JASC 5753
Service difficulty reports · 31,521
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 MALA050624Access Panel · chafedRT FLAP IB END ACCESS PANEL S41AT IS CHAFED AND HAS BEEN REPAIRED IAW MESABA EO 57098 REF EAMS WORK ORDER 212638 TASK 6502.SDR MALA050627Access Panel · chafedLT FLAP IB END ACCESS PANEL S41AT IS CHAFED AND HAS BEEN REPAIRED IAW MESABA EO 57098 REF EAMS WORK ORDER 212638 TASK 5504.SDR CALA0500251Flap Track · corrodedINSPECTION FOUND THE NR 1 FLAP TRACK CORRODED IN THE AFT UPPER HOLE WHERE THE TRANSMISSION IS ATTACHED. THE AREA WAS REWORKED IAW CMM 57-53-15.SDR CALA0500250Flap Track · corrodedINSPECTION FOUND THE NR 2 FLAP TRACK CORRODED IN THE AFT LOWER HOLE WHERE THE TRANSMISSION IS ATTACHED. THE AREA WAS REWORKED IAW CMM 57-53-15.SDR CALA0500249Flap Track · corrodedINSPECTION FOUND THE NR 8 FLAP TRACK CORRODED IN AFT O/B HOLE WHERE THE TRANSMISSION IS ATTACHED. THE AREA WAS REWORKED IAW CMM 57-53-15.SDR 05FDEA02142Skin · damagedLT WING I/B T/E FLAP LWR SKIN MID O/B SECTION HAS CREASE. FOUND CREASE TO BE OUT OF LIMITS IAW SRM 57-50-00 FIG 101. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS ON MAE TRAVELER T5/532877 LOCATED, DRILLED, AND INSTALLED IAW SRM 57-50-00 FIG 206. TREATED/PRSDR DHL2005747502Wedge · delaminatedLEFT WING INBD MID FLAP T/E WEDGE APPROX 61" FROM INBD END HAS AREA OF DELAMINATION ON BOTTOM SKIN. REPAIRED LEFT INBD MID FLAP T/E INNER BOTTOM SKIN AT APPROX 61" FROM INBD END IAW B-727 SRM 51-40-20 PAR 20-22 BY INSTALLING DOUBLER REPAIR.SDR MALA050619Skin · dentedWHILE ACCOMPLISHING C1 INSPECTION, FOUND A DENT ON THE RIGHT OUTBOARD FLAP TAB ABOUT 6 INCHES FROM INBOARD END AND 5 INCHES FROM BOTTOM OF THE TAB.SDR MALA050620Skin · dentedWHILE ACCOMPLISHING C1 INSPECTION, FOUND A DENT ON THE RIGHT OUTBOARD FLAP TAB, ON THE BOTTOM SIDE, 24 INCHES FROM INBOARD END.SDR 05FDEA02119Flap Track · dentedLT WING OB TE FLAP LE HAS DENT BET TRACKS NR 5.SDR AWXA200500974Skin · debondedMCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED DISBOND AREA ON INBOARD END OF THE LT OUTBOARD FORE FLAP. MAINTENANCE REMOVED DISBONDED SKIN AND CORE FROM LT OUTBOARD FORE FLAP IAW BOEING 737-300 SRM 51-70-10-0. FABRICATED REPAIR CORE, FILLER AND REPAIR DOUSDR AWXA200500947Skin · debondedDURING C16 CHECK DISCOVERED DISBOND ARE ON THE UPPER SURFACE OF THE RT OUTBOARD FORE FLAP 119 INCHES FROM INBOARD END. MAINTENANCE CUT OUT DISBOND AREA ON THE UPPER SURFACE OF THE RT OUTBOARD FORE FLAP IAW BOEING 737-300 SRM 51-70-10-0 FIG 9. FABRICATED REPASDR 05FDEA02095Skin · delaminatedRIGHT WING, INBOARD FLAP, FLAP VANE INBOARD LOWER SKIN FOUND DELAMINATED. DELAMINATION MEASURES 40.00 INCHES IN LENGTH BY 17.00 INCHES IN WIDTH. REPAIRED IN ACCORDANCE WITH FEDEX EA 1-5750-87555.SDR MALA050606Access Panel · dentedLT FLAP ACCESS PANEL 