JASC 5730
Service difficulty reports · 27,262
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 FDEA201405231146Skin · crackedRIGHT WING, SKIN AT PRESS REFUEL DOOR, INNER FWD CORNER HAS SUSPECTED CRACK GOING FROM CORNER TO RIVET. INSTALLED REPAIR DOUBLER IAW SRM 57-40-02 REPAIR 7 FIGURE 202 & EA 1-5730-T0308359 PART 1.SDR ASOA2014061810688Skin · corrodedRT WING LOWER WING PLANK ACCESS HOLE 64B LAND CORRODED. COMPLIED WITH EC/TC EO 600-57-81 C/W IAW REO 601R-57-21-030, REV L. MAJOR REPAIR.SDR ASOA2014061810687Skin · corrodedRT WING LOWER WING PLANK ACCESS HOLE FUEL PANEL 650EB LAND CORRODED. COMPLIED WITH EC/TC EO 600-57-81 C/W IAW REO 601R-57-21-030, REV L. MAJOR REPAIR.SDR AALA20140526001Skin · corrodedCENTER WING LOWER SKIN CORROSION NEAR STATION 540. REMOVED CORROSION & ACCOMPLISHED REPAIR IAW EA B737-57-035052.SDR FDEA201405221123Skin · crackedWHILE ACCOMPLISHING FEA 1-5710-F0308148 FOUND POSSIBLE CRACK ON CORNER OF LT WING REFUEL DOOR PNL 519CB. VERIFIED CRACK EXTENDS FROM PANEL EDGE TO THE NEAREST FASTENER HOLE. CUT OUT DAMAGE IAW SRM 57-40-02 REPAIR 7, FIG 202. PERFORMED HFEC INSPECTION IAW NSDR ABXA20140521199Skin Panel · damagedRIGHT WING LE LOWER SKIN HAS A FASTENER HOLE THAT IS OBLONG COMMON TO INBD SIDE BRACE FITTING AT APPROX LES 385. REAMED DAMAGED HOLE TO .658 INCHES DIAMETER IAW REA B657-60901-MR. FREEZE PLUG WAS INSTALLED ON NR 0774, REPAIRED DAMAGED HOLE IAW REA B657-60901SDR SWIA201437983Skin · damagedDAMAGE TO LT WING SKIN LOWER SURFACE JUST AFT OF HOLE NR 86 AND TOOLING MARKS INSIDE OF HOLE 86. C-CHECK, REMOVED DAMAGE ON LT WING LOWER SKIN, AFT OF HOLE 86 IAW REO.SDR FDEA201405201085Skin · crackedDURING PERFORMANCE OF FCD 1-5710-F0308148, FOUND LARGE CRACK AT RT WING NR 1 SLAT AT INBD SLAT TRACK CUT OUT. CUT OUT CRACK & REMOVED ALL DAMAGE IAW SRM 57-40-02. PERFORMED HFEC INSPECTION IAW NTM 20-00-00 PART 6, NO DEFECTS NOTED. PERFORMED RII INSPECTISDR FDEA201405201093Skin · crackedDURING COMPLIANCE OF FCD 1-5710-F0308148, FOUND SKIN CRACKED NEAR ZONE 519, LT WING INBD OF NR 1 ENGINE, JUST AFT OF INBD SLATS. PERFORMED HFEC OF THE SUSPECTED CRACK IN THE LT WING. CRACK APPROXIMATELY INCHES INCHES. INSTALLED FILLER AND DOUBLER IAW EA 1SDR FDEA201405201088Skin · crackedFOUND POSSIBLE CRACK ON LT INBD FUELING PANEL. COMPLIED WITH HFEC OF ABOVE NOTED AREA IAW 06-10-01.001. CRACK NOTED RUNNING FROM INBD CORNER RADIUS TO FIRST FASTENER. INSTALLED REPAIR DOUBLER AND RIBS IAW EA 8-5710-T0308138 PT1.SDR FDEA201405201087Skin · crackedFOUND POSSIBLE CRACK ON LT INBD FUELING PANEL. COMPLIED WITH HFEC OF ABOVE NOTED AREA IAW 06-10-01.001. CRACK NOTED RUNNING FROM INBD CORNER RADIUS TO FIRST FASTENER. INSTALLED REPAIR DOUBLER AND RIBS IAW EA8-5710-T0308138 PT1.SDR FDEA201405201086Skin · crackedFOUND POSSIBLE CRACK ON LT INBD FUELING PANEL. COMPLIED WITH HFEC OF ABOVE NOTED AREA, IAW 06-10-01.001. CRACK NOTED RUNNING FROM INBD CORNER RADIUS TO FIRST FASTENER. INSTALLED REPAIR DOUBLER AND RIBS IAW EA 8-5710-T0308138 