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 A6WA2010410691Fitting · gougedLT FLAP GUIDE FITTING PN 601R14526 IS CHAFED AND GOUGED. BLENDED LT OTBD FLAP GUIDE FITTING IAW REO 601R57-51-143 REV NC.SDR SWAA104514Flap · delaminatedDURING SCHEDULED HC2 CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA104513Flap · delaminatedDURING SCHEDULED HC2 CHECK, FOUND RT WING O/B TRAILING EDGE FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.SDR SWAA104341Flap · puncturedDURING SCHEDULED HC2 CHECK, FOUND LT WING I/B AFT FLAP PUNCTURED. REPAIRED AFT FLAP PER MM.SDR QXEA2010073000447Skin · chafedC CHECK - RT WING OTBD FLAP CHAFED THROUGH TOP COAT AT INBD END, UPPER SURFACE APPROX STA 192.0 TO 209.019. REMOVED CHAFE DAMAGE BY BLENDING IAW SRM 57-52-30-02-01, PARA 1-6B, STEPS 1-11. DIMENSIONS OF BLEND FOUND TO BE OUT OF LIMITS. HFEC AT BLENDED AREA SDR ASAA1048224Skin · chafedLEFT O/B FOREFLAP I/B END LEADING EDGE IS CHAFED. REMOVED LEADING EDGE SKIN AND INSTALLED NEW SKIN.SDR USAA2010080291555Flap · delaminatedCLT - Q5 - MAJOR REPAIR - DELAMINATION ON LEFT WING INBOARD FOREFLAP TRAILING EDGE WEDGE. REPAIRED LEFT WING INBOARD FOREFLAP TRAILING EDGE WEDGE IAW B737 SRM 57-53-02 & 51-70-10.SDR FDEA201007272684Skin · gougedRT INBD FORE FLAP GOUGED AT OTBD LOWER L/E SURFACE. CUT OUT DAMAGED AREA OF SKIN DIM. 1/2" X 1 1/2" IAW SRM 57-50-4 FIG1. FABRICATED REPAIR DOUBLER FROM 2024 T-3 .063" DIM. 3 7/8" X 4 1/2" IAW SRM 57-50-2 FIG 3 AND 57-50-4 FIG 1. INSTALLED REPAIR DOUBLER IASDR FDEA201007272685Skin · gougedLT INBD FORE FLAP GOUGED AT OUTBD LOWER LEADING EDGE SURFACE. REMOVED PREVIOUS REPAIR IAW SRM 51-30-2. FABRICATED REPAIR DOUBLER USING 2024 T-3, .063" X 5" X 5" IAW SRM 57-50-4 FIG 1 AND 57-50-2 FIG 3. INSTALLED NEW REPAIR DOUBLER IAW SRM 57-50-4 FIG 1 AND 51-SDR SWAA104318Flap · delaminatedDURING SCHEDULED HC2 CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR USAA2010082691811Rib · corrodedSAL - Q4 - MAJOR REPAIR - CORROSION ON RIGHT WING INBOARD MID FLAP INBOARD RIB AT WBL 71.24. REPLACED RIGHT WING INBOARD MID FLAP IAW JOB CARD 03C40927014.SDR USAA2010082691810Rib · corrodedSAL - Q4 - MAJOR REPAIR - CORROSION ON RIGHT WING INBOARD MID FLAP OUTBOARD RIB AT WBL 191. REPLACED RIGHT WING INBOARD MID FLAP IAW JOB CARD 03C40927014.SDR QXEA2010072700440Roller · damagedC5 CHECK - LT WING NR 4 FLAP TRACK INBD VERTICAL ROLLER SURFACE HAS SURFACE DAMAGE ALONG AN AREA APPROX 10" LONG AT AFT END, CAUSED BY INBD SIDE ROLLER CONTACT. BEGAN POLISHING THE DAMAGED AREA OF THE TUNGSTEN CARBIDE/COBALT COATING OF THE LT NR 4 FLAP TRACK SDR MALA100102Skin · dentedLT FLAP HAS 2 DENTS IN L/E AT INBD UPPER AREA. REPAIRED COMPOSITE DAMAGE ON LT FLAP L/E DENTS 1 AND 2 IAW EO S57060. THIS EO PROVIDES A GENERIC REPAIR FOR DENTS AND PUNCTURES IN WING FLAP ALUMINUM SKIN AND HONEYCOMB STRUCTURE IAW SRM 57-80-10, AND A COLD BONDSDR SWAA104278Flap · puncturedDURING SCHEDULED 8Y CHECK, FOUND RT WING I/B AFT FLAP PUNCTURED. REPAIRED AFT FLAP PER SRM.SDR SWAA104274Skin · puncturedDURING SCHEDULED OTS CHECK, FOUND RT WING I/B FORE FLAP PUNCTURED ON O/B EDGE ON THE UPPER SKIN. REMOVED AND REPLACED FORE FLAP PER