JASC 5330
Service difficulty reports · 79,281
Reports filed under 5330 · Fuselage Main, Plate/Skin, newest first.
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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 DALA2026052703190Skin · damagedFOUND 3 LIGHTING STRIKE AT STA 181 AND LBL 21 (20 5/8" FROM BL0 & 2-7/8 FROM STA#177.73). C/W PRI ERA 634548-14 REV 0 ALL STEPS ( RGROSS 436426) QC5362 C/W STEP 61- PRI ER/A 634548-14 REV 1. CW ALL STEPS IN PRI ERA 634548-14 REV 3 AND REV 3. C/W ALL STEPS OF PSDR UIEA2026040800162Skin · corrodedM/D STA1241 FWD STR -18L- STR 19L INT SKIN FOUND CORROSION(<P>CORROSION REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, REWORK AREA MEASURED ORG: 0.170" L:8" X W:1.5" X D: 0.020", WITHIN SRM 53-00-01-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO SDR UIEA2026040800163Skin · corrodedM/D STA1241 FWD STR 14R - STR 15R INT SKIN FOUND CORRODED.(<P>CORROSION REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, REWORK AREA MEASURED ORG 0.219" L:5" X W:1.2" X D: 0.024", WITHIN SRM 53-00-01-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FSDR UIEA2026040800164Skin · corrodedM/D STA1241 FWD S-15R-16R INT SKIN FOUND CORRODED.(<P>CORROSION REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, REWORK AREA MEASURED ORG 0.291" L:4" X W:1.5" X D: 0.024", WITHIN SRM 53-00-01-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FURTHER DSDR UIEA2026040800166Skin · corrodedM/D STA 1241 FWD STR 17R - STR 18R INT SKIN FOUND CORROSION(<P>CORROSION REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, REWORK AREA MEASURED ORG 0.220" L:7" X W:1.3" X D: 0.014", WITHIN SRM 53-00-01-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NOSDR UIEA2026040800167Skin · corrodedM/D STA 1480 FWD, S-8L TO S-9L SKIN INT FOUND CORROSION(<P>CORROSION REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, REWORK AREA MEASURED ORG 0.120" L:7" X W:1.4" X D: 0.009", WITHIN SRM 53-00-01-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FURTSDR UIEA2026040800168Skin · corrodedM/D STA 1480 FWD, STR 9L TO STR 10L SKIN INT FOUND CORROSION(<P>CORROSION REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, REWORK AREA MEASURED ORG 0.120" L:6" X W: 2" X D: 0.009", WITHIN SRM 53-00-01-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO SDR UIEA2026040800169Skin · corrodedM/D STA 1480 FWD STR 10L TO STR 11L SKIN INT FOUND CORROSION(<P>CORROSION REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, REWORK AREA MEASURED ORG 0.120" L:5" X W: 1.7" X D: 0.009", WITHIN SRM 53-00-01-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NSDR UIEA2026040800170Skin · corrodedM/D STA1480 FWD STR 14L TO STR 15L SKIN INT FOUND CORROSION(<P>CORROSION REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, REWORK AREA MEASURED ORG 0.090" L: 3.5" X W: 2" X D: 0.011", WITHIN SRM 53-00-01-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NSDR UIEA2026041500185Skin · corrodedM/D - RHS BS 980 TO 1000 STR 13R TO 14R FX SKIN INTERNAL FOUND CORROSION(<P>CORROSION REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, REWORK AREA MEASURED ORG:0.124" L:6" X W:2" X D:0.011", WITHIN SRM 53-00-01-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LSDR UIEA2026041500186Skin · corrodedM/D RHS BS 1000 TO 1020 STR 15R TO 16R FX SKIN INTERNAL FOUND CORROSION(<P>CORROSION REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, REWORK AREA MEASURED ORG: 0.150" L:6" X W:1.5" X D: 0.017", WITHIN SRM 53-00-01-1A-1 ALLOWABLE DAMAGE 1 FIG 10SDR UIEA2026041500187Skin · corrodedM/D RHS BS 1000 TO 1020 STR 16R TO 17R FX SKIN INTERNAL FOUND CORROSION(<P>CORROSION REMOVED AS PER SRM 51-10-02 AND REPORTECTED AS PER SRM 51-20-01, REWORK AREA MEASURED ORG: 0154" L: 3" X W: 1" X D: 0.019", WITHIN SRM 53-00-01-1A-1 ALLOWABLE DAMAGE 1 FIG 101SDR UIEA2026041500188Skin · corrodedM/D - STA 1000 AFT, S-10L TO S-11L INTERNAL SKIN FOUND CORROSION(<P>CORROSION REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, REWORK AREA MEASURED ORG: 0.128", L: 3" X W: 1.5" X D: 0.012", WITHIN SRM 53-00-01-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LISDR UIEA2026041500189Skin · corrodedM/D -STA 1241 FWD STR 13L- STR 14L INT SKIN FOUND CORROSION(<P>CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, REWORK AREA MEASURED ORG 0.220" L: 4" X W: 2.5" X D: 0.018", WITHIN SRM 53-00-01-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMISDR UIEA2026041500190Skin · corrodedM/D - STA 1241 FWD STR 14L - STR 15L INT SKIN FOUND CORRODED.(<P>CORROSION REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, REWORK AREA MEASURED ORG 0.220" L : 7" X W: 2" X D: 0.017", WITHIN SRM 53-00-01-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. SDR UIEA2026041500191Skin · corrodedM/D STA 1241 FWD STR 15L - STR 16L INT SKIN FOUND CORRODED.(<P>CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, REWORK AREA MEASURE ORG 0.288", L: 4" X W: 3" X D: 0.019", WITHIN SRM 53-00-01-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITSSDR UIEA2026041500192Skin · corrodedM/D STA 1241 FWD STR 16L - STR 17L INT SKIN FOUND CORRODED.(<P>CORROSION REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, REWORK AREA MEASURED ORG: 0.230", L: 6" X W: 2.5" X D: 0.019", WITHIN SRM 53-00-01-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS.SDR UIEA2026041500193Skin · corrodedM/D STA 1241 FWD STR 17L - STR 18L INT SKIN FOUND CORRODED.