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 IPXA10163540Skin · gougedINSPECTION TYPE:10YR, LT WING CTR FLAP UPPER SKIN HAS REPAIR DOUBLER GOUGED. REPAIRED LT WING CTR FLAP UPPER SKIN IAW STA-SA, EA 300-5750-A2759, REV I/R AND UPS EO A300-5750-40453-A.SDR SWAA106494Flap · delaminatedDURING SCHEDULED SPV CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER MM.SDR SWAA106265Flap · delaminatedDURING SCHEDULED CV CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA106230Skin · delaminatedDURING SCHEDULED 12Y CHECK, FOUND LT WING O/B AFT FLAP LOWER SURFACE DELAMINATED. REPAIRED SKIN PER SRM.SDR SWAA106185Flap · delaminatedDURING SCHEDULED 16Y CHECK, FOUND RT WING O/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.SDR SWAA106184Flap · delaminatedDURING SCHEDULED 16Y CHECK, FOUND LT WING FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.SDR SWAA106178Skin · delaminatedDURING SCHEDULED 22Y CHECK, FOUND RT WING O/B FORE FLAP UPPER SKIN I/B DELAMINATED. REPAIRED SKIN PER SRM.SDR FDEA201010124014Carriage · misalignedRT WING T/E FLAP NR 5 FRONT CARRIAGE UPPER BRIDGE WAS FOUND SHIM MIGRATION. EA 6-2750-141636 REPAIR ACCOMPLISHED. GMM 6-2-100 REPAIR CLASSIFIED AS MINOR.SDR FDEA201010124013Carriage · misalignedRT WING T/E FLAP NR4 FRONT CARRIAGE UPPER BRIDGE WAS FOUND SHIM MIGRATION. EA 6-2750-141636 REPAIR ACCOMPLISHED THE REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201010124012Carriage · misalignedRT WING T/E FLAP NR3 FRONT CARRIAGE UPPER BRIDGE WAS FOUND SHIM MIGRATION. EA 6-2750-141636 REPAIR ACCOMPLISHED. THE REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201010124010Carriage · misalignedRT WING T/E FLAP NR 6 FRONT CARRIAGE UPPER BRIDGE WAS FOUND SHIM MIGRATION. EA 6-2750-141636 REPAIR ACCOMPLISHED. THE REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201010124009Carriage · misalignedRT WING T/E FLAP NR6 REAR CARRIAGE LEVER MOUNTING YOKE INBD SHIM MIGRATED. EA 6-2750-414636 REPAIR ACCOMPLISHED. THE REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201010124008Carriage · misalignedLT WING T/E NR 3 TRACK CARRIAGE UPPER BRIDGE INBD SHIM GOT MIGRATION. EA 6-2750-141636 REPAIR ACCOMPLISHED. THE REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR HALA2010101200462Skin · crackedRIGHT WING FLAP OTBD L/E CAP CRACKED DUE TO BIRD STRIKE. OK TO CONTINUE IAW M105 NR589043.SDR REXA201000195Skin · dentedLEFT OUTBOARD FLAP VANE HAD A DENT IN THE VANE LEADING EDGE SKIN APPROXIMATELY 9 INCHES FROM THE INBOARD EDGE AT WS 181.5. THE DAMAGE MEASURES 1.6 INCHES LONG BY 0.9 INCH WIDE WITH A MAXIMUM DEPTH OF 0.095 INCH. TEMPORARY REPAIR IAW STS ENGINEERING EA 5-2010SDR QXEA2010101400595Skin · chafedC4 CHECK - RT INBD FLAP LOWER SIDE CHAFED AROUND INBD FLAP HINGE BOX. BLENDED CHAFED AREA IAW SRM 51-21-06-001-001-A01 TO A MAX DEPTH OF .010" FOUND TO BE WITHIN LIMITS OF SRM 57-52-01-101-001-A01. MAXIMUM DEPTH ALLOWED IS .015". TREATED, PRIMED AND PAINTEDSDR