JASC 5330
Service difficulty reports · 79,293
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 SWIA2026030877397Skin · damagedICE DETECTORS SURROUND HAD TOOLING MARKS, ON BOTH LT & RT. REMOVED SCRATCHES ON FUSELAGE EXTERIOR SKIN ICE DETECTOR SURROUNDS, BOTH RT & LT SIDES IAW SRM 51-12-00-001-001-A01, REWORKED AREAS ARE WITHIN LIMITS PER REO 670-53-11-2295, REV -.SDR IPXA2026031775549Skin · crackedCRACKED PANEL, RT BODY MLG WW INNER LONGERON BOX AREA ,BS 1372. REPAIRED THE DAMAGE IAW EO-96831,REQ1, REV 1, AND EGAT EI F2026A53M-503, REV 1.SDR VNAA202603140006Skin · scratchedRIGHT FUSELAGE SKIN SCRATCHED. WITHIN 661 FLIGHT HOURS FROM REVISION REQUEST, ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IAW APPROVED PROCEDURES OR REPLACE PART. ENGINEERING COMMENTS: SUBMIT AN RFTS WITH UPDATED DAMAGE REPORT.SDR CALA2026090119140Skin · damagedWHILE PERFORMING PHASE 2 GVI, IAW AMM 05-51-19-210-805, FOUND LIGHTNING STRIKE DAMAGE ON LT SIDE OF ACFT FUSELAGE SECTION 41. DAMAGE LOCATED BS 219, ABOVE STR 24, HOLE THROUGH SKIN. HOLE MEASURES 0.265". ACTUAL DAMAGE AROUND HOLE MEASURES 0.451". CLOSEST FASDR SWIA2026030776886Skin · wornSKIN PANEL AT BS 550, LBL47 WORN. REPAIRED THE LT APRON SKIN PANEL BTWN BS 516.85 - 559 IAW REO 601R-53-41-3423, REV -.SDR SWIA2026030776881Skin · wornSKIN PANEL AT BS 550, RBL47 WORN. REPAIRED THE RT APRON SKIN PANEL BETWEEN BS 516.85 - 559 IAW REO 601R-53-41-3423 REV -, SKYWEST CONTINUE CARDS, ITEMS 1-32; 1-22; 1-22,SDR AALA202603104724Skin · damagedAIRCRAFT IN BASE MAINTENANCE: LEFT HAND SIDE OF FUSELAGE SKIN HAS CREASED AREA WITH MULTIPLE SMALL DENTS AT BS 365 BETWEEN STR 15L AND STR 16L. ACCOMPLISHED SKIN REPAIR BETWEEN BS 360 AND BS 380, STR 13L AND STR 17L. PER AA EA 372415.SDR DALA2026031001653Skin · ground damage(LOG 1484200) CATERING TRUCK HIT A/C RESULTING IN DAMAGE IN SECTION 41, AT BS 340-360, LOCATED ON STRINGER 20R. DAMAGE CONSISTS OF AN 8 IN X 4 IN DENT WITH A MAXIMUM DEPTH OF 0.147 INCHES. THE DENT IS ON THE FUSELAGE SKIN AND UNDERLYING STRINGER 20R. REMOVED DSDR DALA2026031001652Skin · damaged(LOG 1484180) FUSELAGE SKIN DAMAGE AT STR 20R STA 360. C/W ERA 632727-14 ORIGINAL SECTION 1. C/W RII OF ERA 632727-14 ORIG SECTION 1.SDR CALA2026031014483Skin · corrodedEVEALUATE CORROSION ON THE WASTE TANKS AREA PAN ASSY. PERFORMED REPAIR ON EXTERNAL SKIN OF THE VACUUM LAVATORY SERVICE DOOR CUTOUT BTW BS 847 - 867, S23L - 25L, MAJOR REPAIRSDR DALA2026030801591Skin · damagedCONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED BTW FR 13 TO FR 14 RH SIDE LEVEL Z=1330 UPPER FUSELAGE (REFERENCE AA CA RD 5100-01821-01A). C/A: COMPLIED WITH ER/A 520355-14 REV.B MATCHES WITH ALL STEPS ON PRI 520355-14 PRI REV 0,1,2,3 ITS SDR DALA2026031001641Skin · crackedSHIP 9523 CRACKS (2EAS) ON UPPER EXTERNAL FUSELAGE SKIN APPROX Y=1087 BTW LONG 13R-14R. CORRECTIVE ACTION: REPAIRED PER ER/A 632448-14 (1482120)SDR CALA2026031014482Skin · damagedPER ECRA 5310-08821 FUSELAGE LIGHTNING