JASC 5330
Service difficulty reports · 79,329
Reports filed under 5330 · Fuselage Main, 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 = '5330' 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 = '5330' 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 DALA2025030301644Skin · wornSHIP 3312 FUSELAGE SKIN WITH BELLY FAIRING 197FB,197GB,197EB, 198HB AND 198GB TOUCH AREA FOUND WORN. CORRECTIVE ACTION: REPAIRED THE AREA PER ERA 624200-14 REV ORIGINAL (0836961)SDR AALA202503037186Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FUSELAGE SKIN AT LAVATORY SERVICE PANEL LOWER EDGE, AT STA 847 FROM S23L TO S25L. ACCOMPLISHED REPAIR PER EA 362278.SDR SWIA202506240301Skin · dentedDENT ON EXTERIOR SKIN AT FASTENER AT FS559.00 BETWEEN STGR3R - STGR4R AS MARKED (C-CHECK RO 06/23/2025) SUSPECTED DENTED AREA AT FS559.00 STGR3R-STGR4R FOUND TO BE A PREVIOUSLY BLENDED AREA. REPAIRED BLEND AREA AT FS544.00-FS559.00+16 STGR2R-STGR5R PER REO 6SDR SWAA2025032601193Skin · cracked#2 TANK UPPER SKIN (INTERNAL) BETWEEN RIB 21 AND RIB 22; AFT UPPER STRINGER END IS CRACKED.<[01] CRACK ON #2 FUEL TANK (INTERNAL). AFT UPPER STRINGER; BETWEEN RIBS 21 AND 22 WAS REPAIRED IAW EA 25-157-00566-WIP1 AND EA 25-157-00566;[02] C/WSDR DALA2025030401680Skin · damagedAIRCRAFT 3717, IN COURSE OF ACCOMPLISHMENT OF A FUSELAGE SKIN REPAIR TO THE NOSE SKIN NEAR THE LH AOA VANE PER ER/A 624396-14, ADDITIONAL INTERNAL ACCESS IS NEEDED TO INSTALL PERMANENT FASTENERS DUE TO STRUCTURE BLOCKING THE REPAIR AREA. THE COCKPITFLOOR SUPPOSDR DALA2025030401677Skin · ground damageAIRCRAFT 3717, WHILE OVERNIGHT IN ATL, A WEATHER EVENT WITH HIGH WIND PUSHED A SET OF GROUND STAIRS INTO THE LEFT SIDE OF THE FUSELAGE BETWEEN STA 177-188. CORRECTIVE ACTION: PERFORMED HFEC INSPECTION, REMOVED DAMAGED AREA AND INSTALLED REPAIR DOUBLERS AND RE-SDR DALA2025030301646Skin · chafedSHIP 3312 CHAFING DAMAGE WAS FOUND ON THE FUSELAGE SKIN AT FR 54 TO FR 55, STR 47 RH TO 50 RH. CORRECTIVE ACTION: REPAIRED PER ERA 624200-14. (0834877)SDR UIEA2025022700171Skin · corrodedCORROSION ON RH FUSELAGE SKIN AT STA 1702, S-45R.(<P>1. ACCOMPLISHED WORK SHEET #50030 (SRM 53-00-01-2R-1 REV. 122). 2. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)SDR SWIA2025052700228Skin · damagedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA79453-601R-53-61-7855 REV N930SW MXCODEID62997-PR - MULTIPLE DAMAGE TO FUSELAGE SKIN BETWEEN FS589 €“ FS605 AND STR20R €“ STR26R. PERFORMED TEMPORARY REPAIR TO FUSELAGE SKIN BETWEEN FS589 - FS605 AND STR20R - STR26RSDR IPXA2025040901673Skin · dented**SDR FILED OPEN** FAULT/ STR/ZONE 100 LOWER HALF OF FUSELAGE (EXTERNAL)R/H. FR 3 APPROXIMATELY