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 A6WA2020010647091Skin · damagedPER CUSTOMER REQUEST, APPLY GENERIC REO 601R-53-11-0048 ON LEFT SIDE SKIN RADIUS AT FS 235. AIRCRAFT REMOVED FROM SERVICE REPAIRED NLG CUTOUT, LH SIDE, AT FS235 I/A/W BOMBARDIER REO 601R-53-11-0048 REV. D.SDR A6WA2020010647094Skin · crackedFUSELAGE SKIN AT AFT RIGHT CORNER NEXT TO SPADE DOOR IS CRACKED. AIRCRAFT REMOVED FROM SERVICE REPAIRED FUSELAGE SKIN IAW REO 601R-53-11-3525 REV-- DATED 01-02-2020.SDR ASOA2020021903017Skin Splice · corrodedDURING C CHECK INSPECTION SKIN SPLICE WAS FOUND CORRODED AT FRAME 60-61 STRINGER 20R-21R. MAINTENANCE REPAIRED I/A/W SRM 53-00-02 AND 51-40-02.SDR SWIA2020021148342Skin · corroded* EXTERIOR FUSELAGE SKIN AT SRT 27 AREA LOCATION AT APPROX FS 559+96 THE IS EVIDENCE OF CORROSION ON SKIN AND RIVET LOCATION (MARKED) (C-CHECK) RO 2/07/2020 COMPLIED WITH PERMANENT REPAIR EXTERIOR FUSELAGE SKIN AT SRT 27 AREA LOCATION AT APPROX FS 559+96, SDR SWIA2020020648231Skin · gouged* APU EXHAUST CUTOUT EXTERIOR SKIN Ï¿½ GOUGES AND EDGE DAMAGE ON AFT SIDE OF CUTOUT (MARKED). (C-CHECK) RO 2/04/2020 REMOVED DAMAGE ON APU EXHUAST CUTOUT EXTERIOR SKIN, REF CRJ 200 SRM. SKIN IS WITHIN LIMITS PER BOMBARDIER REO. SEE CONTINUATION CARD FOR DESDR AALA202001069038Doubler · crackedAIRCRAFT WAS GROUNDED: CRACK AT LOWER EDGE OF EXTERNAL POWER DOOR ACCESS CUTOUT DOUBLER. REPAIRED CUT OUT DOUBLER PER SRM 53-10-15-2R-4.SDR COEA2020032007801Skin · distortedWO 209330 NR 100052 HEAVY CHECK COE/MAJOR REPAIR: NOSE FUSELAGE LOWER L/H AFT SKIN IS DISTORTED AT DME2 ANTENNA FASTENER LOCATIONS, FRAMES 8-9. CORRECTIVE ACTION: REPAIRED PER SRM 531129-300-802-B01.SDR FDEA202001020002Skin · crackedDURING ACCOMPLISHMENT OF HFEC INSPECTION ON FUSELAGE SKIN OF LEFT HAND UNDERWING LONGERON FOUND 02 EACH CRACKS INDICATION AT STATION 1024 AND STATION 1035 STRINGER 37 LEFT. APPROXIMATELY 2.0" IN LENGTH EACH, AS MARKED. FUSELAGE SKIN LEFT HAND UNDERWING LONGESDR DALA2020010600059Doubler · corrodedINTERNAL SKIN DOUBLER LOCATED BETWEEN STRINGER 22L AND STRINGER 26L AND BETWEEN FS 994 AND FS 1053 HAS MULTIPLE AREAS OF CORROSION ON DOUBLER. REMOVED CORROSION, COMPLIED WITH PRI ER/A 584182-14 REV O STEP 7. C/W STEPS 8 AND 9 OF ER/A 584182-14 REV O. RII COMPSDR EE4Y2020010200472Skin · dentedEXTERNAL FUSELAJE SKIN WITH DENTS AND SCRATCH LOCATED BTWN FR27/FR29, BTWN S-24L/S-26L. THE DISCREPANCIES WAS REPORTED TO EMB Y REPAIRED IAW ETD2019-190-164764 AND WITH EO COO-EO-2019-10461.SDR R61A2020012100045Skin · dentedMAJOR