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 UPS08M53107Skin · crackedINSPECTION TYPE:2C RT WING L/E SKIN SPLICE AT XFS669 IS CRACKED. REMOVED CRACKED SPLICE, FABRICATED AND INSTALLED REPLACEMENT IAW DWG ARB3954 AND MD-11 SRM 51-33-01.SDR CA080729007Skin · debonded(CAN) A INSP CARRIED OUT ON WING, SHOWED GAPS IN THE SPAR TO SKIN BOND LINES. DO NOT BELIEVE THIS TO BE AN IMMEDIATE SAFETY ISSUE BUT ARE WORKING QUICKLY AND DILIGENTLY TO GET TO ROOT CAUSE AND CORRECTIVE ACTION.SDR 08FDEA03070Skin · delaminatedPANEL, LEFT WING LOWER SURFACE, FWD OF THE MLG WELL IS DELAMINATED. REMOVED AND REPLACED THE LEFT WING T/E PANEL P/N ARC 0280-503, PO 627171.3 IAW DWG ARC 0448, REV "BG" AND SRM 51-31-01; VOL II.SDR 08FDEA03072Panel · wornLEFT WING INBD L/E PANEL 516 HB IS WORN ON THE EDGE OF THE PANEL. BLENDED PANEL 516 NB AND FOUND TO BE OUT OF LIMITS IAW SRM 57-00-01; VOL I. FABRICATED DOUBLER IAW SRM 57-00-01; VOL I. ALODINED AND PRIMED IAW SRM 51-21-01; VOL II. PAINTED DOUBLER IAW SSDR 08FDEA03069Skin · crackedRIGHT WING L/E PANEL 615 DB IS CRACKED AT A FASTENER HOLE. FABRICATED A NEW REPAIR DOUBLER & LOCATED THE HOLES IAW SRM 57-00-01 & 57-10-00 VOL I PG 12-A FIG 4. ALODINED & PRIMED IAW SRM 51-21-01; VOL II. INSTALLED IAW SRM 51-31-01 VOL II.SDR 2008UALA03974Skin · crackedUPPER LT WING L/E SURFACE, JUST OUTBOARD OF NR 2 ENG, HAS CRACK APPROX 4 FEET IN LENGTH, ORIENTATED IN A FORE TO AFT DIRECTION. DOUBLER MANUFACTURED. LAID UP & DRILLING FASTENER HOLES. DOUBLER REPAIR INSTALLED.SDR 2008FA0000537Skin · corrodedSURFACE CORROSION (PITTING) DISCOVERED ON BOTH WINGS LOWER SURFACES ADJACENT TO AND OB OF WHEEL WELLS, CORROSION DEEMED UNUSUALLY SEVERE. (K)SDR 08FDEA03054Skin · corrodedFUEL TANK ACCESS CUTOUT 641EB HAS CORROSION. REPAIR CARRIED OUT IAW SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.SDR 08FDEA03068Skin · corrodedFUEL ACCESS PANEL CUTOUT 541CB HAS CORROSION. REPAIR CARRIED OUT IAW B757-200 SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.SDR 08FDEA03067Skin · corrodedFUEL ACCESS PANEL CUTOUT 541BB HAS CORROSION. REPAIR CARRIED OUT IAW B757-200 SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.SDR 08FDEA03066Skin · corrodedFUEL TANK ACCESS CUTOUT 641AB HAS CORROSION. REPAIR CARRIED OUT IAW B757-200 SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.SDR 08FDEA03065Skin · corrodedFUEL TANK ACCESS CUTOUT 641BB HAS CORROSION. REPAIR CARRIED OUT IAW B757-200 SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.SDR 08FDEA03064Skin · corrodedFUEL TANK ACCESS CUTOUT 641CB HAS CORROSION. REPAIR CARRIED OUT IAW B757-200 SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.SDR 08FDEA03063Skin · corrodedFUEL TANK ACCESS CUTOUT 641DB HAS CORROSION. REPAIR CARRIED OUT IAW B757-200 SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.SDR 08FDEA03062Skin · corrodedFUEL TANK ACCESS CUTOUT 642DB HAS CORROSION. REPAIR CARRIED OUT IAW B757-200 SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.SDR 08FDEA03061Skin · corrodedFUEL TANK ACCESS CUTOUT 642CB HAS CORROSION. REPAIR CARRIED OUT IAW B757-200 SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.SDR 08FDEA03060Skin · corrodedFUEL TANK ACCESS CUTOUT 642BB HAS CORROSION. REPAIR