STG44 / STG 40 THEREIA A DENT .DOT 113-20(DARIO CAMACHO) VERIFIED RESTORATION OF ALL OXYGEN SYSTEM, STORAGE BOX IAW-A300 AMM 35-11-11/401.SDR SWIA2025030500228Skin · dentedDENT ON R/H SIDE OF REAR FUSELAGE BETWEEN FRAMES 97-98, STRINGERS 23R-25R. (C-CHECK RO 3/4/2025) PERFORMED DOUBLER REPAIR ON R/H SIDE OF REAR FUSELAGE BETWEEN FRAMES 97-98, STRINGERS 23R-25R REF EMB SRM 53-30-01/REPAIR09P. SEE CONTINUATIN CARD FOR WORK SDR DALA2025030401678Doubler · corrodedAIRCRAFT 3742, DURING H CHECK AT AEM (SAL), WHILE EXECUTION OF INSPECTIONS IN THE FWD CARGO COMPARTMENT (INTERNAL, CPCP) AS PER JOB CARD 5300-2594, CORROSION WAS FOUND AFFECTING SKIN DOUBLER PN 143A3233-2, LOCATED BETWEEN BSTA520/BSTA540 AND STR28R/STR28L. CORSDR YENA2025030300221Skin · corrodedDURING HEAVY MAINTENANCE: FUSELAGE / REAR FUSELAGE / BOTTOM SKIN / FR 75-76 & STR 31-36 LH / WASTE ACCESS DOUBLER / CORROSION DAMAGE – TEMPORARY REPAIR; REFERENCES: /1/ AIRBUS CANADA REO 500-53-61-1672 /2/ AIRBUS CANADA DRAWING 500-53-61-1672 (CONTAINED IN REFSDR YENA2025030300219Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION FOUND WASTE DOUBLER CUTOUT; REF AVIANOR WO JB-3112-C01 NR3024 WASTE DOUBLER (P/N C01342310-111) FOUND OUT OF LIMITS AS PER ASRP, REPAIRED IAW JETBLUE EC NO. AC25-126-01 AND REO 500-53-61-1672 TEMPORARY REPAIR DVI OF DISCREPASDR VNAA2025022811102Skin · gougedAFT FUSELAGE LOWER SKIN PANEL, GOUGING BETWEEN FS1031 - FS1040 AND S-21R - S-26R / INCORPORATED PERMANENT REPAIR REO 690-53-61-1516 REV -- TO THE FUSELAGE FS 1000.00 - FS 1051.30 & STR 20R - STR 27. (MHI MRT STATEMENT OF WORK ORDER # MIS-6305)SDR AALA202502285256Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FUSELAGE SKIN UNDER LEFT HAND RAM AIR INLET AT BS 500I BETWEEN S22L AND S23L. ACCOMPLISHED DOUBLER REPAIR PER EA 362009..SDR DALA2025030501722Skin · not reportedSHIP 3410 ERA 619402-14 REV E ISSUED FOR SKIN CUTOUT REINFORCEMENT REPAIR. SECTION II: PERMANENT REPAIR ACCOMPLISHED IN MSP. FOLLOW-ON ACTION REQUIRED. CORRECTIVE ACTION: PERFORMED FOLLOW UP INSPECTION PER ERA. OK TO CONTINUE. (0831942)SDR DALA2025030301609Skin · crackedAIRCRAFT 3747, RH SIDE OF FUSELAGE EXTERNAL POWER PANEL CUT OUT FWD EDGE IS CRACKED. CORRECTIVE ACTION: ACCOMPLISHED REPAIR AT EXTERNAL POWER RECEPTICAL DOOR IAW B737 SRM 53-10-15-2R REPAIR 5. DEFERRED TO MONITOR, IAW B737 SRM 53-10-15-2R REPAIR 5 PAGE 4 FIG. SDR AALA202502285850Cover Plate · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT ATG ANTENNA/COVER PLATE BETWEEN FR 56 AND FR 57, BETWEEN S42L AND S43L. REPLACED COVER PLATE PER SRM 51-72-11.SDR DXTR202502270055Skin · gougedGOUGE, TAILCONE, AFT UPPER MIDDLE SKIN. ACCOMPLISHED