REPAIR: FORWARD FUSELAGE LOWER SKIN AT FRAME 21 TO 22, BETWEEN STGR 24R TO 25L HAS MULTIPLE DENTS AND HOLES IN SKIN. R&R FWD FUSELAGE LOWER SKIN AT FR21 TO 22 BETWEEN STR 24R TO 25L IAW ETD2020-170-000006 REV B AND SRM 51-41-02, 51-43-05, 51-21-07, 51-4SDR IPXA2020010315551Skin · crackedFUSELAGE SKIN CRACK AT RH SIDE PACK DOOR UPPER AFT AREA. CORRECTIVE ACTION: REPAIRED IAW E.O. MD11-5330-75031-A. THIS IS A MAJOR REPAIR.SDR COEA2020032000001Skin · corrodedWO 209330 NR 100014 HEAVY CHECK COE/MAJOR REPAIR: FRAME 14 SKIN FLANGE IS EXFOLIATED BETWEEN STRINGERS 20R-21R LEVEL 2 CORROSION CORRECTIVE ACTION: REPAIRED PER SRM 530000-300-828-A01.SDR CALA2020010600069Skin · dentedDENT ON ENTERIOR SKIN FROM INSIDE OUT FED OF AFT DRAIN MAST APPROX STSTION 1590 C/W HFEC PER NDT MANUAL PART 6, OF FUSELAGE DENT , EXTERIOR SKIN- INSIDE OUT , FWD OF AFT DRAIN MAST AT APPROX STA-1590. NO CRACK INDICATIONS NOTED AT THIS TIME. PERFORMED INTERIMSDR SWIA2020021848664Skin · gouged*SEVERAL GOUGES IN FUSELAGE SKIN AFT OF LOW PRESSURE AIR GROUND CONNECTION DOOR BETWEEN FS 1029 TO 1044 AND STRINGER 21RH TO 26RH (C-CHECK) RO:2/14/2020REPAIRED GOUGES FOR FUSELAGE SKIN AFT OF LOWER PRESSURE AIR GROUND CONNECTION PER REO. SEE CONTINUASDR R61A202001080018Skin · dented***WHILE A/C WAS OUT OF SERVICE FOR A HEAVY CHECK*** LH FWD FUSELAGE SKIN, UNRECORDED DENT BTWN FR 10-11 & STGR 17L-18L. DENT FOUND TO BE WITHIN PERMANENT ALLOWABLE LIMITS PER ETD2020-170-000468. A/C REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.SDR CALA2020010600066Skin · dentedFOUND DAMAGE ON LOWER FUSELAGE BETWEEN STATION 1241 AND 1263 FWD OF BULK CARGO DOOR DAMAGE LOCATION IS STA 1263 STR 34 L. DENT IS APPROX 9"L X 6" W AND DEPTH IS APPROX .241 DEEP. A/Y MEASURES 24.89. DENT OUT OF LIMITS REF SRM A/D 1 53-00-01. NOT THE BULK CARGOSDR CALA2020010600063Skin · dentedDENT LH SIDE UNDER SECOND WINDOW BETWEEN FR23 & 24, JUST ABOVE GOLD STRIP. REPORTED BY MOVE TEAM EVALUATED DENT: D=.036" T=.079" A=2.0". DENT IS TYPE 1, ZONE 1. ACCOMPLISHED EXTERNAL DVI (TEMPORARY SOLUTION), NO DEFECTS NOTED IAW SRM 53-11-11-283-012. MUST ACSDR SIMA2020010230003Skin · crackedDURING HMBV INSPECTION, QC FOUND RH AFT FUSELAGE SKIN CRACKED IN 2 AREAS ON FR 75 STGR 3R-C/A-REPAIRED CRACKS ON RH AFT FUSELAGE SKIN AT FR 75 AND STGR 3R IAW EMB 145 SRM 53-31-01-RE REPAIR #11. (REPAIR MATERIALS: DOUBLER 2024-T3, 0.080?, FILLER: 2024-T3, 0.0SDR YENA2020010200722Skin · gougedDURING HEAVY MAINTENANCE, GOUGE - EXTERNAL SKIN FR64 +20" STR26L; (REF AEROMAN NR 