CARRIED OUT IAW B757-200 SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.SDR 08FDEA03059Skin · corrodedFUEL TANK ACCESS CUTOUT 642AB HAS CORROSION. REPAIR CARRIED OUT IAW B757-200 SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.SDR 08FDEA03058Skin · corrodedFUEL TANK ACCESS CUTOUT 641MB HAS CORROSION. REPAIR CARRIED OUT IAW SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.SDR 08FDEA03057Skin · corrodedFUEL TANK ACCESS CUTOUT 641LB HAS CORROSION. REPAIR CARRIED OUT IAW B757-200 SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.SDR 08FDEA03056Skin · corrodedFUEL TANK ACCESS PANEL CUTOUT 641KB HAS CORROSION. REPAIR CARRIED OUT IAW B757-200 SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.SDR 08FDEA03055Skin · corrodedFUEL TANK ACCESS CUTOUT 641JB HAS CORROSION. REPAIR CARRIED OUT IAW B757-200 SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.SDR 08FDEA03053Skin · corrodedFUEL TANK ACCESS CUTOUT 641FB HAS CORROSION. REPAIR CARRIED OUT IAW B757-200 SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.SDR 08FDEA03052Skin · corrodedFUEL TANK ACCESS CUTOUT 641HB HAS CORROSION. REPAIR CARRIED OUT IAW B757-200 SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.SDR 08FDEA03051Skin · corrodedFUEL TANK ACCESS CUTOUT 641GB HAS CORROSION AND BARE METAL. REPAIR CARRIED OUT IAW B757-200 SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.SDR FDEA200807223014Skin · crackedRT WING L/E FOUND CRACK ON LEADING EDGE LOWER EXTERNAL SIDE. REPAIRED SKIN IAW SRM 57-10-00 FIG 68 SHT 2 VOL I.SDR 08FDEA03015Skin · crackedRT WING DROOP LEADING EDGE TOP SURFACE FOUND CRACKED. REPAIR CARRIED OUT AT RT WING DROOP LEADING EDGE TOP SURFACE AS PER SRM 57-10-00 FIG 30 VOL I. REPAIR CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-100.SDR 08FDEA03016Panel · corrodedFOUND CORROSION AT TRANSITION OF SHROUD BOX AND TOP SKIN PANEL RT OUTER WING REPAIR PERFORMED BY CORROSION BLEND OUT, RIB CUT AND INSTALLING AN INFILL AND EXTERNAL PLATES IAW DRAWING R572-40274, APPROVED BY RAS /BAE/1007435/2008 ISS A AND EA 6-5720-123005.SDR 08FDEA03014Skin · crackedRT WING L/E FOUND CRACK ON LEADING EDGE LOWER EXTERNAL SIDE.SDR ASAA0843327Skin · corrodedEXFOLIATION CORROSION FOUND ON UPPER WING SKIN AT FS 608.5 RBL 62 REPAIRED IAW EA 5710 01153.SDR ASAA0843326Skin · corrodedEXFOLIATION CORROSION FOUND ON UPPER WING SKIN AT FS 592 RBL 63 REPAIRED IAW EA 5710 01153.SDR ASAA0843325Skin · corrodedEXFOLIATION CORROSION FOUND ON UPPER WING PLANK AT FS591, RBL67 REPAIRED IAW EA 5710 01153.SDR ASAA0843324Skin · corrodedEXFOLIATION CORROSION FOUND ON UPPER WING PLANK AT FS 661, RBL 57 REPAIRED IAW EA-5710 01153.SDR 08FDEA03003Panel · wornLEFT WING T/E PANEL 541 BB IS WORN. BLENDED PANEL 541 BB IAW DC/MD-10 SRM 57-00-01; FIG 1-A; VOL I. FOUND TO BE OUT OF LIMITS IAW DC/MD-10 SRM 57-00-01; FIG 1-A; VOL I AND SRM 57-32-01; VOL I. LOCATED AND DRILLED HOLES IAW DC/MD-10 SRM 51-31-01, VOL II.SDR 08FDEA03002Panel · corrodedRIGHT WING T/E PANEL 641 BB HAS CORROSION AROUND FASTENER HOLES. REMOVED THE CORROSION IAW SRM 51-21-01; PG 28; VOL II. ORIGINAL MATERIAL 0.032 IAW SRM 57-32-01; FIG 2; VOL III. MATERIAL LOSS 0.010. REMAINING MATERIAL 0.022. FOUND TO BE OUT OF