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 A6WA201140400Plate · chafedRT INBD FLAP INBD LUG PLATE CHAFED ON INBD AND OTBD SIDE. REPAIRED RT INBD FLAP INBD LUG PLATE ON INBD AND OTBD SIDE IAW REO 601R-57-52-1536 AND 601R-57-52-1708.SDR ZZDA2011474Vane · dentedRIGHT AFT MOVEABLE VANE, DENTED. ACCOMPLISHED MOVEABLE VANE FILLER AND DOUBLER REPAIR PER B717 SRM 57-53-01 REPAIR 1 AND B717 SRM 51-70-02 REPAIR 3.SDR VNAA2011051200005Skin · dentedDURING SCHEDULED MAINTENANCE REPAIRS WERE MADE TO A DENT ON THE LEFT INBOARD FLAP SKIN AT WS 55. INSPECTION AND REPAIR WAS ACCOMPLISHED USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.SDR A6WA201140402Skin · chafedRT INBD FLAP VANE L/E CHAFED. EVALUATED, BLENDED, ALODINED, PRIMED AND TOP COATED IAW REO 601R-57-52-004.SDR A6WA201140404Skin · chafedLT INBD FLAP IN L/E CHAFED. EVALUATED, BLENDED, PRIMED, ALODINED AND TOP COATED IAW REO 601R-57-52-004.SDR IPXA11M66524Skin · dentedLT WING INBD FLAP UPPER SKIN DENTED. REPAIRED IAW SRM 57-00-01. REPAIR 1 AND EO MD11-5750-41731-B.SDR IPXA11666523Skin · dentedDENT NR 1 D449024 AND DENT NR 2 D449025 LT WING INBD AFT FLAP T/E WEDGE LWR SURFACE DENTS. REPAIRED BOTH DENTS USING ONE REPAIR IAW SRM 51-70-10-2R AND EO B767-5 750-41819-B.SDR IPXA11666522Skin · dentedD449026 DENT NR 3 LT WING INBD AFT FLAP T/E WEDGE LWR SKIN DENT REPAIR. REPAIRED IAW SRM 51-70-10-2R AND EO B767-5750-42592-A.SDR IPXA11666521Skin · dentedDENT 4 LT WING INBD AFT FLAP T/E WEDGE LWR SKIN REPAIR. REPAIRED IAW SRM 51-70-10-2R AND EO B767-5750-42593-A.SDR USAA2011060600010Strut · corrodedSAL - S4 - CORROSION ON INTERNAL CAVITY OF INTERCONNECTING STRUT AT LEFT WING AT WS 486 RIB 9. REPLACED INTERCONNECTING STRUT AT LEFT WING AT WS 486 RIB 9 IAW A319 AMM 27-51-44.SDR DALA1133663232Skin · puncturedRT WING INBD FLAP L/E PUNCTURED REMOVED DAMAGED SKIN AND CORE, FABRICATED INNER SKIN AND BONDED, FABRICATED CORE AND BONDED, FABRICATED REPAIR PLIES AND BONDED, SANDED SMOOTH TO CONTOUR, SEALED EXPOSED FIBERS, CLEANED AREA, APPLIED PRIMER AND PAINT, WORK PERFOSDR IPXA1M67065Vane · chafedINSPECTION TYPE:4C, LT INBD FLAP VANE UPPER SURFACE EXTERIOR CHAFE DAMAGE IN 3 LOCATIONS. REPAIRED LT INBD FLAP VANE IAW SRM 57-50-80, REPAIR 2 AND SRM 51-62- 01, PARA 9.SDR IPXA11M66859Skin · dentedINSPECTION TYPE:4C, LT INBD FLAP LOWER SURFACE HAS 14 DENTS WITH CRACK PRESENT. REPAIRED LT INBD FLAP LOWER SKIN APPROX STA XIFH 191 IAW EO MD11-5750-42851-A AND STASA EA 011-5753-01-A3120, REV IR.SDR SWIA201126224Vane · chafedRIGHT INBOARD FLAP VANE MID SPAN CHAFED TO LIMITS. (C-CHECK) REPLACED RIGHT INBOARD FLAP VANE PER SRM.SDR WRLA20110506478Support Fitting · crackedCRACK ON INBD HINGE SUPPORT OF LT OTBD T/E FLAP.SDR AALA20110506TUL03Skin · dentedLEFT WING FLAPS INBOARD FLAP HAS 2 EACH DENTS WITH SCRATCH IN BOTTOM SKIN CENTER AREA. FABRICATED FILLER AND DOUBLER AND INSTALLED FLUSH REPAIR AT CUT OUT PER SRM 57-01-00 FIGURE 5, SHEET.SDR A6WA201140477Bracket · chafedLT INBD FLAP INBD HINGE BOX HAS CHAFING TOP BRACKET INBD SIDE. R & R LT INBD FLAP INBD HINGE BOX INBD SIDE BRACKET IAW SRM 51-42-13.SDR UALA2011050602240Flap · damagedRIGHT