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 FDEA2020063071371Skin · chafedFORWARD CARGO COMPARTMENT DOOR CUTOUT STATION 1009 LONGERON 40 RIGHT HAND TO LONGERON 41 RIGHT HAND FOUND CHAFING.SDR SWIA202053109Skin · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE. FOUND DENT IN FUSELAGE AT FS 233.00 ON RBL 7.5 ON THE EDGE OF THE CUTOUT FOR THE NLG. COMPLIED WITH TEMPORARY REPAIR, PER REO 690-53-11-1128 REV: A DATED: 2019-07-16. PERMANENT REPAIR IS TO BE DONE WITHIN 2300 FLIGHT SDR SWIA202082051849Skin · damagedRT FUSELAGE APRON SKIN PANEL, UPPER ATTACHMENT ROW OF RIVETS AT WL 72.50, FROM BS 797 AFT TO BS 847, HAD NUMEROUS FASTENERS SMOKING, LOOSE, AND PULLING THROUGH THE SKIN. PERMANENTLY REPAIRED AND REINSTALLED RT FUSELAGE APRON SKIN PANEL, UPPER ATTACHMENT ROWSDR IXXA20200720030Skin · dentedAIRCRAFT GROUNDED FOR HEAVY MAINTENANCE SCHEDULED VISIT. PER CUSTOMER REQUEST, PLEASE REVIEW AND VERIFY N311AZ DENT AND BUCKLE REPORT ITEM #8 CONFORMS TO B767 SRM 53-00-01 REPAIR 12. REVIEWED DENT AND BUCKLE REPORT ITEM #8, PERFORMED CONFORMITY OF REPAIR
IN ASDR KCSA202006261099Doubler · cracked2 INCH CRACK ON DOUBLER AT STA 420 BETWEEN S-6 R AND S-7 R AFT OF CREW SERVICE DOORSDR FDEA202006261366Skin · crackedDURING HIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT ON EXTERNAL SURFACE OF FUSELAGE WITHIN A 2 INCH RADIUS OF ALL HOLES COMMON TO THE LEFT HAND UNDERWING LONGERON AND FUSELAGE SKIN FOUND 01 EACH CRACKS ON THE SKIN APPROXIMATE 0.7" AT STATION 1030 BETWEENSDR FDEA202006261365Skin · crackedDURING HIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT ON EXTERNAL SURFACE OF FUSELAGE WITHIN A 2 INCH RADIUS OF ALL HOLES COMMON TO THE RIGHT HAND UNDERWING LONGERON AND FUSELAGE SKIN FOUND 01 EACH CRACKS ON THE SKIN APPROXIMATE 0.6" AT STATION 1030 BETWEESDR JR2R2020062612110Skin · puncturedFUSELAGE PUNCTURED BY JETBRIDGE BETWEEN FR21-22 AND STRINGERS 14-15SDR IPXA2020070657409Skin · corrodedINSPECTION TYPE:3C EXTERIOR FUSELAGE SKIN HAS CORROSION BETWEEN STA 2154.0 TO 2163.8 AND BETWEEN L33L TO 35L. REPAIRED CORRODED EXTERIOR FUSELAGE SKIN BETWEEN STA 2154.0 TO 2163.8 AND BETWEEN L33L TO 35L IAW SRM 53-70-01 REPAIR 3 FIG 201. (MAJOR)SDR IPXA2020070657407Skin · corrodedINSPECTION TYPE:3C EXTERIOR FUSELAGE HAS CORROSION BETWEEN STA 2150.0 TO 2163.8 AND BETWEEN L33R TO 35R. REPAIRED CORRODED EXTERIOR FUSELAGE SKIN BETWEEN STA 