JASC 5313
Service difficulty reports · 36,274
Reports filed under 5313 · Fuselage Main, Longeron/Stringer, 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 = '5313' 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 = '5313' 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 IPXA2025092467530Stringer · crackedSTRINGER CRACK, FWD SIDE OF STA 2180 S-13R. PERFORM EO-95204-REQ1 REV.1 AND EI NO.F2025A53M-2025 REV.1. VERIFY REPAIR IS ACCOMPLISHED PER GMM 04.02.01.15SDR IPXA2025092367676Stringer · crackedSTRINGER CRACK, FWD SIDE OF STA 2360 S-11L REPAIRED I.A.W SWPM 20-10-11 , 20-10-12 REV.89 INSTALLED WIRE BUNDLE SUPPORT CLAMPS AT MAIN DECK STA 2350 BETWEEN S-9L TO S-13L AND CONDITION CHECK NORMAL. PERFORM EO-95193-REQ1 REV.1 AND EI NO.F2025A53M-2048 REV.1.SDR IPXA2025092167607Stringer · crackedSTRINGER CRACK, AFT SIDE OF STA 2180 S-18L (LEVEL1) (REPAIR) INSPECTION COMPLETED FOR EGAT WORK SHEET NO.50700 STEP 30 - RESPECTIVELY PART MARK THE REPAIR PARTS. RII COMPLETED FOR EGAT WORK SHEET NO.50700 STEP 31.SDR IPXA2025092267448Stringer · crackedSTRINGER CRACK, FWD AND AFT SIDE OF STA 2180 S-21L (LEVEL1) (REPAIR). FABRICATED REPAIR SPLICE I.A.W. EGAT WORK SHEET NO. 50694 STEP 14 (SRM 53-60-03-2R-12 REV.46/TR:53-160)PERFORMED THE HEAT TREATMENT FROM 7075-O TO T62 CONDITION I.A.W. EGAT WORK SHEET NO.:50SDR IPXA2025092267623Stringer · crackedSTRINGER CRACK, FWD AND AFT SIDE OF STA 2180 S-20L (LEVEL1) (REPAIR).FABRICATED REPAIR SPLICE I.A.W. EGAT WORK SHEET NO. 50695 STEP 14 (SRM 53-60-03-2R-12 REV.46/TR:53-160).PERFORMED THE HEAT TREATMENT FROM 7075-O TO T62 CONDITION I.A.W. EGAT WORK SHEET NO.:50SDR IPXA2025092267652Stringer · crackedSTRINGER CRACK, FWD AND AFT SIDE OF STA 2180 S-22L (LEVEL1) (REPAIR)FABRICATED REPAIR SPLICE I.A.W. EGAT WORK SHEET NO. 50696 STEP 14 (SRM 53-60-03-2R-12 REV.46/TR:53-160).PERFORMED THE HEAT TREATMENT FROM 7075-O TO T62 CONDITION I.A.W. EGAT WORK SHEET NO.:506SDR IPXA2025092267421Stringer · crackedSTRINGER CRACK, FWD AND AFT SIDE OF STA 1960 S-10R (LEVEL1) (REPAIR). PERFORMED SRM 53-60-03-2R-4 REV.46/TR:53-155 AND EGAT WORK SHEET NO.50698 STEPS 1-43. PERFORMED EO-95172-REQ1 REV.1 & EI NO.F2025A53M-2097 REV.0 AND EGAT WORK SHEET NO.50698.SDR SWI2025F01907Stringer · corrodedSTR 20R IS CORRODED ON THE WEB AND FREE FLANGE BETWEEN FS364 & 379. REMOVED AND REPLACED CORRODED STRINGER AND FLANGE WITH NEW STRINGER AND FABRICATED FLANGE AT STR 20R PER REO 690-53-21-2042 REV--. ALL STEPS OF REO COMPLIED WITH IN THEIR ENTIRETY. PERFORMEDSDR IPXA2025092254119Stringer · crackedSTRINGER CRACK, AFT SIDE OF STA 1960 S-40L (LEVEL1) (REPAIR). IAW EGAT WORK SHEET 50688 