JASC 5730
Service difficulty reports · 27,269
Reports filed under 5730 · Wing, Plate/Skin, 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 = '5730' 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 = '5730' 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 KCSA081146Skin · corrodedCORROSION AT CENTER WING TANK UPPER SKIN SEAM AT STA 1050 RBL 92.SDR 08FDEA00778Panel · puncturedRT WING, INBD UPPER T/E FIXED PANEL P/N ARC0269-502 HAS A PUNCTURE ON THE LOWER SIDE. REMOVED DAMAGE FROM THE AREA; PREPPED AREA FOR BONDING; FABRICATED REPAIR CORE PLUG & DOUBLERS; LAYED UP AND BONDED IAW SRM 51-31-01 VOL III FIG 4 & SRM 51-71-00 VOL II SDR 08FDEA00777Panel · dentedRT MLG AREA PANEL ABOVE THE MLG ACTUATOR IS DENTED. REMOVED DAMAGED AREA, PREPPED AREA FOR BONDING, FABRICARED REPAIR CORE PLUG & DOUBLERS. LAYED UP & BONDED IAW SRM 51-31-01 VOL III FIG 1 & 51-71-00 VOL II PG 1. SEALED, PRIMED & PAINTED IAW SRM 51-31-01 VOL SDR DLM90080604Skin · gougedREPAIR ON RT WING L/E STA XCW 121 IS GOUGED. REPAIRED RT WING L/E, IAW DELTA ERA 467132-14 REV ORIG DATE ISSUED 26MAR08 VIA AAR EA 12567 REV I/R DATE ISSUED 26MAR08.SDR HALA0800381Skin · corrodedLEVEL 1 CORROSION ON RT WING LOWER SURFACE, STRINGER L15, BETWEEN RIBS 5 AND 7, CORROSION ON FASTENER HEADS. AREA PAINT STRIPPED IAW SOPM 20-30-02, REV 104. LIGHT CORROSION REMOVED FROM FASTENER HEADS BY GLASS BEADING IAW SRM 51-10-02, REV 76, NEGLIGIBLE MATSDR HALA0800382Skin · corrodedLEVEL 1 CORROSION ON RT WING LOWER SURFACE, RIB 8 AFT OF STRINGER L-6, CORROSION ON FASTENER HEADS. AREA PAINT STRIPPED IAW SOPM 20-302, REV 104. LIGHT CORROSION REMOVED FROM FASTENER HEADS BY GLASS BEADING, IAW SRM 51-10-02, REV 76. NEGLIGIBLE MATERIAL REMSDR HALA0800380Skin · corrodedCORROSION ON RT WING LOWER SURFACE, RIB 7 AFT OF STRINGER L6, SURROUNDING RIVET HEADS. REPAIR IN WORK.SDR HALA0800379Skin · corrodedCORROSION ON RT WING LOWER SURFACE, RIB 8 FWD OF STRINGER L10, CORROSION FOUND SURROUNDING RIVET HEADS. REPAIR IN WORK.SDR UPS08551762Skin · chafedINSPECTION TYPE:C-2 LW LWR SKIN T/E CHAFED IB AND OB OF NR 1 FLAP TRACK. REPAIRED LT WING LWR SKIN IAW ATS ER 08-1340.SDR 08FDEA00736Panel · damagedLT WING MOST INBD LOWER T/E PANEL AT THE FUEL TANK SUMP PANEL HAS DENTS AND THE REPAIR DOUBLER IS MISSING. REPLACED MISSING DOUBLER IAW SRM 51-71-11 VOL II. REFINISHED REPAIR IAW SRM 51-71-00 VOL II & SRM 51-21-01 VOL II.SDR 08FDEA00735Skin · gougedRT WING PANEL 641LB INTERIOR SKIN IS GOUGED (2 PLACES). REPAIRED THE TWO GOUGED AREAS BY REMOVING THE DAMAGE. FABRICATING A NEW CORE PLUG, FILLER & DOUBLERS USING BONDING REPAIRS IAW SRM 51-71-00; VOL II. ALODINED, PRIMED, SEALED AND PAINTED IAW