FR-680A-0063-14787 REV - DATED 2-20-25 AND FAA FORM 8110-3 DATED 02/20/2025; FIELD REPAIR - GOUGE, TAILCONE, AFT UPPER MIDDLE SKIN, FS 605.00 AND WL 169.00.SDR REXA2025041400423Skin · corrodedFOUND CORROSION ON INNER SKIN AROUND WHAT APPEARS TO BE A SKIN PLUG RIVET AT APPROXIMATELY F.S. 286 BETWEEN STGR 26R AND STGR 25R. REPAIRED IAW ENDEAVOR AIR EA NO: CRJ753-18599 REV. IR DATED 3/11/2025.SDR SWAA2025031099605Skin Panel · crackedFSD FWD SURROUND PANEL IS CRACKED AT THE OUTLET CUTOUT.<[01] REPAIRED FSD FWD SURROUND PANEL CRACK AT OUTLET CUTOUT IAW CMM 25-00-66 REPAIR 1-1 SECTION 4.B.; REPAIR 2-1 SECTION 3.B. AND SECTION 4.B; AND ENG. DWG 25200003 PG. 11 ITEM 1.12.SDR DALA2025030301608Skin · dentedAIRCRAFT 3750, DURING INSPECTIONS, TWO (2) DENTS WITH CREASE WERE FOUND ON THE SKIN (PN 141A3521-11) AT APPROX. BS 196 AND BS 203, BELOW STR 24L. DAMAGE TOLERANCE EVALUATION (DTE) REQUIRED FOR FUSELAGE SKIN REPAIR INSTALLED BETWEEN STA 196 - 203 & S24L PER ER/SDR JR2R20250226738Skin · dentedRH SIDE FUSELAGE BETWEEN FRAMES 20 AND 21 AND IN BETWEEN STRINGERS 20 AND 21 HAS A DENT THAT IS OUT OF LIMITS.SDR AALA202506208254Skin Panel · crackedAIRCRAFT IN BASE MAINTENANCE: DAMGED HOLE IN FORWARD SKIN PANEL RT. MAINTENANCE PERFORMED TIME LIMITED REPAIR LOCATED ON FUSELAGE RT SIDE FR 16 FWD SKIN PANEL/ DOOR SURROUND PANEL.SDR SWIA2025041812Skin · deformedEXTERIOR LOWER SKIN PANEL, FS700 STG21L, PREVIOUS REPAIR IS DEFORMED, HN00223204 (C-CHECK RO 04/17/2025)COMPLETED REPAIR STEPS 1 TO16 FOR DOUBLER REPAIR AND SECTION FRAME OF REF. REO 601R-53-61-8299 REV --, DATE 2025-04-10 AND DWG 600-36029, REV. D. M-337SDR CALA2025031102708Skin · dentedDENT REPORTED ABOVE FIRST OFFICERS SLIDING WINDOW 2R, AT SECTION 41 AT STATION 188, PROXIMATELY 12 INCHES ABOVE TO 2RSLIDING WINDOW PERFORMED INTERIM REPAIR PER PART 1 OF ECRA 5310-08523. PERFORM REPETIVE INSPECTION AT EVERY CYCLE PER PART 2 INSPECTIONS AND ASDR N6WA2025022501Skin · dentedFUSELAGE SKIN DAMAGED AT FS250 TO FS280 AND STRINGERS 17R TO 20R. PERFORMED REPAIR TO THE FUSELAGE SKIN AT FS250 TO FS280 AND STRINGERS 17R TO 20R IAW MHIRJ REO 670-53-11-2095 AND GOJET EO C550-53MR-055-O.SDR DALA2025022701522Skin · cracked(LOG 0826895) CRACK ON INTERNAL DOUBLER ON EXTERNAL POWER RECEPTACLE CUT OUT IN FWD LOWER EDGE, APPROXIMATELY IN STA 233. FUSELAGE SKIN ON AREA EXTERNAL POWER RECEPTACLE CUT OUT IN FWD LOWER EDGE WAS REPAIRED PERMANENTLY, CATEGORY B, PER B737-800 SRM 53-10-15-SDR AALA202502251010Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LOWER FUSELAGE SKIN AROUND POTABLE WATER DRAIN AT BS 953, BETWEEN S26L AND S27L, AT LBL 8.5. ACCOMPLISHED DOUBLER REPAIR PER EA 362120 AND SRM 51-40-02 