LIMITS IASDR KCSA081331Skin · corrodedLT WING SKIN AT WS 993 TO WS 995 HAS CORROSION. (A)SDR 08FDEA02963Panel · delaminatedLEFT WING T/E PANEL 541 IB IS GOUGED. REMOVED DAMAGE. FABRICATED REPAIR DOUBLERS AND FILLERS. PREPARED FOR BONDING. BONDED AND CURED REPAIR DOUBLERS AND FILLERS IAW DC/MD-10 SRM 51-71-00; VOL II. APPLIED SEALANT AND PRIMER IAW DC/MD-10 SRM 51-71-00; VOL ISDR 08FDEA02964Panel · chafedLEFT WING L/E PANEL 518 FB IS CHAFED. REPAIRED THE LT WING INBD L/E PANEL 518 FB BY REMOVING THE DAMAGED AREA AND BONDED A FILLER AND DOUBLER IAW SRM 51-71-00; VOL II. PRIMED AND PAINTED IAW SRM 51-21-02; VOL II.SDR 08FDEA02961Panel · dentedLEFT WING FAIRING PANEL 535BL HAS NUMEROUS DENTS. REPAIRED DENTS IN THE LEFT WING FAIRING PANEL 535 BL WITH REPAIR DOUBLERS IAW SRM 51-71-00; VOL II.SDR 08FDEA02962Panel · dentedLEFT WING FAIRING PANEL 536 BL HAS DENTS. REPAIRED THE DENTS ON THE LT WING OUTBD FAIRING PANEL 536 BL WITH REPAIR DOUBLERS IAW SRM 51-71-00; VOL II.SDR 08FDEA02957Skin · crackedLT WING OUTBD FLAP CRACK ON LOWER SKIN. REPAIRED SKIN IAW SRM 57-10-00 FIG 85 VOL I.SDR 08FDEA02953Skin · corrodedFOUND CORROSION ON LT WING TOP SKIN RIB 26-27 LT REPAIR PERFORMED BY BLEND OUT CORROSION, NDT FOR CORROSION FREE CONDITION IAW RAS/BAE/1007630/2008 ISS A, APPROVED BY EA 6-5720-123019.SDR 08FDEA02939Panel · crackedPANEL 3617 BOTTOM AFT END CRACKED REPAIRED PANEL 3617 REF SRM 51-40-9 STEPS 3D, 4E, 4F, PGS 3-7 AND AMM 51-20-051 PG1, AMM 51-20-151-7 PG 1. THIS IS CLASSIFIED AS A MINOR REPAIR.SDR 08FDEA02920Skin · corrodedFOUND CORROSION AT LT WING BOTTOM SKIN UPPER SURFACE RIB 8. REPAIR PERFORMED BY BLEND OUT THE CORROSION, NDT FOR CORROSION FREE CONDITION INSTALLING STEEL PLATES IAW RAS/BAE/1007329/2008 ISS A, APPROVED BY EA 6-2910-120038.SDR 08FDEA02919Skin · wornFOUND ELONGATED HOLES ON LT WING BOTTOM SKIN, RIB 8, IN AREA OF HYDRAULIC FITTINGS. REPAIR PERFORMED BY REAM UP THE HOLES AND INSTALL REPAIR BUSHES IAW DRAWING R571-50532, APPROVED BY EA 6-2910-120038.SDR 08FDEA02918Skin · wornFOUND ELONGATED HOLES ON RT WING BOTTOM SKIN, RIB 8, IN AREA OF HYDRAULIC FITTINGS REPAIR PERFORMED BY REAM UP THE HOLES AND INSTALL REPAIR BUSHES IAW DRAWING R571-50532, APPROVED BY EA 6-2910-120038.SDR SWAA2013012311700Skin Panel · crackedLEFT WING LOWER SKIN PANEL ABOVE THE O/B MID SPAR FITTING HAS A 0.55" CRACK. (REF NRC B583433) PERFORMED INTERIM REPAIR PER EA 1-A57-3318. REINSPECT EVERY 720 DAYS FOR CRACK PROPAGATION. PERFORM A PERMANENT REPAIR ON OR BEFORE THE 28Y CHECK.SDR KCSA081319Skin · corrodedLT WING LOWER SKIN CORRODED AT APPROX 1300. (A)SDR 2008FA0000507Skin · damagedAIRCRAFT WAS BROUGHT IN FOR INSPECTION OF DOUBLER ROW OF RIVETS AT WING STA 209.016. RIVETS WERE FOUND SMOKING AND PAINT WAS POPPED ON THE RIVET HEADS. USED BOROSCOPE TO INSPECT RIVET BUCKTAILS. FOUND ALL OF THE RIVETS IN THE DOUBLER ROW OF THE SKIN LAP AT SDR 2008FA0000503Skin · damagedAIRCRAFT WAS BROUGHT IN FOR PHASE INSPECTION. DURING INSPECTION A DOUBLER ROW OF RIVETS AT WING STATION 209.016 WERE FOUND WITH PAINT POPPING OFF OF THE RIVET HEADS. USED BOROSCOPE TO INSPECT RIVET BUCKTAILS. FOUND ALL OF THE RIVETS IN THE DOUBLE ROW OF THE
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