OUTBD L/E MID FLAP AT INBD LOC OF NR 8 ARM FITTING. DMG IS A 4'X3' CUTOUT W- INBD L/E RIB CRACKED 1.5' FROM L/E. RT OB FOREFLAP LE IS DELAMINATED, 10" AREA MIDWAY ON FLAP. DAMAGE IS 10" X .75" 10 FEET FROM INBD END. ACTUAL DELAMINATED AREA IS 4"X.75".SDR UALA2011050502204Bushing · mismanufacturedNR 7 FLAP TRACK NEW SEQUENCE CARRIAGE FWD END TOGGLE ROLLER BUSHINGS ARE NOT REAMED. REPLACED SEQ CARRIAGE ROLLER BUSHINGS & FITTING, PUT NEW BUSHINGS IN THE PARTS BIN ABOVE DOOR 2 LT.SDR ASAA1179606Flap · delaminatedRIGHT WING OUTBOARD FLAP TRAILING EDGE FLAP INBOARD LOWER CORNER DELAMINATED. REMOVED DAMAGE FABRICATED REPAIR PARTS AND INSTALLED IAW B737 700 SRM 51 70 10 REPAIR 4.SDR DALA1131431701Fairing · delaminatedLT INBD MAIN FLAP L/E FAIRING FOUND DELAMINATED AND REPAIRED PER SRM 57-53-01 REPAIR 1 AND SRM 51-70-05 FIG 5.SDR UALA2011050502205Skin · delaminatedRIGHT O/B FOREFLAP L/E IS DELAMINATED, 10 INCH AREA MIDWAY ON FLAP. REFER TO SRM FOR ALLOWABLE DAMAGE. DAMAGE IS 10" X .75" 10 FEET FROM INBOAD END. ACTUAL DELAMINATED AREA IS 4"X .75". AREA WAS CLEANED AND SPEED TAPED.SDR UALA2011050502200Bushing · missingNR 8 FLAP CARRIAGE UPPER SEQ. CARRIAGE STOP IS MISSING THE O-B BUSHING. REINSTALLED NEW BUSHING.SDR UALA2011050502199Roller · out of toleranceNR 7 FLAP TRACK SEQUENCE CARRIAGE, INBD ROLLER IS MISSING AND THE O-B ROLLER IS INSTALLED BACKWARDS. REPLACED PER MM.SDR UALA2011050502198Arm · bentNR 7 FLAP TRACK O-B GUIDE ARM IS BENT. REPLACED GUIDE ARM.SDR UALA2011050402192Lever · bentRT OTBD FLAP, INBD ATTACH LEVER IS BENT. REPLACED RT OTBD FLAP INBD ATTACH LEVER WITH SERVICEABLE PART.SDR UALA2011050402185Skin · gougedLT WING INBD FWD FLAP FAIRING LOWER SURFACE HAS A GOUGE APPROX 3" LONG, 1-4" DEEP, EXTENDING INTO HONEYCOMB. REPAIRED PER GNMM 1-0-1-024.SDR IPXA1666372Skin · wornINSPECTION TYPE:C, RT WING OTBD T/E AFT FLAP UPPER SURFACE PANEL 688KT INBD FWD AREA FOUND WORN. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R, REPAIR 4, FIG 202, SHEET 1, REV 59.SDR HNAA2011051700135Flap Track · corrodedRT NR 2 FLAP TRACK HAS PITTING AND CORROSION ON MATING SURFACE AND HEAVY WEAR AND PITTING ON ROLLER SURFACE. R & R FLAP TRACK WITH NEW HARDWARE IAW AMM57-50-26.SDR IPXA1666366Skin · misrepairedINSPECTION TYPE:C, LT WING OTBD MID FLAP L/E MID AREA EXISTING REPAIR (NON STANDARD) REPAIR REDO. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A, FIG 5, REV 59.SDR IPXA1666308Skin · misrepairedINSPECTION TYPE:D, LT WING OTBD MID FLAP L/E MID AREA. NON STANDARD REPAIR. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A, FIG 5, REV 59.SDR DALA1130451817Fairing · delaminatedRT WING O/B FLAP I/B LEADING EDGE FAIRING WAS DELAMINATED AND REPAIRED PER SRM 57-53-01 REPAIR 1 TABLE 1 AND SRM 51-70-03 PAR 4A.SDR FDEA201105031707Stop Fitting · crackedLT WING T/E OTBD FLAP UP-STOP FITTING FOUND CRACKED, R & R IAW SRM 51-33-01, REV 46. FLAP OPS CHECK C/OUT IAW AMM 27-50-30-5, REV 69.2 FOUND SATISFACTORY.SDR FDEA201105031706Stop Fitting · crackedRT WING T/E OTBD FLAP UP-STOP FITTING FOUND CRACKED. R & R IAW SRM 51-33-01, REV 46. FLAP OPS CHECK C/OUT IAW AMM 27-50-30-5, REV 