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 USAA2012062200010Flap · corroded2S CHECK - CORROSION ON OUTBOARD FLAP BETWEEN WS 670 TO WS 732 AT FLAP RIB 6. REPLACED OUTBOARD FLAP IAW A319 AMM 27-54-62-400-001-A & EA 104060.SDR DALA1237720910Skin · crackedRIGHT WING OTBD TRAILING EDGE FLAP, LEADING EDGE SURFACE CRACKED AT XW 251. FOUND REPAIR DOUBLER TO BE CRACKED, REMOVED DOUBLER AND ACCOMPLISHED ERA 503745-14 REV ORIGINAL DURING CPCP/PSV.SDR USAA2012061100009Wedge · delaminatedQ4 CHECK - DELAMINATION ON LEFT WING INBOARD AFT FLAP TRAILING EDGE WEDGE 29 INCHES FROM OUTBOARD END ON THE UPPER SURFACE. REPAIRED AFT FLAP TRAILING EDGE WEDGE IAW B737-400 SRM 51-70-10.SDR SWIA201230894Cap · damaged(C-CHECK) RIGHT FLAP VANE CENTER LEADING EDGE CAP IS DAMAGED. REPLACED PER SRM.SDR USAA2012060400025Flap · damagedC2 CHECK - CORE DAMAGE ON LEFT OUTBOARD FLAP OUTBOARD LOWER EDGE. REPAIRED LEFT OUTBOARD FLAP OUTBOARD LOWER EDGE IAW B737-400 SRM 51-70-10 REPAR 4 FIG 202.SDR ABXA20120601360Spar · corrodedRIGHT WING INBOARD FLAP MID SPAR WEB UPPER CORD IS CORRODED INSIDE RIGHT INBOARD MAIN FLAP AT WBL 97. REPAIRED CORRODED CORD IAW B767 SRM 51-70-12 FIG 1, ACFT WAS GROUNDED.SDR USAA2012060400024Flap · debondedC2 CHECK - DEBONDING ON LEFT WING TRAILING EDGE AFT FLAP AT OUTBOARD EDGE. REPAIRED LEFT WING TRAILING EDGE AFT FLAP AT OUTBOARD EDGE IAW B737 SRM 51-70-06 REPAIR 6 FIG 13.SDR SWAA2012060404550Flap · delaminatedRIGHT WING I/B MAIN FLAP DELAMINATED. REMOVED AND REPLACED MID FLAP PER EA.SDR USAA2012070200027Skin · corrodedQ4 CHECK - RIGHT OUTBOARD TRAILING EDGE MID-FLAP HAS MULTIPLE (3) AREAS OF CORROSION; 1"X1"X.002"; 1.5"X1"X.005"; 1.5"X1.5"X.006" ON UPPER LEADING EDGE SURFACE FROM WBL 262 TO WBL 400. REMOVED AND REPLACED MID-FLAP ASSEMBLY.SDR USAA2012062600007Spar · corroded3S CHECK - LEVEL 2 GALVANIC CORROSION ON LEFT WING FRONT SPAR OF OUTBOUND FLAP LEADING EDGE BETWEEN WS 7792 TO WS 8268, RIB 14 TO RIB 15. REPLACED LEFT WING FRONT SPAR OF OUTBOUND FLAP LEADING EDGE BETWEEN WS 7792 TO WS 8268, RIB 14 TO RIB 15 IAW A320 SRM 51-SDR DXTA2012060404983Skin · crackedFOUND LT FLAP SKIN CRACKED DURING MAINTENANCE. VISUALLY INSPECTED AND CLEANED AREA OF LT FLAP AT WS 251.18 AT FWD FROM T/E. 10X MAGNIFICATION REVEALED A HAIRLINE CRACK 1.175" IN LENGTH ALONG RIVET ROW AND EXTENDING BEYOND THE 6 RIVETS. AREA HAS CHIPPED PAINSDR FDEA201205302013Skin · chafedRT INBD MAIN FLAP UPPER SKIN CHAFED. REPAIR ACCOMPLISHED IAW EA 757-5752-16-F3928, REV A, MAJOR REPAIR.SDR SWAA2012060604686Flap · delaminatedRIGHT WING I/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP IAW MM.SDR SWAA2012060604685Carriage · corrodedLEFT WING O/B MIDFLAP I/B CARRIAGE SPINDLE CORRODED. REMOVED AND REPLACED CARRIAGE PER MT.SDR SWAA2012061805037Flap · delaminatedLEFT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP IAW AMM.SDR FDEA201205281989Skin · misrepairedLT WING INBD FLAP, INBD SEGMENT UPPER SURFACE MISREPAIRED. CARRIED OUT REPAIR IAW SRM 57-00-01, REPAIR 2, FIG 201, REV 49. EO 1-5100-7-5001B, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201205281988Skin · misrepairedLEFT WING INBD FLAP MISREPAIRED. CARRIED OUT REPAIR IAW SRM 