEN RIB9A-RIB10 AND STR 2.1-STR 2.2, APPROX D=0.5" & D=0.010". DENT OUT OF LIMITS IAW A300-600 SRM 57-50-00 FIG 101 P 107. CUTOUT DENT FABRICATED REPAIR DOUBLER 8.5X14.0 INCHES. LOCATED AND DRILLED AND INSTALLSDR UALA2012012300445Skin · wornLEFT WING NR 2 FLAP UPPER SURFACE SKIN OUTBOARD EDGE HAS A WORN SPOT. REPAIRED FLAP PER ECRA 5750-04419 ON SCAL LOG 9955553 DURING HMV 4 CHECK.SDR AALA20120120TUL15Wedge · damagedRIGHT INBOARD FLAP WEDGE HAS DAMAGE TO TOP INBOARD AND OUTBOARD EDGES. REPAIRED FLAP WEDGE PER SRM 51-70-06, AARD 51-00-00-014 AND EA MD80-57-021341.SDR QXEA2012012300019Skin · damagedLEFT INBD FLAP LOWER SKIN HAS 4 WORKING RIVETS APPROX MID FLAP. R & R 4 RIVETS IAW SRM 51-42-45-02-01.SDR QXEA2012012300018Skin · damagedLEFT INBD FLAP UPPER SKIN HAS 4 WORKING RIVETS NEAR OTBD END. R & R 4 RIVETS IAW SRM 51-42-45-02-01.SDR SWAA1201102Flap · delaminatedLEFT WING LOWER SURFACE OF O/B AFT FLAP DELAMINATED AT I/B END OF T/E. REPAIRED AFT FLAP PER SRM.SDR AALA20120126AFW03Flap · debondedRIGHT TRAILING EDGE OUTBOARD FLAP HAS SMALL DELAMINATION 172 INCHES FROM OUTBOARD END. ACCOMPLISHED HOT BONDED REPAIR PER SRM 57-53-01.SDR AALA20120126AFW02Flap · debondedRIGHT TRAILING EDGE OUTBOARD FLAP HAS SMALL DELAMINATION 80 INCHES FROM OUTBOARD END. ACCOMPLISHED HOT BONDED REPAIR PER SRM 57-53-01.SDR QXEA2012012300014Skin · chafedLT OTBD FLAP UPPER SKIN IS CHAFED BETWEEN STA YW-209.019 AND YW-281.019. SMOOTHED OUT CHAFED DAMAGE IN FLAP REF RD 8/4-57-1594. CONFIRMED CRACK FREE, MIN REMAINING THICKNESS .036" REF NTM 51-00-01-250-801, PT 6 AND 51-00-02-250-801 PT4. REPAIRED IAW RD 8/4-SDR QXEA2012012300013Skin · chafedRT INBD FLAP UPPER SKIN HAS AREAS OF CHAFING. SMOOTHED OUT AREAS OF CHAFE DAMAGE IAW RD 8/4-57-1595. MIN REMAINING THICKNESS .029", CONFIRMED CRACK FREE REF NTM 51-00-01-250-801 PT 6 AND 51-00-02-250-801 PT 4. COMPLIED WITH TASK RD 8/4-57-1209, PERMANENT RESDR QXEA2012012300012Skin · chafedRT OTBD FLAP UPPER SKIN HAS CHAFED PAINT BETWEEN STA YW-201.000 AND YW-281.019. BLENDED OUT CHAFED DAMAGE IAW RD 8/4-57-1594. CONFIRMED CRACK FREE REF NTM 51-00-02-250-801 PT 4 AND 51-00-01-250-801 PT 6. FLAP SKIN FOUND TO BE WITHIN LIMITS IAW RD 8/4-57-159SDR A6WA201240234Actuator · damagedLEFT INBD FLAP, LT INBD FLAP VANE ACTUATOR DAMAGE BLENDED DAMAGE AREA ON LT FLAP INBD, FLAP VANE ACTUATOR IAW SRM 51-12-00.SDR IPXA2B71279Wedge · delaminatedINSPECTION TYPE:C, LEFT WING OTBD AFT FLAP T/E WEDGE UPPER SURFACE OTBD AREA DELAMINATED. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A FIG 5, REV19.SDR IPXA2B71277Fairing · delaminatedINSPECTION TYPE:C, LT WING OTBD T/E MID FLAP INBD L/E FAIRING DELAMINATED. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A(1) FIG 5, REV 19.SDR SWAA120445Flap · delaminatedDURING SCHEDULED 2HC2 CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR IPXA2M71687Vane · chafedINSPECTION TYPE:4C, RT OTBD FLAP VANE IS CHAFING ON PANEL LANDING OTBD OF OTBD TRACK. REPAIRED RT OTBD FLAP VANE IAW EO MD11-5750-45951-A AND STA SA EA 011- 5750-01-A3650 REV IR.SDR AALA20120126AFW04Skin · debondedLEFT OUTBOARD FLAP, LOWER SURFACE JUST OUTBOARD OF MID CANOE DISBONDED. REMOVED DAMAGE AND REPAIRED AREA PER SRM 51-70-07-0G.SDR IPXA2B71278Fairing · puncturedINSPECTION TYPE:C, LT WING OTBD T/E AFT FLAP OTBD L/E FAIRING PUNCTURE HOLE. FIBERGLASS PREPREG LAY UP REPAIT CARRIED OUT IAW SRM 51-70-06, PAR 5D, FIG 6, REV 19.SDR SWAA1201125Flap · delaminatedRIGHT WING I/B FORE FLAP UPPER SURFACE IS DELAMINATED AT 35-INCH I/B OF O/B END. REPAIRED FORE FLAP PER SRM.
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