SRM 51-21-02SDR 08FDEA00732Panel · delaminatedFOUND DELAMINATION ON PANEL NR 535BR AT EXTERNAL SKIN. REPAIRED THE DELAMINATED AREA BY REMOVING DAMAGED AREA, & BY FABRICATING & BONDING A FILLER & DOUBLER IAW SRM 51-71-00 VOL II. RESTORED FINISH IAW SRM 51-71-00; VOL II.SDR 08FDEA00731Skin · delaminatedFOUND DELAMINATION ON PANEL NR 535HL EXTERIOR SKIN. REMOVED DAMAGE & REPAIRED PANEL IAW SRM 51-21-01; VOL II. ALODINED & PRIMED REPAIR AREA IAW SRM 51-21-01 VOL II. PAINTED PANEL IAW SRM 51-21-01; VOL II. MINOR REPAIRSDR 08FDEA00730Skin · gougedGOUGED INTERNAL SKIN ON PANEL 535GL, ON THE PARTS RACK. REPAIRED INTERNAL SKIN PANEL 535 GL BY REMOVING THE DAMAGE & BLENDING & REMOVING BURRS. FABRICATED REPAIR DOUBLER & BONDED DOUBLER TO THE PANEL. VACUUMED COMPLETING CURE OF BOND & REMOVING EXCESS ADHESSDR 08FDEA00723Panel · delaminatedLT WING PANEL 541GB IS DELAMINATED ON THE BACK SIDE. REPAIRED PANEL 541GB LT WING PANEL BY FABRICATING AND BONDING A SKIN DOUBLER & REPAIR PARTS IAW SRM 51-71-00; VOL II CH 17 & ARC0264 DWG. MINOR REPAIRSDR 08FDEA00722Panel · puncturedLT WING PANEL 541CR IS PUNCTURED AND DELAMINATED ON THE LOWER SIDE. REMOVED THE DAMAGE AND REPAIRED PANEL IAW SRM 51-71-00; VOL II. ALODINED AND PRIMED THE REPAIR AREA IAW SRM 51-21-01; VOL II. MINOR REPAIR.SDR 08FDEA00721Access Panel · delaminatedLT WING PANEL 541BB IS DELAMINATED ON THE BACK SIDE. REPAIRED LT WING CONTROL ACCESS PANEL 541 BB BY FABRICATING & BONDING NEW INNER & OUTER SKINS, DOUBLERS & CORE IAW EA 8-5710-116968;SDR 2008UALA01174Skin · corrodedFOUND CORROSION ON CENTER WING UPPER SURFACE AT BS 965, BL0. MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION. FABRICATED & INSTALLED REPAIR SHIMS. ACCMP HFEC OF HOLES, NO DEFECT NOTED OVER SIZED HOLES.SDR 08FDEA00682Panel · corrodedRT WING PANEL 650 MB; INTERIOR SURFACE HAS FRETTING AROUND THE FASTENER HOLES. CLEANED AREAS AROUND THE FASTENER HOLES; CHECKED THE LIMITS AND FOUND TO BE OUT OF LIMITS IAW A310-300 SRM 57-20-16; PAGE 108; FIG 103. REPLACED WITH NEW PART A5735003900000; PO6SDR 08FDEA00681Panel · corrodedRT WING VENT TANK PANEL 650 LB, HAS FRETTING AT THE INTERIOR FASTENER HOLES. CLEANED FRETTING AROUND THE FASTENER HOLES; CHECKED LIMITS AND FOUND TO BE OUT OF LIMITS IAW A310-300 SRM 57-20-16; PAGE 108; FIG 103. REPLACED WITH NEW PART A5735003900000 PO 61028SDR UPS08851870Skin · crackedINSPECTION TYPE:C3 LEFT WING O/B LEADING EDGE EXTERIOR SKIN CRACKED AROUND SCREW HOLE AT I/B END. CUT OUT DAMAGE, FABBED AND INSTALLED REPAIR DOUBLER IAW SRM 57-2-1 FIG H.SDR UPS08851822Skin · crackedINSPECTION TYPE:C3 POSSIBLE CRACK AT DRAIN HOLE, LT WING OB LE IB SECTION LOWER SURFACE NEAR STA XFS 