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 QXEA2012103001359Flap Track · wornLT NR 5 FLAP TRACK INBD UPPER FLANGE HAS A WORN AREA. POLISHED WORN AREA TO REMOVE LOOSE MATERIAL AND BROKE SHARP EDGES REF SRM 57-50-50-02-01. CONFIRMED AFFECTED AREA CRACK FREE REF HORIZ NTM 8.2.1.1. MEASURED TRACK MIN REMAINING THICKNESS IS .259". MATERIASDR AALA20121030005Skin · damagedINBOARD FLAP, INBOARD WEDGE, GOUGED BOTTOM EDGE. REMOVED DAMAGE FROM LOWER SKIN PER SRM 57-01-00 FIGURE 5 SHEET 2. DAMAGE IS 22 INCHES FROM TRAILNG EDGE AND 20 INCHES FROM INBOARD EDGE. DYE PEN INSPECTION REVEALS NO CRACK INDICATION. INSTALLED PERMANENT FLSDR FDEA201210293773Carriage · gougedNR 3 FLAP TRACK CARRIAGE OTBD LOWER FITTING GOUGED. COMPLIED WITH EA F-2750-154109 WINGS-LT INBD FLAP CARRIAGE ASSY-GOUGE ON ROLLER SUPPORT ASSY.SDR IPXA12676078Skin · dentedLT WING INBD AFT FLAP HAS A DENT. REPAIR IAW EO B767-5750-48832-B.SDR QXEA2012102601360Skin · damagedLEFT OTBD FLAP HAS AREA OF CHAFE DAMAGE ON OTBD UPPER SKIN. BLENDED DAMAGE IAW RD 8/4-57-1594. DAMAGED AREA FOUND TO BE IN LIMITS IAW RD 8/4-57-1594. MAX AMOUNT REMOVED .004". APPLIED SURFACE PROTECTION IAW RD 8/4-57-1594, STEPS 7 & 8. CONFIRMED AFFECTED ARESDR USAA2012112600035Flap · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON RIGHT WING OUTBOARD AFT FLAP BETWEEN WS 486 TO WS 166 & BETWEEN RIB 9 TO RIB 20. REPLACED RIGHT WING OUTBOARD AFT FLAP IAW EA 503570.SDR FDEA201210253743Hinge · brokenDISCOVERED DROP PANEL OTBD OF CENTER FLAP FAIRING MISSING. HINGE THAT ATTACHES TO BOTTOM OF WING AND PANEL IS BROKEN AT EVERY LOBE. INSTALLED DOOR PANEL IAW EA 8-5720-164721. ACFT OK FOR SERVICE.SDR SWAA2012111509419Support Angle · crackedLOWER SUPPORT ANGLE CRACKED - I/B SIDE OF NR 3 FLAP TRACK FAIRING CUTOUT (MARKED). REMOVED AND REPLACED LOWER SUPPORT ANGLE I/B SIDE NR 3 FLAP TRACK FAIRING PER SRM 51-40-02.SDR SWAA2012111509381Plate · crackedWAFFLE PLATE IS CRACKED ON O/B SIDE OF NR 3 FLAP TRACK AT O/B FASTENER HOLE. REMOVED AND REPLACED WAFFLE PLATE ON O/B SIDE OF NR 3 FLAP TRACK, PER SRM 51-40-02.SDR A6WA20121101584Guide · chafedRIGHT O/B FLAP ROLLER GUIDE FITTING IS CHAFED. REPAIRED RIGHT O/B FLAP ROLLER GUIDE FITTING IAW REO 601R-57-53-956. REV -.SDR A6WA20121101581Fitting · chafedLEFT O/B FLAP ROLLER GUIDE FITTING IS CHAFED. REPAIRED LEFT O/B FLAP ROLLER GUIDE FITTING IAW REO 601R-57-53-956 REV -.SDR SWAA2012120710361Fairing · delaminatedNR 3 FLAP TRACK FAIRING DELAMINATED ON I/B SIDE (MARKED). MOD INSTALLED TEMPORARY