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 DALA2024081508163Skin · crackedCORROSION ON LOWER SKIN OF CENTER FUEL TANK BTW STA APROX Y=696 AND ON STA Y=655 INTERNAL STRUCTURE AT RH CANTED KEEL. SUMMARY OF NRC 00492: CORROSION LEVEL 2. CORROSION ON LOWER SKIN OF CENTER FUEL TANK BTW STA APROX Y=696 AND ON STA Y=655 INTERNAL STRUCTURE SDR SWAA2024081425940Doubler · crackedEXTERNAL POWER DOOR RECEPTACLE DOUBLER CRACKED AT LOWER EDGE. DAMAGE AREA IS L-1.0' X W-0.03125'.<[01] ACCOMPLISHED EA 24-153-02232. REF TSR 2024005780. OK TO CONTINUE PER TLD.SDR SWI2024F01270Skin · chafedLH LOWER WING PLANK AND AFT WING SPAR @ APPROX. WS48.00 IS CHAFFED BY THE WING TO BODY FAIRING 193AB (MARKED) (C-CHECK RO 10/26/2024) (FILED CLOSED)REPAIRED LH LOWER WING PLANK AND AFT WING SPAR AT APPRO. WS48.00 AS PER REO NO. 601R-57-21-880 REV. -D DATE: 201SDR SWIA20240813Skin · crackedNLG AFT DOOR FUSELAGE SKIN CUT OUT, THE AFT RH CORNER POSSIBLE CRACK IN THE RADIUS (MARKED) (C-CHECK RO 10/26/2024) (FILED OPEN)COMPLIED WITH ALL STEPSF MHIRJ REO 601R-53-11-048 REV-D DATED 2015-06-10 AND REO 601R-53-11-3943 REV -- DATED 2024-09-02 IN THE REPSDR NACA2024081300001Skin · corrodedFUSELAGE SKIN EXTERIOR SURFACE CORROSION AT STA 1417 TO 1461 AND S-8R. NAC EO 767-53-0058REV IR (09-10-2020) SRM 53-00-01-1A-1 / NRC 0412, 0527, 0354, 0403, 0388, 0389, 0524, 0737, 0387,0356, 0397, 0375 EARN N399CM-026 RDR SJX-NAC-24-0113-14B /SJX-NAC-24-0122SDR SWAA2024091225377Skin · corrodedCORROSION ON FUSELAGE CROWN SKIN AROUND FASTENERS IN ROWS FROM STA 1016 TO STA 1016+23; RBL 9; 12; 13; AND LBL 12.<[01] REPAIRED PER EA 24-153-02292 DATED 29-AUG-2024.;[02] VERIFIED CORRECTIVE ACTION COMPLETE.SDR DALA2024081908257Skin · damagedSHIP 659 FUSELAGE / SKIN / STA 1701, S-15R S-16R / DAMAGE UNDER EXISTING REPAIR. ER/A 488007-14 REV B REQUIRES STAGE 3 DTE APPROVAL. CORRECTIVE ACTION: REF ERA 488007-14. (0500074)SDR ASAA2024081253153Lap Joint · corrodedR/H LWR FUSELAGE LAP JOINT AT AFT CARGO DOOR STA 787 STR 23R HAS SIGNS OF CORROSION. GROUNDED - YES. ACCOMPLISHED CATEGORY "B" MINOR REPAIR AT RH LOWER FUSELAGE LAP JOINT AT AFT CARGO DOOR CUTOUT ON SKIN PANELS 146A3251-32 AND 146A3231-49 AT STA 797 STGR 23R ISDR ASAA2024081253152Butt Joint · corrodedSIGNS OF CORROSION AT L/H STA 360 STR 24L TO 26L SEC 41 BUTT JOINT. GROUNDED - YES. ACCOMPLISHED CATEGORY "A" MINOR REPAIR TO LH FUSELAGE SKINS 141A3521-33 & 143A3232-28 AT STA 360 BETWEEN STGR 24L-26L IAW EA 800-53EA-27427 REV 00.SDR ASAA2024081253151Lap Joint · corrodedL/H UPPER LAP SEAM AT STA 616 TO STA 627 STR 4L HAS SIGNS OF CORROSION. GROUNDED - YES. ACCOMPLISHED CATEGORY "A" MINOR REPAIR TO LH UPPER LAP SEAM SKIN PANELS 144A3111-18 AND 144A3111-19 AT STA 616-639 STGR 4L IAW EA800-53EA-27428 REV 01.SDR ASAA2024081253104Lap Joint · corrodedL/H MID LAP SEAM AT STA 663.75 TO STA 706 STR 10L HAS SIGNS OF CORROSION. GROUNDED - YES. ACCOMPLISHED CATEGORY "A" MINOR REPAIR AT LH MID LAP SEAM ON SKIN PANELS 144A3111-19 AND 144A3321-3 AT STA 663-706 STGR 10L IAW EA 800-53EA-27439 REV 00.SDR ASAA2024081253103Lap Joint · corrodedR/H LWR FUSELAGE WINDOW LAP JOINT AT STA 500 STR 14R HAS SIGNS OF CORROSION. GROUNDED - YES. ACCOMPLISHED CATEGORY "A" MINOR REPAIR TO RH LOWER FUSELAGE WINDOW LAP JOINT SKIN PANELS 143A3151-98 AND 143A3252-29 AT STA 500D-500C STGR 14R IAW EA 800-53EA-27419 RESDR ASAA2024081253101Skin · corrodedFUSELAGE SKIN AT LOWER LAP SEAM STGR 23L BETWEEN STA 907-927 HAS SIGNS OF CORROSION. GROUNDED - YES. ACCOMPLISHED CATEGORY "B" MINOR REPAIR TO LH LOWER FUSELAGE LAP SEAM SKIN PANELS 147A3110-3 AND 147A3400-4 AT STA 897-947 STGR 23L IAW EA 800-53EA-27422 REV 00SDR ASAA2024081253097Skin · corrodedL/H FUSELAGE WINDOW LAP JOINT AT STA 727B STR14L HAS SIGNS OF CORROSION 15-22. GROUNDED - YES. ACCOMPLISHED CATEGORY "B" MINOR REPAIR AT LH FUSELAGE WINDOW LAP JOINT ON SKIN PANELS 146A3151-93 AND 146A3201-32 AT STA 727A-727D STGR 14L IAW EA 800-53EA-27437 REVSDR ASAA2024081253096Skin · corrodedR/H LWR LAP JOINT AT STA 853 TO STA 875 STR 23R HAS SIGNS OF CORROSION 10-22. GROUNDED - YES. ACCOMPLISHED CATEGORY "A" MINOR REPAIR TO RH LOWER LAP JOINT SKIN PANELS 146A3251-32 AND 146A3231-49 AT STA 847-887 STGR 23R IAW EA 800-53EA-27426 REV 00.SDR R61A2024082900369Skin · misrepaired***MAJOR***WRONG REPAIR DOUBLER INSTALLED ON AC. MX REPLACED DOUBLER FR 19-20 STR23R-24R IAW SRM 53-10-01 REPAIR 12. ***MAJOR***SDR YENA2024081301119Skin · damagedDURING HEAVY MAINTENANCE: FUSELAGE / REAR FUSELAGE / SKIN PANEL BETWEEN FR80-81 & STGR 1R-3R / ELONGATED HOLES & EXISTING REPAIR - PERMANENT REPAIR; REFERENCES: /1/ AEROMAN EA 53-9033-24 COVER & P1-P2 /2/ AIRBUS RDAF 81440328/004/2024 ISSUE B /3/ AIRBUS TD/814SDR SWAA2024091938213Skin · damagedPERFORM PERMANENT REPAIR ON FUSELAGE SKIN AT STA 932 AND 935 STR 21L 2024-512156<[01] TOOL USED IN STEP 5: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N:60009161631; DUE DATE: 11-MAR-25;[02] PERFORMED REPAIR ON FUSELAGE SKIN BTW BS927 TO BS947.5 AND BTW STSDR DALA2024081308105Skin · dentedSHIP 3408 GROUND CREW REPORTS DENT ON AFT CARGO DOOR SURROUND. CORRECTIVE ACTION: DAMAGE IS AT FR65, STR42RH/42ARH. 1.250" IN LENGTH, .312" IN WIDTH, .078" DEPTH. PERFORMED REWORK PER A330 SRM 53-41-11-283- 022. DAMAGE IS IN ZONE