2150.0 TO 2163.8 AND BETWEEN L33R TO 35R IAW SRM 53-70-01 REPAIR 3 FIG 201. (MAJOR)SDR ABXA20200721140Skin · corrodedSTA 1186 SR 38R, FUSELAGE SKIN DOUBLER REPAIR. AIRCRAFT WAS GROUNDED.SDR ABXA20200721138Skin · damagedBS 1330 SR 33L FUSELAGE SKIN DOUBLER REPAIR. AIRCRAFT WAS GROUNDED.SDR EE4Y2020062411477Skin · scratchedUPPER FUSELAGE BETWEEN BS 787+11.25" AND BS 1016,STR 4L SKIN WITH SCRIBE LINES IN SEVERAL PLACES.IT WAS REPAIRED FOLLOWING REPAIR INSTRUCTIONS UNDER SERVICE REQUEST:4-4739952886 AND IAW EO COO-EO-2020-11331-R00.(REF JOB A1J004-2-136)SDR EE4Y2020062411474Skin · scratchedUPPER FUSELAGE BETWEEN BS 727 AND BS 887 STR 4R SKIN WITH SCRIBE LINES IN SEVERAL PLACES.IT WAS REPAIRED FOLOWING REPAIR INSTRUCTIONS UNDER SERVICE REQUEST: 4-4741406401 AND I.A.W COOPESA EO# COO-EO-2020-11094-R01.(REF JOB A1J004 2-139)SDR EE4Y2020062411476Skin · scratchedUPPER FUSELAGE BETWEEN BS 360 AND BS 540 STR 4R,SKIN WITH SCRIBES LINES IN SEVERAL PLACES. IT WAS REPAIRED FALLOWING REPAIR INSTRUCTIONS UNDER SERVICE REQUEST: 4-4726377762 AND I.A.W COOPESA EO# COO-EO-2020-11117-R00. ( REF JOB A1J004 2-137)SDR EE4Y2020062411475Skin · scratchedUPPER FUSELAGE BETWEEN BS 540 AND BS 727 STR 4R,SKIN WITH SCRIBES LINES IN SEVERAL PLACES. IT WAS REPAIRED FOLLOWING REPAIR INSTRUCTIONS UNDER SERVICE REQUEST: 4-4740007260 AND I.A.W COOPESA EO# COO-EO-2020-11153-R00. (REF JOB A1J004 ITEM 2-138)SDR EE4Y2020062411473Skin · scratchedUPPER FUSELAGE BETWEEN BS 540 AND BS 727 STR 10R,SKIN WITH SCRIBES LINES IN SEVERAL PLACES. IT WAS REPAIRED FOLLOWING REPAIR INSTRUCTIONS UNDER SERVICE REQUEST: 4-4738386530 AND I.A.W COOPESA EO# COO-EO-11350-R00.(REF JOB A1J004 ITEM 2-127)SDR EE4Y2020062411478Skin · scratchedUPPER FUSELAGE BETWEEN BS 727 AND BS 887 STR 4L SKIN WITH SCRIBES LINES IN SEVERAL PLACES. IT WAS REPAIRED FOLOWING REPAIR INSTRUCTIONS UNDER SERVICE REQUEST:4-4740007260 AND I.A.W COOPESA EO# COO-EO-11110-R02.(REF OB A1J004 ITEM 2-135)SDR SWAA2020072329674Skin · dentedEXTERNAL SKIN HAS A DENT BS 856 AND 2 INCHES ABOVE STR 21R. MEASUREMENTS OF DENT ARE L: 3.714;W:2.303 ; Y:0.062; W/Y:37 AT LOWER FUSELAGE (1EA) / PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN LOC BTW BS 847 TO BS 867 AND BTW STRG 20R TO STRG 22R AT LOWER FUSELAGSDR ABXA20200721139Skin · damagedSTA 1239 SR39L-39R REMOVED NICK FROM INTERNAL SKIN AREA. AIRCRAFT WAS GROUNDED.SDR SWAA2020071499417Skin · dentedFUSELAGE SKIN HAS A DENT AT BS 927+2'; 1'ABOVE S-20L. DENT AT BS 927+2'; 1' ABOVE STR 20L FUSELAGE SKIN WAS REPAIRED IAW EA 20-153-00945 REV IR DATED 07/10/2020 & ATS ER 20-02811 REV IR DATED 07/10/2020.SDR IPXA2020071097567Skin · corrodedINSPECTION TYPE:3CCENTER WING BOX UPPER SKIN HAS CORROSION AT STA. XCW= -87.7 ABOVE STR. 15.REPAIRED CORRODED CENTER WING BOX UPPER SKIN AT STA. XCW= -87.7 ABOVE STR. 15 IAW VT-SAA EA 011-5730-01-A8388 REV. I/R AND UPS EO MD11-5730-77106-A. (MINOR)SDR SWAA2020071494247Doubler · crackedEGPR SURROUND DOUBLER IS CRACKED AT THE FWD MIDDLE LOCATION (BETWEEN HINGES). EGPR SURROUND DOUBLER CRACK AT THE FWD MIDDLE LOCATION REPAIRED IAW ATS ER 20-02810; REV IR; DATED 06-JUL-2020 AND PER EA NR 20-153-00946 REV IR.SDR SWAA2020071494246Doubler · crackedEGPR SURROUND DOUBLER IS CRACKED AT THE AFT LOWER CORNER. EGPR SURROUND DOUBLER CRACK AT THE AFT LOWER CORNER REPAIRED IAW ATS ER 20-02810; REV IR; DATED 06-JUL-2020 AND PER EA NR 20-153-00946 REV IR.SDR IPXA2020071097568Skin · corrodedINSPECTION TYPE:3C, CENTER WING BOX UPPER SKIN HAS CORROSION AT STA. XCW= -11 ABOVE STR. 15.REPAIRED CORRODED CENTER WING BOX UPPER SKIN AT STA. XCW= -11 ABOVE STR. 15 IAW VT-SAA EA 011-5730-01-A8391 REV I/R, AND EO MD11-5730-77097-A. (MINOR)SDR IPXA2020071097565Skin · corrodedINSPECTION TYPE:3C, CENTER WING BOX UPPER SKIN HAS CORROSION AT STA. XCW= 55.5 AT STR. 15.REPAIRED CORRODED CENTER WING BOX UPPER SKIN AT STA. XCW= 55.5 AT STR. 15 IAW VT-SAA EA 011-5730-01-A8393 REV. I/R AND UPS EO MD11-5730-77095-A. (MINOR)SDR IPXA2020071097563Skin · corrodedINSPECTION TYPE:3C, CENTER WING BOX UPPER SKIN HAS CORROSION AT STA. XCW= 47 AND STR. 15.REPAIRED CORRODED CENTER WING BOX UPPER SKIN AT STA. XCW= 47 AND STR. 15 IAW VT-SAA EA 011-5730-01-A8386 REV. I/R AND UPS EO MD11-5730-77099-A. (MINOR)SDR IPXA2020071097562Skin · corrodedINSPECTION TYPE:3C, CENTER WING BOX UPPER SKIN HAS CORROSION AT STA. XCW= 2 AND STR. 15.REPAIRED CORRODED CENTER WING BOX UPPER SKIN AT STA. XCW= 2 AND STR. 15 IAW VT-SAA EA 011-5710-01-A8392 REV. I/R AND UPS EO MD11-5730-77090-A. (MINOR)SDR IPXA2020071097561Skin · corrodedINSPECTION TYPE:3C, CENTER WING BOX UPPER SKIN HAS CORROSION AT STA. XCW= -111 AT STR. 12.REPAIRED CENTER WING BOX UPPER SKIN AT STA. XCW= -111 AT STR. 12 IAW EA 011-5710-01-A8390 REV. I/R AND EO MD11-5730-770859-A. (MINOR)SDR