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 IXXA10WSAP005SSkin · corrodedDURING ROUTINE C-CHECK INSP, FOUND CORRODED FASTENERS ON RT WING BETWEEN STATION WS404- WS538. REMOVED CORRODED FASTENERS. INSTALLED NEW FASTENERS IAW SRM 51-40-02 REV 101 AND SRM 51-20-01 REV 101.SDR IXXA10WSAP004SAccess Panel · corrodedDURING ROUTINE C-CHECK INSP FOUND CORROSION ON RT WING ACCESS PANEL NR 633AB, 642AB, 642BB AND 642CB. REMOVED CORROSION. FOUND TO BE WITHIN LIMIT’S. PERFORMED NDT. NO CRACK’S OR CORROSION. CLEANED, TREATED AND PRIMED AREA IAW SRM 57-20-01 FIGURE 201 REV 10SDR IXXAWSAP002SAccess Panel · crackedDURING ROUTINE C-CHECK INSP, FOUND RT WING FUEL PUMP ACCESS PANEL NR 631AB CRACKED. REMOVED CRACKED ACCESS PANEL. INSTALLED NEW PANEL IAW MM 20-11-000 REV 97.SDR USAA2010012090151Panel · debondedSAL - BC7 - MAJOR REPAIR - DEBOND ON LEFT WING CLOSING PANEL 540DZ. REPLACED LEFT WING CLOSING PANEL 540DZ IAW A320 AMM 57-27-11.SDR IPXA09B58032Skin · delaminatedRT WING INBD MID FLAP LWR SURFACE DELAM 2" 64.5 FROM INBD EDGE 13" FROM BOTTOM. REPAIRED IAW EO B747-5750-36113-A COMPOSITE REPAIR.SDR SWAA098035Skin · crackedDURING SCHEDULED 2HC2 CHECK, FOUND LT WING UPPER WING SKIN CRACKED AT WBL 157. REPAIRED SKIN PER EA.SDR IXXA100006SSkin · crackedLT WING LOWER SKIN CRACKED AT STATION 428.0. REPAIRED SKIN IAW CASTLE SKETCH 20100104028.SDR IXXA100002SSkin · crackedRT WING LOWER SKIN CRACKED BETWEEN FWD AND AFT OF STRINGER 62. REPAIRED SKIN IAW SRM 57-2-1.SDR FDEA200912234509Skin · corrodedDURING INSP LT WING LWR SURFACE FOUND SUSPECT CORROSION UNDER SKIN OF OTBD AILERON AND AROUND HEADS OF FASTENERS. REPAIRED AREA IAW SRM 57-10-00, FIG 85, SHT 3, VOL I.SDR FDEA200912224498Panel · crackedLT WING L/E FOUND CRACK ON CHORD FIXED PANEL. REPAIRED L/E LOWER STRINGER IAW SRM 57-10-00 FIG.49 VOL.1.SDR FDEA200912224497Doubler · crackedLT WING L/E FOUND CRACK ON INTERNAL DOUBLER. REPAIRED DOUBLER IAW SRM 57-10-00 FIG.71 VOL.1SDR ASOA200901454Access Panel · crackedFOUND RT WING LOWER PLANK FUEL ACCESS HOLE 650CB HAS MULTIPLE INDICATIONS NOTED APPROX 5.0: AREA INBD SIDE NON-CRITICAL 70 PERCENT FSH FAILED NDT INSPECTION. COMPLIED WITH EC/TC EO 600-57-81 C/W IAW REO 601R-57-21-030 REV G AND FORWARDED ALL REQUIRED FORMS TOSDR ASOA200901453Access Panel · crackedFOUND LT WING LWR PLANK FUEL ACCESS HOLE 540DB HAS MULTIPLE INDICATIONS AROUND ENTIRE CIRCUMFERENCE OF LANDING 70 PERCENT FSH FAILED NDT INSP, NON-CRITICAL & CRITICAL AREAS. COMPLIED WITH EC/TC EO 600-57-81 C/W IAW REO 601R-57-21-030 REV G AND FORWARDED ALL RSDR ASOA200901452Access Panel · crackedFOUND LT WING LWR PLANK FUEL ACCESS HOLE 540CB HAS 2 INDICATIONS NOTED, INBD SIDE NON-CRITICAL AREA OF LANDING 50 PERCENT FSH APPROX 2.0" IN LENGTH, FAILED NDT INSP. COMPLIED WITH EC/TC EO 600-57-81 C/W IAW REO 601R-57-21-030 REV G AND FORWARDED ALL REQUIRED SDR QXEA2009122401086Access Panel · corrodedLINE CHECK. RT WING FUEL PANEL 624 FT HAS PITTING