B. INSPECTION ZONE 2 OPTIMIZEDSDR ASAA2024081052791Skin · corrodedEXTERIOR SKIN HAS 3 AREAS OF CORROSION BS. 727 TO BS.887 STR. 4R LOWER SKIN. GROUNDED - YES. REMOVED CORROSION AT 3EA LOCATIONS BETWEEN BS 727 TO BS 887 STR 4R LOWER SKIN AND REPAIRED ALL DAMAGE LOCATIONS IAW ASA EA 800-53EA-27601. REPAIR DOUBLER LOCATION BETWSDR DALA2024081408130Skin · damagedSHIP 662 SECTION I REPAIR TO FUSELAGE SKIN AT STA1885 AND S-17R REQUIRES REPETITIVE INSPECTIONS PER SECTION II OF ERA 619908-14 CORROSION. CORRECTIVE ACTION: REF ERA 619908-14. (0495014)SDR DALA2024081408129Skin · damagedSHIP 662 SECTION I REPAIR TO FUSELAGE SKIN AT STA1885 AND S-17R REQUIRES PERMANENT REPAIR PER SECTION III OF ERA 619908-14 CORROSION. CORRECTIVE ACTION: REF ERA 619908-14. (0495016)SDR DALA2024081208036Skin · damaged(LOG 6169784) LIGHTNING STRIKE ON DEPARTURE APPEARED TO HIT THE FORWARD PART OF THE AIRPLANE. FLIGHT ATTENDANT REPORTED LOUD POP AND WEIRD NOISE AT THE 1L DOOR POSITION. NO OTHER ELECTRICAL ANOMALIES ASSOCIATED W/ LIGHTNING STRIKE. FOUND BURNT MARK ON CAPT. AOSDR DALA2024081207994Skin · scratchedSHIP 3164 UPPER FUSELAGE, BETWEEN FRAMES 54 AND 55 AND STRINGERS 4R AND 5R, SKIN IS SCRATCHED. CORRECTIVE ACTION: REWORKED DAMAGE PER A319 SRM 53-41-11-283-001. (0493362)SDR U2RA2024090800050Skin · dentedREF HAECO XMN (TX9Y778Y) NRC#:KUL6825 - EXISTING DENT AND BLEND-OUT WERE FOUND ON FUSELAGE SKIN AT STA 500, STR-38R-STR-39R. DEVIATIONS OCCUR WHEN PERFORM THE B747-400SF SRM 53-00-01/REPAIR 12 REPAIR.SDR CALA2024090302354Skin · scratchedDURING MX WALK AROUND FOUND SCRATCH ON L/H SIDE OF FUSELAGE .75" FWD OF STA. 500F & 3" AFT OF STA. 500F ON S26L. REF SRM 53-00-01-1A-5 MEASUREMENTS AS FOLLOWS 3.65" L X 0.022"W ADDITIONAL PICTURE X 0.033"D. W/Y =6.666 GOUGE IS THROUGH 2 EA RIVETS. DAMAGE IS OUSDR SCNA20240820305Skin · dentedWORK ORDER FS240105 NR002: POSSIBLE DENT WITH 2 BLIND FASTENERS INSTALLED THRU SKIN AND STRINGER STA 440 STR 28R. - - RESOLUTION: DENT WITH CREASE ON SKIN AT STRINGER STA 440 STR 28R REPAIRED IAW EA 24009 REV IR.SDR SWIA2024081208Skin · damagedCOMPLY WITH REPAIR AUTHORIZATION: RA92795-ETD2024-170-019819 MXCODEID76651-PR - SKIN DAMAGE ON FORWARD FUSELAGE SKIN FR18-FR19 AND STGR 21R- STGR22R. PER ETD ETD2024-170-019819 PERFORM PERMANENT REPAIR. DUE AT 14559 CYCLES , PART NUMBER: , SERIAL NUMBER: , POSSDR FDEA202408081109Skin · corrodedFOUND EXFOLIATION CORROSION ON EXTERIOR SKIN SURFACE ADJACENT TO L/H APY DOOR FWD HINGE POINT AREA COMPLIED WITH MAJOR REPAIR CLASSIFICATION. E.A. #-F-5330-T0380244 P1 FUSELAGE-PLATES AND SKIN- LH APU COMPARTMENT SKIN PANEL REPAIR BETWEEN STA. 1885.20 AND