541AT IS DENTED AND HAS BEEN REPAIRED IAW MESABA EO NR S57060. REF: EAMS WORK ORDER 212675 TASK 5504.SDR UPS05445144Structure · corrodedINSPECTION TYPE:C RIGHT WING I/B MID FLAP T/E WEB UPPER CHORD CORRODED REVEALED AT 104"- 108" AS MARKED (COUNT FROM I/B). CORROSION BLEND OUT 0.054" X 3/4" X 3" EXCEED SRM 57-50-01 FIG 3 LIMITS, CHORD REPAIRED AS PER HX RS R57-55-35354 & UPS ENGINEERING FILE SDR UPS05445143Structure · corrodedINSPECTION TYPE:C RIGHT WING I/B MID FLAP T/E WEB UPPER CHORD CORROSION REVEALED AT 73" - 78" AS MARKED (COUNT FROM I/B). CORROSION BLEND OUT 0.083" X 3/4" X 3" EXCEED SRM 57-50-01 FIG 3 LIMITS. CHORD REPAIRED AS PER HX RS R57-55-35354 & UPS ENGINEERING FILESDR A6WA200540265Skin · chafedLT WING IB FLAP, IB END AT FLAP STA 50.498 IB BELOW THE LEADING EDGE IS CHAFED FROM THE STUB FAIRING. CHAFE MEASURES 1.50 INCH LONG X .50 INCH WIDE X .035 INCH DEEP. (K)SDR A6WA200540264Skin · dentedLT WING IB FLAP INNER SKIN IS DENTED BETWEEN FLAP STATION 142 AND 147 AT THE INTERCOSTAL SPAR AREA. DEN MEASURES .850 INCH LT X .800 INCH X .067 INCH DEEP. PERFORMED REPAIR BY CUTTING OUT DAMAGE AND INSTALLING 11.5 INCH X 3 INCH FLUSH REPAIR IAW SRM REPAIR SDR SWAA052164Skin · delaminatedDURING SCHEDULED RON CHECK, FOUND RT WING INBD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR 05FDEA02029Skin · dentedRT WING T/E INBD FLAP LOWER SURFACE INBD SECTION HAS DENT (31" FROM INBD END AND 7" FROM T/E). CHECKED ALLOWABLE DENT LIMIT FOUND OT OF LIMIT ACTUAL DENT 0.1405, ALLOWED IS ONLY 0.14" PER SRM 57-50-00 PAGE 105. REMOVED DAMAGE IAW SRM 57-50-00 FIG 205 PAGE 22SDR MALA050601Access Panel · chafedDURING 4Y/2Y CHECK IN BNA FOUND RT FLAP ACCESS PANEL 641AT IS CHAFED AT THE INBOARD END AND HAS BEEN REPAIRED IAW MESABA EO#S57095. REF: EAMS WORKORDER 212650 TASK 6503SDR IXXA05RNG035SSupport Fitting · crackedDURING ROUTINE "C" CHECK, CRACKS 2.023" AND 0.521" LONG WERE FOUND ON THE LEFT WING OUTBOARD FLAP AT FITTING STA XF 409.6675 OUTBOARD. FITTING WAS REPAIRED IAW EWO ATI 57-025 AND EO ATI-071105. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR.SDR IXXA05RNG034SSupport Fitting · crackedDURING ROUTINE "C" CHECK, CRACK 0.5220" LONG WAS FOUND ON THE LEFT WING OUTBOARD FLAP AT FITTING LOCATED AROUND STATION XF 339.7232 OUTBOARD. LEFT WING OUTBOARD FLAP SUPPORT FITTING WAS REPAIRED IAW EWO ATI 57-024 AND EO ATI-071005. FAA FORM 8110-3 WAS ISSUESDR IXXA05RNG033SSupport Fitting · crackedDURING ROUTINE "C" CHECK, CRACK 0.2740" LONG WAS FOUND ON THE LEFT WING OUTBOARD FLAP AT FITTING LOCATED AROUND STATION XF 339.7232 INBOARD. LEFT WING INBOARD FLAP SUPPORT FITTING WAS REPAIRED IAW EWO-ATI-57-023 AND EO ATI-070905. FAA FORM 8110-3 WAS ISSUED ASDR IXXA05RNG032SSupport Fitting · crackedDURING ROUTINE "C" CHECK, CRACK 0.385" LONG WAS FOUND ON THE LEFT WING