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 JJBA20260220059Skin · dentedFUSELAGE EXTERNAL SKIN, LT, AT FR 9, STR 17L, HAS A DENT. REPAIRED DENT IN FUSELAGE EXTERNAL SKIN, LT AT FR 9 STR 17L.SDR JJBA20260220058Skin · damagedACFT HAS A CREASE AFT OF GROUND POWER RECEPTACLE DIRECTLY UNDER ICE DETECTOR ON LH SIDE. REPAIRED CREASE AFT OF GROUND POWER RECEPTACLE DIRECTLY UNDER ICE DETECTOR ON LH SIDE BY CUT OUT AND INSTALLATION OF REPAIR DOUBLER, TRIPLER, AND FILLER.SDR CALA2026020913629Skin · corrodedNEW INNER LAV PAN STRUCTURE REQUIRES HOLES LOCATED AND DRILLED. REF LPN 7696962DISASSEMBLED OLD LAV PAN ASSY TO USE AS A TEMPLATE REF SRM 51-40-02 2 EA CLIPS, 1 EA SHIM, AND 1EA ZEE CHANNEL BENT/DAMAGED MARKED MAJOR AND RII REF LPN 7696962. THIS LOGPAGE IS ASDR IPXA2026021059426Skin Panel · corrodedMAJOR REPAIR, CORROSION FUSELAGE SKIN STA 1410 BETWEEN S-38R AND S-39R. (REPAIR. ACCOMPLISHED THE REPAIR I.A.W SRM 53-00-01 REPAIR 29 REV. 94 AND EGAT EI NO.F2026A53M-286 REV.1 AND UPS EO-96454-REQ1 REV1.SDR DALA2026020500829Skin · corrodedDURING H CHK AT STAG, CORROSION WAS NOTED ON THE FUSELAGE SKIN BETWEEN BS 1197+165 AND 1197+187. A REPAIR WAS INSTALLED IAW ER/A 631872-14, SECT I. FOLLOW ON ACTION IS REQUIRED FOR SECT. II REPEAT INSPECTIONS. ACCOMPLISH ER/A 631872-14 SECT. II REPEAT INSPESDR SWIA2026013175106Skin · mechanic errorDURING STARLINK INSTALLATION A STRINGER RIVET WAS MISDRILLED AT FWD RIGHT SKIN, STRINGER 2R, BS 437. THIS HAS BEEN DETERMINED TO BE A MAJOR REPAIR, COMPLIED WITH MAJOR REPAIR OF FWD RIGHT SKIN, STRINGER 2R, BS 437 IAW STARLINK EO SPX-00011260. COMPLIED WITH TSDR SWAA2026030566069Skin · corrodedCORRODED SKIN, BS 807 - 827, STRINGERS 27R - 27L, WL 148. PERFORMED A REPAIR IAW EA 26-153-00408-WIP1, EA 26-153-00408-WIP2, EA 26-153-00408-WIP3, EA 26-153-00408-WIP4, & EA 26-153-00408.SDR KY7A2026021000038Skin · corrodedCORROSION WAS FOUND AT THE FWD TIP OF THE LH FUSELAGE SKIN. REPAIRED PER EO-53-034SDR CALA2026020213475Skin · dentedLEFT FUSELAGE SKIN AT BS 198 ABOVE S-25 +2.0" WAS DENTED. THE DENT IS 3.65" LONG AND 2.5" WIDE AND DEPTH IS 0.065". REPAIRED THE DAMAGED SKIN BETWEEN BS 188 - 203.8, S21L-25L IAW ESR-WI 2024183-19-14589, & EC/RA 5310-08787. PERFORM AN INSPECTION OF THE FUSDR IPXA2026021021755Skin · crackedMAJOR REPAIR. FUSELAGE SKIN CRACK AT BS 560 S-23L - S-24L. (REPAIR) . ACCOMPLISH THE REPAIR I.A.W SRM 53-00-01-2R-13 REV.64 