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 HALA2026090300196Skin · corrodedDURING A 3 YR CHECK AT SIAEP, INSPECTION AS PER MPD TASK ZL-500-02-1, CORROSION HAS BEEN FOUND ON THE LT WING BOTTOM SKIN PANEL 1 LOWER SURFACE AT THE FORWARD SPAR BETWEEN RIB 8-9. DAMAGE EXCEEDS ITS ALLOWABLE DAMAGE LIMITS IAW SRM 57-21-11-283-014. RI-HAL-57-SDR ASAA2024010348174Skin · corrodedLEFT WING TOP SKIN, EVIDENCE OF CORROSION AROUND THE BONDING POINT GROUNDED - YES. REMOVED CORROSION ORIG .150, MATERIAL LOSS .004, REMAINING .146 FOUND TO BE WITHIN LIMITS, HFEC, BHEC, DVI NO DEFECTS NOTED REMOVAL AND REINSTALL BONDING SPIGOT MEASUREMENTS 1.8SDR R61A2024010300773Skin · crackedWHILE IN HEAVY CHECK - R/H WING LOWER SKIN AT RIB 4A HAS CRACK. PERFORMED TEMPORARY REPAIR BY CUTOUT, FILLER/DOUBLER REPAIR ON RH WING LOWER SKIN AT RIB 4A IN ACCORDANCE WITH, REF ETD2023-170-031160.SDR IPXA2024012434330Access Panel · crackedFAULT - CRACK PNL, RH WING LOWER OUTD MAIN FUEL PUMP ACCESS PNL(REPLACE) REVIEWEDSDR IPXA2024010334330Access Panel · unknown*SDR FILED OPEN* FAULT - CRACK PNL, RH WING LOWER OUTD MAIN FUEL PUMP ACCESS PNL(REPLACE) OK TO WORKSDR IPXA2024012425536Skin Panel · crackedFAULT- CRACK SKIN PNL, LH WING NO.2 FLAP TRACK AFT FAIRING(REPAIR) REVIEW COMPLETESDR IPXA2024010325536Unknown · unknown*SDR FILED OPEN* FAULT- CRACK SKIN PNL, LH WING NO.2 FLAP TRACK AFT FAIRING(REPAIR) REMOVED FITTING I.A.W SRM 51-40-02-0G REV.88SDR IPXA2024011214418Skin · bentFORMER, RH WING OUTBD FXD LE NOSE SKIN, OSS 565.90 (REPLACE) I.A.W AMM 27-81-31-024-001 REV.140 REMOVED CURTAIN OF RH WING L/E FORMER ASSY, OSS 565.9. I.A.W AMM 27-81-31-424-019 REV.140 INSTALLED CURTAIN OF RH WING L/E FORMER ASSY, OSS 565.9. I.A.W AMM 27-81-3SDR UIEA2023122801036Unknown · unknownDENT ON LH WING INBD AFT UPPER SKIN AT 92" FROM INBD EDGE AND 4.5" FROM AFT EDGE(<P>PART WAS REPAIRED IAW OEM MANUAL SRM 57-53-01-2R-1. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023122401013Unknown · unknownDENT ON LH WING INBD AFT UPPER SKIN AT 92" FROM INBD EDGE AND 4.5" FROM AFT EDGE(<P>PART WAS REPAIRED IAW OEM MANUAL SRM 57-53-01-2R-1. NO FURTHER DEFECTS NOTED.</P>)SDR DALA2024010200033Unknown · unknownSHIP 3128 TOOLING DAMAGE AT FASTENER HOLE IN MANHOLE SURROUND FOR RIGHT WING PANEL 640JB. CORRECTIVE ACTION: REPAIRED PER ERA 614663-14. (0132864)SDR JR2R20231230969Skin · chafedLH WING LEADING EDGE PANEL CHAFED AT #2 PYLONSDR JR2R20231230942Skin · chafedRH WING LEADING EDGE PANEL CHAFED AT #2 PYLONSDR DALA2024010200041Unknown · unknownSHIP 3128 RH WING LOWER SKIN PANEL #2 AND MANHOLE ACCESS PANEL 640JB WERE FOUND WITH A DRILL START AND DOUBLE DRILL HOLE CONDITION COMMON TO ONE ATTACH BOLT HOLE. CORRECTIVE ACTION: REPAIRED PER ERA 614663-14. (0131258)SDR IPXA2024011279972Panel · erodedEROSION PNL SKIN, RH WING UPPER SURFACE PNL NO.611PT (REPAIR) REMOVE THE DAMAGE MATERIALS AND CLEAN.MEASURE THE DAMAGE AREA (LENGTH:2", WIDTH:1",4" FROM INBOARD EDGE, AT LEADING EDGE). BOND THE REPAIR PLIES WITH FILM ADHESIVE CURED AT 350°F FOR 180 MINUTES WISDR IPXA2023122879972Unknown · unknown*SDR FILED OPEN* FAULT - EROSION PNL SKIN, RH WING UPPER SURFACE PNL NO.611PT (REPAIR)SDR EE4Y2023122719062Skin · misrepairedLH WING, MAIN BOX T/E LOWER SKIN, AT RIB 10 AND RIB 11 WITH EXISTING REPAIR WITHOUT RECORDS. NOTE: THE LH WING, LOWER SKIN WAS REPAIRED AS PER EMBRAER ETD2023-190-031226 GUIDELINES AS STATED IN COOPESA ENGINEERING ORDER NO: COO-EO-2023-18979-R00 