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 CALA2021061800888Skin · corrodedFUSELAGE SKIN IS CORRODED AND BULGED AT THE LAVATORY BLOWER EXHAUST PORT. CORROSION IS ON INNER SKIN THAT IS SANDWICHED BETWEEN EXHAUST PORT NEEDS DISSASEMBLE FOR REWORK REMOVED AFT CARGO WASTE TANK PANELS 141SW, 141QW, 141PW AND 141 MW TO FACILITATE MAINTENSDR DALA2024080407742Skin · ground damageSHIP 3238 DISC: A/C WAS STRUCK BY BAGGAGE CART RESULTING WITH DENTS AND GOUGES ALONG LAP SPLICE BELOW STR 36, FROM FR10 - FR17. PREVIOUS REV B INSTALLED REPAIR DOUBLER AT FR 16. AT CURRENT CHECK EXISTING DEN TS AND GOUGE FOUND NEAR DOUBLER AT FR16. C/A: **DTE SDR K11A2021081800065Skin · crackedCRACK IN FUSELAGE SKIN @ A DOME NUT HOLE STA 530 BETWEEN STR 27L & 28LSDR REXA2021080600529Skin · gougedTOILET SERVICE DOOR AT FS365.00 IS HITTING THE FUSELAGE AND GOUGING IT. 900-53-900-105 - REWORK AND BLENDED IAW EA CRJ953-11795 REV IRSDR SWAA2021072684739Skin · crackedCRACK INDICATION ON EXTERNAL SKIN LOCATED AROUND FIRST FASTENER HOLE IN THE AREA UNDER DRAG LINK ASSEMBLY; COMMON TO THE BS540 BULKHEAD CHORD BETWEEN S-21L AND S-22L AT LOWER FUSELAGE ; 2021-269864 / [01] ACCOMPLISHED EA 5331-E-14519; [02] ACCOMPLISHED EA 5331SDR FDEA202106161713Skin · dentedLH FUSELAGE APPROX STA.1894 BETWEEN L43-L44 - DENT ON SKIN. REPAIRED DAMAGED SKIN REF SRM 53-20-00 FIG.6 SHEETS 12-13 VOL. 1 AND SRM 51-31-01 VOL. 2.SDR A6WA202107097820Frame · dentedAFT FUSELAGE FRAME DENT FS672.20Ï¿½ STR26R-S27. ***AIRCRAFT REMOVED FROM SERVICE*** HAND DRESSED FRAME AT AFT FUSELAGE FS672.20Ï¿½ STR26R-S27. DAMAGE MEASURES L = 1.300Ï¿½ X W = 0.700Ï¿½ X D = 0.048Ï¿½. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTSDR FDEA202106151543Skin · dentedFUSELAGE SKIN EXTERNAL SURFACE FOUND 1EA DENT AT STA1480 - STA1500, S23R - S24R REPAIRED THE DENT AT FUSELAGE SKIN EXTERNAL SURFACE STA1480 - STA1500, S23R - S24R PER EA F-5330-168309 A P4, EA TITLE: FUSELAGE - PLATE AND SKIN - SKIN PANEL DOUBLER REPAIR BESDR EE4Y2021071313372Skin · corrodedDURING THE STRUCTURAL INSPECTION IT WAS FOUND AT CENTER FUSELAGE III LOWER SKIN PANEL, EXTERNAL SKIN WITH CORROSION LOCATED BETWEEN FR86/87 AND BETWEEN STR- 27L/28L, THE DAMAGE WAS REPAIRED INSTALLING EXTERNAL DOUBLER REPAIR AS PER E.O. # COO-EO-2021-12988 R00SDR A6WA202107097823Skin · dentedAFT FUSELAGE SKIN DENT FS625.30 + 13.5Ï¿½ S24R AND S25. ***AIRCRAFT REMOVED FROM SERVICE*** HAND DRESSED DENT ON SKIN AT FS625.30 + 13.5Ï¿½ AND S24R AND S25R. MEASURES L = 0.650Ï¿½ X W = 0.500Ï¿½ X D = 0.005Ï¿½. HFEC PERFORMED WITH NO INDICATIONS. RESTORED SSDR REXA2021062900424Skin · gougedFUSELAGE OUTER SKIN GOUGED AT STGR 27 BETWEEN FS 897.00 AND FS 913.00. REPAIRED PER ENDEAVOR EA CRJ953-11713, REV. IR DATED 6/8/21. REPAIRED PER EA 953-11713 REV IR DATED 6-8-2021. REMOVED AND RE-INSTALLED BELOW FLOOR DISTRIBUTION DUCT IAW CRJ 900 AMM 21-23SDR SWAA2021061883197Skin · corrodedFUSELAGE SKIN BAS CORROSION AROUND WATER SERVIVE DOOR CUTOUT. BLENDED CORROSION. EVALUATED MATERIAL LOSS TO BE .004' ORIG .063' REMAINING .059' WITHIN LIMITS IAW SRM 53-00-01-1A-1. APPLIED ALODINE IAW AMM 51-21-41-370-803 & PRIMER IAW AMM 