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 R61A2023122100754Doubler · corrodedWHILE IN HEAVY CHECK - DURING THE REMOVAL AND INSTALLATION OF WASTE ACCESS PANEL 152AR HINGE, CORROSION WAS FOUND ON WASTE INTERNAL DOUBLER. REMOVED AND REPLACED WASTE INTERNAL DOUBLER BETWEEN FR 88-89. REF EMB SRM 51-40--08.SDR ASAA2023122148168Skin · gougedLESSOR ITEM 613; (74470) SEVERAL DENT/GOUGES MARKS ON FUSELAGE SKIN FR 52/56 AND STRG 39/41 RH GROUNDED - YES. REMOVED DAMAGE ORIG .236 MATERIAL LOSS .008, REMAINING .228 ACCOMPLISHED HFEC AND DUI NO DEFECTS NOTED APPEARANCE OF DENT WAS MULTIPLE LAYERS OF PAINSDR A6WA202312218687Skin · dented4 DENTS ON EXTERIOR LOWER SKIN AT FS 672.20 AND STRINGER 27. CUST W/O: 332319 JOB CARD: 453-900-501 EXTERIOR LOWER SKIN AT FS559.0 +112 - S755.0 AIRCRAFT REMOVED FROM SERVICE. PERFORMED HAND DRESS ON 4 EA DENTED AREAS (P1 TO P4) TO REFORM SKIN TO ORIGISDR DALA2024121611761Skin · damagedER/A 613880-14 ISSUED FOR BIRD STRIKE DAMAGE TO THE FWD FUSELAGE. FOLLOW ON ACTION (DTE) IS REQUIRED. DTE IS REQUIRED. ER/A 613880-14 SECTION I APPROVAL IS LIMITED TO 12 MONTHS. ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) IS REQUIRED FOR CONTINUE SERVSDR SWIA2024021931220Skin · chafedFS969.00 - FS985.00 STRG 27 SKIN REPAIR DOUBLER CHAFFED IN 2EA AREAS (MARKED) (C-CHECK RO 2/18/2024) REMOVED 1EA BOTTOM DOUBLER, 1EA TOP DOUBLER, 2EA FILLERS, 2EA TAPERED SHIMS & 4EA DOME NUTPLATES REF.CRJ700 SRM 51-42-21-001-001-A01, CRJ700 SRM 51-42-06-SDR IXXA2023122904Skin · damagedLIGHTENING STRIKE STA 742 S4RSDR IXXA2023122902Rivet · damagedLIGHTENING STRIKE DAMAGE AT STA 654+34 S22LSDR IXXA2023122901Skin · damagedLH FUSELAGE-LIGHTENING STRIKE AT STA 408 STR 30LSDR DALA2023122710651Unknown · unknownERA 613880-14 ISSUED FOR BIRD STRIKE SKIN REPAIRS. AIRCRAFT OPER ATED WITH RVSM RESTRICTIONS PER A220 MEL 53-00-00V. ERA613880-14 ISSUED. ACCOMPLISH SECT.III WITHIN 30 DAYS AFTER S ECTION I. ADDITIONAL ENGINEERING APPROVALS (ERA REVISION) REQUIR ED FOR SERVICESDR DALA2023122210531Unknown · unknownSHIP 670 CORROSION ON EXTERNAL/INTERNAL SKIN BTW STA= 760 AND STA=770 BTW S19R AND S20R AT LOWER CTR FUSELAGE. CORRECTIVE ACTION: SUMMARY OF NRC S/N 00314, CORROSION ON EXTERNAL/INTERNAL SKIN BTW STA=760 AND STA=770 BTW S19R AND S20R AT LOWER CTR FUSELAGE WAS SDR DALA2023122210529Unknown · unknownSHIP 0683 FUSELAGE / SKIN / FS508-FS520, S-28L TO S-28R / FWD LOWER ATG4 ANTENNA / REMOVAL. CORRECTIVE ACTION: REF ERA 614548-14. (0119244)SDR