INBOARD FLAP AT FITTING LOCATED AROUND STATION XF 97-6090 INBOARD. LEFT WING OUTBOARD FLAP SUPPORT FITTING WAS REPAIRED IAW EWO ATI 57-022 AND EO ATI-070805. FAA FORM 8110-3 WAS ISSUED APSDR MALA050592Access Panel · chafedDURING 4Y/2Y CHECK FOUND RT FLAP ACCESS PANEL 641AT IS CHAFED OUT OF LIMITS ON THE INBOARD END AND HAS BEEN REPAIRED IAW MESABA EO#S57094 REF: EAMS WORK ORDER 612613 TASK 6507SDR ASAA0540365Flap · splitLT OB AFT FLAP IB END T/E SPLIT. REMOVED AND REPLACED LT OB FLAP IAW AMM. (K)SDR ASAA0580393Vane · chafedOKC - DURING HV CHECK, FOUND LEFT NR 3 OUTBOARD FLAP VANE L/E REPAIR DOUBLER IS CHAFED. REPLACED DOUBLER. (M)SDR 05FDEA01990Fairing · delaminatedRH WING NR 4 FLAP TRACK FAIRING AT FWD O/B LWR SURFACE HAS DELAM.SDR ASAA0540359Wedge · dentedLT IB MID FLAP AFT WEDGE HAS NUMEROUS DENTS. REMOVED DAMAGED AREA. FABRICATED AND INSTALLED FILLERS AND DOUBLERS AND INSTALLED REPAIR PIECES IAW SRM. (K)SDR ASAA0540358Skin · debondedLT OB AFT FLAP PREVIOUSLY INSTALLED REPAIR IS DEBONDING AT IB AFT CORNER. REMOVED DAMAGED AREA. FABRICATED AND INSTALLED FILLER AND DOUBLER AND INSTALLED REPAIR PIECES IAW SRM. (K)SDR ASAA0540354Skin · dentedRT IB MID FLAP AFT WEDGE HAS NUMEROUS DENTS. REMOVED DENTED AREA OF LOWER SKIN, FABRICATED AND INSTALLED FILLERS AND DOUBLERS IAW SRM. (K)SDR DHL2005747512Skin · gougedLT WING INBOARD TRAILING EDGE FORE FLAP OUTBOARD LOWER LEADING EDGE REPAIR DOUBLER IS GOUGED THRU. REMOVED EXISTING REPAIR IAW B727 SRM 51-30-2. FABRICATED NEW REPAIR DOUBLER 3.95 X 4.55 INCH FROM 2024-T3 .063 IAW B727 SRM 57-50-4. ALODINED AND PRIMED, INSTSDR AWXA200500920Bolt · corrodedMCN - DURING C18 CHECK DISCOVERED CORROSION ON RETAINING BOLTS FOR THE LT INBOARD MID FLAP GIMBAL SUPPORT. NO CORROSION REMOVAL LIMITS AVAILABLE FOR RETAINING BOLTS FOR THE LT INBOARD MID FLAP GIMBAL SUPPORT. MAINTENANCE REMOVED AND REPLACED BOLTS ON THE LT SDR 05FDEA01976Hinge · corrodedRT WING, I/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03 PG 442-443. FABRICATED BUSHING AND INSTALLED AS PER EA 1-5750-87612.SDR SWAA052077Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA052063Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND LT WING INBOARD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.SDR AWXA200500934Flap · deterioratedDURING C4 CHECK DISCOVERED COMPOSITE DETERIORATED AT TRAILING EDGE OF THE INBOARD FLAP ON THE LT WING. MAINTENANCE GROUND DOWN AND CLEANED THE SURFACE OF THE INBOARD FLAP, TRAILING EDGE, L/H WING IAW AIRBUS A320 SRM 57-52-00. APPLIED GLASS FABRIC AND LAMINATSDR ASO2005F00004Flap · damagedDURING TAKEOFF, TOWER INFORMED CREW THAT TIRE DEBRIS WAS NOTICED ON RUNWAY AFTER DEPARTURE. THERE WERE NO INDICATIONS OF ENGINE DAMAGE AND AC CONTINUED. EMERGENCY WAS DECLARED AND EMERGENCY VEHICLES WERE REQUESTED TO BE ON STANDBY