AND SRM 51-10-01.SDR CALA2025022402444Skin · dentedFUSELAGE SKIN DENTED AT APPROX STA 382 ON STRINGER 8R. DENT REPAIRED IAW ECRA 5310-08503 AT IHC BASE VISIT ON NON-ROUTINE 2377794. CATEGORIZED AS MAJOR REPAIR AND RII INSPECTED. ESFR CREATED. DMG LP 3782513 CREATED PER ECRA PART F AND DENT DOT APPLIED. DIP LP SDR CALA2025022402439Doubler · noneDISCREPANCIES BETWEEN INSTALLATION DRAWING AND EXISTING FASTENER LOCATIONS DURING LAYOUT OF L1 DOOR SURROUND STRUCTURE DOUBLER PREVENTIVE MODIFICATION L1 DOOR SURROUND STRUCTURE DOUBLER PREVENTIVE MODIFICATION ACCOMPLISHED IAW EA 5330-04213 OP 4 REV D WITH DEVSDR YENA2025022500204Skin · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR16 RH SIDE AT HOLE A. CRACK DIRECTION 9 OCLOCK (VIEW FROM OUTSIDE) AND CRACK LENGTH 0.100 INCHES (1EA); PERFORMED PERMANENT REPAIR LOC. ON DOUBLE JOGGLE AREA HOLE A ON FR16 RH SIDE IAW A320 SRM 53-11-12-30SDR YENA2025022500203Skin · crackedDURING HEAVY MAINTENANCE: CRACK INTERNAL STRUCTURE SECTION CONNECTION FRAME 66 AT LEVEL STR23 L AND BETWEEN Y1292 TO Y1732 AT AFT GALLEY AREA; REMOVED AND REPLACED INTERNAL STRUCTURE SECTION CONNECTION AND FASTENERS LOCATED FRAME 66 AT LEVEL STR23L AND BETWEENSDR AALA202502249221Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: LEFT HAND RAM AIR INLET SKIN HAS CORROSION AROUND BONDING STRAP BRACKET. COMPLETED INSTALLATION OF REPAIR DOUBLER AND SHIMS. PER EA 362009.SDR CALA2025022402434Skin · damagedSKIN WAVINESS - EXAMINATION (AT THE STATIC PORTS) SKIN WAVINESS EXAMINATION - L/H FUSELAGE FOUND DENT BETWEEN LEFT AND RIGHT STATIC PORTS.MEASURED DENT JUST FWD OF AIRCRAFT LEFT- AFT STATIC PORT AT STATION BS 764 AND WL139. DENT MEASURED 1.625 " X 1.50" ; DEPTSDR AALA202502249135Skin · wornAIRCRAFT IN BASE MAINTENANCE: WORN AREA ON FUSELAGE INNER SKIN LOCATED AT BS 283 BETWEEN STR 2L AND 3L. REPAIRED SKIN, PER B737 SRM 53-00-01-2R-REPAIR 6.SDR SWIA20250311221Skin · damagedFOUND LIGHTNING DAMAGE TO FUSELAGE SKIN AT FS 661.00 STRINGER 26R TO BE OUT OF LIMITS COMPLIED WITH PERMENANT REPAIR OF LIGHTNING DAMAGE TO FUSELAGE SKIN AT FS 661.00 STRINGER 26R PER REO 690-53-31-921 REV -. DAMAGE DETERMINED TO BE A MAJOR REPAIR.SDR SWAA2025031098253Panel · crackedFSD FWD SURROUND PANEL IS CRACKED AT THE OUTLET CUTOUT<[01]. REPAIRED FSD FWD SURROUND PANEL CRACK AT OUTLET CUTOUT IAW CMM 25-00-66 REPAIR 1-1 SECTION 4.B.; REPAIR 2-1 SECTION 4.B; AND ENG. DWG 25200003 PG. 11 ITEM 1.12.SDR SIMA20250221003Skin · corrodedSSI 53-23-009: EXTERNAL FUSELAGE SKIN HAS CORROSION AT LOWER EDGE OF AFT CARGO DOOR CUTOUT AT AREA COVERED BY SCUFF PLATE. (LEVEL 2 CORROSION) BLENDED OUT CORROSION ON EXTERNAL FUSELAGE SKIN AT LOWER EDGE OF AFT CARGO DOOR CUTOUT AT AREA COVERED BY SCUFF PLATESDR LR7A2025022103748Skin · damagedDURING SCHEDULED C-14 CHECK UNDER JOB CARD HAC5321, FOUND RH AFT FUSELAGE SKIN DAMAGED AT FS924, RBL61, WL215. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR#0639.SDR JJBA202502265044Skin · dentedDENTS ON RH CENTER FUSE I SKIN, BTW SKIN JUNCTION 02 AND FR 15 AND BTW STR 16R-17R. REPAIR DOUBLER ON RH CENTER FUSE I SKIN, BTW FR 14-15 AND BTW STR 16R-17RSDR SIMA20250221002Skin · dentedREF AML PAGE 125000206 ITEM #1 AND NRTC 316-ABI-00121 FUSELAGE EXTERNAL SKIN HAS A DENT AT FR 23 BETWEEN STR 24R/25R. (MAJOR REPAIR). REQUIRES ADDITIONAL INFORMATION IN THE CORRECTIVE ACTION TAKEN BLOCK. CUT OUT DAMAGED AREA OF FUSELAGE SKIN AT FR 23 BTW STGR SDR SWIA2025022401Skin · damagedFOUND LIGHTNING DAMAGE TO FUSELAGE SKIN AT FS 661.00 STRINGER 26R TO BE OUT OF LIMITS (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESSSDR 7C7A202502220008Skin Panel · crackedWHILE PERFORMING INSPECTIONS PER AD 2017-20-05, PARA (G), BOEING SB 757- A CRACK MEASURING 1.2" IN LENGTH WAS FOUND ON FUSELAGE SKIN PANEL P/N 141N3312-7 AT THE S-4R LAP SEAM BETWEEN BS 418 AND 439. DAMAGE WAS REPAIRED IAW BOEING MESSAGES C04-C04-25-0006-01C SDR AALA202504096150Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: DURING THE ACCOMPLISHMENTS OF CPCP 53-210-00 TASK, LEFT HAND RAM AIR MODULE ON FUSELAGE SKIN BETWEEN BS 500G TO 500H AND STR 22L TO STR 24L HAS CORROSION. REMOVED CORROSION. PER B737 SRM 51-10-02 AND PER B737 SRM 53-00-01-1A PROCSDR IPXA2025030651444Bear Strap · crackedMAJOR REPAIR, FOUND CRACK ON THE NO.1 FWD ENTRY DOOR LH AFT LOWER CORNER BEAR STRIP. (REPAIR) INSTALL SCUFF PLATE I.A.W AMM 53-13-01-424-005 REV.144 AND EGAT WORK SHEET NO: 50133 REPAIR INSTRUCTIONS STEP D.25(7).(8).(9).(10). INSTALL DOOR WAY LINING I.A.W AMMSDR JJBA202502265043Repair · damagedREPAIR DOUBLER ON LH CENTER FUSE I SKIN, BTW FR 19-20 AND BTW STR 14L-15L. REPAIR DOUBLER REMOVED TO INVESTIGATE ON LH CENTER FUSE I SKIN BTW FR19-20 AND BTW STR 14L-15L. LH CENTER FUSE I SKIN REPAIR.SDR DALA2025022001288Skin · unknownSHIP 3361 AD / EM-EO TASK -FUSELAGE SKIN FOUND EXISTING REINFORCING REPAIR AT FR3, BETWEEN Z-136.7 AND Z-336.7 LH AREA. CORRECTIVE ACTION: COMPLIED WITH ER/A 484296-14 REV.B. ASSOCIATED ER/A 484296-14. (0819971)SDR SWIA20250422219Skin · dentedFUSELAGE EXTERNAL SKIN HAS 1EA. DENT/ LOCATED BETWEEN FS 755.00-789.75, BETWEEN STRGS 12L AND 13L. (C-CHECK RO 04/21/2025)REMOVED DAMAGE AND REPAIRED IAW REO 601R-53-71-234 REV -- DATED 3/21/25, COMPLETED TASK CARD 51-900-1003-SKY AND ATTCHED COMPLETED FORM 3
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