INSTRUCTIONS (SDR EE4Y2023122719061Skin · misrepairedRH WING, MAIN BOX T/E LOWER SKIN, AT RIB 10 WITH EXISTING REPAIR WITHOUT RECORDS. NOTE: THE RH WING, LOWER SKIN WAS REPAIRED AS PER EMBRAER ETD2023-190-031227 GUIDELINES AS STATED IN COOPESA ENGINEERING ORDER NO: COO-EO-2023-18978-R00 INSTRUCTIONS ( FOR ADDITISDR AALA202403267270Skin Panel · corrodedAIRRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TRAILING EDGE TOP SKIN PANEL LOWER SURFACE BETWEEN RIB 13 AND RIB 17. REPAIRED SKIN PANEL PER EA 350498.SDR AALA202403267046Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TRAILING EDGE TOP SKIN PANEL LOWER SURFACE BETWEEN RIBS 14 AND 17. REPAIRED SKIN PANEL PER EA 350524.SDR AALA202403227270Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TRAILING EDGE TOP SKIN PANEL LOWER SURFACE AT RIB 14 PLUS 10 INCHES. REPAIRED SKIN PANEL PER EA 350498.SDR AALA202403225710Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TRAILING EDGE TOP SKIN PANEL LOWER SURFACE BETWEEN RIBS 10 AND RIB 11 PLUS 14 INCHES. REPAIRED SKIN PANEL PER EA 350524.SDR REXA2024102901100Panel · chafedL/H WING PANEL 584ET IS CHAFFED. BURNISHED CHAFE SMOOTH IAW CRJ 900 SRM 51-12-00-001-001-A01. MATERIAL LOSS .021 (MAX ALLOWED .015) OUT OF ALLOWABLE LIMITS IAW CRJ 900 SRM 57-52-01-101-001-A01. RECEIVED NEW SERVICEABLE PART PANEL 584ET PN CC670-14027-3 LOCATESDR AALA202403224175Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TRAILING EDGE TOP SKIN PANEL LOWER SURFACE BETWEEN RIB 20 AND RIB 21 PLUS 8 INCHES. REPAIRED SKIN PANEL PER EA 350498.SDR SWAA2024020639817Panel · crackedRIGHT WING PANEL 671FB INNER FACE HAS CRACK.<[01] APPLIED PERMANEMT REPAIR ON DAMAGE AREA AS MARKED ON RIGHT WING PANEL 671FB AS PER B737 SRM 51-70-04-2R-1 PARAG 4-D-F; MATERIAL USED PO#2040614; PO#1690463; EQUIPMENT USED: TEMPERATURE CONTROL ID160354; DUE DATSDR R61A2024012000017Skin · crackedDURING WING SKIN INSPECTION FOUND A CRACK ON LOWER RH WING SKIN 3 INCHES LONG, BETWEEN RIBS 16 @17 AND 6 INCHES AFT OF FWD SPAR. REPAIRED IAW ETD2024-170-000982 REV B. ALSO REF VP-053087-2023 N/R 4 FOR WORK PERFORMED.SDR CALA2023122003681Skin · corrodedDURING OK TO CLOSE INSPECTION PANEL 621BT, ON RH WING TOP SKIN PANEL APPROX RIB 10 AND STRINGER 11, A CORROSION SPOT WAS FOUND. IDT, COMPLIED WITH FINAL VTMAE EA 320-5720-13-A3467 REV- AND UAL EC/RA #5721-01484,IDT.SDR R61A2023121800746Skin · crackedAFT CARGO DOOR SURROUND AFT SEAL REST CORRODED. REPLACED REST IAW SRM 51-40-02SDR R61A2023121800744Skin · crackedR/H WING FIXED L/E TOP SIDE SLAT TRACK #4 CUTOUT BTWN L/E RIB 14-15 REPAIRED IAW SRM 57-49-01 REPAIR 6. HFEC CUTOUT "NO CRACKS FOUND" SEE AWS FOR DETAILS. TWO 40343-10.SDR AALA202403261904Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TRAILING EDGE TOP SKIN PANEL LOWER SURFACE AT RIB 11. REPAIRED SKIN PANEL PER EA 350498.SDR AALA202403261362Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TRAILING EDGE TOP SKIN PANEL LOWER SURFACE BETWEEN RIB 7 AND RIB 8. REPAIRED SKIN PANEL PER EA 350498.SDR AALA202403261636Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TRAILING EDGE TOP SKIN PANEL LOWER SURFACE AT RIB 7 PLUS 5.5 INCHES. REPAIRED SKIN PANEL PER EA 350524.SDR YENA2023122001614Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION UPPER SURFACE OF TOP SKIN BTW RIB19 AND RIB20 AT FRONT SPAR DATUM ON LH WING; REF TO AEROMAN WO 2023 364/1 NR 2023-682713, PERFORMED PERMANENT REPAIR ON UPPER SURFACE TOP SKIN PANEL 2 