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 ASAA0540483Skin · dentedOKC - FOUND RIGHT INBOARD AFT FLAP IS DENTED 36 INCHES FROM INBOARD END. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR SKIN AND DOUBLER IAW 737-400 SRM 51-70-10. (M)SDR ASAA0540476Fitting · corrodedOKC - FOUND RIGHT INBOARD MID FLAP OUTBOARD TORQUE TUBE FITTING CORRODED. REMOVED AND REPLACED TORQUE TUBE FITTING IAW 737-400 SRM 51-40-02. (M)SDR QXEA200501315Panel · wornYYC - LEFT WING INBOARD FLAP, INBOARD PANEL 584ET WORN IN LEADING EDGE. REMOVED DAMAGE IAW CRJ-700 SRM 51-12-00-001-001-A01. RESTORED FINISH.SDR QXEA200501310Fairing · chafedYYC - RIGHT WING LOWER SURFACE HAS CHAFED DAMAGE FROM THE FLAP HINGE FAIRING AT WS 128. BLENDED CHAFFED AREA IAW CRJ-700 SRM 51-12-00-001-001-A01. MATERIAL LOSS .002". RESTORED FINISH.SDR QXEA200501309Skin · chafedYYC - RIGHT INBOARD FLAP LOWER EXTERIOR SURFACE HAS CHAFED MARKS UNDER THE INBOARD AND OUTBOARD HINGE FAIRINGS. BLENDED OUT DAMAGE IAW CRJ-700 SRM 57-52-101-101-001-A01. MATERIAL LOSS .009" RESTORED FINISH.SDR QXEA200501306Skin · damagedYYC- LEFT INBOARD FLAP LOWER EXTERIOR SURFACE HAS GRAVEL DAMAGE. BLENDED OUT DAMAGE, REMOVED .008" MATERIAL IAW CRJ-700 SRM 57-52-01-101-001-A01. RESTORED FINISH.SDR DHL2005742526Skin · chafedRT WING O/B MID FLAP CHAFFED EXISTING REPAIR I/B TOP. REMOVED EXISTING REPAIR. FABRICATED AND INSTALLED FORMED ANGLE REPAIR 7" BY 2.30" BY .75" FROM 2024-T3 .063 IAW B727 SRM 57-20-2 FIG 5, 51-20-1 PARA 7, 51-30-6 FIG 3 51-10-2, 51-40-3 FIG 1 AND 51-30-2 PARSDR DHL2005742524Skin · debondedLT I/B AFT FLAP HAS AREA OF DISBOND NEAR I/B END. FABRICATED AND INSTALLED DOUBLER REPAIRS 8.2" BY 7.5" AND 5.2" BY 4.5" FROM 2024-T3 .016 AND 5.1" BY 4.4" FROM BMS 4.4 HONEYCOMB IAW B727 SRM 51-40-20, 51-40-23 AND 57-50-2 NOTE G.SDR DHL2005742523Skin · dentedLT I/B FORE FLAP L/E NEAR CENTER HAS DENTS IN SKIN. REMOVED DENTED SKIN. FABRICATED AND INSTALLED REPAIR SKIN 8" BY 8" FROM 2024-T3 .040 IAW B727 SRM 51-10-1 AND 51-30-2.SDR DHL2005742522Skin · chafedLT O/B MID FLAP I/B END L/E CUT AND CHAFED. REMOVED DOUBLER IAW B727 SRM 51-10-1 AND 51-30-2. FABRICATED AND INSTALLED DOUBLER REPAIR 7" BY 6.0" BY 3.2" FROM 2024-T3 .040 IAW B727 SRM 51-10-2, 57-50-4.SDR DHL2005742514Skin · gougedRT OB FORE FLAP LEADING EDGE HAS 2 EACH GOUGES ABOUT 12 INCHES OB OF IB EDGE. FABRICATED AND INSTALLED REPAIR DOUBLER 8 INCHES X 3 INCHES FROM 024-T3 .050 FOR RT OB FORE FLAP LEADING EDGE IAW 57-50-4, 51-30-2 AND 51-10-2.SDR DHL2005742501Skin · damagedLEFT O/B FLAP I/B END LEADING EDGE GROOVED AND CHAFED. FABRICATED EXTERNAL REPAIR 4 X 4 INCHES FROM 2024-T3 .050. LOCATED, DRILLED, DEBURRED IAW B727 SRM 57-50-4, ALODINED AND PRIMED REPAIR IAW B727 SRM 51-10-2, INSTALLED DOUBLER REPAIR IAW B727 SRM 51-30-2 SDR 05FDEA02979Flap Track · corrodedRT WING OUTBD FLAP, OUTBD TRACK HAS SURFACE CORROSION AND CHAFING ON FACES AND ROLLERS SLIDING TRACKS. REMOVED AND REPLACED NR 8 FLAP TRACK IAW MM 27-51-031-4.SDR 05FDEA02978Flap Track · corrodedRT WING INBD FLAP OUTBD TRACK NR 6 HAS CORROSION, PITTING, AND CHAFING ON FACES AND ROLLERS SLIDING TRACKS. REPLACED NR 6 FLAP TRACK ASSY IAW MM 27-51-031-4.SDR SWAA052834Skin · delaminatedDURING SCHEDULED RON CHECK, FOUND RIGHT OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA052793Skin · delaminatedDURING SCHEDULED 1/4D CHECK, FOUND LT WING OUTBOARD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.SDR AWXA200501269Skin · debondedGYR - MAJOR REPAIR - DURING C20 CHECK, DISCOVERED DISBOND ARE ON THE LOWER SURFACE OF THE RT INBOARD FORE FLAP LOWER SKIN, OUTBOARD END AT WING STA 190 AND WBL 128. MAINTENANCE REMOVED DISBONDED SKIN IAW BOEING 737-300 SRM 51-70-10-2. FABRICATED REPAIR FILLESDR IXXA05RNG072SSkin · corrodedDURING INSPECTION CHECK WAS FOUND A CORROSION ON RT INBOARD FLAP EXTERIOR SURFACE, BETWEEN STA XW3-XW92 (VIEW LOOKING UP). RT WING INBOARD FLAP SKIN WAS REMOVED AND REPLACED IAW DOUGLAS DRAWING 5642960. RIVETS WERE INSTALLED IAW DC8 SRM 51-1-21 PAGE 1 TO 7.SDR AWXA200501173Stiffener · crackedMCN - DURING C18 CHECK DISCOVERED STIFFENER ASSY CRACKED, .75" IN LENGTH, INSIDE THE LT OUTBOARD MID FLAP, 100" FROM INBOARD END OF FLAP. MAINTENANCE WAS UNABLE TO REPAIR DUE TO THE LOCATION OF THE DAMAGE. MAINTENANCE REMOVED AND REPLACED THE LT OUTBOARD MIDSDR AWXA200501156Skin · debondedGYR - DURING C20 CHECK, DISCOVERED THE LT OUTBOARD AFT FLAP LOWER AND UPPER EDGE AREA DEBONDED, FROM WBL 224.40 TO WBL 231.4. MAINTENANCE REMOVED DAMAGED ARE ON THE AFT FLAP LOWER AND UPPER SURFACE IAW BOEING 737-300 SRM 51-70-10-2R. FABRICATED CORE AND DOUBSDR 05FDEA02836Attach Fitting · corrodedRT WING, I/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED. REPAIR CARRRIED OUT AS PER EA 1-5750-87634.SDR 05FDEA02835Attach Fitting · corrodedRT WING, I/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87634.SDR 05FDEA02834Attach Fitting · corrodedRT WING, I/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. CORROSION REPAIR CARRIED OUT AS PER EA 1-5750-87634.SDR AWXA200501155Wedge · delaminatedGYR - DURING C20 CHECK DISCOVERED THE LT WING INBOARD FLAP, MID FLAP PANEL 7220, DELAMINATED AT UPPER SKIN. MAINTENANCE REMOVED DAMAGED SKIN AND CLEANED AREA IAW BOEING 737-300 SRM 51-70-10-2R. FABRICATED DOUBLER AND FILLER AND BONDED TO SKIN AT THE LT WING SDR SWAA052754Skin · delaminatedDURING SCHEDULED RON CHECK, FOUND RT WING INBOARD T/E AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER SWA EA & SRM.SDR SWAA052753Skin · delaminatedDURING SCHEDULED RON CHECK, FOUND RT WING INBOARD T/E AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER SWA EA & SRM.SDR SWAA052747Skin · delaminatedDURING SCHEDULED A1 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR ASAA0540442Wedge · gougedOKC - FOUND RIGHT INBOARD FLAP TRAILING EDGE WEDGE GOUGED IN TWO PLACES. REPLACED RIGHT INBOARD FLAP TRAILING EDGE IAW B737-400 SRM 51-40-5, AND 08. (M)SDR DHL2005748750Skin · dentedL/WING I/B AFT FLAP HAS DENT ON UPPER SURFACE I/B END. CUT OUT DENTED AREA ON LT IMB AFT FLAP APPROX 2" DIA FAB FILLER APPROX 2" DIA AND DOUBLER APPROX 5" DIA FROM .012 2024 T3 PO NR 900534 BONDED FILLER AND DOUBLER CURED CLEANED PRIMED AND EALED IAW B727 SRMSDR IXXA05RNG059SFitting · crackedDURING INSPECTION CHECK WAS FOUND RT OUTBOARD FLAP, INBOARD FLAP HINGE FITTING AT STA XF339.7332 CRACKED. DAMAGE WILL BE REPAIRED IAW EWO ATI-57-042 AND FAA