SWAA106109Skin · delaminatedDURING SCHEDULED 22Y CHECK, FOUND RT WING O/B FORE FLAP SKIN DELAMINATED. REPAIRED SKIN PER SRM.SDR SWAA106103Flap · puncturedDURING SCHEDULED 22Y CHECK, FOUND RT WING I/B FORE FLAP PUNCTURED. REPAIRED FORE FLAP PER SRM.SDR REXA201000194Skin · dentedTWO DENTS WERE FOUND ON THE LEFT WING INBOARD FLAP UPPER SKIN. THE DAMAGES ARE LOCATED INBOARD OF WS = 121.5 AND APPROXIMATELY 4 INCHES FROM THE TRAILING EDGE FASTENER ROW. THE LARGER DENT MEASURES 1.86 INCHES BY 1.37 INCHES WITH A MAXIMUM DEPTH OF 0.020 INCSDR FDEA201010103983Skin · damagedLEFT WING T/E FLAP AT RIB 15 UPPER SURFACE HAS 3 EACH CHAFE MARKS. REPAIRED CENTRE FLAP UPPER SKIN USING DOUBLER REPAIR SCHEME IAW SRM 57-50- 00 PAGE 219 FIG 205.SDR SWAA106032Support · crackedDURING SCHEDULED 16Y CHECK, FOUND LT TRAILING EDGE FLAP ANGLE SUPPORT CRACKED. REMOVED AND REPLACED SUPPORT PER SRM AND BAC DWG.SDR SWAA106028Spindle · corrodedDURING SCHEDULED 20Y CHECK, FOUND RT WING O/B MID FLAP I/B CARRIAGE SPINDLE ENCLOSURE CORRODED. REMOVED AND REPLACED SPINDLE ENCLOSURE ASSY PER MM.SDR A6WA201040840Vane · chafedRT INBD FLAP VANE (MOVEABLE) IS CHAFED IN 3 LOCATIONS ON L/E CHAFED AREAS WERE BLENDED, TREATED AND FOUND TO BE WITHIN ALLOWABLE LIMITS IAW REO 601R-57-52-004, REV C.SDR A6WA201040842Vane · chafedLT INBD FLAP VANE (MOVEABLE) IS CHAFED IN 3 LOCATIONS ON L/E CHAFED AREAS WERE BLENDED, TREATED AND FOUND TO BE WITHIN ALLOWABLE LIMITS IAW REO 601R-57-52-004.SDR SWAA106062Flap · delaminatedDURING SCHEDULED MV1 CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR DALA1025795810Skin · puncturedDURING "L" CHECK FOUND PUNCTURE IN UPPER SKIN OF LT WING T/E INBD AFT FLAP. REPAIRED IAW SRM 51-70-17 3F, 3G, 4B, PAGES 16-55, FIG 24.SDR A6WA201040844Guide · chafedLT WING OTBD FLAP ROLLER GUIDE CHAFED. C/W REO 601R-57-51-143, REV NC.SDR A6WA201040841Guide · chafedRT OTBD FLAP ALIGNMENT GUIDE (FLAP SIDE CHAFED) AND ROLLER IS STIFF AND CRUNCHY C/W REO 601R-57-53-832.SDR A6WA201040843Fitting · chafedRT OTBD FLAP ALIGNMENT FITTING CHAFED, C/W REO 601-57-51-143, REV NC.SDR A6WA201040768Attach Fitting · chafedLT OTBD FLAP ROLLER ATTACH FITTING CHAFED. REPAIRED IAW REO 601R-57-53-883 REV.SDR SWAA105991Flap · delaminatedDURING SCHEDULED HC2 CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER SRM.SDR SWAA105931Flap · puncturedDURING SCHEDULED 22Y CHECK, FOUND LT WING I/B FORE FLAP PUNCTURED. REPAIRED FORE FLAP PER SRM.SDR FDEA201010063953Rib · crackedFASTENER HOLES WERE FOUND CRACKED AT RIB25A OF LEFT WING INBD FLAP IAW EO E6-5750-7-5003, PT1. THE REPAIR CLASSIFIED AS MINOR GMM 6-2-100.SDR SWAA105862Flap · delaminatedDURING SCHEDULED 20Y CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER SRM.SDR SWAA105861Skin · delaminatedDURING SCHEDULED 22Y CHECK, FOUND LT WING AFT FLAP UPPER SKIN DELAMINATED AT O/B END. REPAIRED AFT FLAP PER SRM.SDR SWAA105856Flap · delaminatedDURING SCHEDULED 16Y CHECK, FOUND LT WING FORE FLAP DELAMINATED