STEP:11-21, SRM 53-60-03-2R-9, REV 46, TR 53-150. PERFORMED EO-95191-REQ 1 REV.1 AND EI F2025A53M-2128 REV.0 AND EGAT WORK SHEET 50688.SDR IPXA2025092254156Stringer · crackedSTRINGER CRACK, FWD SIDE OF STA 1960 S-42L (LEVEL1) (REPAIR) RII COMPLETED FOR EGAT WORK SHEET NO.50693 STEP 20. PERFORMED EO-95192-REQ1 REV.1 AND EI NO.F2025A53M-2143 REV.0 AND EGAT WORK SHEET NO.50693SDR IPXA2025092254125Stringer · crackedSTRINGER CRACK, FWD SIDE OF STA 1960 S-38L (LEVEL1) (REPAIR) RII COMPLETED FOR EGAT WORK SHEET NO.50692 STEP 20. PERFORMED EO-95188-REQ1 REV.1 AND EI NO.F2025A53M-2140 REV.0 AND EGAT WORK SHEET NO.50692SDR IPXA2025092254168Stringer · crackedSTRINGER CRACK, AFT SIDE OF STA 1960 S-38L (LEVEL1) (REPAIR). PERFORMED SRM 53-60-03-2R-9 REV.46 / TR: 53-150 AND EGAT WORK SHEET NO.50691 STEPS 1-20.PERFORMED EO-95188-REQ1 REV.1 AND EI NO. F2025A53M-2140 REV.0 AND EGAT WORK SHEET NR 50691.SDR IPXA2025092254147Stringer · crackedSTRINGER CRACKED, AFT SIDE OF BS 1960 S39L (LEVEL1) (REPAIR). IAW EGAT WORK SHEET 50689, STEPS 11-21, SRM:53-60-03-2R-9, REV 46, TR 53-150. PERFORM EO-95190-REQ 1, REV 1, & EI F2025A53M-2127, REV 0, & EGAT WORK SHEET 50689.SDR IPXA2025092255048Stringer · crackedSTRINGER CRACK, AFT SIDE OF STA 1960 S-42L (LEVEL1) (REPAIR).PERFORMED SRM 53-60-03-2R-9 REV.46 / TR: 53-150 AND EGAT WORK SHEET NO.50690 STEPS 1-20.PERFORMED EO-95192-REQ1 REV.1 AND EI NO.F2025A53M-2143 REV.0 AND EGAT WORK SHEET NR 50690.SDR IPXA2025092541438Stringer · crackedMAJOR REPAIR, STRINGER CRACKED, AFT SIDE OF BS 740, S42L. PERFORM EO-95167-REQ1, REV 1 AND EI F2025A53M-2129 REV 0, AND EGAT WORK SHEET 50687.SDR IPXA2025092241519Stringer · crackedMAJOR REPAIR - STRINGER CRACKED, FWD SIDE OF BS 740, S39L. PERFORMED EO-95267-REQ 1, REV 1 & EI F2025A53M-2009, REV 2.SDR IPXA2025092141490Stringer · crackedSTRINGER CRACKED, FWD & AFT SIDE OF BS 740, S47L. PERFORMED SRM 53-20-03-2R-5 REV.46, TR 53-161, & EGAT WORK SHEET 50685, STEPS 1-21. PERFORMED EO-95169-REQ 1, REV 1, & EU F2025A53M-2105, REV 0 & EGAT WORK SHEET 50685.SDR IPXA2025091541450Stringer · crackedMAJOR REPAIR - STRINGER CRACKED, FWD AND AFT SIDE OF BS 740, S43L. PERFORMED EO-95168-REQ 1, REV 1, & EI F2025A53M-2184, REV 1, & EGAT WORK SHEET 50686.SDR IPXA2025091541511Stringer · crackedMAJOR REPAIR - STRINGER CRACKED, FWD AND AFT SIDE OF BS 740, S47R. PERFORMED EO-95170-REQ 1, REV 1, EI F2025A53M-2217, REV 0 & EGAT WORK SHEET 50684.SDR SWIA20251110905Stringer · corrodedSTGR 24R BETWEEN F.S. 333 AND F.S. 347 IS CORRODED. (FILED CLOSED)REMOVED CORROSION ON STRG 24R FS 333 AND FS 347, EVALUATED WORKED AREA FOUND TO BE OUT OF LIMITS,FABRICATED SECTION