PT1.SDR FDEA201405201084Skin · crackedRIGHT WING NR 16 SLAT TRACK CUT OUT HAS POSSIBLE CRACK ON LE SKIN. CRACK FOUND WHILE ACCOMPLISHING FEA 1-5710-F0308148. VERIFIED CRACK. CUT OUT DAMAGE IAW ERS 14-03138. PERFORMED HFEC INSPECTION OF DAMAGE REMOVAL IAW NTM 20-00-00 PART 6, NO DEFECTS NOTED.SDR FDEA201405201083Skin · crackedWHILE ACCOMPLISHING FEA1-5710-F0308148 FOUND POSSIBLE CRACK ON NR 13 LT WING SLAT TRACK CUT OUT. VERIFIED CRACK EXTENDS FROM PANEL EDGE TO THE NEAREST FASTENER HOLE. THIS IS AT SLAT TRACK 14 CUT OUT NOT AT 13. NO CRACK AT SLAT TRACK 13 FOUND. REMOVED DAMAGSDR MTNA20140520013Skin Panel · corrodedFOUND LT WING LOWER SKIN PANEL INTERNAL CORROSION AT JET PUMP SUPPORT SEATING BETWEEN RIBS 4 & 5, STIFFENERS 8 - 9. REPAIRED IAW SRI DT S-2157 14-21832 DATED 4/11/2014. APPROVED DATA IS SHEET DO TS-2644 10 5790.SDR 7AHR201405202163Skin · corrodedCORROSION LT WING SKIN AREA BETWEEN WS 150 & WS558. REMOVED CORROSION AND SENT MEASURMENTS TO FLIGHT VEHICLE CONSULTING FOR EVALUATION. BLENDED AREAS WERE FOUND TO BE IN LIMITS IAW FVC DWG 57-13170-1 WITH 8110-3 APPROVAL.SDR ASOA2014061710677Skin · crackedCRACK FOUND ON RT WING LOWER WING PLANK FWD SPLICE JOINT RWS 65.75. COMPLIED WITH REO 601R-57-21-2188. MAJOR REPAIR.SDR FDEA201405191082Skin · crackedRIGHT WING PRESSURE REFUEL PANEL 619CB CRACKED. FOUND WHILE ACCOMPLISHING FEA 1-5710-F0308148. REPAIRED IAW EA 1-5730-T0308294.SDR FDEA201405191081Skin · crackedLT WING LE SKIN FWD OF OTBD SIDE OF SLAT DRIVE MECHANISM PANEL FOUND TO BE CRACKED. CRACK FOUND WHILE ACCOMPLISHING FEA 1-5710-F03081 48. CONFIRMED CRACK DURING HFEC INSPECTION IAW NDTSPM PT 6. CRACK EXTENDS FROM CORNER OF CUT OUT TO 1/4 INCH PAST FASTENER.SDR FDEA201405191072Skin · crackedFOUND POSSIBLE SMALL CRACK RT WING ROOT LE. COMPLIED WITH HFEC IAW SPM 06-10-01001. CRACK NOTED .750 INCH LONG. REMOVED CRACK AT OTBD CORNER OF FIRE BOTTLE ACCESS DOOR LOWER SKIN. MADE CUT OUT IAW SRM 57-10-00 FIG 68. PERFORMED HFEC INSPECTION IAW NTMSDR MTNA20140521014Panel · corrodedFOUND PANEL 521DT & 522CT HOUSINGS CORRODED OUT OF LIMITS ON REMOVABLE PANEL PN S57112322200. REPAIRED IAW SRI DT S-2001 14-21784 ISSUE A DATED 4/5/2014. APPROVED DATA IS SRAS DT S-2001 14 8440.SDR SWIA201437674Access Panel · crackedLEFT WING NR 5 FUEL ACCESS PANEL, RIB 21 UPPER SURFACE HAS 1 CRACKED SKIN SUPPORT MOST FWD. R & R 1 CRACKED UPPER SKIN CLEAT ABOVE THE LT WING NR 5 FUEL ACCESS PANEL AT RIB 21 IAW SRM AND AMM.SDR SWIA201437673Access Panel · crackedLT WING NR 6 FUEL ACCESS PANEL RIB 23 HAS 1 CRACKED UPPER SKIN SUPPORT. R & R 1 CRACKED UPPER SKIN CLEAT ABOVE THE LT WING NR 6 FUEL ACCESS PANEL AT RIB 23 IAW SRM AND AMM.SDR SWIA201437672Access Panel · crackedLEFT WING NR 5 FUEL ACCESS PANEL RIB 21 UPPER SURFACE HAS 1 CRACKED SKIN SUPPORT CENTER OF RIB. R & R 1 CRACKED UPPER SKIN CLEAT ABOVE THE LT WING NR 5 FUEL ACCESS PANEL AT RIB 21 IAW SRM AND AMM.SDR FDEA201405191080Skin · crackedFOUND CRACK ON INBD FWD CORNER OF SLAT DRIVE MECHANISM