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 2024F00248Doubler · corrodedTHE LH AND RH WING FUEL PANELS HAVE CORROSION PRESENT IN MULTIPLE AREAS.SDR SWIA20241115008Skin · crackedRH WING MAIN BOX LOWER SKIN (LOWER SURFACE) ALONG SPAR 01 HAS SUSPECTED CRACK AT RIVET IN BETWEEN SLAT #3 AND #4. (C-CHECK RO 10/30/2024) (FILED CLOSED)REPAIRED CRACK IN RH WING MAIN BOX LOWER SKIN AT RIB 20 BY FILLER AND DOUBLER REPAIR REF ETD2024-170-027059SDR DALA2024101009946Skin · corrodedSHIP 3143 CORROSION WAS FOUND IN TOP SKIN PANEL 2, TRAILING EDGE OVERHANG AREA, LH WING. CORRECTIVE ACTION: REPAIR PER ERA 619900-14. (0598728)SDR CALA2024100902611Skin · damagedB757-06-3-0301 - GOUGE LEADING EDGE SKIN MAIN I/B FLAP I/B TRACK LH WING. DOT 46-12. REPAIRED LH WING I/B MAIN FLAP NOSE SKIN L/E IAW B757-300 SRM 57 -53-01-219-2 (MAJOR REPAIR)SDR EE4Y2024100820979Skin · no discrepancyPER ALLIANCE TASK CARD SB190-57-0056, WILL BE PERFORMED ON THE AIRCRAFT THE SB190-57-0056, HOWEVER, DURING THE RH WING AFTER REINFORCEMENT LAYOUT PROCESS, HAS BEEN NOTICED THAT THE SB REINFORCEMENT IS INTERFERING WITH AN EXISTING REPAIR INSTALLED PER ETD2019-1SDR FDEA202410081442Doubler · crackedLEFT WING - FIXED LEADING EDGE RIB DOUBLER AT STATION XOS 789 FOUND CRACK ABOUT 2". CRACKED RIB DOUBLER AT LEFT WING - FIXED LEADING EDGE STATION XOS 789 REMOVED AS PER MD-11 SRM 51-31-01-0G. DOUBLER FABRICATED AS PER DOUGLAS DRAWING: ARB3954 REVISION K ANSDR IPXA2024103107260Skin · gougedRH WING AT L/E UPPER SURFACE IS GOUGED AT APPX STA XORS 855 ATA 57-40 MARKED 84-12. REPAIR ACCOMPLISHED IAW: SRM 57-40-02-2R-3 REPAIR 3 (REV 71).SDR R61A2024102800512Skin · crackedR/H WING SLAT #2 I/B TRACK CUTOUT FOUND FLE SKIN CRACKSDR CALA2024100802606Skin · crackedCRACK ON GAP PANEL LH WING. DOT 46-23. THE GAP PANEL WAS REPAIRED AND REINSTALLED IAW B757 SRM 57-41-01 2R-3 REPAIR 3 AND AMM B757 26-18-01-424-032 AND SRM B757 51-40-0 2-0G-0.SDR FDEA202410051422Doubler · crackedRIGHT WING - FIXED LEADING EDGE RIB DOUBLER AT STATION XOS 667 FOUND CRACK ABOUT 1" INCH. CRACKED RIB DOUBLER AT RIGHT WING - FIXED LEADING EDGE STATION XOS 667 REMOVED AS PER MD-11 SRM 51-31-01-0G. DOUBLER FABRICATED AS PER DOUGLAS DRAWING: ARB3954 RSDR SWAA2024102844868Skin · crackedDURING HFEC INSPECTION; CRACK FOUND IN COUNTERSINK OF 1EA FASTENER AT 12:00 POSITION LOCATED ON LH WING L/E SKIN I/B OF NACELLE STRUT; 2 FASTENERS FROM LOWER EDGE.<[01] ?REFER TO FAULT TTG8Q00W53ZW WHERE EA 24-157-02791 WAS ADDED AS A SUBTASK.?;[02] VERIFIED CSDR DALA2024100509714Skin · damagedSHIP 3144 ELONGATED HOLE LOWER SURFACE REFORCING PLATE LOC. BTW RIB 7 AND RIB 8 ON LH WING. CORRECTIVE ACTION: REPLACED REFORCING PLATE LOC. BTW RIB 7 AND RIB 8 ON LH WING AS PER A319 SRM 57-21-11-300-005. (0590797)SDR SWAA2024110144363Access Panel · delaminatedDELAMINATED HOLE (2EA) IN ACCESS PANEL 661CB AT RT WING 2024-600552<[01] TOOL USED: CALIPER PN: 500-197-30; SN: B20189521; DUE DATE: 26-JAN-25;[02] TOOL USED: HOT BONDER PN: HCS9200B SN: 15102320; DUE DATE: 25-JAN-25;[03] TOOL USED: SCALE PN: SPX222; SN: C4107SDR DALA2024100409671Skin · crackedAIRCRAFT 3064, ON WALK AROUND FOUND DENT IN LEADING EDGE SLAT #2 LEFT WING, WITHIN LIMITS FOR TEMPORARY REPAIR. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR LOC. LEADING EDGE SLAT #2 LEFT WING AS PER A321 SRM 57-40-00-300-075 FIGURE 001. (LP 0588733)SDR SWAA2024111144373Access Panel · damagedPANEL 661BB WITH ELONGATED ATTACHING HOLE ON IB SIDE.<[01] 1. ACCOMPLISHED PULSE-ECHO ULTRASONIC INSP. FOR DELAMINATION ON PANEL 661BB & ELONGATED HOLE'S; CRACKED AND BULGING HOLE'S WITH LOCATIONS IDENTIFIED. <BR><BR>2. ACCOMPLISHED 24 HOUR DRYOUT AT PANEL #66SDR AALA202410314776Panel · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN LEFT WING PANEL AT LEVEL OF WS 968.50. REPLACED PANEL PER SRM 51-40-02-0G AND DRAWING 115W3500.SDR SWAA2024102844043Panel · damagedLEFT WING UPPER SURFACE PANEL 571AT; I/B AFT CORNER UPPER SURFACE HOLE FASTENER ELONGATED<[01] APLIED PERMANENT REPAIR ON DAMAGE AREA AS MARKED ON PANEL #571AT AS PER B737 51-70-04-2R-0 PARAG 4-N-2 MATERIAL USED: RESIN 3804 PO#2066573; FIBERGLASS PO#1690463 ANSDR AALA202412196295Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING UPPER SKIN PANEL #2 TRAILING EDGE AT RIB 13 PLUS 5 INCHES. REPAIRED SKIN PANEL PER EA 358925.SDR AALA202412187516Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TRAILING EDGE TOP SKIN PANEL #2 LOWER SURFACE AT RIB 10. REPAIRED SKIN PANEL PER EA 358925.SDR SWAA2024102843671Panel · crackedCRACKED L-CLIP ON R/W T/E PANEL 651FB FWD SIDE 27' FROM O/B END<[01] REMOVED AND REPLACED L-CLIP ON R/W T/E PANEL 651FB FWD SIDE 27' FROM O/B END IAW SRM 51-40-02-02-0G;[02] VERIFIED CORRECTIVE ACTION ITEM 1; CARD COMPLETE.SDR IPXA2024102380040Skin · corrodedLEFT WING OVER WING FILLER CAP HAS CORROSION 52-00. ACCOMPLISHED THE REPAIR PER 757-200PF SRM 57-20-01-2R-6 REPAIR 6 REV 121SDR SWI2024F00906Skin · gougedRH WING FIXED LEADING EDGE SKIN HAS 3 GOUGES BETWEEN RIB 32 AND 33. (C-CHECK RO 10/6/2024) (FILED-OPEN)PERFORMED PERMANENT DOUBLER REPAIR ON RH WING FIXED LEADING EDGE SKIN BETWEEN RIB 32-33 REF. ETD2024-170-026273. SEE CONTINUATION CARD FOR FURTHER WORK PERFOSDR SWIA20240930Skin · gougedLH WING FIXED LEADING EDGE SKIN EXTERNAL SURFACE HAS ONE EACH GOUGE AT RIB 32. (C-CHECK RO 10/6/2024) (FILED OPEN)CUT AWAY DAMAGED SECTION OF SKIN AND INSTALLED DOUBLER REPAIR ON LH WING FIXED LEADING EDGE SKIN AT RIB 32. REF: ETD2024-170-026351. WEIGHT OF REPSDR DALA2024100109594Skin · corrodedSHIP 3148 CORROSION UPPER SKIN LOWER SURFACE TRAILING EDGE OVERHANG AREA AT LEVE L RIB 15 ON RH WING. CORRECTIVE ACTION: REPAIRED PER ER/A 619616-14. (0584629)SDR CALA2024100102536Skin · damagedGEN ITEM;EA 5720-03041 REV E OP 015/// JC EA 5720-03041 REV E LH UPPER SKIN & DRAG FITTING FASTENER HOLE NO 5 HAS HFEC OPEN HOLE DEFECT INDICATION, CONTACT ENGINEERING FOR REPAIR INSTRUCTIONS ENTER EC/RA NO ON STEP 1.4. REPORTED BY V921197SDR AALA202412175626Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TRAILING EDGE TOP SKIN PANEL #2 LOWER SURFACE OVERHANG BETWEEN RIB 9 AND RIB 11. REPAIRED SKIN PANEL PER EA 358949.SDR SWIA202411040929Access Panel · corrodedCORROSION FOUND ON FUEL ACCESS PANEL OPENING 610BB. FWD JUST OUTBOARD OF CENTER. (MARKED) (FILED CLOSED)REPAIRED CORROSION DAMAGE ON FUEL ACCESS PANEL OPENING 610BB, FWD JUST OUTBOARD OF CENTER WITH REFERENCE TO REO 601R-57-21-030 REV "-L" DATED 2014-02-05. PSDR SWAA2024110143311Panel · pulledL/W T/E PANEL 561CB HAS SEVERAL PULLED FASTENER HOLE ON AFT END (MARKED)<[01] L/W T/E PANEL 561CB HAD SEVERAL PULLED FASTENER HOLE ON AFT END REPAIRED IAW SRM 51-70-04-2R-9;[02] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.SDR A6WA202409298831Skin · erodedRH OUTBOARD LEADING EDGE SKIN P/N 601R12074-4 OUT OF LIMITS AFTER EROSION REMOVAL. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED RH OUTBOARD LEADING EDGE P/N 601R12074-4 AT WS350.348 TO WS389.00. REF CRJ-200 SRM 51-42-06, AND 51-42-13 REV 39. UPPER EDGSDR UIEA2024092400941Skin · wornLH WING, AT WBL 97.5 , BTW STA 785.9 AND STA 830 WING LOWER SKIN WITH WEAR.(<P>LH WING, AT WBL 97.5 , BTW STA 785.9 AND STA 830 WING LOWER SKIN DAMAGE WAS REPAIRED IAW FVCI #24153-3 AN APPROVAL FORM FAA 8110-3 WAS ISSUED. NO FURTHER DEFECTS NOTED</P>)SDR SWAA2024110143006Panel · pulledL/W T/E PANEL 561BB HAS PULLED FASTENER HOLES (MARKED)<[01] L/W T/E PANEL 561BB HAD PULLED FASTENER HOLES REPAIRED IAW SRM 51-70-04-2R-9;[02] VERIFIED JOB COMPLETESDR SWAA2024110143305Panel · pulledL/W T/E PANEL 561AB HAS SEVERAL PULLED FASTENER HOLE ON AFT END (MARKED)<[01] L/W T/E PANEL 561AB HAD SEVERAL PULLED FASTENER HOLE ON AFT END REPAIRED IAW SRM 51-70-04-2R-9;[02] VERIFIED JOB COMPLETESDR SWAA2024110143306Panel · pulledR/W T/E PANEL 661CB HAS PULLED FASTENER HOLES ON AFT END (MARKED)<[01] R/W T/E PANEL 661CB HAD PULLED FASTENER HOLES ON AFT END REPAIRED IAW SRM 51-70-04-2R-9;[02] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.SDR SWAA2024110143307Panel · pulledR/W T/E PANEL 661AB HAS PULLED FASTENER HOLES ON AFT END (MARKED)<[01] R/W T/E PANEL 661AB HAD PULLED FASTENER HOLES ON AFT END REPAIRED IAW SRM 51-70-04-2R-9;[02] VERIFIED JOB COMPLETESDR SWAA2024110143309Panel · pulledR/W T/E PANEL 661BB HAS PULLED FASTENER HOLES ON AFT END (MARKED)<[01] R/W T/E PANEL 661BB HAD PULLED FASTENER HOLES ON AFT END 51-70-04-2R-9;[02] VERIFIED JOB COMPLETESDR IPXA2024100154148Panel · missingAFTER BLOCK IN MECHANIC INFORMED ME OF LEFT WING LOWER PANEL MISSING INSTALLED NEW PANEL PER SRM 51-40-20SDR DALA2024093009561Skin · corrodedSHIP 3148 CORROSION WAS FOUND ON TOP SKIN PANEL 2, TRAILING EDGE OVERHANG AREA, ON THE RH WING. CORRECTIVE