OF STRINGER 24R FROM FS 333 AND FS 347 FROM B0530020BF STRINGER EXTRUSION, SDR AALA202510239031Stringer Splice · damagedAIRCRAFT IN BASE MAINTENANCE: ELONGATED HOLE ON LOWER SPLICE OUTBOARD SIDE ON LOWER SILL LOC. STR23R AT LEVEL FR66 AFT GALLEY AREA. MEASURE IS 0.043 IN. MAINTENANCE REPLACED LOWER SPLICE OUTBOARD SIDE ON LOWER SILL LOC. STR23R AT LEVEL FR66 AFT GALLEY AREA, IASDR AALA202510236165Stringer Splice · damagedAIRCRAFT IN BASE MAINTENANCE: ELONGATED HOLE ON UPPER SPLICE INBOARD SIDE ON LOWER SILL LOC. STR23R AT LEVEL FR66 AFT GALLEY AREA. MEASURE IS 0.049 IN. MAINTENANCE REPLACED UPPER SPLICE INBOARD SIDE LOC. STR23R AT LEVEL FR66 AFT GALLEY AREA, IAW A320 SRM 51-72SDR AALA202510233940Stringer Splice · elongatedAIRCRAFT IN BASE MAINTENANCE: ELONGATED HOLE ON UPPER SPLICE OUTBOARD SIDE ON LOWER SILL LOC. STR23R AT LEVEL FR66 AFT GALLEY AREA. MEASURE IS 0.05 IN. MAINTENANCE REPLACED UPPER SPLICE OUTBOARD SIDE LOWER SILL LOC. STR23R AT LEVEL FR66 AFT GALLEY AREA, IAW A3SDR IPXA2025092725310Stringer · crackedSTRINGER CRACK, AFT SIDE OF STA 2360, STA 2377 AT S-6L (LEVEL 2) (REPAIR).REMOVED UPPER CORNER BRACKET FROM LOWER FUSELAGE, WING/BODY FAIRING 194CR IAW B757-200PF SRM 51-40-02-0G-0.FABRICATED UPPER CORNER BRACKET R/H FROM P/N: SHT-7075T6-0.063/12 BATCH: 000323SDR IPXA2025092625040Stringer · crackedSTRINGER CRACKED, FWD SIDE OF BS 2598 S5L LEVEL 2. PERFORM EO-95354-REQ1 REV.1 AND EI F2025A53M-2043 REV 1.SDR IPXA2025091824996Stringer · crackedSTRINGER CRACK, FWD SIDE OF STA 2598 S-7R LEVEL 2. ACCOMPLISHED REPAIR IAW EO-95138-REQ1 REV.1 AND EGAT EI F2025A53M-2075 REV.0 AND SRM 53-80-03-2R-2 REV.46 / TR53-152 AND EGAT WORK SHEET NR.50683.SDR IPXA2025092525306Stringer · crackedSTRINGER CRACKED, AFT SIDE OF BS 2360, BS 2377 AT S5R (LEVEL 2) PERFORM EO-95265-REQ1 REV.1 AND EI F2025A53M-2037 REV 2.SDR IPXA2025092525301Stringer · crackedSTRINGER CRACK, AFT SIDE OF BS 2360, BS 2377 TO BS 2380 AT S-5L (LEVEL 2). PERFORM EO-95266-REQ1 REV 1 AND EI F2025A53M-2035 REV 2.SDR IPXA2025091824925Stringer · crackedSTRINGER CRACK, FWD SIDE OF STA 2598 S-8L LEVEL 2. (REPAIR). VERIFY REPAIR IS ACCOMPLISHED PER GMM 04.02.01.15 REQUIREMENTS. PAPER FINAL COMPLETED. ACCOMPLISHED REPAIR I.A.W UPS EO-95140-REQ1 REV.1 AND EGAT EI NO.F2025A53M-2076 REV.0 AND SRM 53-80-03-2R-2 REV.SDR FDEA202509051646Longeron Splice · damagedDAMAGED LONGERON SPLICE AT STATION 1811 AND LONGERON 36 REWORKED DAMAGED SPLICES IAW 51-21-10.SDR AALA202510280456Stringer · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION STRINGER 43L BTW FR 56 AND FR 57 IN AFT CARGO COMPARTMENT MEASURE OF CORROSION AREA L= 8.191 IN, W= 0.848 IN, D= 0.003 IN. MAINTENANCE PERFORMED PERMANENT REPAIR (SPLICE REPAIR) ON STRINGER 43L BTW FR55 TO FR58 IN AFT CSDR HNAA2025100300674Stringer · damagedSTRINGER 14R HAS AN OVERSIZED HOLE AT FR2. RAR STRINGER 14R BTW FR 1A-6 IAW EMB 145 SRM 51-40-02. DURING REPLACEMENT FOUND 13 HOLES BETWEEN FR 2-3 TO ONLY HAVE 1.5D EDGE DISTANCE. 