SEAL WITH TWO LAYERS OF ALUMINUM FOIL (SPEED TAPE) TO PROTECT DAMAGE AREA FROM MOISTURE INTRUSION AND/OR EROSION.SDR SWAA2012102608871Skin · puncturedLEFT WING PUNCTURED ON I/B FORE FLAP LOWER SURFACE. REPAIRED FORE FLAP IAW SRM.SDR DALA1509763258Structure · damagedRT INBD FLAP DAMAGED. REPAIRED.SDR QXEA2012102101329Skin · chafedLEFT INBD FLAP UPPER SURFACE HAS CHAFING FROM WING T/E PANEL. BLENDED CHAFED AREA AND FOUND IN LIMITS IAW RD 8/4-57-1595. MATERIAL LOSS FOUND TO BE .001". APPLIED SURFACE PROTECTION IAW RD 8/4-57-1595. CONFIRMED BLENDS CRACK FREE IAW RD 8/4-57-1595.SDR QXEA2012102101327Flap Track · damagedRT NR 3 LOWER FLAP TRACK UPPER SURFACE HAS AN AREA OF MISSING CARBIDE COATING. BLENDED IAW RD 8/4-57-1511. MEASURED AREA FOUND TO BE OUT OF LIMITS IAW RD 8/4-57-1511. CONIFRMED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801 PT 1. MATERIAL LOSS FOUND TO BE ISDR WVER2012102195614Skin · damagedRIGHT INBOARD FLAP HAS MULTIPLE AREAS OF DAMAGE BETWEEN FLS 15.0 AND FLS 65.5 ON LOWER SKIN FROM TRAILING EDGE TO FWD EDGE. REPAIRED IAW BOMBARDIER REO 670-57-52-160.SDR CA121114005Fairing · cracked(CAN) 1.5" CRACK FOUND IN FLAP FAIRING SKIN ON RT WING JUST OTBD OF OTBD FLAP SCREWJACK ON UPPER PORTION OF SKIN STRUCTURE. MFG CONSULTED AND REPLACED WITH NEW.SDR SWAA2012111509433Fairing · crackedLEFT WING FLAP TRACK FAIRING 544AB FWD EDGE CRACKED. REPAIRED FAIRING IAW EA.SDR A6WA20121101580Skin · dentedLEFT I/B FLAP LOWER SKIN SURFACE HAS A DENT. REPAIRED DENT ON LEFT I/B FLAP LOWER SKIN IAW CRJ 200 SRM 57-52-00 SECTION B FIGURE 202 (SHEET 3).SDR A6WA20121101583Guide · wornRIGHT WING CONTACT POINT OF THE RIGHT O/B FLAP ROLLER GUIDE IS WORN. MEASURED & BLENDED AREA FOUND TO BE WITHIN LIMITS IAW B/A REO 601R-57-51-143.SDR FDEA201210183664Hinge Bracket · damagedRIGHT WING OTBD FLAP INBD HINGE LOWER MOUNT INBD HOLE REPAIR BUSHING FOUND DAMAGED. REPAIR ACCOMPLISHED AS PER EA 1-5750-127716, REVISION B, PART 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.SDR 2012FA0000729Tube · gougedWHILE CARRYING OUT A B-CHECK INSPECTION ON THE LT FLAP, IT WAS NOTED THE LT FLAP TUBE ASSEMBLY HAD A LARGE GOUGE IN IT.SDR SWAA2012110909199Flap · puncturedLEFT WING INBOARD AFT FLAP PUNCTURED FWD OF T/E. REPAIRED OF AFT FLAP IAW SRM & MM.SDR HALA2012101700220Structure · damagedLT WING TE FLAP DAMAGED. REPAIRED IAW E105-481167.SDR A6WA20121031575Vane · chafedLEFT AND RIGHT FLAP VANE VENT L/E CHAFED. BLENDED 5 EA AREAS ON RIGHT & LEFT FLAP VANE L/E FOUND 5 AREAS TO