AT I/B END. REPAIRED FORE FLAP PER SRM.SDR FDEA201010043901Skin · gougedLT INBD FORE FLAP LE IS GOUGED AT WBL 237. CUTOUT DAMAGED AREA DIM: 1 1/8" X 1 5/8" IAW B727 SRM 51-10-1 AND FABRICATED DOUBLER FROM 2024T3 .063 DIM: 5 3/8" X 4" IAW SRM 57-50-4 FIG 1 AND INSTALLED DOUBLER IAW SRM 51-30-2.SDR REXA201000185Skin · damagedLEFT AND RIGHT INBOARD FLAP VANES HAD WEAR DAMAGE ON THE LEADING EDGE SKINS AT THREE LOCATIONS PER SIDE. THE DAMAGE LOCATIONS OCCURRED AT WS = 56.3, WS = 89.0 AND WS = 139.0.THE AFFECTED COMPONENTS ARE AS FOLLOWS: LEFT INBOARD FLAP: P/N 601R14002-1, SERIAL NUSDR FDEA201010023870Skin · delaminatedFOUND 2EA AREAS OF DELAMINATION ON RT OUTBOARD FLAP TRAILING EDGE, ONE AREA WAS 4"L X .78"W X .093" D. THE SECOND AREA WAS 1.34"L X 1.28"W WITH A BULGE OF .50" ON THE TOP SIDE OF THE SKIN. BOTH AREAS WERE ON THE TOP SKIN OF THE TRAILING EDGE BETWEEN RIB 2 ANSDR DALA1024953129Trunnion · damagedDURING L-CHECK FOUND WEAR AND CHAFE DAMAGE TO RIGHT INBOARD WING FLAP TRUNNION. REPLACED PER CMM 57-52-51, COMPLIED WITH ERA 484249-14AD.SDR IPXA10163295Skin · gougedINSPECTION TYPE:10YR, LT WING CTR FLAP UPPER SKIN REPAIR IS CHAFED. REPAIR SURVEY NR139-W3-01. ACCOMPLISHED REPAIR ON LT WING CTR FLAP UPPER SKIN IAW EA 300-5750-01-A2726 I/R.SDR ZZDA2010475Skin · dentedRIGHT INBOARD AFT FLAP SKIN, DENTED. ACCOMPLISHED FLAP SKIN COMPOSITE REPAIR PER B737 SRM 51-70-10.SDR FDEA201010013851Skin · crackedTHE LT WING OTBD FLAP , SECOND FROM INBD WEDGE SEGMENT UPPER SKIN, HAS AN APPROX 2" LONG CRACK IN THE FWD MID SECTION AT APPROX STA OF 565.SDR FDEA201010013849Skin · damagedLEFT OUTBD FLAP UPPER SKIN IS DAMAGED, LOCATED OUTBD OF CENTER HOIST POINT. REMOVED AND REPLACED LEFT OUTBD FLAP UPPER SKIN IAW SRM 51-31-01 AND SRM 57-10- 00, MAJOR REPAIR, THIS IS CLASS B REPAIR AND REQ. REPECTIVE INSP IAW SRM 57-10-00 FIG. 7, SHEET 2.SDR DALA1026029868Vane · dentedDURING M-CHECK FOUND DENT IN RT CTR FIXED VANE ON UPPER SIDE. REPAIRED IAW SRM 57-50-09, SRM 57-03, SRM 51-70-2, SRM 51-10-3, AMMS 27-51-03 & AMM 27-61-06.SDR SWAA105845Skin · delaminatedDURING SCHEDULED 16Y CHECK, FOUND LT WING FORE FLAP UPPER SKIN O/B EDGE DELAMINATED. REPAIRED FORE FLAP PER MM.SDR SWAA105803Flap · delaminatedDURING SCHEDULED SPV CHECK, FOUND LT WING O/B AFT FLAP T/E DELAMINATED. REPAIRED AFT FLAP PER SRM.SDR SWAA105854Flap · delaminatedDURING SCHEDULED MV1 CHECK, FOUND LT WING O/B TRAILING EDGE AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP ASSY PER MM.SDR CA101018011Bracket · brokenRT INBD BRACKET, 31003-07, BRACKET REMPLACED, 4-57 DOUBLE INSP C/OUT. SYS TESTED OK. IN DESCENT, RT FLAP DIDN`T GO DOWN, THE PILOT THUS KEPT THE FLAPS UP FOR LANDING. RT INBD BRACKET WAS FOUND BROKEN. BRACKET REPLACED, RIVETING ACCORDING TO AC 4313-1B, PARSDR FDEA201009273738Skin · debondedRT OTBD FLAP - LOWER SKIN BTW RIB2 AND RIB3 FOUND DEBONDED. REPAIRED IAW E.A. 6-5750-144062.
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