AND EGAT WORK SHEET NO.60081 REVIEWED TASK PER GMM-MTX 09.05.01.09.SDR JR2R20260129774Doubler · crackedATG-4 AFT ANTENNA DOUBLER HAS A 4 INCH CRACK. NDT VERIFIED. REPAIRED SKIN.SDR SWIA2026012875774Skin · crackedFOUND CRACKED ON SKIN, HYDRAULIC BAY AT 193.00 SKIN. REMOVED AND REPLACED HYD. BAY AT FS193.00 SKIN. REF. REF. REO 690-53-11-2152 REV. -- . C/W SKYWEST TASK CARD 51-900-1002-SKY STRUCTURAL MAJOR REPAIRMAJOR REPAIR C/PAINT DEFERRED TO SKYWEST AFTER REPAIRS ANSDR VNAA20260329016Skin · dentedDENTS FOUND ON FUSELAGE SKIN UNDER RH VENTRAL FIN AT FS 1083, FS 1088, FS 1093, AND FS 1095. DENTS ON FUSELAGE SKIN UNDER RH VENTRAL FIN BTW FS1069.75 AND 1162.00 AND STR20R-STR23R WERE REPAIRED PER REO 670-51-00-085 REV. -A, REO 690-53-61-1745 REV. -- AND RESDR VNAA20260329015Skin · corrodedFIVE DENTS FOUND ON FUSELAGE SKIN UNDER VENTRAL FIN AT FS 1082, FS1085, FS 1087, FS1130 AND FS 1179. DENTS ON FUSELAGE SKIN UNDER VENTRAL FIN AT FS 1082.00, FS1085.00, FS 1087.00, FS1130.00 AND FS 1179.00 WERE REPAIRED PER REO 670-51-00-085 REV. -A, REO 690-5SDR VNAA20260304026Skin · dentedSEVERAL DENTS ON THE SKIN OF ALONG THE SETTLEMENT AREA VENTRAL FIN LT & RT. THE SKIN WAS REPAIRED IAW REO 670-51-00-085, REV A, REO 690-53-71-104, REV-, REO 690-53-61-1737, REV -, AND REO 690-53-61-1738 REV -.SDR IPXA2026020707464Skin Panel · crackedMAJOR REPAIR, FOUND CRACK ON THE NO.1 FWD ENTRY DOOR LH AFT LOWER CORNER SKIN. ACCOMPLISHED THE REPAIR I.A.W SRM 53-10-01-2R-1 REV. 94 AND EGAT WORK SHEET NO: 60075 AND UPS EO-87307-REQ7 REV2.SDR IPXA2026020977464Skin · crackedMAJOR REPAIR. FOUND A CRACK ON THE NR1 FWD ENTRY DOOR LT AFT LOWER CORNER SKIN. INSTALLED ENTRY DOOR SCUFF PLATE IAW AMM 53-13-01-424-005, REV 147. INSTALLED ENTRY DOOR DOORWAY LINING IAW AMM 52-12-02-404-025, REV 147.SDR FDEA202601280095Skin · dentedUPPER FUSELAGE BETWEEN BS 1941 AND 1963.8 TWO DENTS, APPLIED PERMANENT REPAIR AT UPPER FUSELAGE BETWEEN BS 1941 AND 1963.8 IAW SRM 53-80-01-1A, FIG 101, SHEET 2, NOTE C, & SRM 51-70-10-2R.SDR CALA2026012913426Skin · gougedRAMP REPORTED GOUGE ON FUSELAGE BY AFT SERVICE DOOR DOOR 2L, INSPECTED GOUGE AND DENT IAW SRM 51-10-02 . GOUGE AND DENT OUT OF LIMITS IAW SRM 53-00-1-1A-1. ACCOMPLISHED STEPS 4A, B, ,C, AND D OF SRM 53-80-01-2R-5, REMOVED DAMAGE & FASTENERS. REPAIR AREA REQUSDR VNAA202601280021Access Panel · corrodedCORROSION ON ACCESS PANELS 542AZ, 622EZ AND 599AB. ACCESS