(<P>CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, REWORK AREA MEASURED, ORG: 0.220" L: 9" X W: 2" X D: 0.027", WITHIN SRM 53-00-01-1A-1 ALLOWABLE DAMAGE 1 FTG 101 LIMISDR UIEA2026041500197Skin · corrodedCORROSION FOUND AT STA 1720 S44L SKIN INNER SURFACE ( APPROX 2.5" X 2.25" )(<P>CORROSION REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, REWORK AREA MEASURED ORG: 0.071", L: 6" X W: 2.5" X D: 0.006", WITHIN SRM 53-00-01-1A-1 ALLOWABLE DAMAGE 1SDR UIEA2026041500198Skin · corrodedM/D RHS BS 980 TO 1000 STR 15R TO STR 16R FX SKIN INT FOUND CORROSION(<P>CORROSION REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, REWORK AREA MEASURED ORG: 0.150" L: 6" X W: 1.5" X D: 0.014", WITHIN SRM 53-00-01-1A-1 ALLOWABLE DAMAGE 1 FIG 10SDR UIEA2026042700252Skin · misrepairedFUSELAGE SKIN AT STA 2564-2575 STR 38R - STR 42R FOUND UNIDENTIFIED EXISTING REPAIR(<P>SKIN REPAIRED AS PER RI-53-80-18257 REV B. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026042800256Skin · corroded1EA CORROSION FOUND ON FUSELAGE LOWER SKIN INNER SURFACE AT STA 2185 STR 47R(<P>SKIN CORROSION AREA REPAIRED AS PER RI-53-60-18178 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2026042800260Skin · cracked2EA CRACK WERE FOUND ON SKIN 2EA FASTENER RUNNING AFT ON RH FUSELAGE SKIN LAP BETWEEN BS 1438 AND BS 1460 STR 23R(<P>SKIN LAP CRACK AREA REPAIRED AS PER RI-53-40-18228 REV. NO FURTHER DEFECTS NOTED</P>)SDR IPXA2026061809637Washer · missingMAJOR REPAIR, DUE TO PERFORM INSPECTION, NO WASHER INSTALLED UNDER FASTENERS HEAD ON DOUBLER, LH SIDE. ACCOMPLISH REPAIR IAW EO-97812 REQ1 REV.1 AND EO-96283-REQ2, REV 1.SDR IPXA2026061809643Washer · missingDUE TO PERFORMED INSPECTION, NO WASHER INSTALLED UNDER FASTENERS HEAD ON DOUBLER, RH SIDE. ACCOMPLISH REPAIR IAW EO-97813 REQ1 REV.1 AND UPS EO-96283-REQ3 REV.1.SDR DALA2026052803222Skin · crackedCRACK ON EXTERNAL FUSELAGE SKIN STA 1087 LONG 14 RH. REPAIRED PER PRI 634296-14 (1606252) (AIRCRAFT GROUNDED)SDR AALA202605277663Skin · crackedAIRCRAFT IN BASE MAINTENANCE: DURING THE CURRENT MAINTENANCE VISIT IN PIT, WHILE ACCOMPLISHINGJC 26T22053007, AFATIGUE CRACK RADIATING FROM A FASTENER HOLE WAS FOUND AT FR13/14 AND Z+780-Z+950 ONTHE RH SIDE. MAINTENANCE REPAIRED SKIN IAW EA 375396.SDR DALA2026052603164Skin · damagedSKIN DAMAGE AT STR 19R JUST AFT OF FRAME 500H. COMPLIED WITH ER/A ER/A 634485-14 REV ORIGINAL PRI REV "0", "1", "2", "3" REPAIR INSTRUCTIONAL STEPS, ENSURE ALL ER/A ER/A 634485-14 REV ORIGINAL PRI REV "0", "1", "2", "3" REPAIR INSTRUCTIONAL STEPS ARE COMPLETEDSDR DALA2026052603158Skin · damagedWHILE IN SEA, MTC REPORTED 3 LIGHTNING STRIKES ON FWD NOSE FUSELAGE AT STA 181, LBL 21. ALL THREE ARE IN THE SAME OPEN BAY. MAINTENANCE REPAIRED DAMAGE PER ERA 634548-14. (LOG 1606265 - AIRCRAFT WAS GROUNDED).SDR AALA202605222113Skin