MM.SDR IPXA10M62097Vane · damagedINSPECTION TYPE:4C, RT OTBD FLAP VANE HAS EDGE DAMAGE AT LWR OTBD END REMOVED DAMAGE, PERFORMED WET LAY-UP REPAIR IAW STA-SA EA011-5750-01-A2616, REV A AND EO MD11-5750-39209-B.SDR IPXA10M62071Vane · delaminatedINSPECTION TYPE:4C, RT INBD FLAP VANE DELAMINATED, SEPARATION AT T/E AND DISTORTED AT OTBD UPPER SURFACE. R & R RT INBD FLAP VANE WITH SERVICABLE UNIT.SDR ASAA1048218Skin · delaminatedLEFT O/B FLAP AFT FLAP I/B UPPER SURFACE DELAMINATED. REPAIRED FLAP.SDR ASAA1048148Skin · chafedRIGHT I/B FORE FLAP UPPER SURFACE PREVIOUS REPAIR CHAFED. REMOVED DAMAGED AREA AND INSTALLED DOUBLER REPAIR.SDR ASAA1048147Skin · delaminatedRIGHT I/B FORE FLAP UPPER SURFACE HAS DELAMINATION. REMOVED DAMAGED AREA AND INSTALLED DOUBLER REPAIR.SDR ASAA1048146Skin · delaminatedLEFT I/B FOREFLAP UPPER SURFACE HAS DELAMINATION ON EXISTING REPAIR. REMOVED DAMAGED AREA AND INSTALLED DOUBLER REPAIR.SDR ASAA1048145Skin · delaminatedLEFT I/B FORE FLAP UPPER SURFACE HAS DELAMINATION ON EXISTING REPAIR. REMOVED DAMAGED AREA AND INSTALLED DOUBLER REPAIR.SDR ASAA1048129Skin · chafedLEFT WING I/B AFT MID FLAP UPPER I/B SKIN CHAFED AT PREVIOUS REPAIR. REMOVED DAMAGED SKIN AND INSTALLED NEW REPAIR.SDR A6WA201040553Skin · chafedLT INBD FLAP VANE LOWER L/E SKIN CHAFED/GOUGED IN 3 PLACES JUST ABOVE ACTUATOR, DAMAGE COMING FROM BRIDGE BRACKET HARDWARE BEING TOO LONG (SCREWS TOO LONG) REPAIRED LT INBD FLAP VANE LOWER L/E SKIN IAW SRM 57-52-00, FIG 202.SDR A6WA201040552Skin · chafedLT INBD FLAP VANE LOWER L/E SKIN CHAFED AT FLAP STA 117.00 ABOVE OTBD ACTUATOR REPAIRED IAW SRM 57-52-00, FIG 202.SDR A6WA201040550Skin · chafedLT INBD FLAP MOVEABLE VANE L/E SKIN CHAFED, 3 AREAS LOCATED INBD CTR AND OTBD. REPAIRED IAW B/A REO 601R-57-52-004, REV C.SDR ASAA1048107Skin · gougedRIGHT WING O/B FORE FLAP IS GOUGED ON THE O/B END LOWER SURFACE. CUT OUT DAMAGE AND INSTALLED DOUBLER.SDR IPXA0162018Skin · gougedINSP TYPE:10YR RT INBD FLAP UPPER SKIN REPAIR DOUBLER IS GOUGED ACCOMPLISHED REPAIR IAW EO A300-5750-39205-A, PARA 6A.SDR IPXA10161857Skin · chafedINSPECTION TYPE:10YR, LT WING CTR FLAP UPPER SKIN CHAFED, APPROX 12" FWD OF RUB STRIP AND OTBD OF NR3 FLAP TRACK. ACCCOMPLISHED REPAIR IAW EO A300-5750-39128-A.SDR IPXA10M61539Vane · damagedINSPECTION TYPE:2C, LT WING INBD FLAP VANE T/E HAS A CHIP BETWEEN MIDDLE AND OTBD TRACKS. PERFORMED REPAIR IAW STA SA EA 011-5750-01-A2575, REV I/R AND AUTHORIZED BY EO MD11-5750-3900-A.SDR UIEA2010072100117Structure · crackedDURING A2 CHECK INSP DAMAGE WAS FOUND, RT WING INBD MID FLAPS CRACKED. PERMANENT REPAIRS ACCOMPLISHED IAW THE SRM 51-70-07 PAR 5A. THE REPAIRS ACCOMPLISHED IAW PART 1 ARE CATEGORY A AND WERE PERFORMED IAW SRM 51-70-07 PARA 5A.SDR IPXA10M61494Vane · damagedINSPECTION TYPE:2C, LT WING OTBD FLAP VANE OTBD LOWER EDGE HAS WEAR DAMAGE AND MISSING MATERIAL. REMOVED DAMAGE, FILLED AREA AND BONDED REPAIR PLIES IAW STA-SA EA 011-5750-01-A2559 I/R AND EO MD11-5750-38951-A.SDR USAA2010073091549Flap · delaminatedCLT - Q1 - MAJOR REPAIR - DELAMINATION ON RIGHT WING OUTBOARD FORE FLAP TRAILING EDGE WEDGE. REPLACED RIGHT WING OUTBOARD FORE FLAP IAW B737 AMM 27-51-37.SDR FDEA201007202604Angle · crackedRT WING T/E CENTER FLAP OTBD EDGE 1 EA ANGLE CRACKED. REMOVED THE DAMAGE ANGLE AND INSTALL BY NEW ONE IAW SRM 57-53-11. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201007202603Angle · crackedRT WING T/E OUTER FLAP INBD EDGE 1EA ANGLE CRACKED. REMOVED THE DAMAGED ANGLE AND INSTALL BY NEW ONE. IAW SRM 57-54-11 REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR SWAA104239Skin · delaminatedDURING SCHEDULED 16Y CHECK, FOUND RT WING AFT FLAP O/B SKIN DELAMINATED. REPAIRED SKIN PER SRM.SDR SWAA104227Skin · puncturedDURING SCHEDULED 12Y CHECK, FOUND RT WING I/B AFT FLAP LOWER SURFACED PUNCTURED. REMOVED AND REPLACED AFT FLAP PER SRM.SDR SWAA104217Flap · delaminatedDURING SCHEDULED 16Y CHECK, FOUND RT WING O/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.SDR SWAA104210Skin · delaminatedDURING SCHEDULED 14Y CHECK, FOUND LT WING O/B AFT FLAP INNER SKIN I/B CORNER DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR IPXA10561870Structure · chafedINSPECTION TYPE:C2, DURING INSP OF LT OTBD MAIN FLAP L/E INBD END, NOTED ADDITIONAL CHAFING IAW EO B757-5750-29979, STEP A (4). REPAIRED FLAP L/E IAW EO B757-5750-39142-A AND ATS ER NR10-3587.SDR IPXA10561310Attach Fitting · looseINSPECTION TYPE:C3, WHILE WORKING CLOSE, FOUND 672HB FWD INBD MOUNT FITTING LOOSE AT ATTACHMENT TO FLAP. REPAIRED IAW ER NR 10-3566 DATED 7-24-10.SDR FDEA201007192596Structure · crackedRT WING, INBD FLAP, MID FLAP, AFT CHORD IS CRACKED AT WBL 112. CUTOUT SECTION CHORD CRACKED AT RT WING INBD FLAP MIDFLAP WBL 112 DIM: 47.6250" IAW SRM 51-40-4, FIG 1 AND FABRICATED SECTION CHORD FROM BAC 1503100046 7075T6 DIM: 47.6250 " & SPLICE DIM: 8.5" IAW SDR USAA2010082591797Bolt · corrodedSAL - Q4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON 4 RETAINING BOLTS OF LEFT INBOARD MID FLAP CARRIAGE BETWEEN RSS135.23 TO RSS259.38. REPLACED 4 RETAINING BOLTS OF LEFT INBOARD MID FLAP CARRIAGE BETWEEN RSS135.23 TO RSS259.38 IAW JOB CARD 03C30927014.SDR USAA2010081991713Carriage · corrodedSAL - Q4 - MAJOR REPAIR - RIGHT INBOARD MIDFLAP OUTBOARD FLAP CARRIAGE OUTBOARD HALF WITH CORROSION IN THE EXTERNAL SURFACE OF THE AFT MAIN BEARING. REPLACED RIGHT INBOARD MIDFLAP ASSEMBLY IAW JOB CARD 03C40927014.SDR SWAA104184Spindle · crackedDURING SCHEDULED MV2 CHECK, FOUND RT WING NR 8 FLAP SPINDLE CRACKED. REMOVED AND REPLACED SPINDLE PER MM.SDR SWAA104183Spindle · crackedDURING SCHEDULED MV2 CHECK, FOUND RT WING O/B FLAP NR 7 CARRIAGE SPINDLE CRACKED. REMOVED AND REPLACED SPINDLE PER MT.SDR USAA2010082391750Flap · delaminatedSAL - Q4 - MAJOR REPAIR - DELAMINATION ON LEFT WING INBOARD FOREFLAP 7 INCHES FROM LEADING EDGE & 15 INCHES INBOARD END BETWEEN WBL 78 TO WBL 96. REPAIRED LEFT WING INBOARD FOREFLAP 7 INCHES FROM LEADING EDGE & 15 INCHES INBOARD END BETWEEN WBL 78 TO WBL 96 ISDR A6WA201040556Vane · chafedRT FLAP VANE HAS 3 AREAS OF CHAFING OTBD AND MID CHAFING POINTS IN LIMITS OF REO 601R-57-52-004, REV C. REPLACED INBD L/E IAW SRM.SDR SWAA104186Flap · delaminatedDURING SCHEDULED MV1 CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.
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