2019-400559) PERFORMED REPAIR ON EXTERNAL SKIN FR64 +15" TO FR65 +2" AND BETWEEN STR25L +1" TO STR27L IAW SRM A320 53-41-11-300-036. THIS REPAIR IS CAT "A" WITH NO INSP REQUIRED.SDR DALA2019123097604Skin · damagedACFT SKIN DAMAGED JUST FWD OF WATER SERVICE PANEL, REPAIR FOR ERA 584168-14 ORIGSDR COEA2020011509801Skin · corrodedMINOR REPAIR: LEVEL 2 CORROSION LT WINDOW NR 12 LOWER AREA BETWEEN FRAMES 29-30. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0087723_01...13704 ISSUE B, DATED 1/10/2020.SDR COEA2020011508801Skin · corrodedMINOR REPAIR: LEVEL 2 CORROSION AT NR 8 WINDOW UPPER AREA FRAMES 24-25. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0088003_01...13701 ISSUE B, DATED 1/1/2020.SDR CALA2020010600058Skin · corrodedB777-53-3-7117 EMP- STA 2344.5-2370 RH INTERNAL SKIN STR 40R TO 43R SURFACE AREA FOUND CORROSION REFER TO NR LP:9131366 INTERIM REPAIR WAS ACCOMPLISHED ON HAECO NRC 9131366 IAW ECRA 53 31-02557. PER PART 1.2 OF THE ECRA, A DIP IS REQUIRED TO ACP INI TIAL INSP SDR DALA2020010407701Skin · cracked(AIRCRAFT 7102, L/P 1421303) RH FUSELAGE SKIN APPROX STA 1028 AND STA 1033 STR 37R FOUND 02 EA HOLE SURFACE CRACKS. CORRECTIVE ACTION: REPAIRED IAW DELTA PRI 583826-14AD REV 1 STEP 11D.SDR DALA2020010407700Skin · damaged(AIRCRAFT 7102, L/P 1421298) FOUND HOLE RH FX SKIN AREA AT APPROX. STA 1033 BETWEEN STR 36R AND 37R SKIN SURFACE (02 EA) WITH ABRASION. CORRECTIVE ACTION: DAMAGE TRIMMED OUT AND REPAIRED IAW DELTA ERA 583814AD REV ORIGINAL DUE TO CRACK FOUND ON BOTH 02 EA HOLESDR DALA2020010407698Skin · cracked(AIRCRAFT 7102, L/P 1421291) LH FUSELAGE SKIN APPROX STA 1028 AND STA 1033 STR 37L FOUND 02EA HOLES SURFACE CRACK. CORRECTIVE ACTION: TRIMMED-OUT AND REPAIRED I.A.W DELTA PRI 583827-14AD REV 1 STEP 11D.SDR DALA2020010407697Skin · damaged(AIRCRAFT 7102, L/P 1421282) LH FX SKIN AREA AT APPROX. STA 1033, BETWEEN STR 36L AND STR 37L FOUND HOLE SURFACE (02 EA) WITH ABRASION DAMAGE (WITHIN TRIM LINE). CORRECTIVE ACTION: TRIMMED-OUT AND REPAIRED I.A.W DELTA ERA 583827-14AD REV ORIGINAL.SDR DALA2019122907587Skin · corrodedCORROSION FOUND JUST AFT OF LAV SVC PANEL. CORROSION ALSO NOTED FURTHER AFT AT PRESSURE DOME AREA. SKIN IS BULGED AND SEPARATED AT SEAM. AREA MARKED. BLENDED CORROSION NEAR AFT LAV SVC PNL. FOUND TO BE WITHIN LIMITS PER MD88 SRM 53-04-1. RESTORED FINISH. CORROSDR SWIA2020020648226Skin · dentedA GROUP OF DENTS WERE FOUND ON THE AFT L/H SIDE OF FUSELAGE UNDER THE L/H ENGINE AFT OF FS 621. (MARKED) (C-CHECK) RO 2/04/2020 HAND DRESSED BACK DENTS ON THE AFT LH SIDE OF FUSELAGE UNDER THE LH ENGINE AFT OF 621 BACK TO ORIGINAL CONTOUR REF BOMBARDIER RESDR SIMA2020010227005Skin · crackedDURING HMBV INSPECTION, QC FOUND LH AFT FUSELAGE SKIN CRACKED AT FR 75 ABOVE STGR 2L.