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 2010FA0000920Panel · corrodedLT WING FUEL TANK ACCESS PANEL 540 FB CORRODED. NO CORROSION REMOVAL LIMITS AVAILABLE IN SRM. PANEL IS LISTED AS PRIMARY STRUCTURE. REPLACED PANEL WITH NEW PART NR D5725130600200.SDR C2XA10SH276Skin · crackedSHV - RT WING UPPER SKIN TRAILING EDGE IS CRACKED AT MIDDLE SPOILER HINGE. REPAIRED SKIN IAW EC5740-01262. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR FDEA201008253122Skin · misrepairedRT WING DROOP L/E INBD EXTERIOR SURFACE FOUND EXISTING REPAIR. EXISTING REPAIR AT RT WING DROOP L/E INBD EXTERIOR SURFACE EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED IAW SRM 57-00-01 FIG 4, VOL I, REV 96. EA8-5750-143409, REPAIR CLASSIFIED AS MAJOR IAW GMM SDR FDEA201008253126Skin · crackedRT WING DROOP, L/E UPPER SKIN FOUND CRACKED. RT WING DROOP L/E UPPER SKIN CRACKED AREA REPAIR CARRIED OUT IAW SRM 57-10-00, FIG 55, VOL I, REV 96. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 111.SDR 2010FA0000889Skin · delaminatedLT WING LOWER L/E PANEL, 521 EB UPPER SURFACE DELAMINATED. REPAIRED PANEL IAW SRM 51-77-13 PARA 2.F(1) FIG 10. PANEL IS LISTED AS PRIMARY STRUCTURE.SDR DALA1026019868Skin · damagedDURING M-CHECK FOUND DAMAGE TO LT WING NR 2 SLAT CTR TRACK CUT OUT SKIN. REPAIRED IAW SRM 57-20-09-801-663A-A, PAGE 226 & SRM 06-10-01-001.SDR TRBACPCP2010051Skin · corrodedLT WING, LOWER SKIN, REAR SPAR AT RIBS 7/8 CORROSION TITANIUM DOUBLER PERMANENT REPAIR. ACCOMPLISHED SRI DO/TS 3217-10-13551 REF ART FORM PL-004-1 FOR DOUBLER FAB, COMPLIED WITH EO E2-57MR-404, REF NDT REPORT AMS 100810-19 FOR HFEC ROTO AND UT VALUES NO DEFESDR FDEA201008233098Skin · misrepairedRT WING FUELING STATION DOOR INBD SIDE FOUND WITH EXISTING REPAIR. EXISTING REPAIR AT RT WING FUELING STATION DOOR INBD SIDE EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW SRM REPAIR SCHEME. RT WING FUELING STATION DOOR INBD SIDE CARRIED OUT REPAIR IAW SDR FDEA201008233097Skin · misrepairedRT WING SLAT TRACK NR10 CUTOUT FOUND WITH EXISTING REPAIR. EXISTING REPAIR AT RT WING SLAT TRACK NR10 CUTOUT EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW SRM REPAIR SCHEME. RT WING SLAT TRACK NR10 CUTOUT, REPAIR CARRIED OUT IAW SRM 57-10-00, FIG 68, VOLSDR FDEA201008233094Skin · misrepairedRT WING UPPER SURFACE FIXED L/E AT XOS 660 FOUND WITH EXISTING REPAIR. EXISTING REPAIR AT RT WING UPPER SURFACE FIXED L/E XOS 660 EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW SRM REPAIR SCHEME. NEW REPAIR ACCOMPLISHED IAW EA NR 8-5730-143420, REPAIR CLASDR FDEA201008233096Skin · misrepairedRT WING SLAT TRACK NR 12 CUTOUT FOUND WITH EXISTING