FORM 8110-3 MUST BE ISSUED APPROVING THIS REPAIR.SDR USAA051068Skin · delaminatedUPPER SKIN OF FLAP T/E WEDGE DELAMINATED. REMOVED PREVIOUS REPAIR AND FABRICATED AND INSTALLED NEW REPAIR IAW SRM 51-70-10. DEFECT SIZE: 2 INCH DIAMETER DELAMINATION.SDR AWXA200501341Skin · delaminatedGYR - MAJOR REPAIR - DURING C20 CHECK DISCOVERED DELAMINATED AREA ON THE LT OUTBOARD AFT FLAP, UPPER SKIN AT WBL 244.40. MAINTENANCE REMOVED DAMAGED SKIN AND CORE FROM LT OUTBOARD AFT FLAP IAW BOEING 737-300 SRM 51-70-10-2R4. FABRICATED CORE AND DOUBLER IAW SDR AWXA200501168Skin · delaminatedGYR - DURING C20 CHECK DISCOVERED,THE RT AFT FLAP, RT WING, ON THE INBOARD END DELAMINATED. MAINTENANCE REMOVED DAMAGED SKIN AND CORE ON THE RT AFT FLAP IAW BOEING 737-300 SRM 51-70-10-2R. FABRICATED DOUBLER AND FILLER IAW BOEING 737-300 SRM 51-70-10-2R. BOSDR AWXA200501163Wedge · debondedMCN - DURING C15 CHECK, DISCOVERED DISBOND AREA ON LOWER SURFACE OF THE RT INBOARD MID-FLAP TRAILING EDGE WEDGE, 35" FROM OUTBOARD END. MAINTENANCE REMOVED DISBOND SKIN ON LOWER SURFACE OF RT INBOARD MID FLAP TRAILING EDGE WEDGE IAW BOEING 737-300 SRM 51-70-1SDR UPS05145483Skin · chafedRT INBD FLAP TOP MID FWD CHAFING. REPAIRED FLAP IAW A300 SRM 57-50-00 FIG 205 AND 51-25-00.SDR 05FDEA02809Attach Fitting · corrodedLT WING, I/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87633.SDR 05FDEA02808Attach Fitting · corrodedLT WING, I/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87633.SDR 05FDEA02806Attach Fitting · corrodedRIGHT WING, NR 7 FLAP TRACK FWD ATTACH FITTING INBOARD FACE CORRODED (27X5709-02). REPAIRED PER E.A. 7-5710-91348.SDR 05FDEA02798Attach Fitting · corrodedLT WING, O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87631.SDR 05FDEA02797Attach Fitting · corrodedLT WING, O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87631.SDR 05FDEA02796Attach Fitting · corrodedLT WING, O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87631.SDR 05FDEA02795Attach Fitting · corrodedLT WING, O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. CORROSION REPAIR CARRIED OUT AS PER EA 1-5750-87631.SDR 05FDEA02794Attach Fitting · corrodedLT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87631.SDR 05FDEA02793Attach Fitting · corrodedLT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. ORROSION REPAIR CARRIED OUT AS PER EA 1-5750-87631.SDR 05FDEA02792Attach Fitting · corrodedLT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87631.SDR 05FDEA02791Attach Fitting · corrodedLT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. CORROSION REPAIR CARRIED OUT AS PER EA 1-5750-87631.SDR UPS05845594Fitting · crackedINSPECTION TYPE:C3 STA 3 LT FLAP TRACK ATTACH POINT IS CRACKED. REMOVED AND REPLACED STA 3 LT FLAP TRACK ATTACH POINT FITTING IAW DC-8 SRM 51-3-0, 51-1-21, AND 51-1-20D.SDR 05FDEA02781Attach Fitting · corrodedRIGHT WING - O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87632.SDR 05FDEA02780Attach Fitting · corrodedRT WING O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87632.SDR 05FDEA02779Attach Fitting · corrodedRT WING O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87632.
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