IPXA2020070657405Skin · corrodedINSPECTION TYPE:3C EXTERIOR FUSELAGE SKIN HAS CORROSION BETWEEN STA 2153.0 TO 2163.8 AND BETWEEN L12R TO 13R. REPAIRED CORRODED EXTERIOR FUSELAGE SKIN BETWEEN STA 2153.0 TO 2163.8 AND BETWEEN L12R TO 13R IAW SRM 53-70-01 REPAIR 3 FIG 201. (MAJOR)SDR SWAA2020062493965Skin · gougedGOUGE FOUND IN THE SKIN AT STRINGER 19L + 5.5' AT BS 500, GOUGE APPROXIMATELY 9.25 LONG. REPAIRED IAW SRM 53-00-01-2R-36 REPAIR 36. CATEGORY B REPAIR.SDR FDEA2020062301298Skin · dentedLOWER LOBE ZONE 100, 500 STR 27R, DENT IN EXTERIOR SKIN. REPAIRED AREA PER B757 SRM 53-00-01-2R REPAIR 29.SDR HNAA2020062900178Skin · crackedRH SIDE FUSELAGE FRAME 79 HAS POSSIBLE SKIN CRACKS AROUND 1 FASTENER. MAINTENANCE: REPAIRED IAW EO1-53-20-0244.SDR SWIA2020080751685Doubler · corrodedTCAS ANTENNA DOUBLER, BS 295 TO 310 HAD SIGNS OF CORROSION. REPLACED THE TCAS ANTENNA DOUBLER IAW DWG, AND SRM.SDR SWIA2020071451321Skin · dentedFUSELAGE SKIN BETWEEN FS589-FS605, STR 21L-22L IS DENTED. (C-CHECK) RO 7/10/2020 DRESSED OUT DENT ON FUSELAGE SKIN BETWEEN FS589-FS605, STR 21L-22L REF REO. EVALUATED AND FOUND TO BE OUT OF LIMITS DUE TO FASTENER PROXIMITY REF SRM. SUBMITTED TO ENGINEERING SDR SWIA2020071451320Skin · dentedFUSELAGE SKIN BETWEEN FS700-FS718, STR 14L-15L IS DENTED. (C-CHECK) RO 7/10/2020 HAND DRESSED DENTS (2EA) ON THE FUSELAGE SKIN BETWEEN FS700-FS718, STR 14L-15L REF REO. AFT DENT FOUND TO BE WITHIN LIMITS. FWD DENT FOUND TO BE OUT OF LIMITS REF SRM. SUBMITTSDR SWIA2020071451319Skin · dentedFUSELAGE SKIN BETWEEN FS589-FS605, STR 24R-26R IS DENTED. (C-CHECK) RO 7/10/2020 HAND DRESSED DENTS (3EA) LOCATED AT FUSELAGE SKIN BETWEEN FS589-FS605, STR 24R-26R REO. ALL THREE DENTS FOUND TO BE OUT OF LIMITS DUE TO DENTS IN ADJACENT PANELS IN THE CIRCUMFESDR HNAA2020062900176Skin · crackedLH SIDE FUSELAGE FRAME 77 HAS POSSIBLE SKIN CRACKS AROUND 3 FASTENERS. REPAIRED THE FUSELAGE EXTERNAL SKIN AT FR 77 STGR 3L AND 6L IAW SRM 53-32-01 RE ITEM 9.SDR 2020F00316Skin · corrodedREPAIR OF CORROSION ON TAILCONE STINGER INNER RIGHTHAND SKIN. TEXTRON AVIATION ENGINEERING REPAIR LETTER DQ26060M1 DATED 06/16/2020.SDR SWAA2020070696287Skin · dentedDENT FOUND ON EXTERIOR FUSELAGE SKIN AT STA 927+14.3; STR 19L. DENT FOUND ON EXTERIOR FUSELAGE SKIN AT STA 927+14.3; STR 19L MEASURED 4.1'L X 3.4'W X .028'D W/Y=121. OUT OF LIMITS DUE TO COMMON WITH STR 19L PER SRM 