DALA2023122210527Unknown · unknownSHIP 6712 FUSELAGE / SKIN / FS508-FS520, S-28L TO S-28R / FWD LOWER ATG4 ANTENNA / REMOVAL. CORRECTIVE ACTION: REF ERA 614547-14. (0119224)SDR DALA2023122210526Unknown · unknownSHIP 0696 FUSELAGE / SKIN / FS508-FS520, S-28L TO S-28R / FWD LOWER ATG4 ANTENNA / REMOVAL. CORRECTIVE ACTION: REF ERA 614241-14. (0119207)SDR YENA2023122101637Unknown · unknownDURING HEAVY MAINTENANCE: AFTER STRG 29R REMOVAL, FOUND CORROSION AT INNER FUSELAGE SKIN LOCATED BETWEEN FR73/74 IN AFT CARGO COMPARTMENT; REF TOMX WO # 2404 NR # 00168 CORROSION AT INNER FUSELAGE SKIN LOCATED BETWEEN FR73/74 IN AFT CARGO COMPARTMENT WAS REMOVSDR YENA2023122101627Unknown · unknownDURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE II / LOWER SKIN / AT STR 29R BETWEEN FR73 – FR74 / CORROSION - PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)SDR UIEA2023121901004Unknown · unknownA PUNCTURED HOLE ON THE FUSELAGE SKIN NEAR STA 1241, BETWEEN S-105L & S-106L(<P>1) ACCOMPLISHED EI T2023A53M-3476 REV 1. 2) JOB COMPLETED AND CONDITION CHECK NORMAL</P>)SDR DALA2023122110475Unknown · unknownSHIP 3309 AD MTC TASK - EXISTING REPAIR FOUND AT FX FR67 STGR 46R - STGR 48R. CORRECTIVE ACTION: EXISTING REPAIR AT FX FR67 STGR 46R - STGR 48R REPAIRED AS PER ER/A 613921-14. (0118023)SDR R61A2024010500779Unknown · pilot errorTAIL STRIKE DURING LANDING BETWEEN FRA 99 AND FRA 100 AND STR 29L TO STR 29R. REPAIRED IAW ETD2023-170-032292 REV A AND TI-170-23-249. ALSO REF VP-054105-2023 N/R #5 & #6 FOR REPAIRS. INSTALLED DOUBLER AT FRAME 100.SDR SWIA2023122600019Unknown · gougedTRANSFER FROM EAML 1264508 : REF EAML 1262050 INSPECTED LEFT NOSE AREA OF REPORTED DAMAGE AND FOUND HOLE MEASURING 0.437"L X 0.500"W INSIDE GOUGE DAMAGE MEASURING 0.875"L X 0.125"W X 0.002"D LOCATED FR 9-10 AND STGR 17L-18L. (FLIGHT 3863 - FILED CLOSED)REMOVSDR SWIA2023122200019Unknown · gougedTRANSFER FROM EAML 1264524 : REF EAML 1262518 FOR AC DAMAGE, INSPECTED LWR LEFT NOSE AREA OF REPORTED DAMAGE AND FOUND GOUGE 1.5"L X 0.25"W WITH PUNCTURE THRU SKIN LOCATED BETWEEN FR 9 AND 10 AND STGR 17L AND 18L. DAMAGE OUT OF LIMITS AND HAS BEEN CLASSIFIED ASDR DALA2023122110450Unknown · unknownSHIP 0670 FUSELAGE / SKIN / BTW STA 760-780 & S18R-20R / CORROSION. CORRECTIVE ACTION: REF ERA 614132-14. (0117468)SDR DALA2023122010423Unknown · unknownSHIP 3166 DENT ON LEFT HAND SIDE OF APU INLET RIGHT IN FRONT OF APU ACCESS DOOR. CORRECTIVE ACTION: REPAIRED PER ERA 614446-14. (4863946)SDR