SDR JR2R20240808833Skin · corrodedAFT CARGO AROUND AFT WASTE DOOR BOX/CUTOUT INTERNAL SIDE CORRODED MULTIPLE PLACES. REPAIREDSDR FDEA202408081093Skin · dentedDURING PERFORM E.A :G-5330-T0368078 - FUSELAGE - PLATES&SKINS - AFT FUSELAGE SKIN PANEL STA 1902.5 - 1907.5, STR 46R - 47R, THE DENT DAMAGE FOR CAT C INTERIM REPAIR WILL BE REPLACED BY CAT A OR B PERMANENT REPAIR. AFT FUSELAGE SKIN AT STA 1902.5-1907.5, STSDR DALA2024080807887Skin · dentedDENTS (2EA) ON FUSELAGE SKIN BTW STA Y=120 TO 144 APPROX AND LONG 18LH TO 19LH. ALSO PJECTION LONG-16LH TO LONG-17LH. SUMMARY OF NRC 00669: FUSELAGE SKIN BTW STA Y=120 TO 144 APPROX AND LONG 18LH TO 19LH. ALSO PJECTION LONG-16LH TO LONG-17LH WAS REPAIRED PER ESDR IXXA2024080802Skin · damagedTHERE IS A DAMAGED FASTENER HOLE, IN THE EXTERIOR SURFACE OF THE FUSELAGE SKIN, WHERE THE LOWER SILL SCUFF PLATE HAS BEEN REMOVED FROM THE 4L DOOR LOCATIONSDR SWAA2024090623559Skin · crackedSTA 312 L/H SIDE HAS A CRACK JUST ON TOP OF L-1 DOOR CUTOUT.<[01] THIS TASK CARD WAS ACCOMPLISHED ON EA NO:M-22-153-01244;[02] CORRECTION TO STEP 1: WORK WAS ACCOMPLISHED ON TASK CARD TTG8Q00V38DR; EA NO:M-22-153-01244.;[03] VERIFIED STEP 2SDR AALA202408271344Bear Strap · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN R1 DOOR FRAME BEAR STRAP AT STA 312, RBL 8. ACCOMPLISHED DOUBLER REPAIR TO FUSELAGE SKIN PER SRM 53-10-01-2R-6 AND EA 356702.SDR SCNA20240816302Skin · corrodedWORK ORDER FS240102: COROSION FOUND ON LH SIDE EXTERNAL FUSELAGE SKIN AT STA 917 BTWN STR21 AND STR22 L, LAV VENT. - - RESOLUTION: REMOVED CORROSION ON LH SIDE EXTERNAL FUSELAGE SKIN AT 917 BTWN STR 21 L STR22 L, LAV VENT IAW B737 SRM 51-10-02 EVALUATED ARE SDR SWIA202408140007Skin · puncturedPUNCTURE ON THE R/H FUSELAGE BETWEEN FS 559+96 AND 559+112 AND BETWEEN STGR 16R AND 17R MEASURING APPROX 3.5" H X 4" L. THIS IS CLASSIFIED AS A MAJOR REPAIR. FORM M-337 INITIATED. (FILED CLOSED) PERFORMED PERMANENT REPAIR ON R/H FUSELAGE BETWEEN FS 559+96SDR GTIA2024080938302Skin Panel · damagedLH FR 12 LIGHTNING STRIKE PERFORME THE PERMANENT REPAIR AS PER AIRBUS REPAIR DOSSIER MESSAGE 81360850/022 RAF-01 CREATED -EVALUATED AND REPAIRED LIGHTNING STRIKE AT LH FR 12 PER EA 5311-2473 REF RDAF 81360550/018/2024 #A CAT A REPAIR PERMANANT NO REINSPECTSDR VNAA202408070010Doubler · corrodedFWD CARGO DOOR SURROUND STRUCTURE SILL PLATE AND ""H"" DOUBLER BETWEEN F.S.533 TO F.S.549 ARE CORRODED. REMOVED DAMAGED JOINT PLATE (H DOUBLER) IAW CRJ-700 SRM 51-42-22-001-001-A01. INSTALLED NEW SERVICEABLE JOINT PLATE PN: SH670-33793-4 IAW CRJ-700 SRM 51-4SDR DALA2024080907934Butt Joint · corroded(LOG 0489295) CORROSION