13 HOLES ARE ACCEPTED AS A PERMANENT REPAIR IAW ETD2025-145-928801 AND EO1-53-2SDR IPXA2025091709687Stringer · crackedCENTER WING UPPER FUEL TANK LOWER STRINGER 41 CRACK AT XCW = -81 REQUIRES PERMANENT REPAIR PER EO 81811-REQ001 ATA 57-11 QC AUDIT C/WSDR DALA2025090806598Stringer · corrodedCORROSION ON STRINGER & STRINGER SPLICE 25LH BTW STA 947-967 AT AFT CARGO. STRINGER & STRINGER SPLICE 25LH BTW STA 947-967 AT AFT CARGO WERE REPAIRED PER B737-800 SRM 53-00-03-2R REPAIR 1.SDR 2025FA0000621Stringer · crackedPERFORMED INSPECTIONS PER AD-2023-12-18 IAW BOEING REQUIREMENTS BULLETIN 747-53A2907. IDENTIFIED CRACKS IN STRINGERS AT THE FOLLOWING LOCATIONS: STA 1740: S-13L, S-14L, S-14R, S-15R STA 1960: S-1L, S-2L, S-3L, S-4L, S-6L, S-8L, S-9L, S-10L, S-11L, S-12L, S-SDR 2025FA0000620Stringer · crackedPERFORMED INSPECTIONS PER AD-2023-14-03 IAW BOEING REQUIREMENTS BULLETIN 747-53A2911. IDENTIFIED CRACKS IN STRINGERS AT THE FOLLOWING LOCATIONS: STA 2598: S-4R, S-5R, S-25R, S-4L, S-5L, S-8L, S-10LSDR CALA2025090808565Stringer · corrodedAFT CARGO BILGE AREA BETWEEN FR 63 & 64 STRINGER 41R HAS CORROSI ON. REMOVED AND REPLACED STRINGER 41R FR59-61 IAW SRM 51-72-11.SDR SWI2025F01762Stringer · corrodedSTRINGER 25R BETWEEN BS 280 TO 295 HAD CORROSION. REMOVED AND INSTALLED A NEW STRINGER BETWEEN BS 280 AND BS 333 IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, AND DWG SH670-31630, REV K. PERFORMED PRESSURE LEAK CHECK IAW AMM 21-31-00-910-801-A01. LESDR SWI2025F01760Stringer · corrodedSTRINGER 25L BETWEEN BS 280 AND 295 CORRODED. REMOVED AND INSTALLED A NEW STRINGER IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND DWG SH670-31630, REV K. PERFORMED PRESSURE LEAK CHECK IAW AMM 21-31-00-910-801-A01. LEAK CHECKED GOOD. COMPLIED WITH SDR SWI2025F01749Stringer · corrodedSTR26R BETWEEN APPROX FS280 TO FS310 HAS CORROSION. REMOVED AND INSTALLED NEW STR26R BETWEEN FS280 AND FS333 REF SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 AND DWG SH670-31630 REV K. PERFORMED PRESSURE LEAK CHECK IAW AMM 21-31-00-910-801-A01. LEAK SDR SWI2025F01748Stringer · corrodedSTR26L BETWEEN FS280 AND FS333 HAS CORROSION. (C-CHECK RO 12/07/2025)REMOVED AND INSTALLED NEW STR26L BETWEEN FS280 AND FS333 REF SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 AND DWG