BE WITHIN ALLOWABLE DAMAGE LIMITS. LEFT INBOARD FLAP VANE L/E OUT OF ALLOWABLE LIMITS, REMOVED UNSERVICEABLE L/E AND INSTALLED SERVICEABLE L/E IAW REOSDR A6WA20121031569Guide · damagedRIGHT O/B FLAP CENTER HINGE ARM GUIDE DAMAGED. FAB SERVICEABLE BRACKET P/N 601R14629 IAW CRJ 200 SRM 51-54-00 AND 51-42-06.SDR IPXA12M76107Skin · crackedINSPECTION TYPE: 2C, RT INBD FLAP UPPER SKIN CRACKED AT XIFH 171.5 APPROX 7.25" FWD OF REAP SPAR PLANE. REPAIRED SKIN IAW SRM 57-00-01, REPAIR 1, FIG 201. (MAJOR)SDR IPXA12M76088Skin · dentedINSPECTION TYPE:2C, ONE INCH DENTED ON UPPER SURFACE OF RT INBD FLAP FIVE INCHES AFT OF REAR SPAR NEAR STA. XIFH195.3 REPAIRED DENT IAW SRM 57-00-01, REPAIR 1, FIG 201. (MAJOR)SDR IPXA12575833Wedge · damagedLT WING OTBD FLAP T/E WEDGE DAMAGED. REPAIR IAW EO B757-5750-48837-A.SDR IPXA12175831Skin · dentedRT WING INBD FLAP LOWER SKIN HAS 2 DENTS/GOUGES. REPAIRED IAW EO A300-5750-48702-B.SDR SWAA2012101708596Flap · puncturedLEFT WING I/B FOREFLAP PUNCTURED. REMOVED AND REPLACED FOREFLAP PER AMM.SDR SWAA2012111509424Support Angle · cracked(LEFT WING) UPPER FIXED TRAILING EDGE PANEL LOWER SUPPORT ANGLE CRACKED JUST I/B OF FLAP PROGRAMMING TRACK. REMOVED AND REPLACED ANGLE IAW SRM.SDR SWAA2012101508528Spindle · corrodedRIGHT WING NR 8 SPINDLE CORRODED. REMOVED AND REPLACED NR 8 SPINDLE IAW MT.SDR R61A201210100591Bearing Support · corrodedWHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE BEARING SUPPORT BETWEEN LEFT 5 & 6 FLAP TORQUE TUBE DRIVES CORRODED. MAINTENANCE REMOVED AND REPLACED BEARING SUPPORT BETWEEN LT 5 & 6 TORQUE TUBE DRIVES IAW EMB 170 AMM 27-51-04. THE AIRCRAFT IS OUT OFSDR R61A201210100587Bearing Support · corrodedWHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE BEARING SUPPORT AT RIGHT WING FLAP TORQUE TUBES F5 AND F6 OUTBOARD SIDE CORRODED. MAINTENANCE REMOVED AND REPLACED THE BEARING SUPPORT IAW EMB 170 AMM 27-51-04. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CSDR UALA2012101005771Flap · damagedRIGHT INBD TRAILING EDGE FLAP BIRD STRIKE OUTBD EDGE. INSPECTED AREA OF I/B FLAP FOR DAMAGE. FOUND DENT 1.25" X 1.75" X .055" LOCATED 10 INCHES FROM AFT EDGE AND 8.5" I/B OF THE CANOE. DENT IS LOCATED IN ZONE 2 AREA,TEMPORARY REPAIR NOT REQUIRED REF AIRBUS SDR SWIA201231947Paint · looseSELECTED FLAPS TO 45 AND FELT A BUMP IN THE CONTROL WHEEL AND PLANE WANTED TO ROLL RIGHT. (FLT 4455) CLEANED ALL FLAP SURFACES AND FOUND RIGHT OUTBOARD FLAP TO HAVE LOOSE PAINT ON LEADING EDGE. DRESSED PAINT. FUNCTIONAL FLIGHT