REPAIR. EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW ANY APPROVED DATA. RT WING SLAT TRACK NR 12 CUTOUT REPAIR CARRIED OUT IAW SRM 57-10-00, FIG 68, VOL I, REV 96. EO 8-5100-7-5001, A7 PART 2, REPAISDR TRBACPCP2010044Skin · corrodedLT WING, LOWER SKIN, REAR SPAR AT RIBS 7/8 CORROSION TITANIUM DOUBLER PERMANENT REPAIR. WAITING FOR COMPLETION OF E0 E2-57MR-404 FOR FURTHER DETAILS.SDR C8GA2010000016Skin · corrodedWHILE IN HEAVY MX PERFORMING INSPECTIONS CORROSION WAS NOTED AT THE LT WING, LOWER SKIN FWD OF FRONT SPAR WS 250-287 BEHIND THE NR1 & NR2 KRUGER FLAP. CORROSION FOUND TO BE OUT OF LIMITS. PERFORMED BLEND-OUT IAW RES-W1 NR 2002564-12 LOSS OF MATERIAL IS .095"SDR VNAA2010082700004Winglet · damagedAT MLB, CREW REPORTED A POSSIBLE LIGHTNING STRIKE ON THE AFT PORTION OF THE LOWER LEFT WINGLET. MAINTENANCE INSPECTED THE AIRCRAFT, PERFORMED REPAIRS TO THE LEFT WINGLET AND REMOVED AND REPLACED A STATIC DISCHARGER ON THE RIGHT WINGLET. CHECKS WERE PERFORMEDSDR FDEA201008203058Skin · corrodedLT WING BOTTOM SKIN LOWER SURFACE HAS CORROSION BETWEEN THE CTR SPAR AND THE REAR SPAR IN NUMEROUS SPOPTS JUST INBD OF THE NR1 PYLON. RIB 7-8. REMOVED SEAL, AFT LOWER FAIRING SECTION, AFT PYLON SECTION AND 3 EA. ATTACH BRACKETS PER SRM 51-40-21, PARA'S 5SDR FDEA201008193050Skin · damagedFOUND A REPAIR DOUBLER ON THE R/W TIP UPPER SURFACE ON THE INBD END OF THE SPLICE STRAP THAT REQUIRES A MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED WING TIP IAW SRM 51-31-01, VOL II. REMOVED AND REPLACED TESDR FDEA201008193045Skin · crackedRT WING FIXED L/E TELESCOPIC DUCT CUTOUT FOUND CRACKED. RT WING FIXED L/E TELESCOPIC DUCT CUTOUT CRACKED INBD AND OTBD AREA TRIMMED AND REPAIRED IAW EA NR 8-5710-143702, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.SDR AALA20100818TUL14Winglet · dentedTWO DENTS ON TRAILING EDGE OF LEFT WINGLET. ACCOMPLISHED REPAIR PER SRM 57-31-02-1A.SDR IPXA10M62271Skin · crackedINSPECTION TYPE:1C, RT WING L/E SKIN SPLICE STRAP ANGLE AT XOS 587 CRACKED. REMOVED STRAP, FABRICATED, AND INSTALLED SPLICE STRAP IAW DWG ARB2931.SDR IPXA10M62270Skin · crackedINSPECTION TYPE:1C RT WING L/E LWR EDGE CRACKED AT XOS 550. REMOVED CRACKED DOUBLER, FABRICATED AND INSTALLED DOUBLER IAW DWG ARB2933.SDR AALA20100823AFW03Skin · crackedLEFT WING SKIN AT AFT PITCH LOAD FITTING TENSION BOLT INSPECTION AND REPAIR. OUTBOARD TENSION BOLT HOLE, CRACK FOUND. ALL REPAIRS TO THIS DISCREPANCY WERE ACCOMPLISHED IAW EA B767-57-011899 AND INCLUDED ALL REFERENCE ATTACHMENTS.SDR TAMF20100062SSkin · corrodedDURING SVC C4, FOUND CORROSION ON LWR SKIN BETWEEN RIB 19, WS 668.2 AND RIB 23 WS 772.2 AFTER BLENDING REMAINING THICKNESS WAS FOUND OUT OF LIMITS, REPAIR WAS PERFORMED WITH EWO 767-57-070 AND SR 1-1664985960.SDR IPXA10M62261Doubler · crackedINSPECTION TYPE:1C, IN LT WING L/E COMPARTMENT BETWEEN THE 2 REFUEL/DEFUEL CONNECTIONS, THE CEILING HAS CRACKS AT FASTENERS AT SEVERAL LOCATIONS. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER, DOUBLER AND ANGLES IAW SRM 57-40-02, REPAIR 9, FIG 203.SDR ABXA201008200115Skin · corrodedLEFT WING LOWER SURFACE SPLICE IS CORRODED ON THE UPPER AND LOWER SURFACE IN THE AREA OF THE REFUELING DOOR. REMOVED CORROSION AND REPAIRED AREA IAW REA B657-58923.SDR FDEA201008122948Skin · misrepairedLT WING TIP AFT CAP AT STA XW 930 FOUND EXISTING REPAIR.REPAIR EVALUATED AND FOUND NOT IN ACCORDANCE WITH ANY SRM REPAIR SCHEME. EXISTING REPAIR REMOVED PER SRM 51-31-01 VOLUME II REVISION 96 AND NEW REPAIR CARRIED OUT PER E.A. 8-5730-140434, REPAIR IS CLASSSDR VGQY2010081200081Skin · crackedLEFT WING L/E BULLNOSE SKIN ADJACENT TO NR 13 KRUEGER FLAP O/B LINKAGE FOUND CRACKED. COMPLIED WITH EN1180-10.SDR VGQY2010081200080Beam · crackedLEFT WING L/E BULLNOSE SKIN ADJACENT TO NR 11 KRUEGER FLAP I/B LINKAGE FOUND CRACKED. COMPLIED WITH EN1180-10, REPAIR FOR 05 EA CRACKS ON WING FIXED L/E LWR PANEL SUPPORT BEAM.SDR FDEA201008112927Skin · cracked(10EA) FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSP AT RT WING LWR SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS=690 AND STA XORS=700. CARRIED OUT REPAIR AS PER EA 1-5710-132468. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REV 110.SDR FDEA201008112925Skin · cracked8 FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSP AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS=690 AND STA XORS=700. CARRIED OUT REPAIR AS PER EA 1-5710-132467. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REV. 110.SDR USAA2010081291651Retaining Ring · corrodedPIT - S5 - MAJOR REPAIR - LEVEL 2 CORROSION ON FUEL PANEL 540GB RETAINING RING. REPLACED FUEL PANEL 540GB RETAINING RING.SDR USAA2010081291650Retaining Ring · corrodedPIT - S5 - MAJOR REPAIR - LEVEL 2 CORROSION ON FUEL PANEL 540CB RETAINING RING. REPLACED FUEL PANEL 540CB RETAINING RING.SDR ABXR2010081100036Skin · dentedDURING A STORM DAMAGE REPAIR MX EVENT A DENT WAS DISCOVERED ON THE RT WING L/E. DENT WAS SMOOTH AND FREE FROM SHARP CREASES LOCATED ON THE LOWER SURFACE AND MEASURED 4.00" LONG X 1.20' WIDE 0.162 DEEP. THE DENT WAS COLD WORKED BACK TO ITS ORIGINAL SHAPE AND CSDR FDEA201008102913Access Panel · crackedLT WING L/E LOWER ACCESS PANEL 519CB CUTOUT FWD INBD CORNER SUSPECTED CRACK. TRIMMED OFF AND REPAIR CARRIED OUT AS PER SRM 57-40-02 FIG. 201 REPAIR 7 REVISION 44. THIS