CORROSION AT SEVERAL LOCATIONS ON MATING SURFACE. REPLACED PANEL.SDR CA091223003Panel · leaking(CAN) DURING ROUTINE INSP OF LOWER WING SURFACE FUEL WAS NOTED LEAKING FOR THE LWR WING AND THE OTBD FUEL VENT. FURTHER INSP IDENTIFIED 2 CRACKS AROUND THE PARAMETER OF THE INSP PANEL WHERE THE FUEL VENT HSG WAS ATTACHED TO THE OUTER PANEL. ACFT WAS DEFUELED,SDR USAA2010010890057Panel · crackedSAL - S4 - MAJOR REPAIR - CRACK ON LEFT WING FUEL TANK CLOSING PLATE BETWEEN RIBS 6 TO RIB 6B. REPLACED LEFT WING FUEL TANK CLOSING PLATE 540DZ BETWEEN RIBS 6 TO RIB 6B IAW A319 AMM 57-27-11.SDR USAA2010011190064Panel · crackedSAL - S4 - MAJOR REPAIR - CRACK ON RIGHT WING FUEL TANK CLOSING PLATE BETWEEN RIBS 5 TO RIB 6. REPLACED RIGHT WING FUEL TANK CLOSING PLATE 640CZ BETWEEN RIBS 5 TO RIB 6 IAW A319 AMM 57-27-11.SDR USAA2010010890052Panel · crackedSAL - S4 - MAJOR REPAIR - CRACK ON RIGHT WING FUEL TANK CLOSING PLATE BETWEEN RIBS 6 TO RIB 6B. REPLACED RIGHT WING FUEL TANK CLOSING PLATE 640DZ BETWEEN RIBS 6 TO RIB 6B IAW A319 AMM 57-27-11.SDR ABXR200912180052Panel · corrodedDURING A ROUTINE HEAVY MX INSP EVENT RT WING T/E PANEL HAS 3 AREAS OF CORROSION/DELAMINATION ALONG THE T/E OF THE PANEL. REMOVED UPPER SKIN AND HONEY COMB CORE, CLEANED CORROSION AND SKIN IAW SRM 51-70-2. ITEM WAS RETURNED TO SERVICE.SDR CA091223001Skin · cracked(CAN) BOTH WINGS, CORRUGATED INNER SKIN CRACK AT MANY PLACES BETWEEN STATION 47.50 THRU 122.50 AND RIBS DAMAGE AT RIVETS JOINT. MANY RIVETS POPPED AT RIBS AND CORRUGATED INNER SKIN JUNCTION. TCCA COMMENTS: AAIR FROM JUL 15/09 SHOWS THAT AIRCRAFT HAS 29411 HSDR FDEA200912154470Doubler · corrodedRT WING T/E CAVITY LANDING GEAR AREA LOWER WING DOUBLER UPPER SURFACE FOUND CORROSIONS. CORROSION REMOVED AND REPROTECTED AT RT WING T/E CAVITY LANDING GEAR AREA LWR WING DOUBLER UPPER SURFACE IAW SRM 51-21-01 REVISION 42 AND FOUND WITHIN LIMIT SRM 57-10-02SDR SWAA097715Skin · crackedDURING SCHEDULED SPV CHECK, FOUND LT WING L/E SKIN CRACKED. REPAIRED SKIN PER SRM.SDR GUUA95157121409ASkin · delaminatedDURING SCHEDULED ROUTINE MX DISCOVERED WING SKIN DELAMINATED AROUND FUEL ACCESS PANEL 632 AT. REMOVED INTERNAL RING CLEAN AREA AND INSTALLED EXTERNAL REPAIR DOUBLER AROUND FUEL ACCESS PANEL.SDR FDEA200912144462Skin · crackedCRACK AROUND FASTENER HOLES (04 EACH) AT RT WING LWR SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS690 TO XORS700 FOUND DURING HFEC. REPAIR CARRIED OUT IAW EA NR1-5710-135698, THIS REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 REVISION 109.SDR FDEA200912144461Skin · crackedCRACK AROUND FASTENER HOLES (06 EACH) AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS690 TO XORS700 FOUND DURING HFEC. REPAIR CARRIED OUT IAW EA 1-5710-135699, THIS REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 REVISION 109.SDR AALA20091216TUL02Skin · damagedDURING AUTO LAND RIGHT WING CONTACTED RUNWAY. AIRCRAFT OUT OF SERVICE FOR INSPECTION AND REPAIR. REPLACED