53-00-01-1A-1 TABLE 102. REPAIRED FUSELAGESDR SWAA2020070693113Doubler · crackedEGPR SURROUND DOUBLER CRACKED AT APPROX STA 232; 8' ABOVE STR 24R. REMOVED DAMAGE ON EGPR SURROUND DOUBLER AT APPROX STA 232; 8' ABOVE STR 24R AND INSTALLED REPAIR PARTS IAW SRM 53-10-15-2R-4.SDR GTIA2020061975206Skin · dentedDENT BTW FRAME 78-79 STRINGER 1 RAF-01 OPENED REF LTPR MRI 5001004957-0010-REPAIR PERFORMED IAW EO 5351-2047 REV.00.FOR ALL WORK PERFORMED SEE LTPR DO 5001004957,LTPR MO 1003184674-0010 AND EO 5351-2047 REV.00.THIS CAT A REPAIR WITH NO ADDITIONAL REQUIREMENTS.SDR SWIA2020090252161Skin · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE: DENT FOUND RT FWD FUSELAGE BETWEEN STRINGERS R25 & R24. REINSPECT NEEDED EVERY 600 HOURS PER REO. PERMANENT REPAIR DUE IN 5300 FLIGHT HOURS BY 38018.2 TAT., PART NUMBER: - , SERIAL NUMBER: 7769, POSITION: C-CHECK ROSDR SWIA2020090252158Skin · damagedCOMPLY WITH SCHEDULED MAINTENANCE CODE: REPAIRED 2 ELONGATED FASTENER HOLES ON FWD FUSE SKIN USED FOR ATTACHING PANEL 131AL PER REO. PERFORM DETAILED VISUAL INSPECTION, PART NUMBER: - SERIAL NUMBER: 7769, POSITION: C-CHECK RO 8/29/2020. PERFORMED DETAILED VISSDR HNAA2020072000203Skin · crackedHEAVY CHECK - 2 POSSIBLE SKIN CRACK AROUND RIVET AT FR 77 BTW STR 5R-6R...CUT OUT DAMAGED SKIN AROUND RIVET IAW SRM 53-32-01. MADE REPAIR BUSHING IAW SRM 53- 32-01 9,H,1-7.SDR HNAA2020072000202Skin · crackedHEAVY CHECK - 2 POSSIBLE SKIN CRACK AROUND RIVETS AT FR 77 BTW STR 7R-8R...CUT OUT DAMAGED SKIN AT UPPER FASTENER IAW SRM 53-32-01. MADE REPAIR BUSHING IAW SRM 53-32-01 9,H,1-7.SDR HNAA2020072000201Skin · crackedHEAVY CHECK - 2 POSSIBLE SKIN CRACK AROUND RIVETS AT FR 80 BTW STR 6L-7L....CUT OUT DAMAGED SKIN AROUND LOWER FASTENER AT FR80 BTW STGR 6L-7L IAW EMB 145 SRM 53-32-01. MADE REPAIR BUSHING IAW EMB 145 SRM 53-32-01 9,H,1-7.SDR SWAA2020070997878Skin · gougedFUSELAGE SKIN HAS A GOUGE AT BS 847+6.5'; .8' BELOW S-1L. DAMAGE REPAIRED PER EA 20-153-00953 REV IR (ATS ER 20-02766 REV IR) REFER TO NRC U181821 FOR TRACKING.SDR SWAA2020070997877Skin · gougedFUSELAGE SKIN HAS A GOUGE AT BS 847+4.5' STR 1. FUSELAGE SKIN GOUGE AT BS 847+4; STR 1 WAS REPAIRED IAW ATS ER 20-02766 REV IR RATED 30JUN20 AND EA 20-153-00953 REV IR.SDR DU4R2020061600047Skin · crackedAIR STAIR DOOR CUTOUT AROUND FWD UPPER HOLE NR 8 WAS CRACKED.
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