PANEL 542AZ WAS REMOVED PER CRJ 900 SRM 51-21-06-001-001-A01 AND WITHIN LIMITS PER CRJ-900 SRM 53-00-00-101-001-A01. W ACCESS PANEL 599BB WAS VERIFIED ( P/N: 601R13442-7) PER CRJ-900 AIPC 27-15-01. ACCSDR DALA2026012800657Repair · no discrepancySHIP 3320 FOUND FUSELAGE SKIN FR 75 -FR76 BETWEEN STR45L AND49L EXISTING DOUBLER REINFORCING REPAIR. CORRECTIVE ACTION: PERFORMED PERMANENT SKIN REPAIR FOR PREVIOUS REPAIR AREA AT FR75-FR76 BETWEEN STGR 45L AND STGR 49L PER A330 SRM 53-41-11-300-015. (1423155)SDR VNAA202601280006Skin · corrodedCORROSION ON EXTERNAL SKIN OF FUSELAGE ON STGR 16RH BTW FS629.00 & FS645.00, FS661.00+16.00 & FS661.00+32.00 BTW STGR 26RH & STGR 27, FS661.00+16.00 BTW STGR 3RH & STGR 3LH AND FS1015.00 & FS1031.00 BTW STGR 23RH & STGR 24RH. CORROSION ON EXTERNAL SKIN OF FUSSDR CALA2026020913628Skin · damagedREFERENCE LP# 7676444, 7676363, 7676416, 7676387, 7676335, & 7672726 FOR INITIAL DAMAGE IDENTIFICATION, NEED TO PERFORM MAJOR REPAIR TO THE AREA ROUGHLY BETWEEN BS827-BS867 & ST26L-ST26R.AVO16525 STEP 1, NEED TO CONFIRM DVI REQUIREMENTS OF STEP 1 HAVE BEEN ACCSDR DALA2026020100734Skin · noneSTAGE III DAMAGE TOLERANCE EVALUATION ( DTE ) REQUIRED FOR FUSELAGE SKIN REPAIR INSTALLED AT FR25 S-13R/14R PER ER/A 627770-14 R EV A. SECTION I IS LIMITED TO 64000FC FROM SECTION I. ER/A TO BE REVISED PRIOR TO THIS LIMIT ELSE REMOVE A/C FROM SERVICE. (LP: 1SDR AALA202601286585Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK RIGHT HAND WING UPPER SKIN TRAILING EDGE AT WING BL 273.30. ACCOMPLISHED REPAIR PER EA 370465B.SDR SWIA2026012676040Plate · scratchedRIGHT TAT CUTOUT HAS MULTIPLE SCRATCHES AT FS280.00 BETWEEN STGR11R AND STGR12R (C-CHECK RO 05/22/2026)INSTALLED REPLACEMENT TAT PROBE MOUNTING PLATE IN REF WITH CRJ900 SRM 51-42-06-001-001-A01 AND DWG CC670-33015 REV. G. COMPLIED WITH TASK CARD 51-900-1002-SDR CALA2026020413581Access Door · dentedRIGHT AFT FUSELAGE, OTBD SIDE OF THE APU FIRE BOTTLE ACCESS DOOR HAS ONE DENT. ACCOMPLISHED REPAIR IAW ECRA 5380-01438 AND EA 757-5380-13-A4248 WITHOUT DEVIATION. THIS IS A PERMANENT REPAIR WITHOUT LIMITATIONS.SDR DALA2026012800684Skin · crackedOPEN HOLE HFEC INSPECTION CARRIED OUT ON THE ALL FASTENER HOLES (5EA) AT THE FORWARD SERVICE DOOR CUTOUT AFT LOWER CORNER. FOUND ONE CRACK FROM THE NR 4 FASTENER HOLE. DAMAGED AREA REPAIRED IAW SRM 53-10-01. (1419957)SDR CALA2026012713347Access Panel · missingLANDING GEAR CONTROL ACCESS DOOR FOUND MISSING ON ARRIVAL PANEL 198GR INTERIM REPAIR ACCOMPLISHED PER ECRA 5390-01096, REF LOG 7723200.SDR SWIA2026030975444Skin · corrodedCORROSION ON FUSELAGE SKIN UNDER LOWER TCAS ANTENNA AT FS310.00 - 319.00 STGR27. MX 31602216 (C-CHECK RO 03/07/2026)REPAIRED AREA ON FUSELAGE SKIN UNDER LOWER TCAS ANTENNA AT FS310-FS319, STRG 27 COMPLIED WITH REO 670-53-21-2809 REV -- DATE 2026-02-12 STEPS 1SDR SWIA2026012475614Skin · scratchedEXTERNAL FUSELAGE SKIN, FS977 STGR 27 HAS SCUFFING COMPLIED WITH CRJ700 MHIRJ REO 670-53-00-290 REV -F DATED: 2019/04/26 (SOLUTION 2, FIGURE 8) & (SOLUTION 1 FIGURE 7)SEE CONTINUE CARD FOR DETAILS,LEAK CHECK GOOD,COMPLIED WITH 51-900-1002-SKY.SDR DALA2026012700600Skin · crackedCRACKED LEFT FUSELAGE EXTERNAL SKIN BS 1087 BTW LONGERONS 13 - 14L. REPAIRED IAW ER/A 631513-14 REV. (1416717)SDR DALA2026012600587Skin · gougedSKIN GOUGED AT FR 36, S28L. REPAIRED THE DAMAGE IAW SRM 53-21-11. (1417434)SDR JJBA20260130082Skin · crackedRF1, CRACK FOUND ON EXTERNAL SKIN AT FR 75 AND BTW STR 1R-3R. BUSHING REPAIR ON RH RF1 UPPER SKIN AT FR75 BTW STR 2R-3RSDR DALA2026012800683Skin · damagedLEFT FUSELAGE SKIN AT BS 1730, WL 200, FOUND FWD SKIN ABRASION. DAMAGED AREA REPAIRED IAW SRM 53-80-01. (1415515)SDR DALA2026012800682Skin · damagedRIGHT FUSELAGE SKIN AT BS 1730, WL 200. FOUND FWD SKIN ABRASION. DAMAGED AREA REPAIRED IAW SRM 53-80-01 (1415504)SDR SWIA2026012375095Skin · dentedDENT ON FUSELAGE SKIN BETWEEN BS 409+80 - 409+96, S18 - 19L, PERMANENT REPAIR OF LT FUSELAGE SKIN IAW REO 601R-53-31-1363, REV CP 31597873 FOR STEP 1, CP 31599706 FOR STEP 2, 31596075 FOR STEP 3, 31599715 FOR STEP 4, 31596400 FOR STEP 5, 31599965 FOR STEPS 7SDR AALA202601269502Doubler · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FUSELAGE SKIN DRAIN DOULBER, BEHIND WHEEL WELL AFT BULKHEAD AT BS 727 S27R. REPLACED DOUBLER PER SRM 51-40-05.SDR DALA2026012700604Skin · crackedREFERENCE ER/A 619241-14. FUSELAGE SKIN, BS 1037, L13 - 14L CRACKED. REPAIRED IAW ER/A 14-619241. (1414757)SDR MASA20260126003Skin · dentedA/C FERRY FROM IAD TO IAH FOR PERMANENT REPAIR APPROVED BY EMB ETD2018-170-128718-E. LT & RT FUSELAGE SKIN DENTS & BLENDOUTS FRAME 75&76SDR SWIA2026012176008Skin · dentedFOUND MULTIPLE DENTS AND SCRATCHES BELOW AND AFT OF THE LOW-PRESSURE AIR GROUND CONNECTION DOOR. IF DAMAGE IS FOUND WITHIN LIMITS, ELIMINATE ALL