Panel · crackedAIRCRAFT IN BASE MAINTENANCE: 2 CRACKS IN FUSELAGE SKIN ORIGINATING FROM THE SAME FASTENER HOLE BETWEEN FR 13 AND FR 14, AND BETWEEN +Z780 AND +Z950. REPAIRED SKIN PER EA EA 375396.SDR DALA2026080404484Skin · damagedSEE LOG PAGE 8612918 FOR ERA 634635-14 REV ORIG SECT I STEP 9 RESTORE FINISHES TO EXTERNAL SURFACES . C/W REP INSP. OF FWD BELLY FAIRING DAMAGE PER ASRP 51-12-00-04AAA-661A-A. SPEED TAPE IN GOOD CONDITION OK. (LP# 8612921; AIRCRAFT WAS GROUNDED)SDR DALA2026052903261Skin · crackedCRACK AND WEAR EXTERNAL SKIN ON AFT CARGO DOOR CUTOUT AFT EDGE BTW LONG 24RH TO LONG 26RH AT LOWER FUSELAGE SECTION. REPAIRED PER B717-200 SRM 53-20-15 (1605105) (AIRCRAFT GROUNDED)SDR CALA2026052916644Skin · damagedFOUND POSSIBLE LIGHTNING STRIKE BTWN BS 500A - 500B, STR 3L. REMOVED DAMAGE, HFEC AREA, NO DEFECTS NOTED. FABRICATED REPAIR PARTS, LOCATED, DRILLED AND INSTALLED, RESTORED COATINGS IAW SRM 53-00-01-2R-1, REPAIR 1, AND UAL ECRA 5310-08866, REV A. THIS IS A CSDR DALA2026052603162Skin · puncturedSKIN DAMAGE (PUNCTURE) JUST ABOVE STR 22R AT FRAME 500G. COMPLIED WITH ER/A 634486-14 REV ORIGINAL PRI REV "0", "1","2" REPAIR INSTRUCTIONAL STEPS, ENSURE ALL ER/A 634486-14 REV ORIGINAL PRI REV "0", "1","2" REPAIR INSTRUCTIONAL STEPS ARE COMPLETED AND MATCH FSDR DALA2026052603161Skin · damagedSKIN DAMAGE AT STR 21R (2 SPOTS) JUST FWD OF FRAME 500F. COMPLIED WITH ER/A 634484-14 REV ORIGINAL PRI REV "0", "1","2" REPAIR INSTRUCTIONAL STEPS, ENSURE ALL ER/A 634484-14 REV ORIGINAL PRI REV "0", "1","2" REPAIR INSTRUCTIONAL STEPS ARE COMPLETED AND MATCH FSDR DALA2026052103099Skin · damagedBIRD STRIKE DAMAGE REPAIR, STA 132.5, BL 0.0. ACCOMPLISH ER/A 634542-14 (1604693) (AIRCRAFT GROUNDED)SDR SCNA20260810341Lap Joint · crackedEXTERNAL FUSELAGE, LAP JOINT AT STRINGER 14R, BS 727I+2, LOWER SKIN CRACKED. THIS CONDITION WAS FOUND DURING THE HFEC HOLE PROBE INSPECTION PER EO COO-EO-2026-24361. PERFORMED PERMANENT REPAIR AT EXTERNAL SKIN SECTION BETWEEN BS 727H & BS 727J, STRINGERSSDR IPXA2026060280694Skin · damagedAFTER REMOVAL OF DME ANTENNA, FOUND SIGNS OF CORROSION. CHECKED LIMITS AT FUSELAGE SKIN AREA ORIGINAL THICKNESS .080 IAW DWG# 143N3471 BLENDED DIMENSIONS L=5.500'', W=2'', X=.004'' MAXIMUM ALLOWABLE X=15%=.012'' AREA FOUND TO BE WITHIN LIMITS IAW B757-200PF SSDR IPXA2026052180694Skin · corrodedAFTER REMOVAL OF DME ANTENNA,, FOUND SIGNS OF CORROSION.SDR DALA2026052003096Skin · corrodedLEVEL 2 CORROSION FOUND ON THE EXTERNAL FUSELAGE SKIN SURFACE NEAR FR 35 AND STGR 1R AND 1L. BLENDED SKIN PER ER/A 634142-14 PRI REV 0,1,2 AND REV ORIGINAL MIN REMAINING THICKNESS WAS .060. (LP 1602651 - AIRCRAFT WAS GROUNDED)SDR REXA2026070301065Skin · corrodedCORROSION ON SUPPORTS FRAME ALSO EXTERNAL