DALA2023121910374Unknown · unknownSHIP 3166 DENT ON SKIN FWD OF FR80 LWR SKIN. CORRECTIVE ACTION: LOCATED FASTENER HOLES AND FABRICATED -1 DOUBLER & -2 FILLER IAW SRM 53-51-11-300-010, INSTALLED -1 & -2 REPAIR PARTS IAW SRM 53-51-11-300-010. (4863949)SDR AALA202401051004Skin · noneAIRCRAFT IN BASE MAINTENANCE: REPLACED FUSELAGE SKIN TEMPORARY REPAIR AT STA 392, FROM S30L TO S31L WITH REPAIR DOUBLER PER ARM 53-00-01-2R-7 REPAIR 7.SDR CALA2023122103704Skin · dentedAFT FUSELAGE 4EA DENTS AROUND TAIL JACKING POINT, REQUIRING EVALUATIONS. REPAIR 04EA DENTS AROUND TAIL JACKING POINT DOOR FR73 AND FR74 B STA: ST ENG BFM. REF ELB 7404529 FOR DMG. BETWEEN STGRS 31RH AND 31LH PER EC/RA 5351-01220, FOUND REPAIR IS PERMANENT REPASDR CALA2023122003694Skin · dentedRIGHT EXTERNAL FUSELAGE SKIN FR25-26 STR 41R-42R HAS 2EA DENTS. REPAIRED RT EXTERNAL FUSELAGE SKIN BETWEEN FR25-26 AND 241R-42R. PER EC/RA # 5321-02124 REV ORIGINAL AND FINAL EA 319-5321-13-A34 55 REV -.SDR CALA2023122003687Skin · dentedAFT FUSELAGE TAIL SECTION FR73 STRINGER 30R-31R HAS INWARD DENT. THIS REPAIR IS CONSIDERED A CAT B REPAIR PER SRI 53-00-11-205-053. FABRICATED AND INSTALLED DOUBLER REPAIR AT FR73 STRINGER 30R-31R REPAIRED DENT TO AFT FUSELAGE TAIL SECTION, FR73 STRINGER CATSDR YENA2023122001615Unknown · unknownDURING HEAVY MAINTENANCE: SMALL DENT LOC. ON LOWER CENTER CUT-OUT DOOR 832 CABIN PASSENGER; (RESOLVED ON W/O: 1271876 TASKCARD: NR-00040) REF TO AEROMAN WO 2023 364/1 NR 2023-760288, EVALUATED DENT LOC. ON LOWER CENTER CUT-OUT DOOR 832 CABIN PASSENGER AND FOUNSDR DALA2023121910407Unknown · unknownDURING REMOVAL OF FASTENERS ON EXTERNAL SKIN BTW STA=767 AND S26R AT LOWER CTR FUSELAGE CORROSION WAS FOUND ON INTERNAL STRINGER AND HOLES FASTENERS REMOVED. SUMMARY OF NRC 00829: INTERNAL STRINGER STA=767 AND S26R AT LOWER CTR FUSELAGE WAS REPAIRED PER B757-SDR AALA202312194839Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FUSELAGE SKIN AT R1 DOOR UPPER HINGE, FORWARD SIDE OF FRAME, BS 291.5, RBL 49. REPAIRED SKIN PER SRM 53-10-01-2R, REPAIR 6 AND EA 349540.SDR VNAA202312160003Skin · dentedHN 120398 DISCREPANCY: FUSELAGE SKIN IS DENTED IN MULTIPLE AREAS UNDER THE FOOTPRINT OF THE LH VENTRAL FIN. CORRECTIVE ACTION: COMPLIED WITH MHIRJ REO 690-53-00-534 REV -- DATED 2023-12-06.SDR VNAA202312160004Skin · dentedHN 120399 DISCREPANCY: FUSELAGE SKIN IS DENTED IN MULTIPLE AREAS UNDER THE FOOTPRINT OF THE RH VENTRAL FIN. CORRECTIVE ACTION: COMPLIED WITH