REPAIR IS CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 110SDR WRLA20100810438Skin · looseHI-LOK LOOSE AT EXTERNAL LWR SKIN OF RT WING STA XORS 231, S- 31.SDR DALA1019190186Skin · crackedRT WING AFT PITCH LOAD FITTING ATTACHED AREA - (2EA) CRACKS FOUND AT THE INBD ROW MOST FWD BOLT HOLE CRACKED AT LOWER SKIN. FREEZE PLUG REPAIRED IAW ER/A 482265-14AD REV A(DL76L102125).SDR FDEA201008102910Skin · crackedRT WING LOWER SKIN PANEL FASTENER HOLE CRACKED. COMPLIED WITH EA 6-5710-136685.SDR 2010FA0000818Panel · corrodedCORROSION ON LT WING PANEL 574BB. NO CORROSION REMOVAL LIMITS AVAILABLE. PANEL IS LISTED AS PRIMARY STRUCTURE. REPLACED PANEL WITH NEW PANEL.SDR 2010FA0000816Access Panel · corrodedCORROSION ON LT WING FUEL TANK ACCESS PANEL 540 HB. NO CORROSION REMOVAL LIMITS FOUND IN SRM. PANEL IS LISTED AS PRIMARY STRUCTURE. REPLACED PANEL WITH NEW PANEL PN D5725132620051.SDR WRLA20100809434Door · chafedREPAIR - CHAFING ON TELESCOPE DUCT DOOR (P/N: ARM0078-12) OF RT WING AT XOS467.10.SDR DALA1019279001Skin · crackedLT WING L/E SKIN/LOWER SURFACE XOS 243 CRACKED. INSTALLED PERMANENT REPAIR IAW ERA 380953-14MA AND ERA 482367-14.SDR EE4Y100314Panel · delaminatedRIGHT WING T/E UPPER FIXED PANEL P/N 5912735-2 DELAMINATED.SDR EE4Y100312Panel · delaminatedRIGHT WING T/E UPPER FIXED PANEL P/N 5912737-2 DELAMINATED.SDR TRBACPCP2010042ASkin · corrodedAN AREA OF CORROSION WAS FOUND PREVIOUSLY AT LT WING LOWER SKIN T/E AT RIB 13 AND A TEMPORARY REPAIRED ON EO E2-57MR-347R1. NOW DURING C-CHECK FINAL REPAIR IS ACCOMPLISHED BY FOLLOWING REPAIR INSTRUCTIONS (SRI) ISSUED BY ATR AND A SRAS TO APPROVE IT. C/A: WAITSDR FXGAN351CE6Skin · corrodedCORROSION FOUND ON WING SKIN STA 167R TO 182R.SDR FXGAN351CE4Doubler · crackedNR 2 ALTERNATE FUEL TANK ACCESS DOOR DOUBLER CRACKED.SDR FXGAN351CE2Skin · corrodedCENTER WING END RIB SKIN AND LOWER ANGLE FOUND CORRODED.SDR FDEA201008062849Skin · crackedDURING WALKAROUND CHECK, RT WING ADJACENT TO NR 3 SLAT L/E TELESCOPIC DUCT CUT-OUT UPPER SECTION FOUND CRACKED.SDR FDEA201008052844Skin · crackedLT WING FIXED L/E ANTI ICE TELESCOPE DUCT DOOR CUT-OUT. EXTERIOR SKIN FOUND CRACKED. REPAIRED AS PER EA 8-5710-140445, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 110.SDR QML3MR0243Skin · delaminatedDURING INSP, FOUND DELAMINATION/PUNCTURE OF RT UPPER WING SKIN IN AREA OF A PREVIOUS REPAIR. DELAMINATION MEASURES APPROX 16" X 7". PUNCTURE IS SCREW HEAD USED IN REPAIR WAS PUSHED THROUGH SKIN.SDR QML3MR0242Skin · puncturedDURING INSP, FOUND PUNCTURE/CRACK OF UPPER WING SKIN APPROX 1" IN LENGTH CAUSED BE IMPACT FROM ABOVE.
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