NUMBER 5 SLAT AND CENTER SECTION RETRACT CABLE. REPLACED NUMBER 15 SLAT TRACK AND RIGHT OUTBOARD FLAP WEDGE. REPLACED NUMBER 1 AND 2 MAIN LANDING GEARSDR FDEA200912114419Skin · misrepairedRT WING DROOP L/E INBD LWR CORNER FOUND EXISTING REPAIR. EXISTING REPAIR AT RT WING DROOP L/E INBD LWR CORNER EVALUATED AND FOUND NOT IAW SRM 57-40-01 FIGURE 201 REPAIR 5 REVISION 42. REPAIR CARRIED OUT IAW EA NR 1-5750-137511, TITLE: WINGS - FLIGHT SURFACES SDR ASOA200901438Skin · crackedINDICATIONS NOTED AT LWR WING PLANK ACCESS HOLE, 640DB AT INBD ON PAINTED AREA OF HOLE APPROX 50 PERCENT FULLSCREEN HEIGHT ARE MARKED ON WING. COMPLIED WITH EC/TC EO 600-57-81 C/W IAW REO 601R-57-21-030 REV G.SDR QXEA2009121601069Skin · gougedC5 CHECK-GOUGE ON LT WING L/E AT WS 294.50. BLENDED GOUGE IAW SRM 51-12-00-001-001-A01. BLEND IS WITHIN LIMITS IAW SRM 57-41-00-101-001-A01. TREATED, PRIMED AND PAINTED IAW SRM 51-21-11-001-001-A01, 51-25-06 AND 51-25-16.SDR A6WA201040003Panel · crackedLT OTBD L/E INNER SKIN PANEL CRACKED. REPLACED LT OTBD L/E INNER SKIN PANEL IAW SRM 51-42-06 AND SRM 51-42-13. (K)SDR UALA2009120703764Panel · crackedRT WING UPPER PANEL HAS APPROX 3FT LONG CRACK. ACCOMPLISHED INTERIM REPAIR, REF UA-EVA-73177. ACCOMPLISHED INTERIM REPAIR, REF UA-EVA-73177. WILL NEED PERMANENT REPAIR BY C CHECK. WILL REQUIRE AUTOCLAVE REPAIR OF EXISTING PANEL OR A NEW PANEL.SDR FDEA200912074364Skin · corrodedLT WING UPPER SURFACE GRAVITY FUEL PORT INBD HAS LEVEL 1 CORROSION AROUND CUT-OUT EXTENDING UNDER SKIN APROX 1" TO 1.5" REPAIRED UPPER WING SKIN AROUND LT UPPER FUEL PORT IAW EA NR 6-5730-135142 AND A/B DWG R57349265 AND RAS NR RAS/BAE/1011485/2009 ISSUE 'A DUSDR CA091208008Skin · missing(CAN) AFTER RETURNING FROM A FLIGHT, THE OPERATOR NOTICED A PIECE APROX 4-6 INCHES WIDE OF THE SHROUD SKIN PN C6W1007-37 WAS MISSING, JUST OTBD OF STN 135. THIS SHROUD SKIN IS SECONDARY STRUCTURE. OPERATOR WAS INSTRUCTED TO DO A VISUAL INSP FOR CRACKING OF TSDR FDEA200912034353Skin · cracked(1) EA FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION AT RT LWR SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS=700. REPAIR CARRIED OUT AT RT WING LWR SKIN ACCESS DOOR CUT OUT BETWEEN STA XORS=690 AND STA XORS=700 IAW EA 1-5710-135677. REPSDR UALA2009120103712Panel · damagedSEVERE TURBULENCE ENCOUNTERED. LT WING T/E FIXED PNL 2 FT SEC LOOSE AT FWD END. WORKING WITH EG FOR EVA TO INTERIM REPAIR. FOUND ADDITIONAL DAMAGE TO SPOILER FIT BEYOND LIMIT. WILL REQ REPLACEMENT. HAVE LT WING TE FIXED PNL 2 FT SEC LOOSE AT FWD END. WORSDR GUUA94957113009ASkin · corrodedDURING SCHEDULED ROUTINE INSP, DISCOVERED RT WING UPPER SKIN T/E CORROSION AND DEBOND BETWEEN WS 133.86 TO WS 173.50. REMOVED DAMAGE AND INSTALLED EXTERNAL DOUBLER REPAIR.SDR DHLA2010807503Skin · crackedLEFT WING UPPER SKIN CRACKED STA XRS 74.000 S-9. PERFORMED MAJOR REPAIR ON LT WING UPPER SKIN AT STA XRS 74.000 S-9 IAW SRM 57-2-1, FIG 17.SDR GLBA20091124FSkin · damagedDURING ROUTINE SCHEDULED MX, SEVERAL DAMAGED FASTNER HOLES ON THE RT WING ON THE AFT SPAR LOWER CAP. MX REPAIRED THE AFFECTED AREA IAW EO 09-1900-57-007. RII INSPECTIONS COMPLIED IAW EO 09-1900-57-007. MATERIALS UTILIZED ARE INCLUDED IN THE EO INSTRUCTIONS.SDR SIMA200932709Skin · dentedDURING MAINTENANCE BASE INSPECTION FOUND THE LEFT WING LOWER SKIN TO BE DENTED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED THE LEFT WING LOWER SKIN IAW EO EM-57MR-421. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR UALA2009111903608Panel · debondedAN 8 FT BY 1 FT UNDER WING PANEL JUST AFT OF LT MLG, ABOUT A 6 FT SECTION DISBONDED AND IS MISSING. FOUND ALL SCREWS IN PLACE. TRIMMED NEW PANEL FROM TEMPLATE. DRILLED AND COUNTERSUNK HOLES. PANEL PRIMED, PAINTED AND INSTALLED.SDR FDEA200911173994Skin · crackedCRACKS FOUND ON FASTENER HOLES DURING HFEC OPEN HOLE INSP ON LT WING LWR SKIN PANEL OUTER WING ACCESS DOOR. REPAIR CARRIED OUT EA 1-5710-132277. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REV 108.SDR FDEA200911173993Skin · crackedCRACK FOUND ON THE FASTENER HOLES DURING HFEC OPEN HOLE INSP ON RT WING LOWER SKIN PANEL OUTER WING ACCESS DOOR. REPAIR CARRIED OUT IAW EA 1-5710-132278. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REV 108.SDR FDEA200911173992Skin · crackedLT WING - L/E LWR ACCESS PANEL 518FB INBD FWD CORNER CUT-OUT FOUND CRACK. TRIMMED OFF AND REPAIRED CARRIED OUT IAW SRM 57-40-02 FIG 201 REPAIR 7 REV 42 AND EA 1-5710-132280, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 108.SDR WRLA20091116322Skin · corrodedEXFOLIATION CORROSION - SKIN CTR WING Y=1226~1239 X=-42~-97 WING TANK UPPER SURFACE TOTAL:39 AREA. REPAIRED THE CORROSION AREA IAW EGAT EI W2009A57B-1378 REV 00.SDR WRLA20091116315Skin · corrodedCORROSION - SKIN Y=1226~1228 X=57~61 EXFOLIATION AROUND FASTENERS HEAD CTR WING TANK UPPER SURFACE TOTAL: 3 AREAS. REPAIRED THE CORROSION AREA IAW EGAT EI W2009A57B-1378 REV 00.SDR GUUA94157111409AAccess Panel · delaminatedDURING SCHEDULED ROUTINE MX DISCOVERED RT WING FUEL ACCESS PANEL 631DB LEAKING FUEL. INSTALLED EXTERNAL RING DOUBLER ON WING SKIN AT FUEL ACCESS PANEL 631DB, NO LEAKS NOTED.SDR CA091116007Skin · cracked(CAN) DURING AN INSP, THE UPPER WING SKIN WAS FOUND CRACKED. THE CRACK WAS LOCATED AT THE AFT ATTACHMENT POINT OF THE MAIN FUEL TIP TANK. THE CRACK WAS 3/4 OF AN INCH IN LENGTH JUST FWD OF THE AFT WING SPAR. 2 RIVETS THAT GO THROUGH THE OTBD AILERON ATTACH BRASDR ASAA0946986Skin · crackedLEFT WING UPPER FIXED LE SKIN CRACKED APPROX 14 INCH INBD OF NR 1 PYLON ABOVE NR 1 K FLAP. REPAIRED BY CUTTING OUT DAMAGE INSTALLED FILLER AND DOUBLER.SDR WX0A070468Doubler · crackedDURING BOW 1C/2C/S1/S2/S4, FOUND WING (LT) UPPER BEAVER TAIL DOUBLER CRACKED AT OUTBOARD EDGE. TRIMMED OUT CRACKED AREA AND INSTALLED FILLER PER ESO 80559, DATED 11/5/09 (TEMPORARY REPAIR). ADDRESSED AS REQUIRED.
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