MHIRJ REO 690-53-00-535 REV -- DATED 2023-12-06.SDR DALA2023122110476Unknown · unknownSHIP 3414 FUSE SKIN REPAIR - FR 77, STR 43R - 44R. INSP REQ. CORRECTIVE ACTION: REF ER/A 611644-14. (5100396)SDR SWAA2023121832423Doubler · peelingDOUBLER ON EXTERNAL POWER DOOR CUTOUT HAS PEELED APART<[01] REPAIRED ELECTRICAL GROUND POWER RECEPTACLE SURROUND REF SRM 53-10-15.SDR ASAA2023121448676Skin · damagedLESSOR ITEM 598: (74485) LIGHTNING STRIKE ON FUSELAGE SKIN AT FR 3 8 INCHES FROM CENTER LINE TO RH SIDE GROUNDED - YES. REMOVED AND REPLACED FASTENER WITH LIGHTNING STRIKE MARK. IAW A320 SRM 53-11-11-300-034. AND SRM 51-42-11 AND AIRBUS DWG D3D53M3540 ISSUE BSDR ASAA2023121447510Skin · dentedLESSOR ITEM 568:(74533) DENT ON FUSELAGE SKIN FR 76/77 STRG 21/21/LH GROUNDED - YES. EVALUATED DENT LENGTH=1.6" WIDTH=1.4" DEPTH=.021". 7.2"AFT OF FRAME 76 AND 1.6" BELOW STRINGER 28. D/A= .013125 FOUND TO BE WITHIN LIMITS IAW A320 SRM 53-51-11-283-004. PERFOSDR VNAA202401220010Skin · damagedLIGHTNING STRIKE DAMAGE ON FUSELAGE SKINS AT STR 16R THE SUBJECT CONDITION IS STRUCTURALLY ACCEPTABLE FOR 400 FLIGHT HOURS FROM TIME OF INCORPORATION OF THIS REO AT REV -- LIGHTNING STRIKE DAMAGE ON FUSELAGE SKINS AT STR 16R WAS REPAIRED PER REO 690-53-11-165SDR DALA2023121810320Unknown · unknownSHIP 3251 DISC: ER/A 604897-14 REV A / SECTION II PERMANENT REPAIR. C/A: 604897-14, REV A / THIS LP IS UPDATED TO CORRECT "E" MONITOR TO INSPECTION "N" / THIS LP DOES REQUIRE MAINTENANCE ACTION IS NOT AN ENGINEERING FUNCTION-RELATED RESTRICTION. (LP: 0110023)SDR UIEA2023121200988Unknown · unknownLOWER HALF OF FUSELAGE, LOWER LOBE INTERIOR, BULK CARGO COMPARTMENT, BETWEEN STA 1430 AND STA 1461, AND BETWEEN STGR 23R AND STGR 24R, CORROSION ON SKIN.(<P>LOWER HALF OF FUSELAGE, LOWER LOBE INTERIOR, BULK CARGO COMPARTMENT, BETWEEN STA 1430 AND STA 1461, ANDSDR SWI2024F00016Skin · dentedFS589.00 STRG 26LH - STRG 27, EXTERIOR SKIN DENT (MARKED) (C-CHECK RO 1/22/2024) COMPLIED WITH REO 601R-53-61-8133 REV --, DATED 2023-12-18 STEPS 1 THRU 10, AND ENSURED ALL OTHER REQUIREMENTS OF REO 601R-51-00-309 REV A DATED 2017-08-23 WERE MET.SDR SWI2024F00015Skin · dentedFS574.00 - FS605.00 STRG 24LH - 26LH, 5EA INTERIOR DENTS PROTRUDING EXTERNALLY ON THE FUSELAGE SKIN (MARKED) (C-CHECK RO 1/22/2024) COMPLIED WITH REO 601R-53-61-8133 REV--, DATED 2023-12-18, STEP 1 THRU 10, ENSURED ALL OTHER REQUIREMENTS OF REO 601R-51-00SDR VNAA202401220016Skin · damagedBURN MARK ON FUSELAGE SKIN BTW FS.469.00 