AS PRECAUTION. AC LANDED SSDR 05FDEA01909Hinge · corrodedLT WING - I/B FLAP O/B HINGE (FLAP SIDE ), PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03 PG 442-443. FABRICATED BUSHING AND INSTALLED AS PER EA 1-5750-87606.SDR 05FDEA01902Skin · dentedRT I/B FLAP UPPER SKIN BETWEEN XIFN 151.300 TO 159.300, FOUND WITH EXISTING DENTS, 3 PLACES, AS MARKED. DENT AREA TRIMMED AND REPAIR DOUBLER FABRICATED AND MATERIAL USED AS PER SRM 57-10-00 FIG 34 VOL I AND DRAWING ARC 2740. REPAIR DOUBLER INSTALLED AS PER SRSDR GTIA050210Vane · damagedFOUND LEFT WING OUTBOARD FLAP, OUTBOARD VANE, HOLE IN LEADING EDGE. REPAIRED OUTBOARD VANE IAW MD80 SRM 57-03 PAR 8A. TREATED AND PRIMED AREA. (M)SDR DHL2005747503Skin · delaminatedLT WING INBD MID-FLAP T/E APPROX 61" FROM INBD END HAVE DELAMINATION. REPAIRED LT INBD MID FLAP T/E AT APPROX 61" FROM INBD END IAW B-727 SRM 51-40-20 PAR 20-22 BY INSTALLING DOUBLER REPAIR.SDR AWXA200500917Wedge · delaminatedDURING C18 CHECK DISCOVERED LT INBOARD FORE FLAP LOWER SURFACE DELAMINATED, AT THE INBOARD TRACK ATTACHMENT. MAINTENANCE REMOVED DAMAGED AREA ON THE LT INBOARD FORE FLAP LOWER SURFACE AND CLEANED AREA IAW BOEING 737-300 SRM 51-70-10. FABRICATED FILLER AND DOSDR AWXA200500914Wedge · delaminatedMCN - DURING C18 CHECK, DISCOVERED THE LT OUTBOARD AFT FLAP DELAMINATED AT THE INBOARD END OF THE UPPER AND LOWER SURFACES AT WBL 23.68 TO WBL 235.68. MAINTENANCE REMOVED DAMAGED AREA ON THE LT OUTBOARD AFT FLAP AND PREPARED FOR REPAIR IAW BOEING 737-300 SRM SDR 05FDEA01894Hinge · corrodedLT WING O/B FLAP O/B HINGE (WING SIDE), SIDE LINK ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-09 PG 402-407. REPAIR CARRIED OUT AS PER CMM 57-44-09.SDR DHL2005747505Skin · debondedRT WING INBD MID FLAP T/E APPROX 1/2" FROM INBD END IS DISBONDED. CUT OUT DELAM AREA, FAB FILLER AN DOUBLERS ON TRAVELER NR T-828368. CLEANED UP AN PREP REPAIR AREA AN PARTS FAB. BONDED REPAIR PARTS, TREATED AND PRIMED. COMPLETED REPAIR ON RT WING I/B MID SDR DHL2005747504Skin · crackedCRACK IN T/E FLAP LWR SKIN AT NR 3 ATTACH CUT OUT I/B SIDE LT WING. FABRICATED REPAIR DOUBLER, CHEM TREATED AND PRIMED AND INSTALLED REPAIR DOUBLER IAW B727 SRM 57-50-4,51-10-2 AN 51-20-0 PG 1 OF MM AT T/E FLAP LOWER SKIN NR 3 ATTACH CUTOUT I/B SIDE OF LT WINSDR DHL2005747501Skin · crackedCRACK IN T/E FLAP SHIM AT NR 2 ATTACH CUT OUT I/B SIDE LOWER SIDE LEFT WING. FABRICATED REPAIR DOUBLER, CHEM TREATED AN PRIMED AN INSTALLED REPAIR DOUBLER IAW B-727 SRM 57-50-4,51-10-2 AND 51-20-0 PG 1 OF B727 MM, AT T/E FLAP SKIN AT NR 2 ATTACH CUT OUT I/B LSDR 05FDEA01890Hinge · corrodedLT WING, O/B FLAP O/B HINGE (WING SIDE), ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. REPAIRED AS PER CMM 57-44-09 P402-407 AND EA 1-5750-87592A.
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