PASSED.SDR ASAA2012100993103Fitting · corrodedLEFT INBD MIDFLAP, INBD TORQUE TUBE, INBD RIB HAS SURFACE CORROSION. ACFT GROUNDED. R & R NEW RIB FITTING IAW SRM 51 40 02.SDR 2012FA0000679Bracket · brokenDURING PHASE INSPECTION, THE RT OTBD, INBD FLAP TRACK BRACKET, BROKEN AT UPPER AFT END OF AFT TRACK. FLAP ATTACH POINTS WERE UNDAMAGED. BRACKET REPLACED AND ACFT RETURNED TO SERVICE.SDR SWAA2012111509384Seal · cracked(RIGHT WING) NR 5 FLAP TRACK FAIRING LOWER SPRING ANGLE ON A/C IS CRACKED. REMOVED NR 5 FLAP TRACK FAIRING LOWER SPRING SEAL ANGLE CRACKED, INSTALLED NEW SPRING SEAL IAW SOPM 20-50-01 STEP 7 89264U 10/29/12.SDR UALA2012100905723Fairing · looseRIGHT INBOARD TRAILING EDGE BOTTOM FIXED FAIRING ATTACH SCREWS FOUND LOOSE ON WALKAROUND. TIGHTENED FAIRING PER AMM. RAN FLAPS, CHECKS NORMAL.SDR SWAA2012101108421Carriage · corrodedLEFT WING NR 2 SPINDLE CARRIAGE ASSY CORRODED. REMOVED AND REPLACED NR 2 FLAP CARRIAGE ASSY IAW MT.SDR SWAA2012101108418Spindle · corrodedRIGHT WING NR 8 SPINDLE CORRODED. REMOVED AND REPLACED NR 8 FLAP CARRIAGE SPINDLE ASSY IAW MT.SDR SWAA2012100908344Flap · delaminatedLEFT OUTBOARD AFT FLAP DELAMINATED AT NR 2 FAIRING CONTACT AREA. REMOVED AND REPLACED FLAP ASSY PER MM.SDR UALA2012100805674Skin · corrodedRIGHT WING INBOARD AFT FLAP, UPPER SKIN TRAILING EDGE CORRODED. MAJOR REPAIR ACCOMPLISHED: REPAIRED RT WING INBOARD AFT FLAP TRAILING EDGE WEDGE 2EA AREAS BY BONDING FILLER SKINS & DOUBLERS IAW SRM 57-53-01 & 57-70-10. SEALED DOUBLERS IAW SRM 51-20-05 & BAC SDR UALA2012100805673Skin · corrodedLEFT WING INBOARD AFT FLAP UPPER TRAILING EDGE SURFACE HAS CORROSION. REPAIRED LEFT WING INBOARD AFT FLAP TRAILING EDGE WEDGE 7EA AREAS BY BONDING SKIN FILLERS & DOUBLERS IAW SRM. SEALED DOUBLERS IAW BAC DRG 113T2320 & SRM 51-20-05, PREPPED AND PAINTED AREASSDR LR7A2012100500404Skin · crackedDURING SCHEDULED C-10, CHECK UNDER JOB CARD HC5712, FOUND RT OTBD FLAP LOWER SKIN CRACKED AT OWS 43. REPAIR ACCOMPLISHED IAW SMP 583 FIG 57-70-10.SDR LR7A2012100500403Skin · corrodedDURING SCHEDULED C-10 CHECK, FOUND LT INBD FLAP L/E LOWER SURFACE UNEVEN DUE TO CORROSION BETWEEN SPAR LOWER CAP AND LOWER SKIN. TREATMENT ACCOMPLISHED IAW SMP 583 51-30 AND SMP 515-B 57-50-00, P4. SKIN REPAIR ACCOMPLISHED IAW SMP 583, FIG 51-140-12.SDR LR7A2012100500402Skin · crackedDURING SCHEDULED C-10 CHECK, FOUND LEFT INBD FLAP LOWER SKIN CRACKED AT CWS 140. REPAIR ACCOMPLISHED IAW SMP 583, FIG 51-140-12.
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