STRIKE AT STA 219 ABOVE S-24L- INTERIM REPAIR HAS BEEN ACCOMPLISHED.SDR VNAA202610230061Skin Panel · damagedTEMPORARY DISPOSITION FOR BLENDED LIGHTNING STRIKE DAMAGE TO LOWER FUSELAGE SKIN BETWEEN BS 169 - 170.64. (PREVIOUSLY REPAIRED PER EA A1-690-53-00041) THE SUBJECT CONDITION IS STRUCTURALLY ACCEPTABLE FOR 5600 FLIGHT HOURS FROM TIME OF INCORPORATION OF THIS RESDR REXA2026050400425Doubler · wornWEAR ON DOUBLER BTW FS913.00 AND STGR 26RH TO STGR 26LH WEAR ON DOUBLER BTW FS913.00 AND STGR 26RH TO STGR 26LH WAS REPAIRED PER REO 670-53-00-290 REV FSDR HNAA2026042100341Skin · damagedFWD FUSELAGE, THERE ARE 9 LIGHTNING STRIKES ON EXTERIOR SKIN FROM FR1A-9, STGR 14R-17R. INSTALLED DOUBLER REPAIR ON FORWARD FUSELAGE - SKIN BETWEEN FR.1A-2 AND STRG. 14R -17R. IAW EMB 145 ETD-2026-145-005225 AND PIEDMONT EO1-53-26-0159.SDR ASAA2026030565017Skin · damagedFUSELAGE SKIN UNDER PANEL 191D @ STA 500K HAS LIGHTENING STRIKE. GROUNDED - YES. EVALUATED DAMAGE TO FUSELAGE SKIN AT STA 500K (UNDER PANEL191D) @ STR 28L. FOUND TO BE OUT OF LIMITS DUE TO HOLE DIAMETER & PROXIMITY TO DRAIN PLUG HOLE. GENERATED RFTS. REPAIRED SDR ASAA2026030564995Skin · damagedLIGHTNING STRIKE TO FUSELAGE SKIN AT STA 500E+8" AT STR 28L. GROUNDED - YES. REMOVED AND REPAIRED LIGHTNING STRIKE DAMAGE AT STA 500E + 8" AT STR 28L IAW ASA EA 900ER-53EA-30036 REV 00 THIS REPAIR IS CATEGORY B WITH STAGE 1 APPROVAL STAGE 2 APPROVAL IS REQUIRESDR DALA2026031101678Skin · crackedSHIP 188 CRACK WAS FOUND DURING NDT INSPECTION OF FWD PAX DOOR CUTOUT AFT LOWER CORNER. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM53-10 -01. (1479903)SDR DALA2026031101677Skin · crackedSHIP 188 CRACK WAS FOUND DURING NDT INSPECTION OF FWD SERV DOOR CUTOUT AFT LOWER CORNER. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM53-10-01-2R. (1479894)SDR DALA2026031001646Skin · damagedSHIP 9523 ERA 632448-14 ISSUED FOR REPAIRS TO STA 1087 AND 1076 L13R TO L1 4R FUSELAGE SKIN. CORRECTIVE ACTION: ASSOCIATED ER/A 00-632448 (1480632)SDR DALA2026031001630Skin · corrodedCORROSION EXTERNAL SKIN LOCATED BTW FR 69 TO FR 70 CUT OUT OF DRAIN AND STR 31R TO STR 32R AT LOWER FUSELAGE. COMPLIED WITH ER/A 632109-14 REV. ORIGINAL APPROVED DATE 03-MAR- 26 MATCHES WITH ALL STEPS ON PRI 632109-14 REV 0 IT HAS BEEN VALIDATED. PERFORMED PESDR CALA2026030614386Skin · damagedWHILE PERFORMING CONDITIONAL INSPECTION, PHASE II, IAW AMM 05-51-19-710-801 . FOUND LIGHTNING STRIKE DAMAGE ON FUSELAGE BS 219.8, STRINGER 1. REMOVED LOCK FASTENERS TO SEPARATE SKIN FROM CENTER BEAM. REMOVED LIGHTNING STRIKE DAMAGE IN SKIN . LENGTH OF DAMAGSDR SWAA2026042076614Access Panel · delaminatedDELAMINATED ACCESS PANEL 192BL AT LOWER FUSELAGE. REPAIRED ACCESS PANEL 192BL AT LOWER FUSELAGE IAW SRM 51-70-05-2R-6, REPAIR 6.SDR SWAA2026042076615Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 193AL AT LOWER FUSELAGE. REPAIRED ACCESS PANEL 193AL AT LOWER FUSELAGE IAW SRM 51-70-05-2R-10 REPAIR 10.SDR DALA2026031001637Doubler · crackedCRACK ON INTERNAL PRODUCTION DOUBLER INSIDE OF AFT ACCESSORY COMPARMET IN LONGERON 3 RH,CANTED STA Y= 1178.225 APPROX. CORRECTIVE ACTION: REPAIRED PER B717-200 SRM 53-30-08-2R-9 PROCEDURE 9 REPAIR 9 (1478843)SDR SWIA2026030475429Skin · damagedSKIN DAMAGE IS OUT OF LIMITS AND IS LOCATED ON FRAME 08 TO FRAME 09 AND ALONG STRG 19L. (FLIGHT 3064) REASSESSED DAMAGE ON FWD LEFT SIDE OF AIRCRAFT JUST UNDER CAPTS WINDOW, CONFIRMED DAMAGE LOCATION TO BE LOCATED ON FRM 08 TO FRM 09 AND JUST BELOW STRG 15LSDR DALA2026030801594Skin · noneSHIP 3277 DISC: CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN BTW BE AM 1 TO BEAM 2 AND XP 535.3 TO XP 820.6 AFT LOWER CORNER LH FORWARD PASSENGER CREW DOOR 831 REFERENCE AA CARD 5100-01821- 04A-LF. CONFIRMED DT EVALUATION FOR POSSIBLE FCS REPAISDR DALA2026030501530Support · corrodedAFT CARGO COMP, LOWER SILL SURFACE COVERED BY PLATES, FOUND SURFACE CORROSION NEAR 3 ATTACH SCREWS AND SURFACE CORROSION UNDER SCUFF PLATE AND SURFACE CORROSION UNDER SCUFF PLATE AT 4 LOCATIONS. THIS N/R IS NOT ASSOCIATED WITH COUNTERSINK CORROSION WRITE UPS. SDR DALA2026030501529Skid Shoe · contaminatedAFT CARGO COMP, SURFACE UNDERNEATH SCUFF PLATE FOUND CORROSION PRESENT IN COUNTERSINK AND SURROUNDING AREA OF COUNTERSINK AT HOLE LOCATIONS 1OL, 4OL, 6OL AND 8OL. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 016-0001:5331-01297- 02C/001 00185 REPAIRED PER ERA PRISDR IXXA20260304001Skin Panel · corrodedRIGHT FUSELAGE CLOSEOUT FAIRING PANEL AFT OF MAIN CARGO DOOR FOUND CORROSION AT UPPER AND LOWER DOOR CORNERS NO PART NUMBERS FOUND ON REMOVE PANEL. FABRICATED NEW CLOSEOUT FAIRING PANEL, ASSIGNED NEW P/N 47696FAB01SDR VE7A202603190040Skin · crackedTHE MECHANIC WAS COMPLYING WITH THE ZONE 3 TRANSMISSION INSPECTION WHEN HE FOUND A CRACK. THE CRACK WAS EMANATING FROM THE FORWARD RIGHT HAND PYLON BEAM ATTACHMENT POINT. IT WAS FOUND BECAUSE OF BLACK OIL AROUND THE AREA. HE CLEANED THE AREA AND COMPLETED A DYSDR SWAA2026030976137Access Panel · damagedACCESS PANEL 194BL HAS ELONGATED FASTENER HOLE. PREPPED AND PAINTED ACCESS PANEL 194BL REF M/M 51-21-99. PANEL READY FOR INSTALLATION. REF TTG8Q01ARDBG FOR PANEL 194BL INSTALLATION.SDR REXA2026030900201Skin · corrodedFOUND POSSIBLE CORROSION UNDER BED SEAL FOR PANELS 196DR AND 195EL. REPAIRED FUSELAGE SKIN IAW ENDEAVOR AIR EA CRJ953-21442 REV IR DATED 2/7/2026.SDR DALA2026030401494Skin · corrodedAFT SERVICE DOOR SKIN UNDER SCUFF PLATE, COUNTERSINK HOLES 2OL, 3OL, 4OL, 5OL, 8OL, 9OL, 10OL, 11OL, 12OL AND 13OL HAVE CORROSION IN COUNTERSINKS AND ADJACENT TO COUNTERSINKS. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATIOSDR 2026F00020Skin · crackedEXTERIOR FUSELAGE SKIN ONLY IS CRACKED AT ONE FASTENER HOLE LOCATED L1 DOOR CUT OUT AFT CORNER STA 335 JUST ABOVE STR 20L(VERIFIED WITH HFEC).REPAIRED EXTERIOR FUSELAGE SKIN CRACK AT ONE FASTENER HOLE LOCATED L1 DOOR CUT OUT, AFT CORNER, STA 335 JUST ABOVE STRSDR DALA2026030301441Skin · dentedFUSELAGE SKIN BETWEEN FR 34-35, BELOW S31R DENTED. PERFORMED THE PERMANENT DOUBLER REPAIR ON DENTED AREA. AT EXTERNAL FUSELAGE SKIN C34-C35A AND S30R -S33R IAW ER/A 625812-14, REV B. (1476731)SDR AALA202603032590Skin · crackedAIRCRAFT IN BASE MAINTENANCE. CRACK IN THE FUSELAGE SKIN AT APU DOOR FWD HINGE POINT, BS 1104. ACCOMPLISHED DOUBLER REPAIR IAW SRM 53-80-01-2R-1.SDR VNAA202604110005Skin · damagedLIGHTNING STRIKE DAMAGE TO FUSELAGE SKIN BETWEEN FS202.75 - FS613.00 WITHIN 6500FH, PERFORM A PERMANENT REPAIR IAW APPROVED PROCEDURES. LIGHTNING STRIKE DAMAGE TO FUSELAGE SKIN BETWEEN FS202.75 - FS613.00 WERE REPAIRED PER CRJ-900 SRM 53-00-00-201-003-A03 ANDSDR SWAA2026031176091Skin · crackedDURING OPEN HOLE NDT INSPECTION OF STR 22R, A CRACK INDICATION NOTED AT BS 344+4 AND 344+6 OF STRINGER. REPAIRED IAW EA 26-153-00584.SDR SWAA2026031175789Bear Strap · deformedFWD CARGO DOOR SURROUND DOUBLER (BEAR STRAP) IS DEFORMED AT STA 440; S-27R. SEE EA.126-153-00594 FOR WORK PERFORMED.SDR WX0A2026030432748Skin · dented(AIRCRAFT NOT GROUNDED) (MAJOR REPAIR) LADDER PINNED ADJACENT TO POTABLE WATER SERVICE DOOR. FUSELAGE DENTS & SCRATCH BETWEEN FR 64-65 AT STGR38LH DAMAGED WILL BE REPAIRED IAW SRM 53-41-11-300-036. ORIGINAL DAMAGE RELIEF IAW EA 129-2026-038. STRINGER DAMAGESDR DALA2026030301440Skin · damagedFUSELAGE SKIN JUST FORWARD OF FR 26.2 AND 5 INCHES ABOVE S30L DAMAGED. PERMANENT REPAIR ACCOMPLISHED IAW SRM 53-21-11-300-032. (1475762)SDR DALA2026030301439Skin · dentedFUSELAGE SKIN, BETWEEN FR 34 - 35, BELOW STR 31R DENTED. COMPLIED WITH ERA 625872-14, REV B. (1476158)SDR SWAA2026031175713Skin · crackedSKIN CRACKED BS 344, ABOVE STRINGER 22R. REPAIRED IAW EA 26-153-00584.SDR VNAA202604110003Skin · damagedLIGHTNING STRIKES (2EAS) BTW FS=260.00 TO FS=280.00 AND SGTR 20L AT FUSELAGE SKIN. LIGHTNING STRIKES (2EAS) BTW FS=260.00 TO FS=280.00 AND SGTR 20L AT FUSELAJE SKIN. WAS REPAIRED PER REO 690-53-11-2168 REV. - -SDR VNAA202604110002Skin · damagedLIGHTNING STRIKES (1EA) BTW FS=295.00 TO FS=310.00 AND BTW SGTR 7L TO SGTR 8L AT FUSELAJE SKIN. LIGHTNING STRIKES (1EA) BTW FS=295.00 TO FS=310.00 AND BTW SGTR 7L TO SGTR 8L AT FUSELAJE SKIN WAS REPAIRED PER REO: 690-53-21-2115, REV: - -SDR VNAA202604110001Skin · dentedDENTS (2 EAS) ON EXTERNAL FUSELAGE SKIN BTW FS 1031-1051 AND STGRS 26R-24R. DENTS ON EXTERNAL FUSELAGE SKIN BTW FS 1031-1051 AND STGRS 26R-24R WAS REPAIRED PER REO 690-53-61-1750 REV -SDR IPXA2026032658517Skin · damagedMAJOR REPAIR, TAIL EXTERNAL FUSELAGE, BTWN BS 1896.2 - 1992.8, 11 O'CLOCK POSITION, HAS 11EA POINTS WITH LIGHTNING STRIKE DAMAGE. BONDED REPAIR DOUBLER IAW SRM 51-70-10-2R-2A.SDR IPXA2026032458260Rivet · shearedMAJOR REPAIR. EXTERNAL LOWER FUSELAGE, BS 1460, S29R HAD A SHEAR RIVET, EVIDENCE OF CORROSION INSIDE. VERIFIED REPAIR ACCOMPLISHED PER EO-96803-REQ1 AND VT-MAE EA 757-5360-27-A4377 REV-, PRIOR TO FURTHER FLIGHT.
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