ACTION: REPAIRED PER SECTION II OF ER/A 619616-14.SDR DALA2024093009560Skin · corrodedSHIP 3148 CORROSION WAS FOUND IN TOP SKIN PANEL 2, TRAILING EDGE OVERHANG LH WING. CORRECTIVE ACTION: REPAIRED PER ER/A 619615-14. (0581168)SDR DALA2024093009559Skin · corrodedSHIP 3148 CORROSION WAS FOUND IN TOP SKIN PANEL 2, TRAILING EDGE OVERHANG AREA, LH WING. CORRECTIVE ACTION: REPAIRED PER SECTION II OF 619615-14. (0581147)SDR JR2R20240928372Panel · chafedLH WING PANEL 551AB CHAFED IN 2 AREASSDR QXEA2024092900224Skin · gougedWING LEADING EDGE LH SKIN BETWEEN RIB37-42 GOUGE. COMPLIED WITH EC ETD2024-170-025461 REV B. WING LEADING EDGE LH SKIN BETWEEN RIB37-42 GOUGE.SDR QXEA2024092900223Skin · gougedLH WING FIXED LEADING EDGE GOUGED BEHIND SLAT 4 OB SIDE. REPAIRED LH WING FIXED LEADING EDGE BEHIND SLAT 4 OB SIDE REF ETD 2024-170-025641 REV B.SDR SWAA2024102142594Panel · delaminatedLEFT WING LEADING EDGE PANEL 521TB HAS DELAMINATION ON TWO CORNERS<[01] REPAIRED 2 EACH AREAS OF EDEGE DAMAGE IAW SRM 57-41-01-2R-1 AND SRM 51-70-04-2R-13 REPAIR 13;[02] VERIFIED ITEM 1<BR>C/WSDR CALA2024093000707Skin · crackedPOTENTIAL CRACK IN LH WING LOWER OUTBOARD SKIN PANEL AND S-9 CRACK BETWEEN WSTA 564.5 AND WSTA 591.5.ON THE LH WING LOWER SKIN BETWEEN WSTA 564 AND WSTA 591 ,SDR CALA2024093000706Skin · crackedRH WING LOWER OUTBOARD SKIN PANEL AND S-9 CRACK BETWEENWSTA 564.5 AND WSTA 591.5 ON THE LH WING LOWER SKIN BETWEEN WSTA 564 AND WSTA 591 ,SDR CALA2024093000705Skin · crackedRH WING LOWER OUTBOARD SKIN PANEL AND S-9 CRACK BETWEEN WSTA 564.5 AND WSTA 591.5 REF TO LOG PAGE 9379446 PLANNING TO CONTACT ENGINEERING AFTER 24 JANUARY 2026 BUT BEFORE 24 FEBRUARY 2026 FOR THE INSPECTION REQUIREMENTS. DIP 57-DIP CLOSE THE LOG AND BEGIN NEW SDR R61A2024100100441Skin · crackedCRACK ON RIGHT WING LOWER SKIN INBD OF RIB 17 AND AFT OF SPAR 1. REPAIRED IAW ETD2024-170-025874. MAJOR REPAIR. AIRCRAFT WAS RETURNED TO SERVICE ON 29 SEPT 24SDR VNAA202409240009Skin · nickedSEVERAL NICKS ON LOWER SKIN OF RH INBOARD FLAP FLS 15.00 TO FLS 65.5 AT RH WING. NICKS ON LOWER SKIN OF RH INBOARD FLAP FLS 15.00 TO FLS 65.5 AT RH WING WERE BLEND OUT PER CRJ900 SRM 51-12-00-001-001-A01 AND SECTION BTW FLS15.00 TO FLS 30.00 WAS EVALUATED OUTSDR SWAA2024110140518Access Panel · damagedELONGATED HOLES ACCESS PANEL 561CB AT LT WING 2024-600149<[01] TOOL USED: CALIPER PN:500-196-30 SN:A22348594 DUE DATE:23-JUL-25.;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N:18175478 DUE DATE: 25/JAN/25.;[03] TOOL USED SCALE P/N: CR5200 S/N: 8343110809 DUE SDR SWAA2024093040645Panel · crackedLH WING LOWER FIXED INBOARD TRAILING EDGE PANEL 551FB CRACK DAMAGE<[01] REMOVED PANEL 551FB PER SRM 51-40-02.;[02] LOCATED HOLES IN 551FB PER SRM 51-40-05.;[03] HOLES LOCATED IN NEW PANEL PER SRM 51-40-05;[04] INSTALLED 551FB PANEL PER M/M 57-15-00-400-801
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