FUSELAGE SKIN SETTLEMENT AREA OF FAIRINGS 195AB, 195BB, 195AL, 195DL, 196DR AND 196AR AT LOWER FUSELAGE STRUCTURE BTW FS847.00 TO FS942.00 AND LBL 45.00 TO RBL 45.00. CORROSION ON SUPPORTS FRAME ALSO EXTERNAL FUSELAGESDR DALA2026052103114Skin · damagedIN REFERENCE AMDS 5331-01293-02A-01 JOB #096-0001. STEP 6. DURING THE INSPECTION ELONGATED FASTER HOLE OF THE LOWER FORWARD CORNER OF THE NO. 1 CARGO DOOR CUT OUT WAS FOUND. LOWER FORWARD CORNER OF THE FWD CARGO DOOR CUT OUT WAS REPAIRED PER ER/A 634311-14AD SDR FXGA2026FA0000411Skin · corrodedCORROSION WAS NOTED ON FUSELAGE PLATING @ L/H OVERWING EMERGENCY EXIT DOOR FRAME, LOWER AFT CORNER. REPAIRED PER EO 2608SDR VNAA202607300009Skin · corrodedSEVERAL CORROSION ON INTERNAL FUSELAGE SKIN BTW VERTICAL STAB 55.625% TO VERTICAL STAB 67.5% AND BTW STR 22L TO STR 22R THROUGH ACCESS PANEL 362AR. CORROSION ON INTERNAL FUSELAGE SKIN BTW VERTICAL STAB 55.625% TO VERTICAL STAB 67.5% & BTW STR 22L TO STR 22R TSDR VNAA202607300008Skin · corrodedSEVERAL CORROSION ON INTERNAL FUSELAGE SKIN BTW VERTICAL STAB 55.625% TO VERTICAL STAB 67.5% AND BTW STR 22L - STR 22R THROUGH ACCESS PANEL 362AR. CORROSION ON INTERNAL FUSELAGE SKIN BTW VERTICAL STAB 55.625% TO VERTICAL STAB 67.5% AND BTW STR 22L TO STR 22R SDR SWAA2026061004193Skin · corrodedCORROSION FOUND ON LOWER FUSELAGE SKIN AT BS 400+6'- 400+15' BTW STR 27L- 26L. IAW EA 26-153-01372; THE REWORK IS ACCEPTABLE AS A CONTINUE-IN-SERVICE CONDITION WITH AN INSPECTION THRESHOLD DEFINED IN EA 26-153-01372-DTI.SDR SWIA2026051876218Skin · damagedDURING CUSTOMER WALK ON THE LT SIDE OF THE ACFT JUST AFT OF THE OPERATED BY SKYWEST LOGO, THERE IS PAINT MISSING ON AN AREA OF PREVIOUS DAMAGE. COMPLETE DAMAGE REPORT AND RESTORE SURFACE PROTECTION. REPAIRED THE DAMAGE ON LT FWD FUSELAGE SKIN AT FR 12, STGRSDR R61A2026060400159Doubler · corrodedEXTERNAL SKIN DOUBLER REPAIR IS MISSING THE CUTOUT FILLERS REQUIRED BY ETD2019-170-098492 REV. B.TECHNICIAN REPAIRED AAI DISCREPANCY ITEM #5: REPUBLIC REPAIR #39 - FR 20-21 S17L--18L - EXTERNAL SKIN DOUBLER REPAIR IS MISSING THE CUTOUT FILLERS REQUIRED BY ETD2SDR CALA2026052616542Skin · corrodedCORROSION ON LWR CENTER WNG SKIN OB SIDE ON RIGHT DRAG LINK 2" AFT OF WING FRONT SPAR. (REF AAR N/R 100019659)ACCOMPLISHED REPAIR AT WING CENTER SECTION FORWARD LOWER SKIN PANEL INTERIM REPAIR STA 540 AS REQUIRED PER ECRA #5710-02979, COMPLIANCE WITH THE REQUISDR DALA2026052103106Skin · damagedDURING ACCOMPLISHMENT OF #2 ENGINE CHANGE IN ATL, MTC DISCOVERED MULTIPLE DAMAGE TO THE RHS FUSELAGE SKIN. THE SUBJECT DAMAGE IS LOCATED BETWEEN FR 500E AND FR 500F AT STR 21R. DAMAGE REPAIRED PER ERA 634484-14. (LOG 1600344 - AIRCRAFT WAS GROUNDED).
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