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.

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.Aug 27, 2010 · N508JL · Airbus A320232SDR 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.Aug 27, 2010 · N16954 · Emb EMB145LRSDR 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 Aug 25, 2010 · N562FE · Doug MD1010FSDR 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.Aug 25, 2010 · N562FE · Doug MD1010FSDR 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.Aug 25, 2010 · N508JL · Airbus A320232SDR 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.Aug 23, 2010 · N777NC · Doug DC951SDR 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 DEFEAug 23, 2010 · N426AT · Aerosp ATR72212SDR 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 Aug 23, 2010 · N562FE · Doug MD1010FSDR 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, VOLAug 23, 2010 · N562FE · Doug MD1010FSDR 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 CLAAug 23, 2010 · N562FE · Doug MD1010FSDR 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, REPAIAug 23, 2010 · N562FE · Doug MD1010FSDR 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.Aug 23, 2010 · N426AT · Aerosp ATR72212SDR 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"Aug 23, 2010 · N755DH · Boeing 727225SDR 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 PERFORMEDAug 21, 2010 · N246PS · Cndair CL6002B19SDR 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 5Aug 20, 2010 · N741FD · Airbus A300B4622RSDR 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 TEAug 19, 2010 · N304FE · Doug MD1030FSDR 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.Aug 19, 2010 · N562FE · Doug MD1010FSDR AALA20100818TUL14Winglet · dentedTWO DENTS ON TRAILING EDGE OF LEFT WINGLET. ACCOMPLISHED REPAIR PER SRM 57-31-02-1A.Aug 16, 2010 · N649AA · Boeing 757223SDR 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.Aug 16, 2010 · N275UP · Doug MD11FSDR IPXA10M62270Skin · crackedINSPECTION TYPE:1C RT WING L/E LWR EDGE CRACKED AT XOS 550. REMOVED CRACKED DOUBLER, FABRICATED AND INSTALLED DOUBLER IAW DWG ARB2933.Aug 16, 2010 · N275UP · Doug MD11FSDR 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.Aug 16, 2010 · N360AA · Boeing 767323SDR 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.Aug 15, 2010 · N768QT · Boeing 767241SDR 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.Aug 14, 2010 · N275UP · Doug MD11FSDR 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.Aug 14, 2010 · N785AX · Boeing 767281SDR 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 CLASSAug 12, 2010 · N383FE · Doug MD1010FSDR VGQY2010081200081Skin · crackedLEFT WING L/E BULLNOSE SKIN ADJACENT TO NR 13 KRUEGER FLAP O/B LINKAGE FOUND CRACKED. COMPLIED WITH EN1180-10.Aug 12, 2010 · N815SA · Boeing 7472L5BSDR 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.Aug 12, 2010 · N815SA · Boeing 7472L5BSDR 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.Aug 11, 2010 · N615FE · Doug MD11FSDR 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.Aug 11, 2010 · N615FE · Doug MD11FSDR USAA2010081291651Retaining Ring · corrodedPIT - S5 - MAJOR REPAIR - LEVEL 2 CORROSION ON FUEL PANEL 540GB RETAINING RING. REPLACED FUEL PANEL 540GB RETAINING RING.Aug 11, 2010 · N102UW · Airbus A320214SDR USAA2010081291650Retaining Ring · corrodedPIT - S5 - MAJOR REPAIR - LEVEL 2 CORROSION ON FUEL PANEL 540CB RETAINING RING. REPLACED FUEL PANEL 540CB RETAINING RING.Aug 11, 2010 · N102UW · Airbus A320214SDR 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 CAug 11, 2010 · N801EA · Boeing 727225SDR 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 110Aug 10, 2010 · N615FE · Doug MD11FSDR WRLA20100810438Skin · looseHI-LOK LOOSE AT EXTERNAL LWR SKIN OF RT WING STA XORS 231, S- 31.Aug 10, 2010 · N380WA · Doug MD11FSDR 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).Aug 10, 2010 · N186DN · Boeing 767332SDR FDEA201008102910Skin · crackedRT WING LOWER SKIN PANEL FASTENER HOLE CRACKED. COMPLIED WITH EA 6-5710-136685.Aug 10, 2010 · N741FD · Airbus A300B4622RSDR 2010FA0000818Panel · corrodedCORROSION ON LT WING PANEL 574BB. NO CORROSION REMOVAL LIMITS AVAILABLE. PANEL IS LISTED AS PRIMARY STRUCTURE. REPLACED PANEL WITH NEW PANEL.Aug 10, 2010 · N526JL · Airbus A320232SDR 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.Aug 10, 2010 · N526JL · Airbus A320232SDR WRLA20100809434Door · chafedREPAIR - CHAFING ON TELESCOPE DUCT DOOR (P/N: ARM0078-12) OF RT WING AT XOS467.10.Aug 9, 2010 · N279WA · Doug MD11FSDR DALA1019279001Skin · crackedLT WING L/E SKIN/LOWER SURFACE XOS 243 CRACKED. INSTALLED PERMANENT REPAIR IAW ERA 380953-14MA AND ERA 482367-14.Aug 9, 2010 · N901DE · Doug MD88SDR EE4Y100314Panel · delaminatedRIGHT WING T/E UPPER FIXED PANEL P/N 5912735-2 DELAMINATED.Aug 9, 2010 · N563PC · Doug DC915FSDR EE4Y100312Panel · delaminatedRIGHT WING T/E UPPER FIXED PANEL P/N 5912737-2 DELAMINATED.Aug 9, 2010 · N563PC · Doug DC915FSDR 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: WAITAug 7, 2010 · N426AT · Aerosp ATR72212SDR FXGAN351CE6Skin · corrodedCORROSION FOUND ON WING SKIN STA 167R TO 182R.Aug 7, 2010 · N351CE · Doug C118ASDR FXGAN351CE4Doubler · crackedNR 2 ALTERNATE FUEL TANK ACCESS DOOR DOUBLER CRACKED.Aug 7, 2010 · N351CE · Doug C118ASDR FXGAN351CE2Skin · corrodedCENTER WING END RIB SKIN AND LOWER ANGLE FOUND CORRODED.Aug 7, 2010 · N351CE · Doug C118ASDR FDEA201008062849Skin · crackedDURING WALKAROUND CHECK, RT WING ADJACENT TO NR 3 SLAT L/E TELESCOPIC DUCT CUT-OUT UPPER SECTION FOUND CRACKED.Aug 6, 2010 · N372FE · Doug MD1010FSDR 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.Aug 5, 2010 · N396FE · Doug MD1010FSDR 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.Aug 5, 2010 · N408MA · Bell 222BSDR QML3MR0242Skin · puncturedDURING INSP, FOUND PUNCTURE/CRACK OF UPPER WING SKIN APPROX 1" IN LENGTH CAUSED BE IMPACT FROM ABOVE.Aug 5, 2010 · N408MA · Bell 222B
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