598. STOP DRILLED CRACK, FAB AND INSTALLED REPAIR DOUBLER IAW SRM 57-3-1, E O DC85720-4087-B, 51-1-8.SDR TAMF20080001SAccess Door · corrodedDURING INSPECTION CHECK, FOUND LT WING 541AB MAIN FUEL TANK ACCESS DOOR OUTER SKIN WITH A SCRATCH AND CORROSION. DAMAGED AREA WAS REPAIRED IAW EWO 767-57-038 AND BOEING SERVICE REQUEST 1-771920168. THIS REPAIR IS CLASSIFIED AS MAJOR REPAIR. FAA FORM 8100-9 SDR UPS08851790Skin · gougedINSPECTION TYPE:C3 RT WING OB LE UPPER ATTACH SCREW HOLE GOUGED AND DAMAGED ABOVE PNL 518 C. CUT OUT DAMAGE, FABBED AND INSTALLED REPAIR DOUBLER,IAW SRM 57-2-1 FIG 38, 51-1-8, 57-2-0, 57-3-1.SDR UPS08851789Skin · gougedINSPECTION TYPE:C3 RT WING OB LE UPPER SCREW HOLE GOUGED AND DAMAGED,IB OF ACCESS PANEL51 7B. CUT OUT DAMAGE, FABBED REPAIR AND INSTALLED IAW SRM 57-2-1,51-3-1, 51- 1-8SDR UIEA200800065Panel · crackedLT WING UPPER FIXED T/E PANEL AT WS 744.0 HAS A CRACK 6 INCHES FROM AFT EDGE OF PANEL. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 51-40-09, FIG 2, SHEET 1, 2 AND 5 PREPREG 250 DEGREES F CURE PER SRM 51-40-12. REF: ATLAS AIR EO NR 4757A420.SDR 2008FA0000258Tape · looseDURING FLIGHT, THE FABRIC PATCH CAME OFF. THE AC WAS LANDED WITH SOME DIFFICULTY BUT WITHOUT INCIDENT. IT IS SPECULATED THE AIR STREAM GOT UNDER A LOOSE TAPE AND LIFTED THE ENTIRE PATCH FROM THE WING INCLUDING RIPPING THE FABRIC CLIPS OUT OF THE RIBS. IT ISSDR AMTA200800187Skin Panel · corrodedRT WING FUEL TANK ACCESS 631BB HAS PITTING CORROSION ON LOWER SKIN PANEL AND CLAMP RING. REMOVED PITTING CORROSION ON RT WING FUEL TANK ACCESS LANDING IAW B737-800, SRM 51-10-02-1A-1, ORG MAT .200, MAT LOSS .002, REM MAT .198, FOUND TO BE WITHIN LIMITS IAW SRSDR AMTA200800181Skin Panel · corrodedLT WING FUEL TANK ACCESS 532DB HAS PITTING CORROSION ON LWR SKIN PANEL LANDING AND CLAMP RING. REMOVED PITTING CORRODION ON LT WING FUEL TANK ACCESS LANDING, SRM 51-20-002-0G, ORG MAT .204, MAT LOSS .004, REM MAT .200, FOUND TO BE WITHIN LIMITS IAW SRM 57-20-SDR AMTA200800180Skin Panel · corrodedLT WING FUEL TANK ACCESS 531AB HAS PITTING CORROSION ON LOWER SKIN PANEL LANDING AND CLAMP RING. REMOVED PITTING CORROSION ON LT FUEL TANK ACCESS LANDING IAW SRM 51-10-02-0G, ORG MAT .202, MAT LOSS .005, REM MAT .197, FOUND TO BE WITHIN LIMITS IAW SRM 57-20-0SDR AMTA200800179Skin Panel · corrodedLT WING FUEL ACCESS 531BB HAS PITTING CORROSION ON LOWER SKIN PANEL LANDING AND CLAMP RING. REMOVE PITTING CORROSION ON LT FUEL TANK ACCESS LANDING IAW B737-800, SRM 51-10-02-0G, ORG MAT .201, MAT LOSS .004, REM MAT .197, FOUND TO BE WITHIN LIMITS IAW SRM 578SDR AMTA200800178Skin Panel · corrodedLT WING FUEL TANK ACCESS 532AB HAS PITTING CORROSION