SH670-31630 REV K. PERFORMED PRESSURE LEAK CHECK IAW AMM 21-31-00-SDR SWIA202512080030Stringer · corrodedSTRINGER 27 BETWEEN APPROX BS 280 TO JUST AFT OF BS 295 HAS CORROSION. REMOVED AND INSTALLED NEW S27 FROM BS 280 TO JUST AFT OF BS 295 IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01, AND DWG SH670-31630 REV K. PERFORMED PRESSURE LEAK CHECK IAW AMMSDR DALA2025083106427Stringer · corrodedAFTER REMOVE ACCES PANEL N/P 284A6813-3 ON INTERNAL FWD E/E: CORROSION WAS FOUND ON S-27L BTW STA.348.2 TO STA.380. STRINGER S-27L BTW STA. 348.2 TO STA. 380 WAS REPAIRED PER B737-800 SRM 53-00-03-2R PROCEDURE 1. REPAIR 1. (LP 1173288)SDR DALA2025083006414Stringer · corrodedAFTER REMOVE ACCESS PANEL N/P 284A6813-3 ON INTERNAL FWD E/E: CORROSION WAS FOUND ON S-L28-LH BTW STA.348.2 TO STA.380. CORROSION LEVEL 2, STRINGER 28 LH BTW STA 380 TO STA 362 WAS REPAIRED PER B737-800 SRM 53-00-03-2R PROCEDURE 1. REPAIR 1. (LP 1171591)SDR KCSA202508291148Longeron Fitting · crackedFOUND R/H LONGERON EXTENSION FITTING TO BE CRACKED WITH EDDY CURRENT INSPECTIONSDR SWIA2025F01348Stringer · no discrepancyREMOVED FWD RIVETS ON REMOVED STGR 22L BETWEEN FS193.00 AND FS202.75 TO FOM AS CALLED OUT BY REO 670-53-11-2170 REV -- DATE 9-22-25. SEE CP 30714031 (FILED CLOSED)REINSTALLED REMOVED RIVETS ON STGR 22L BETWEEN FS193.00 AND FS202.75 IAW SRM 51-42-06, SRM 51-42SDR SWIA2025F01347Stringer · no discrepancyREMOVED FWD RIVETS ON STGR 21L BETWEEN FS193.00 AND FS202.75 TO FOM AS CALLED OUT BY REO 670-53-11-2170 REV -- DATE 9-22-25.. SEE CP 30714031 (FILED CLOSED)REINSTALLED REMOVED RIVETS ON STGR 21L BETWEEN FS193.00 AND FS202.75 IAW SRM 51-42-06, SRM 51-42-20 ANSDR SWIA202509240828Stringer · no discrepancyREMOVED FWD RIVETS ON STGR 19L BETWEEN FS193.00 AND FS202.75 TO FOM AS CALLED OUT BY REO 670-53-11-2170 REV -- DATE 9-22-25. SEE CP 30714031 (FILED CLOSED)REINSTALLED REMOVED RIVETS ON STGR 19L BETWEEN FS193.00 AND FS202.75 IAW SRM 51-42-06, SRM 51-42-20 AND SDR VNAA202508280070Stringer · corrodedSTRINGER 24R BETWEEN FS 349.00 AND FS 379.00 IS CORRODED. INSTALLED NEW STRINGER SEGMENT FROM FACTORY SPLICE AT FS 333 TO CUT-LINE BETWEEN FS 364 TO FS 379 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND SRM REPAIR 53-00-03-201-001-A01. INSTALLED SPLICE AT FS 333 STRSDR VNAA202508280045Stringer · corrodedSTRINGER 24L BETWEEN FS 295.00 AND FS 310.00 IS CORRODED. CORRECTIVE ACTION: NSTALLED STRINGER 24L BETWEEN FS280 TO FACTORY SPLICE AT FS 333 IAW CRJ 700 SRM 51-42-06-001-001-A01. INSTALLED SPLICE AT FS 333 STRINGER 24L IAW CRJ 700 SRM 51-42-06-001-001-A01. SH6
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