TO FS 477.40 AND BTW STGR13RH TO STGR14RH. BURN MARK ON FUSELAGE SKIN BTW FS.469.00 TO FS 477.40 AND BTW STGR13RH TO STGR14RH WAS REPAIRED PER REO 670-53-00-045 REV. -K DISPOSITION: 1. B-PERMANENT DISPOSITION/. B3/.SDR VNAA202401220013Skin · corrodedCORROSION ON INNER SKIN SURFACE AT THE MAIN AVIONICS BAY DOOR CUTOUT BTW FS 364.00 TO FS394.00, BTW STGR 25LH TO 25RH. THE MAIN AVIONICS BAY DOOR CUTOUT BTW FS 364.00 TO FS394.00, BTW STGR 25LH TO 25RH WAS REPAIRED PER REO 690-53-21-032 REV - -SDR VNAA202401220008Skin · damagedBURN MARK ON FUSELAGE SKIN BTW FS 533.00 TO FS 549.00 AND BTW STGR13RH TO STGR14RH. BURN MARK ON FUSELAGE SKIN BTW FS 533.00 TO FS 549.00 AND BTW STGR13RH TO STGR14RH WAS REPAIRED PER REO 690-53-31-801 REV. --SDR VNAA202401220007Skin · damagedBURN MARK ON FUSELAGE SKIN BTW FS 477.40 TO FS 485.00 AND BTW STGR13RH TO STGR14RH. BURN MARK ON FUSELAGE SKIN BTW FS 477.40 TO FS 485.00 AND BTW STGR13RH TO STGR14RH WAS REPAIRED PER REO 690-53-31-801 REV. --SDR SWAA2024011631480Skin · corrodedFUSELAGE EXTERNAL SKIN HAS CORROSION AROUND AIR PHONE BLANK OFF PLATE BS 440+10; STR 27L - 28L<[01] REFER TO FAULT TTG8Q00Q9LX7 FOR REPAIR RESOLUTION.;[02] VERIFIED CORRECTIVE ACTION 1SDR SWAA2024011631803Skin · corrodedFUSELAGE EXTERNAL SKIN HAS EVIDENCE OF CORROSION AROUND AIR PHONE BLANK OFF PLATE BS 400+10; STR 27L - 28L<[01] AS PER EA 23-153-03768; THE REWORK IS ACCEPTABLE AS A CONTINUE-IN-SERVICE CONDITION WITHOUT REPETITIVE INSPECTIONS AND NO TERMINATING ACTION REQUIRESDR SWAA2024011631437Access Panel · delaminatedDELAMINATED ACCESS PANEL 193CL AT LOWER FUSELAGE 2023-756785<[01] TOOL USED: CALIPER P/N: 500-197-30; S/N: 15120589; DUE DATE: 13-FEB-24.;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N: 18196127 DUE DATE: 22-JAN-24.;[03] TOOL USED HOT BONDER P/N: HCS9200B-AV SDR SWAA2024011631439Access Panel · crackedCRACK AROUND OF THE HOLE ACCESS PANEL 193AL AT LOWER FUSELAGE 2023-756786<[01] TOOL USED: CALIPER P/N: 500-197-30; S/N: 15120589; DUE DATE: 13-FEB-24.;[02] TOOL USED: SCALE P/N: SPX621 S/N:8340225451 DUE DATE: 16-AUG-24.;[03] TOOL USED: HOT BONDER P/N: HCS9200SDR DALA2023121510287Unknown · unknownCORROSION ON INNER SKIN ON STA Y 627 BTW LONG 28RH AND LONG 29RH BILGE AREA AT FWD COMPARTMENT. SUMMARY OF NRC 00072: CORROSION LEVEL 2. INNER SKIN ON STA Y 627 BTW LONG 28RH AND LONG 29RH BILGE AREA AT FWD COMPARTMENT WAS REPAIRED PER ERA 598923-14 REV. A AND
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