DOOR CUT OUT LT WING. CONFIRMED CRACK BY HFEC INSPECTION IAW NDTSPM PT 6. PERFORMED HFEC INSPECTION IAW NTM 20-00-00 PART 6, NO DEFECTS NOTED. INSPECTED DAMAGE REMOVAL, NOT ACCEPTED. RADIUS ON DAMAGE SDR FDEA201405191079Skin · crackedCRACK IN LOWER LE PANEL ON LT WING JUST INBD OF OTBD SLAT MARKED. INSTALLED REPAIR ON ARB2933-13 IAW EA 1-5710-T0308224 P1. INSTALLED REPAIR ON LE SKIN IAW SRM 57-40-02 REPAIR 7 & EA 1-5710-T0308224 P 1. PAINTED REPAIR AREA IAW SRM 51-51-02.SDR FDEA201405191071Skin · crackedRIGHT WING NR 10 SLAT TRACK CUT OUT HAS POSSIBLE CRACK ON LE OF WING. CRACK FOUND WHILE ACCOMPLISHING FEA 1-5710-F0308148. VERIFIED CRACK, MARKED END OF CRACK. HFEC IAW NDTSPM PART 6,06-00-06. CUT OUT DAMAGED AREA IAW SRM 57-40-02 REPAIR 7. COMPLIED WITSDR CALA2014051991059Skin · corrodedLEFT WING LOWER FUEL TANK PANEL LANDINGS 540 NB HOLES C & F & 540HB HOLE N WERE FOUND CORRODED. HOLES WERE BUSHED & BRIDGING PLATES INSTALLED IAW SRM 57-21-11 PARA 5 B FIG 202. INSPECTION REQUIRED IAW SRI 57-21-11-2-002-00 3 B TBL 203. FIRST INSPECTION 4360SDR CALA2014051991058Skin · corrodedRIGHT WING LOWER FUEL TANK PANEL LANDINGS 650 AB HOLE B & 640 MB HOLE K WERE FOUND CORRODED. HOLES WERE BUSHED & BRIDGING PLATES INSTALLED IAW SRM 57-21-11 PARA 5 B FIG 202. INSPECTION REQUIRED IAW SRI 57-21-11-2-002-00 3 B TBL 203. FIRST INSPECTION 43600FCSDR CALA2014051991057Skin · corrodedLEFT OVERWING FILLER ADAPTOR LAND UPPER SURFACE WAS FOUND CORRODED. CORROSION WAS REMOVED IAW SRM 57-21-11 PARA 5 E FIG 205. MAXIMUM MATERIAL LOSS WAS 0.017, MAX ALLOWABLE IS 0.020.SDR FDEA201405182091Skin · crackedLEFT WING FIXED LE SKIN CRACKED AT THE PRESS REFUELING DOORWAY PANEL 518FB INBD FWD. REPAIRED IAW SRM 57-10-00 & EA 8-5710-T0308261 SEQ 231.SDR FDEA201405182089Skin · crackedRIGHT WING NR 3 SLAT ANTI-ICE TELESCOPING DUCT CUT OUT IS CRACKED AT UPPER INBD & OTBD CORNERS. REPAIRED IAW EA 8-5710-T0308270.SDR FDEA201405182088Skin · crackedLEFT WING FIXED LE SKIN CRACKED AT THE TAI DUCT CUT OUT TOP OTBD CORNER. REPAIRED IAW EA 8-5710-T0308271 PART 1.SDR YENA20140518097Skin · corrodedDURING HEAVY MAINTENANCE VISIT, CORROSION WAS REPORTED AT ONE LOCATION ON THE LT WING, UPPER SKIN PANEL, LOWER SURFACE, T/E BETWEEN RIBS 14-15, REAR SPAR DATUM. REMOVED CORROSION BY BLEND OUT, PERFORMED NDT AND REPLACED FASTENERS WITH THE BLENDED AREAS AS OVESDR FDEA201405181067Skin · crackedLEFT WING SLAT DRIVE MECHANISM DOOR INBD LE CRACKED TO RIVET. REMOVED PANEL 518DB FOR SHEET METAL ACCESS. REMOVED REQUIRED FASTENERS & TRIMMED OUT CRACK IAW SRM 51-30-00 VOL 2 & SRM 57-10-00 REPAIR. NEEDS HFEC FOR CRACK CONTAINMENT. FABRICATED FILLER PO 16SDR FDEA201405171059Skin · crackedSKIN FOUND TO HAVE CRACK INDICATIONS DURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON RT WING LOWER SKIN ACCESS PANEL CUT OUT BETWEEN XORS 683.4 & XORS 713.6. REPAIRED IAW SRM 57-20-02 FIGURE 201 REPAIR 5 REVISION 55. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 SDR A6WA201441574Skin · gougedUPPER SURFACE OF LWR WING PLANK IS GOUGED AT WS 88.5. REPAIRED GOUGED UPPER SURFACE OF LWR WING PLANK IAW REO 601R--57-21-2192 DATED 5-21-14.SDR ASOA20140516068Access Panel · corrodedDURING C-CHECK RT WING ACCESS PANEL 532AB FOUND CORRODED ON BACKSIDE AROUND FASTENER HOLES. MAINTENANCE BLENDED CORROSION AND REMAINED WITHIN ALLOWABLE LIMITS IAW EC5720-01178. ACFT APPROVED FOR RETURN TO SERVICE.SDR ASOA20140516067Access Panel · corrodedDURING C-CHECK, RT WING ACCESS PANEL 632AB FOUND CORRODED ON BACKSIDE AROUND FASTENER HOLES. MAINTENANCE BLENDED CORROSION. REMAINED WITHIN ALLOWABLE LIMITS IAW EC5720-01178. ACFT APPROVED FOR RETURN TO SERVICE.SDR UIEA2014051600192Skin · corrodedCORROSION ON THE LOWER SKIN, UPPER SURFACE OF RT WING FRONT SPAR SKIN PANEL AT OLES 1504. REPAIR THE DAMAGE AREA IAW EI NO T2014A57B-1349 REV 3.SDR UIEA2014051600187Skin · corrodedCORROSION ON THE LT WING LOWER SKIN UPPER SURFACE NEAR FSSI 453.04. REPAIRED THE DAMAGE AREA IAW EI NO T2014A57B-1258 REV 3.SDR UIEA2014051600195Skin · corrodedCORROSION SKIN, AROUND SUMP DRAIN HOLE OF RT WING INSPAR LOWER SURFACE, WS 1480. REPAIR THE DAMAGED AREA IAW EI NO T2014A57B-1190 REV 2. PERFORM LEAD CHECK IAW JC 4428A108 REV 0.SDR FDEA201405151022Skin · crackedSKIN FOUND TO HAVE CRACK INDICATIONS DURING HIGH FREQUENCY EDDY CURRENT INSPECTION AT RT WING LOWER SKIN ACCESS DOOR CUT OUT BETWEEN XORS 683.4 & XORS 713.6. REPAIRED IAW SRM 57-20-02 FIGURE 201 REPAIR 5 REVISION 55. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 RSDR FDEA201405151021Skin · crackedSKIN FOUND TO HAVE CRACK INDICATIONS DURING HIGH FREQUENCY EDDY CURRENT INSPECTION AT LT WING LOWER SKIN ACCESS PANEL CUT OUT BETWEEN XORS 683.4 & XORS 713.6. REPAIRED IAW SRM 57-20-02 FIGURE 201 REPAIR 5 REVISION 55. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 SDR FDEA201405151045Skin · corrodedLT WING UPPER SKIN AT EDGE OF BODY SPLICE CORRODED. REPAIRED IAW EA F-5730-T0307309, STEPS 1 - 9, PT 1.SDR EB1R201405140001Skin · corrodedFOUND CORROSION ON THE UPPER AFT SURFACE OF THE LT WING SKIN AT WBL 93.0-WBL 99.0 AT REAR SPAR, AND WBL 135.0 AT REAR SPAR, AND WBL 130.0- WBL 134.0 AT S-13. CLEAN CORROSION AND REPAIRED AREAS IAW MFG MESSAGE CIN-CIN-14-0007-11B AND SRM 57-20-01.SDR SWAA2014060228604Panel · crackedLEFT WING UPPER TE PANEL CRACKED AT FWD OTBD CORNER OF NR 4 SPOILER CUT OUT. REPAIRED PANEL IAW SRM.SDR FDEA201405141004Skin · crackedLEFT WING, SLAT TRACK NR 12 LOWER CUT OUT SKIN AT XOS 776 FOUND CRACKED. REPAIRED IAW SRM 57-40-02 FIGURE 201 REPAIR 7 REVISION 55. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 121.SDR FDEA201405131044Skin · crackedPOST FLIGHT WALK AROUND, FOUND POSSIBLE CRACK AT RT REFUELING DOOR INBD RADIUS ON WING. INSTALLED DOUBLER IAW SRM 57-10-00 & EA 8-5710-T0308147.SDR FDEA201405130990Skin · crackedEVIDENCE OF A CRACK IN THE SKIN AT THE RT WING REFUEL DOOR INBD FWD CUT OUT. REPAIRED IAW EA 8-5710-T0308087 PT1.
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