ON STA 360 INTERNAL BUTT JOINT SPLICE DOUBLER AT LBL 6 2" O/B OF STR 28L. REMOVED DAMAGE AND REPAIRED INTERNAL BUTT JOINT SPLICE DOUBLER @ STA 360, LBL 6.2 O/B OF STR 28L PER ER/A 619535-14.SDR DALA2024080907927Skin · corroded(LOG 0489043) CORROSION ON FUSELAGE INTERNAL SKIN FROM STA 294.5-344 STR 24L. REMOVED DAMAGE AND REPAIRED FUSELAGE INTERNAL SKIN @STA 294.5-344, STR 24L PER ER/A 619628-14 REV. ORIGINAL.SDR DALA2024080807892Skin · bulgedSHIP 662 SKIN BULGE FOUND AT APROX STA 440 STR 23R. CORRECTIVE ACTION: COMPLIED WITH ER/A 619846-14 REV ORIGINAL SKIN REPAIR AT STA 440 STR 23R(0489282)SDR SWIA202411150806Skin · damagedDURING DETAILED VISUAL INSPECTION FOR PREVIOUSLY REPAIRED BLOWN OUT HOLE ON FUSELAGE LOCATED AT PANEL 132AL FOUND FREEZE PLUG MISSING. CAMP28644781 (C-CHECK RO 10/26/2024) (FILED CLOSED)FABRICATED AND INSTALLED FREEZE PLUG IAW REO 601R-53-11-162 REV -D 2019-02SDR SWIA2024102806Skin · damagedDURING DETAILED VISUAL INSPECTION FOR PREVIOUSLY REPAIRED BLOWN OUT HOLE ON FUSELAGE LOCATED AT PANEL 132AL FOUND FREEZE PLUG MISSING. CAMP28644781 (C-CHECK RO 10/26/2024) (FILED OPEN)FABRICATED AND INSTALLED FREEZE PLUG IAW REO 601R-53-11-162 REV -D 2019-02-0SDR COEA2024102304921Skin Panel · dentedWO 256293 NR 200068 HEAVY CHECK COE/MAJOR REPAIR DISCREPANCY: DENT AT R/H EXTERNAL FUSELAGE FRAME 17 BETWEEN STRINGERS 14R AND 15R. CORRECTIVE ACTION: REPAIRED PER ATR42 SRM 530000-300-807-A01.SDR SCNA20240813300Repair · unknownWWORK ORDER FS 2400102: SCRATCH FOUND ON EXISTING REPAIR, L/H SIDE EXTERNAL FUSELAGE AFT OF L2 DOOR APPROX BS 1016 BTWN STR 12L AND STR 17L. - - CORRECTIVE ACTION: ACCOMPLISHED DOUBLER REPAIR AT LH SIDE EXTERNAL FUSELAGE SKIN BTWN STA 1016 TO STA 1040 BTWN STRSDR DALA2024080807911Skin · corroded(LOG 0487749) DURING INSPECTIONS, CORROSION WAS FOUND ON THE INTERNAL SURFACE OF THE UPPER SKIN PANEL (PN 141A3112-9), BETWEEN APPROX. BS 304 AND BS 344, AT STR 24L LAP SPLICE. CORROSION REPAIRED PER ERA 619628-14.SDR DALA2024080807896Skin · corrodedSHIP 662 DTA MONITOR INSPECTION LOG REF ERA 619846-14 FUSELAGE / EXTERNAL SKIN / STA 440, BETWEEN S-22R AND S-23R / CORROSION. CORRECTIVE ACTION: REF ERA 619846-14. (1487941)SDR DALA2024080807893Door · damagedSHIP 5656 DAMAGE AT L2 DOOR (FUSELAGE STA. 640 / STR. 18L TO 20L / DENT & GOUGE. CORRECTIVE ACTION: REF NR 001 ON WP # 706300 20AUG24. CW ERA 619917-14AD. (0487582)SDR N6WA2024080706Skin · gougedFUSELAGE SKIN REPAIR AT FS977 STGR27 TRIPPLER HAS GOUGE DAMAGE. REPAIRED GOUGE DAMAGE AT FS977.0 STGR 27 IAW REO 670-53-00-290 AND EO C700/900-53MR -007-R2.
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