-C/A-PERFORMED PERMANENT REPAIR TO CRACK ON LH REAR FUSELAGE I SKIN AT FR 75 ABOVE STGR 2L IAW EMB 145 SRM 53-31-01-RE REPAIR #11. (REPAIR MATERIALS: DOUBLER 2024-T3, 0.080?, SDR SWIA2020020648225Skin · dentedD: DENT WITH CREASE FOUND ON RIGHT SIDE OF AIRCRAFT. COMPLIED WITH TEMPORARY REPAIR PER REO. PERMANENT REPAIR DUE WITHIN 3100 FLIGHT HOURS. DUE BY TAT 40484.3 / RA # 47273 / C: MCI / NOTE: BUILT MX CODE TO TRACK 50 FLIGHT HOUR LPI INSP OR EDDY CURRENT INSP.SDR CALA2020010600047Skin · chafedB757-53-3-6075 SUPPORT BRACKET CHAFING INTO AFT FUSELAGE SKIN PA NEL STA 1797 STR 17L. RL030 REF ST ENG N/R 0079023 BLENDED AND CHECKED LIMITS TO CHAFING AT AFT FUSELAGE SKIN PANEL STA 1797 S-17L L=2.5 W=.75 D=.030 OUT OF LIMITS IAW B757-2 SRM 53-80-70 PG 106 SDR R61A201912271436Skin · dentedDURING OVERNIGHT MAINTENANCE, A DENT WAS DISCOVERED AT FRAMES 9-10, STRINGERS 20R-21R. THE REPAIR WAS ACCOMPLISHED IAW SRM 53-10-01, REPAIR 12P. ACFT WAS RETURNED TO SERVICESDR FDEA201912240001Skin · damagedFUSELAGE HAS IMPACT DAMAGE AT STA 1109 AT STR 4L REPAIRED FUSELAGE SKIN PER E.A. H-5330-T0351626 PART 1.SDR NACA2019122400174Skin · crackedBS340, WL208 3 CRACKS FOUND AT L1 DOOR AFT LOWER CORNER ON FUSELAGE SKIN. CONTACT PEMCO ENGINEERING, SDR STILL OPENSDR SWIA2020013148006Skin · corrodedCORROSION ON SKIN DOUBLER FOR ANTENNA BETWEEN FS295.00 - FS310.00, STGR27 - STGR26R, MARKED (C-CHECK) RO 1/28/2020 REMOVED CORROSION FROM SKIN DOUBLER FOR TCAS ANTENNA BETWEEN FS295.00- FS310.00, STGR27-STGR26R REF CRJ200 SRM. FOUND TO BE OUT OF LIMITS. INSDR FDEA201912233282Skin · crackedHFEC SURFACE INSPECTION CARRIED OUT ON THE RIGHT HAND SIDE OF THE FUSELAGE SKIN COMMON TO THE UNDERWING LONGERON WITHIN A 2 INCHES RADIUS OF THE FASTENER HOLES FOUND CRACK APPROXIMATE 1/2" AT STATION 1027 STRINGER 37 RIGHT. FUSELAGE SKIN UNDERWING LONGERON WISDR CALA2020010600027Skin · dentedAFT CARGO DOOR CUTOUT UPPER FORWARD CORNER APPROX. STA 810, HAS A DENT AT EDGE. [MKD 78-85]. REF. AAR N/R 99862094 ORIGINATED AFT CARGO DOOR UPPER RIGHT CORNER EDGE STA810 HAS EXISTING DAMAG E W=1.1Y=.033W/Y=33. THIS IS A CAT B REPAIR.DOUBLERREPAIR WAS AC COSDR CALA2020010600026Skin · damagedFWD CARGO DOOR CUTOUT FWD UPPER CORNER HAS EXISTING DAMAGE ON EDGE REF AAR N/R 99861866 UPDATED MAA CODE FIX USING VENDOR MAA SCREEN