FRONT SPAR AT RIBS 19-20 LH WING. I.A.WSDR YENA2023122001603Unknown · unknownDURING HEAVY MAINTENANCE: WINGS / LH WING / TOP SKIN PANEL 2 / UPPER SURFACE / FRONT SPAR AT RIBS 19-20 / BONDING SPIGOT / CORROSION - PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)SDR AALA202404157197Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TRAILING EDGE OVERHANG TOP SKIN PANEL LOWER SURFACE BETWEEN RIB14 AND RIB15. REPAIRED SKIN PANEL PER EA 350314.SDR AALA202404158139Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TRAILING EDGE OVERHANG TOP SKIN PANEL LOWER SURFACE BETWEEN RIB 10 AND RIB 11 PLUS 13.272 INCHES. REPAIRED SKIN PANEL PER EA 350314.SDR AALA202404125408Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TRAILING EDGE OVERHANG TOP SKIN LOWER SURFACE BETWEEN RIBS 10 AND 11. REPAIRED SKIN PANEL PER EA 350323.SDR AALA202404123671Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TRAILING EDGE OVERHANG TOP SKIN LOWER SURFACE AT RIB 14. REPAIRED SKIN PANEL PER EA 350323.SDR 2024FA0000127Skin · crackedR/H WING AFT WING WALK SKIN CRACKED ON CORRUGATED SKIN. REPLACED WING WALK SKIN ASSY WITH NEWSDR 2024FA0000112Skin · crackedR/H WING FWD WING WALK SKIN CRACKED ON CORRUGATED SKIN. REPLACED WING WALK SKIN ASSY WITH NEWSDR AALA202403264022Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TRAILING EDGE TOP SKIN PANEL LOWER SURFACE AT RIB 8. REPAIRED SKIN PANEL PER EA 350498.SDR AALA202402272624Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING UPPER SURFACE TRAILING EDGE TOP SKIN PANEL AT RIB 5 PLUS 26 INCHES. REPAIRED SKIN PANEL PER SRM 57-21-11-283-026.SDR 2024FA0000129Skin · crackedR/H WING AFT WING WALK SKIN CRACKED ON CORRUGATED SKIN. REPLACED WING WALK SKIN ASSY WITH NEWSDR IPXA2023122865964Panel · dented**SUPPLEMENTAL SDR**LEFT WING LOWER INBD LE ACCESS PANEL #511HB HAS DENT APX 6 INCHES FROM FWD EDGE AND 10 INCHES FROM INBD EDGE.***SM26/LMX4*** INSTALLED NEW PANEL #511HB PER AMM 20-11-00-912-001SDR IPXA2023121365964Access Panel · unknown*SDR FILED OPEN* LEFT WING LOWER INBD LE ACCESS PANEL #511HB HAS DENT APX 6 INCHES FROM FWD EDGE AND 10 INCHES FROM INBD EDGE.***SM26/LMX4*** C/W EO. ITEM REQUIRES REPAIR OR REPLACEMENT WITHIN 10 DAYS WITH REPETITIVE INSPECTIONS AT INTERVALS NOT TO EXCEED EVERSDR 2024FA0000128Skin · crackedR/H WING AFT WING WALK SKIN CRACKED ON CORRUGATED SKIN. REPLACED WING WALK SKIN ASSY WITH NEWSDR 2024FA0000113Skin · crackedR/H WING FWD WING WALK SKIN CRACKED ON CORRUGATED SKIN. REPLACED WING WALK SKIN ASSY WITH NEWSDR SWAA2023121530686Skin · crackedL/H WING LOWER LEADING EDGE PANEL 521CB IS DAMAGED ON THE INBOARD AFT CORNER. LOWER OUTER SKIN IS CRACKED 0.350 INCHES FROM INBOARD EDGE AND CRACK MEASURES 0.700 INCHES LONG.<[01] PERFORMED TIME LIMITED REPAIR ON PANEL 521CB IAW TSR 2023009725; ON FAULT TTG8Q0SDR SWAA2023121530890Skin · crackedRH WING INBOARD FIXED LEADING EDGE LOWER SKIN PANEL AT WBL 107.24 HAS A CRACK IN LEADING EDGE OF THE PANEL THAT IS APPROXIMATELY 0.400 INCH LONG.<[01] CRACKS VERIFIED; END LOCATED AND MARKED;[02] INSPECTED PER SRM 57-41-01 .. REF DRAWING 116A2132. DETERMINED TSDR SWAA2023121530891Panel · crackedRH WING INBOARD FIXED LEADING EDGE LOWER SKIN PANEL AT WS 158.25 HAS A CRACK IN LEADING EDGE OF THE PANEL THAT IS APPROXIMATELY 0.400 INCH LONG.<[01] CRACK VERIFIED PER BOEING NDT MANUAL PART 6 51-00-00 PROCEDURE 23; END LOCATED AND MARKED;[02] CRACK VERIFIED
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