EVIDENCE OF DAMAGE. COMPLIED REPAIR TO FUSELAGE SKIN BETWEEN FS 574.00 AND FS 605.00 STGR 20R TO STRG 27 IAW REO:SDR VNAA20260329013Skin · dentedTEMPORARY DISPOSITION TO FUSELAGE SKIN DENT BETWEEN FS280.00 AND FS295.00 AND BETWEEN STRINGER 18R AND 19R SUBJECT CONDITION IS ACCEPTABLE FOR 4050 FLIGHT HOURS FROM THE TIME OF INCORPORATION OF THIS REO AT REV. FUSELAGE SKIN DENT BETWEEN FS280.00 AND FS295.0SDR VNAA20260329012Skin · corrodedCORROSION ON INNER SKIN (ABOVE STRUT BAY LIGHT) BTW REAR SPAR AND AUXILIARY SPAR AREA THOUGH ACCESS PANEL 542AZ AT LH MLG STRUT BAY. CORROSION ON INNER SKIN (ABOVE STRUT BAY LIGHT) BTW REAR SPAR AND AUXILIARY SPAR AREA THOUGH ACCESS PANEL 542AZ AT LH MLG STRSDR VNAA202603280011Skin · corrodedCORROSION ON INNER SKIN PANEL ON REAR SPAR TO AUXILIARY SPAR AREA THROUGH ACCESS 642AZ AT RH MLG WW. INNER SKIN PANEL ON REAR SPAR TO AUXILIARY SPAR AREA THROUGH ACCESS 642AZ AT RH MLG WW WAS REPAIRED PER EA NO.5740-2026-0225 REV.-- SECTION III -PERMANENT RESDR DALA2026012800672Skin · deformedDURING PERFORMANCE W/C 5100 - 2360 INSPECTION, ANTENNA DOUBLER AT BS 687, FOUND SKIN DEFORMED AT S35R. DAMAGED AREA REPAIRED IAW SRM 53-00-01. (1412446)SDR FDEA202601210089Repair · out of limitsEXISTING REPAIR ON FUSELAGE SKIN AT FR22-FR23 STGR51L-STGR53L REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE SKIN AT FR22 - FR23 STGR51L-STGR53L NO REPAIR RECORD FOUND. REMOVED THE EXISTING REPAIR AND RE-REPAIRED THE SKIN IAWSRM 53-10- SDR CALA2026012713357Skin · corrodedFOUND RT FWD LOWER SKIN CORRODED AT WING ROOT. PERFORMED REPAIR IAW ECRA 5731-01759, PART 1 ON WCS FWD LWR SKIN PANEL AT BS 54 AT RBL 57,SDR JR2R20260121230Doubler · corrodedAFT CARGO ENTRY AFT INTERNAL DOUBLER/TRIPLER BETWEEN STR27R-STR28R BETWEEN FR79-FR81 HAS EXFOLIATING CORROSION. REPLACED PER SRM.SDR VNAA202604110010Skin · damagedLIGHTNING STRIKE DAMAGE BETWEEN FS202 AND FS220 WITHIN 5340.2 FLIGHT HOURS AFTER SECTION I (STARTING AT 10,087.8 FH), ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IN ACCORDANCE WITH APPROVED PROCEDURES OR REPLACE PART. LIGHTNING STRIKE DAMAGE BETWEEN FS20SDR REXA2026030900158Skin · corrodedCORROSION ON INTERNAL SKIN BTW FS 677.00 AND FS693.00 STGR 26L TO 26R BELOW FLOOR. CORROSION ON INTERNAL SKIN BTW FS 677.00 AND FS693.00 STGR 26L TO 26R BELOW FLOOR WAS REPAIRED PER REO 690-53-31-1118 REV - -
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