EVALUATE AND CONTACT TOMC FWD CARGO DOOR UPPER RIGHT CORNER EDGE STA 400+8 INCHES TO THE R IGHT STR 17R TO STR 20R HAD EXISTINGSDR DALA2019122307514Skin · corrodedFUSELAGE INTERNAL SKIN AT BS 1065 TO 1087 BETWEEN STRINGERS 39L TO 39R, FOUND CORROSION. REF TO CPCP TASK 53-544-00. THE CORROSION ON FUSELAGE INTERNAL SKIN AT BS 1065 TO 1087 BETWEEN STRINGERS 39L TO 39R WAS REPAIRED IAW PRI 583419-14, REV 0 . THE PRI 583SDR CALA2020010600015Doubler · corroded(B737-06-3-0442) AFT CARGO COMPARTMENT, CORROSION AT STA 847-867 IN BETWEEN INTERCOSTALS AT LBL 17 AND REPAIR AS REQUIRED. REF BY PEMCO NRS 2664N457. REMOVED CORROSION AT STA 847-867 IN BETWEEN INTERCOSTALS AT LBL 17-21. REMOVED .026 MAT .064 MAT REMAINS OF ORSDR SWAA2020012040620Skin · corrodedCENTER AREA BELOW AFT CARGO FLOOR HAD LIGHT SKIN CORRODED AT BS 727E+11, BETWEEN STR 27L TO STR 27R. REPAIRED SKIN PER SRM.SDR COEA2020011510801Skin · corrodedMINOR REPAIR: LEVEL 2 CORROSION FWD CARGO DOOR CUT OUT FWD UPPER AREA AT FRAME 14. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0087479_01...13687 ISSUE B, DATED 1/7/2020.SDR COEA2020011406801Skin · corrodedMINOR REPAIR: LEVEL 2 CORROSION LT WINDOW NR 6 TOP AREA BETWEEN FRAMES 23-24. CORRECTIVE ACTION: REPAIR PER SRAS ES_0087717_01...13705 ISSUE B, DATED 1/10/2020.SDR COEA2020011405801Skin · corrodedMINOR REPAIR: LEVEL 2 CORROSION LT WINDOW 10 UPPER AREAS BETWEEN FRAMES 27-28. CORRECTIVE ACTION: REPAIR PER SRAS ES_0087717_01...13705 ISSUE B, DATED 1/10/2020.SDR COEA2020011404801Skin · corrodedMINOR REPAIR: LEVEL 2 CORROSION LT WINDOW NR 9 BOTTOM AREA BETWEEN FRAMES 26-27. CORRECTIVE ACTION: REPAIR PER SRAS ES_0087717_01...13705 ISSUE B, DATED 1/10/2020.SDR CALA2020010600010Skin · dentedDENT ON FUSELAGE LEFT SIDE BETWEEN PRESSURE RELIF VALVE AND ELEV.STATIC PORT ABOUT 36" BELOW PUNCTURE THROUGH FUSELAGE SKIN AT APPROX STA 1445 AND 1" ABOVE S-25L REMOVED DAMAGE TO THE AFFECTED SKIN AERA STA 1445 AND STR 25 L REF 53-00-01. INSPECTION WILL NEEDSDR CALA2020010600008Skin · crackedFUSELAGE SKIN 1/2" CRACK F/S 1654 AT LWR SHEAR TIE FASTENER ABOVE STR 8R. REPAIRED FUSELAGE SKIN CRACK AT F/S 1654 AT LOWER SHEAR TIE FASTENER ABOVE STR 8R IAW B767 SRM 53-80-01 REPAIR 4 ADD RII INSP ACCOMPLISHEDSDR R61A202001020001Skin · dented2 DENTS WITH CREASES DISCOVERED AT LEFT FORWARD FUSELAGE BETWEEN FRAMES 1-2 AND STRINGERS 20L-24L. AC WAS REPAIRED IAW ETD 2019-170-164693A. MAJOR REPAIR/FCBS 53-10-00-004. AC WAS RETURNED TO SERVICE ON 01-02-2020.
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