ON LOWER SKIN PANEL LANDING AND CLAMP RING. REMOVED PITTING CORROSIN ON LT WING FUEL TANK ACCESS LANDING IAW B737-800, SRM 51-20-02-0G, ORG MAT .202, MAT LOSS .002, REM MAT .200, FOUND TO BE WITHIN LIMITS ISDR AMTA200800177Skin Panel · corrodedLT WING FUEL TANK ACCESS 532BB HAS PITTING CORROSION ON LOWER SKIN PANEL LANDING AND CLAMP RING. REMOVED PITTING CORROSION ON LT WING FUEL TANK LANDING IAW B737-800 SRM 51-10-02-0G, ORG AT .207, MAT LOSS .005, REM MAT .202, FOUND TO BE WITHIN LIMITS IAW SRM 5SDR AMTA200800176Skin Panel · corrodedLT WING FUEL TANK ACCESS 532CB HAS PITTING CORROSION ON LOWER SKIN PANEL LANDING AND CLAMP RING. REMOVED PITTING CORROSION ON LT FUEL TANK ACCESS LANDING 532 CB IAW B737-800, SRM 51-10-02-0G, ORG MAT .202, MAT LOSS .003, REM MAT .199, FOUND TO BE WITHIN LIMITSDR AMTA200800175Skin Panel · corrodedLT WING FUEL TANK ACCESS 532EB HAS PITTING CORROSION ON LOWER SKIN PANEL LANDING AND CLAMP RING. REMOVED PITTING CORROSION ON LT WING FUEL TANK ACCESS LANDING 532EB IAW, SRM 51-20-02-0G, ORG MAT .204, MAT LOSS .001, REM MAT .203, FOUND TO BE WITHIN LIMITS IAWSDR AMTA200800174Skin Panel · corrodedLT WING FUEL TANK ACCESS 532FB HAS PITTING CORROSION ON LWR SKIN PANEL LANDING AND CLAMP RING. REMOVED PITTING CORROSION ON LT WING FUEL TANK ACCESS LANDING IAW B737-800, SRM 51-10-02-0G, ROG MAT .205, MAT LOSS .003, REM MAT .202, FOUND TO BE WITHIN LIMITS IASDR AMTA200800173Skin Panel · corrodedLT WING FUEL TANK ACCESS 532GB HAS PITTING CORROSION ON LWR SKIN PANEL LANDING AND CLAMP RING. REMOVED PITTING CORRIOSION ON LWR FUEL TANK ACCESS LANDING 532GB IAW SRM 51-10-02-0G, ROG MAT .202, MAT LOSS .002, REM MAT .200, FOUND TO BE WITNIN LIMITS IAW SRM 5SDR AMTA200800172Skin Panel · corrodedLT WING FUEL TANK ACCESS 532HB HAS PITTING CORROSION ON LWR SKIN PANEL LANDING AND CLAMP RING. REMOVED PITTING CORROSION ON LWR FUEL TANK ACCESS LANDING 532HB IAW B737-800, SRM 51-01-02=0G, ORG MAT .206, MAT LOSS .004, REM MAT .202, FOUND TO BE WITHIN LIMITS SDR AMTA200800170Skin Panel · corrodedLT WING FUEL TANK ACCESS 532KB HAS PITTING CORROSION ON LWR SKIN PANEL LANDING AND CLAMP RING. REMOVED PITTING ON LWR FUEL TANK ACCESS LANDING 532KB IAW B737-800, SRM 51-10-01-0G, ORG MAT .205, MAT LOSS .003, REM MAT .202, FOUND TO BE WITHIN LIMITS IAW SRM 57SDR AMTA200800169Skin · corrodedLT WING FUEL TANK ACCESS 532LB HAS PITTING CORROSION ON LOWER SKIN PANEL LANDING. REMOVED PITTING CORROSION ON LWR FUEL TANK ACCESS LANDING IAW SRM 51-01-02-0G, ORG MAT .205, MAT LOSS .003, REM MAT .202, FOUND TO BE WITHIN LIMITS IAW 57-20-01-1A, PERFORMED FLSDR UPS08851868Skin · crackedINSPECTION TYPE:C3 SKIN AROUND LT CENTER L/E INBOARD HOIST ATTACH POINT IS BULGING AND CRACKED. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR DOUBLERS IAW SRM 51-1-21, 57-2-00 FIG 2A, 51-1-8 , 51-1-26.SDR AMTA200800168Skin Panel · corrodedLT WING FUEL TANK ACCESS 532MB HAS PITTING CORROSION ON LOWER SKIN PANEL LANDING AND CLAMP RING. REMOVED PITTING CORROSION ON LT FUEL TANK ACCESS LANDING 532MB IAW SRM 51-01-02-0G, ORG MAT .176, MAT LOSS .003, REM MAT .173, FOUND WITHI8N LIMITS IAW SRM 57-20-SDR AMTA200800166Skin Panel · corrodedLT WING FUEL TANK ACCESS 532PB HAS PITTING CORROSION ON LOWER SKIN PANEL LANDING AND CLAMP RING. REMOVED PITTING CORROSION ON LT FUEL TANK ACCESS LANDING 532PB IAW SRM 51-01-02-0G, ORG MAT .175, MAT LOSS .003, REM MAT .170, FOUND WITHIN LIMITS IAW SRM 57-20-0SDR AMTA200800165Skin Panel · corrodedLT WING FUEL TANK ACCESS 532QB HAS PITTING CORROSION ON LOWER SKIN PANEL LANDING AND CLAMP RING. REMOVED PITTING CORROSION ON LT FUEL TANK ACCESS LANDING 532QB, IAW B737-800, SRM 51-01-02-0G, ORG MAT .176, MAT LOSS .006, REM MAT .170, FOUND WITHIN LIMITS IAW SDR AMTA200800164Skin Panel · corrodedLT WING FUEL TANK ACCESS 532RB HAS PITTING CORROSION ON LOWER SKIN PANEL LANDING AND CLAMP RING. REMOVED PITTING CORROSION ON LT FUEL TANK ACCESS LANDING 532RB IAW B737-800, SRM 51-01-02-0G ORG MAT .176, MAT LOSS .004, REM MAT .172, FOUND WITHIN LIMITS IAW SRSDR AMTA200800163Skin Panel · corrodedLT WING FUEL TANK ACCESS 532AB HAS PITTING CORROSION ON LOWER SKIN PANEL LANDING AND CLAMP RING. REMOVED PITTING CORROSION ON LT WING FUEL TANK ACCESS LANDING IAW SRM 51-01-02-0G, ORG MAT .176, MAT LOSS .001, REM MAT .175, FOUND WITHIN LIMITS IAW 57-20-01-1A,SDR HALA0800360Skin · corrodedLEVEL 1 CORROSION ON LEFT WING TOP SURFACE, AT REAR SPAR, LEFT WING STATION 802. REPAIRED PER SRM 57-20-01.SDR 08FDEA00643Skin · crackedHFEC OPEN HOLE INSPECTION CARRIED OUT AND FOUND 7 HOLES WITH CRACK INDICATION AT LT WING ACCESS DOOR 536AB CUT OUT. REPAIR CARRIED OUT AS PER EA 1-5710-109925, PART 1. REPAIR CLASSIFIED AS MAJOR AS PER PER GMM 6-2-100.SDR 08FDEA00635Panel · crackedLT WING L/E SKIN PANEL BY NR 2 SLAT O/B TRACK AREA IS CRACKED AT FASTENER HOLE. REMOVED SKIN PANEL IAW SRM 51-40-02. FABRICATED NEW SKIN PANEL ON MAE TRAVELER NR T7/687621FROM 7075 - T6 - .050C IAW SRM 51-10-02. INSTALLED FABRICATED SKIN PANEL IAW SRM 51-40SDR DHL2008753506Skin · cracked"C" CHECK LT WING L/E CRACKED AT NR 4 SLAT O/B TRACK CUTOUT. REMOVED PAINT LT WING L/E NR 4 SLAT O/B TRACK IAW MM 51-20-1. STOP DRILLED WITH .250 AT THE END OF THE CRACK IAW SRM 51-10-1. FAB DOUBLER REPAIR IAW SRM 57-30-4 FIG 11 AND SRM 51-20-1 FIG 7. TREA
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