57-00-01, REPAIR 1 FIG 201, REV 49. EO 1-5100-7-5001B PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.SDR SWAA2012061404904Rib · crackedRIGHT WING INBOARD MIDFLAP INBOARD EDGE RIB CRACKED. REMOVED AND REPLACED RIB IAW SRM AND DWG.SDR SWAA2012060404564Skin · puncturedRIGHT WING I/B AFT FLAP LOWER SURFACE PUNCTURED. REPAIRED AFT FLAP IAW SRM.SDR REXA2012060100681Vane · chafedLEFT INBOARD FLAP VANE ACTUATOR CHAFED 0.2 INCHES BY 0.050 INCHES BY 0.002 INCH DEEP AND 0.25 INCH BY 0.1 INCH BY 0.003 INCH DEEP. REPAIRED IAW REO 601R-57-52-1920.SDR A6WA201240639Vane · chafedRT INBD FLAP VANE HAS 3 CHAFED SPOTS ON L/E. REPAIRED RT INBD FLAP VANE L/E IAW REO 601R-57-52-004, REV C AND SRM 51-12-00, 51-21-11, 51-25-06, 51-25-16, 51-25-26.SDR A6WA201240638Vane · chafedLEFT INBD FLAP VANE IS CHAFED. REPAIRED LT INBD FLAP VANE IAW ROE 601R-57-52-004, REV C AND SRM 51-12-00, 51-21-11, 51-25-06, 51-25-16 AND 51-25-26.SDR SWIA201231136Skin · dentedLEFT INBOARD FLAP LOWER SKIN IS DENTED. (C-CHECK) REPAIRED LEFT INBOARD FLAP LOWER SKIN AS PER CRJ 200 SRM.SDR IPXA12M74051Vane · chafedINSPECTION TYPE:4C, LT INBD FLAP VANE CHAFE DAMAGE AT INBD T/E UPPER SURFACE. REPAIRED LT INBD FLAP VANE UPPER SURFACE INBD T/E IAW SRM 57-50-80. REPAIR 2 WET LAY-UP.SDR IPXA12673771Skin · dentedINSPECTION TYPE: 7C, LT WING INBD AFT FLAP UPPER SURFACE DENT. METAL HOT BOND REPAIR PERFORMED IAW EO B767-5750-47346-A AND HAECO RS R-57-57-37356, REV A.SDR MASA2012052934825Skin · dentedRIGHT WING INBOARD FLAP LOWER SKIN HAS A DENT AT FLS 42.00. DENT MEASURES 7.850L X 2.780W X .047D. PERFORMED A MAJOR REPAIR BY CUTTING OUT DAMAGED AREA. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM'S 57-52-01-201-001-A01 REPAIR TYPE IV AND 51-25-01-001-001SDR UALA2012052302905Bolt · shearedRT INBD TE FLAP ONE BOLT SHEARED. REMOVED AND REPLACED BOLT.SDR SWAA2012053104511Flap · delaminatedLEFT WING I/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR 7AHR201205222468Fairing · damagedNR 3 FLAP FAIRING FORWARD LOWER L/E IS DAMAGED. REPAIRED IAW SRM`S 51-30-2, & 51-40-3.SDR DALA1318223766Skin · delaminatedLARGE AREA OF DELAMINATION. IAW ER/A 458852-14, REPLACED UPPER AND LOWER SKINS, CORE AND T/E WEDGE ERA 458852-14.SDR IPXA12673770Skin · dentedINSPECTION TYPE: 7C, LT WING INBD AFT FLAP UPPER SURFACE DENT. METAL HOT BOND REPAIR PERFORMED IAW EO B767-5750-47346-A AND HEACO RS R-57-57-37356, REV A.SDR IPXA2673760Panel · delaminatedINSPECTION TYPE: 7C, RT WING INBD MAIN FLAP T/E FIXED PANEL LOWER SURFACE DELAMINATED AT NR 1 SUPPORT ARM AREA COUNT FROM INBD COMPOSITE WET LAY UP. REPAIR CARRIED OUT IAW SRM 51-70-17, PAR 4A (1) FIG 10, REV 52.SDR IPXA2673757Fairing · delaminatedINSPECTION TYPE: 7C, RT W INBD MAIN FLAP OTBD L/E FAIRING DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05, PAR 5A(1). FIG 5, REV 52.SDR IPXA2673755Panel · delaminatedINSPECTION TYPE: 7C RT WING INBD MAIN FLAP AFT T/E PANEL LOWER SURFACE DELAMINATED AT NR 2 SUPPORT ARM AREA COUT FROM INBD COMPOSITE WET LAY UP. REPAIR CARRIED OUT IAW SRM 51-70-17 PAR 4A (1) FIG 10, REV 52.SDR IPXA2673754Panel · delaminatedINSPECTION TYPE: 7C, RT WING INBD MAIN FLAP T/E FIXED PANEL LOWER SURFACE DELAMINATED. COMPOSITE