69.2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.SDR HNAA2011051700130Fitting · corrodedRT NR1 FLAP TRACK THROUGH BOLT FITTING IS CORRODED. R & R NECESSARY HARDWARE WITH NEW HARDWARE.SDR HNAA2011051700131Flap Track · corrodedRT NR 1 FLAP TRACK HAS CORROSION ON THE MATING SURFACE AND HEAVY WEAR AND PITTING ON THE ROLLER SURFACE. R & R FLAP TRACK WITH NEW HARDWARE IAW AMM 57-50-11.SDR SWAA113321Flap · delaminatedDURING SCHEDULED MV2 CHECK FOUND DELAMINATION LT OUTBD AFT FLAP. REMOVED AND REPLACED FLAP PER MM.SDR SWAA113262Skin · delaminatedDURING SCHEDULED SPV CHECK FOUND RT INBD FOREFLAP METAL BOND REPAIR (UPPER SURFACE) DELAMINATED. REPAIRED RIGHT I/B FOREFLAP PER SRMSDR DALA1130369875Vane · damagedI/B FLAP FIXED VANE THE AFT ATTACH POINT HAS METAL PEELING UP. REPAIRED DISCREPANT AREA ON I/B FLAP FIXED VANE IAW SRM 51-30-2 PAGE 1, SRM 51-70-2 PARAGRAPH 18(4) PAGE 91&92, SRM 57-50-9 PAGE 5 PER DWG PL591004, SRM 51-70-2 PARAGRAPH 26 PAGE 269-274, SRM 51-7SDR DALA1130071201Skin · debondedRIGHT I/B AFT FLAP LWR SURFACE IS DISBONDED AND REPAIRED PER SRM 51-70-10 REPAIR 2 FIG 203 AND SRM 57-53-01 REPAIR 1 FIG 201.SDR DALA1129721817Fairing · damagedRT WING O/B FLAP L/E NOSE FAIRING 666BT HAD A ELONGATED FASTENER HOLE AND WAS REPAIRED PER THE SRM 57-53-01 REPAIR 1 TABLE 1 AND SRM 51-70-03 FIG 10.SDR SWAA113190Flap · warpedDURING SCHEDULED 18Y CHECK, FOUND LT WING I/B FORE FLAP WARPED. REMOVED AND REPLACED FLAP PER MM.SDR IPXA1666392Fairing · misrepairedINSPECTION TYPE:C, LT WING INBD MID FLAP L/E INBD AREA EXISTING REPAIR (NON STANDARD) REDO. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A, FIG 5, REV 59.SDR IPXA1666391Skin · misrepairedINSPECTION TYPE:C, RT WING INBD FORE FLAP T/E LOWER SURFACE MID AREA EXISTING REPAIR (NON STANDARD REPAIR) REDO. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5C, FIG 2, REV 59.SDR SWAA113178Flap · delaminatedDURING SCHEDULED 2HC2 CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED FROM I/B END. REMOVED AND REPLACED AFT FLAP PER MM.SDR UIEA2011042600249Skin · damagedTHE PURPOSE OF THIS EO IS TO DOCUMENT A MAJOR REPAIR. DURING WALK-AROUND INSP, MX REPORTED LT OTBD MID FLAP - WBL 597 - WBL 730 - T/E - DELAMINATION/DAMAGE (PN: 65B01925-311C / SN: 000551) - T/E MEASURING 11.0 FT. X 7.5 IN. (REF FIGURE 1). (DISPOSITION WAS MASDR IPXA1666393Skin · misrepairedINSPECTION TYPE:C, RT WING INBD FORE FLAP T/E LOWER SURFACE INBD AREA EXISTING REPAIR (NON STANDARD) REDO. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A (1) FIG 5, REV 59.SDR IPXA1666390Skin · misrepairedINSPECTION TYPE:C, RT WING INBD FORE FLAP T/E LWR SURFACE INBD AREA EXISTING REPAIR (NON STANDARD) REDO. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5C, FIG 2, REV 59.SDR IPXA1666343Fairing · delaminatedINSPECTION TYPE:C, RT WING INBD FORE FLAP OTBD L/E FOUND DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A (1) FIG 5, REV 59.SDR IPXA1666342Skin · delaminatedINSPECTION TYPE:C, RT WING INBD FORE FLAP L/E OTBD FAIRING SKIN FOUND DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A, FIG 5, REV 59.
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