WET LAY UP REPAIR CARRIED OUT IAW SRM 51-70-17 PAR4A (1) FIG 10, REV 52.SDR A6WA201240623Cap · gougedLEFT INBD FLAP END CAP GOUGED ON TOP L/E. R & R END CAP LT INBD FLAP IAW SRM 51-41-11, 51-42-06, 51-42-13, 51-23-00.SDR IPXA12573654Skin · dentedLT WING INBD MAIN FLAP DENTED. REPAIRED IAW EO B757-5750-47248-A.SDR QXEA2012051900388Flap Track · damagedRT WING NR 4 FLAP TRACK HAS AN AREA OF COATING MISSING ON INBD SIDE ROLLER RUNNING SURFACES. AREA HAS BEEN PREVIOUSLY BLENDED - NO SHARP EDGES OR LOOSE MATERIAL NOTED. MEASURED DAMAGE ALLOWED IAW RD 8/4-57-1238. MIN REMAINING THICKNESS .153, CONFIRMED CRACKSDR QXEA2012051900387Flap Track · damagedLT WING NR 5 FLAP TRACK HAS AREAS OF COATING MISSING ON INBD AND OTBD SIDE ROLLER RUNNING SURFACES. BLENDED ON INBD AND OTBD SIDE IAW RD 8/4-57-1238. REMAINING THICKNESS INBD .143 OTBD .144, BOTH SIDES CONFIRMED CRACK FREE REF NTM 51-00-04-910-801 PT1 AND 51SDR CA120525002Spring · broken(CAN) FLAP RETURN SPRING WAS FOUND BROKEN AT ATTACH POINT DURRING PREFLIGHT INSPECTION.SDR A6WA201240614Vane · chafedLEFT INBD FLAP VANE L/E CHAFED IN 3 PLACES. BLENDED AREAS ON LT INBD FLAP VANE L/E IAW REO 601R-57-52-004, REV C AND SRM 51-12-00. TREATED AREA SRM 51-21-11, 51-25-06, AND 51-25-26.SDR IPXA12673774Skin · dentedINSPECTION TYPE: 7C, LT WING INBD AFT FLAP LOWER SURFACE DENTED. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R, REPAIR 4, FIG 201, SHEET 1, REV 52.SDR IPXA12673773Skin · dentedINSPECTION TYPE: 7C, RT WING INBD AFT FLAP LOWER SURFACE DENTED. METAL HOT BOND REPAIR PERFORMED IAW EO B767-5750-47345-A AND RS R-57-57-37355, REV A.SDR IPXA12673772Skin · dentedINSPECTION TYPE: 7C, RT WING INBD AFT FLAP LOWER SURFACE DENTED. METAL HOT BOND REPAIR PERFORMED IAW EO B767-5750-47345-A AND RS R-57-57-37355, REV A.SDR IPXA2673759Wedge · delaminatedINSPECTION TYPE: 7C, RT WING OTBD FLAP T/E WEDGE UPPER SURFACE MID AREA DELAMINATED FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A(1) FIG 9, REV 52.SDR IPXA2673758Wedge · delaminatedINSPECTION TYPE: 7C, LT WING OTBD FLAP T/E WEDGE UPPER SURFACE MID AREA DELAMINATED AT 174" FROM INBD EDGE FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A(1), FIG 9, REV 52.SDR IPXA2673756Wedge · delaminatedINSPECTION TYPE:7C, LT WING OTBD T/E FLAP, T/E WEDGE, UPPER SURFACE MID AREA DELAMINATED AT 213" FROM INBD EDGE. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A(1) FIG 9, REV 52.SDR USAA2012052100013Wedge · delaminatedRON - DELAMINATION ON LEFT OUTBOARD TRAILING EDGE FLAP AT WS 415L, TRAILING EDGE WEDGE. REPAIRED LEFT OUTBOARD TRAILING EDGE FLAP AT WS 415L, TRAILING EDGE WEDGE IAW B737-400 SRM 51-70-10.SDR FDEA201205181865Hinge Fitting · corrodedLT WING OTBD FLAP, INBD FORWARD HINGE LOWER ATTACHMENT INBD BORE FOUND WITH CORROSION. REWORK CARRIED OUT IAW EA 8-5750-160613, PART 1C STEP 1 TO 9. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201205181864Hinge Fitting · corrodedLEFT WING OTBD FLAP, INBD FORWARD HINGE LOWER ATTACHMENT OTBD BORE FOUND WITH CORROSION. REWORK CARRIED OUT IAW EA 8-5750-160613, PART 1C, STEP 1 TO 9. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
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