51-21-72-370-804. SDR IPXA2021061470560Skin · damagedINSPECTION TYPE:N/A**SUPPLEMENTAL SDR** IMPACT DAMAGE TO FUSELAGE SKIN, LONGERON, TEAR STRAP AND SHEAR CLIP.ACCOMPLISH REPAIRS IN ACCORDANCE WITH EO MD11-5310-80619-ASDR MK1Y20210614002Skin · damaged: FUSELAGE SKIN, SEC 43, STA 616, STR 30R: MAINTENANCE FOUND EXISTING BLEND OUT ON FUSELAGE EXTERNAL SKIN THAT IS NOT PERMITTED IAW SRM 53-00-01, FIG 101, ADL 1, TABLE I, DETAIL II.SDR MK1Y20210614001Skin · damagedFUSELAGE SKIN, STA 1351-STA 1375, STR 29R-30R AND STA 1417-STA 1427, STR 32L-33L: THIS REA INCLUDES SEVERAL NRC’S: M0049, M0051, M0063. MAINTENANCE FOUND EXISTING BLEND OUTS ON FUSELAGE EXTERNAL SKIN THAT IS NOT PERMITED IAW SRM 53-00-01, FIG 101, ADL 1, TABLESDR MASA20210706266Skin Splice · corrodedCORROSION ON SKIN SPLICE FS280 BTW STGR 24R TO 25L AT E/E COMPARTMENT. (E/E).CORROSION ON SKIN SPLICE FS=280 BTW STGR 24RH TO 25LH WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 PAR.5-D AND SRM 53-00-01-101-001-A01 PAR. 4SDR DALA2021061803316Skin · dentedSHIP 1811 RAMP REPORTED 2 DENTS FORWARD OF 2L DOOR. 6FT FWD AND 3 FT LOWER OF 2L DOOR PERFORMED DVI OF DENTS PER SRM 53-00-01. C/W ERA 592193-14. (LP 7837700)SDR CALA2021061400860Skin · scratchedSURFACE SCRATCH ON L/H CAPT STATIC PORT. ON AAR NR 99905150 BLENDED AREA @ L/H CAPT STATIC PORT SKIN ORIGINAL MAT 0.080 ALLOWABLE MAT LOSS .003, MAT LOSS 0.002, MAT REMAINING 0.078 FOUND TO BE WITHIN LIMITS IAW B737-900 SRM 53-30-01 TABLE 101.SDR SWIA202160511Doubler · corroded*CORROSION ON ANTENNA MOUNT DOUBLER ON STGR 27 BETWEEN FS 295.00 - 310.00 (C-CHECK RO 8/18/2021) REMOVED AND REPLACEDWITH NEW ANTENNA MOUNT DOUBLER AT STR 27 BETWEEN FS295.00-310.00 REF CRJ 900 SRM 51-42-06-001-001-A01 DRAWING SH670-32364 REV A. LEAK CHSDR DALA2021061503266Skin · cracked(LOG 1838175) DURING INSPECTION FOUND CRACK AND DEFORMED ON FWD FUSELAGE CUTOUT OF EXTERNAL POWER RECEPTACLE ACCESS DOOR. ELECTRICAL GROUND POWER RECEPTACLE SURROUND DOUBLER WAS REPAIRED PER B737-800 SRM 53-10-15-2R REPAIR 5 FIG. 203 AND REPAIR 4.SDR CALA2021061400857Skin · damagedSUPPORT TASK: FOUND AIRCRAFT DAMAGE AFT OF R2 DOOR ON SKIN (UNPR ESSURIZED AREA). REPAIRED SKIN BETWEEN FR72-73 STQR 24RHIAW EA 210070AND EC/RA NO 5351-01181. WORK ACCOMPLISHED ON AAR NR 99897653 BY TECH V920656 AND AAR QC V895387. RII INSPECTION PERFORMED BY SDR CALA2021061400855Skin · corrodedB767-06-3-7022 - FX STA 1219 S38L AREA FOUND SUSPECT CORRODED. R EF N/R L/P 9130407 GENERATE A DIP FOR INSPECTION REQUIREMENT AS PER EC/RA 5360-0160 3 REV-PART 2 ADD EMP:V896876 FUSELAGE SKIN STA1219 STR38L INTERIM REPAIRED AS PER EC/RA5360-0 1603 REV-PART1 ATSDR R61A2021062800511Skin · gougedCFIII EXTERNAL SKIN HAS GOUGE DAMAGE BETWEEN FR87-88 AND STR 23L-25L. REPAIRED EXTERNAL SKIN GOUGE DAMAGE IAW ETD2021-170-018776 REV.ASDR HNAA2021062400286Skin · damagedSMALL PROTRUSION ON EXTERNAL SKIN JUST FWD OF FRAME 24 BETWEEN STR 17R-18R. REPAIRED SMALL PROTRUSION ON EXTERNAL SKIN JUST FWD OF FRAME 24 BETWEEN STR 17R-18R IAW PIEDMONT EO1-05--21-0146, AND EMB145 SRM 53-22-01.SDR SWAA2021061482596Skin · crackedRAMP REPORTED A CRACK IN THE EXTERNAL POWER DOOR CUTOUT. / PERFORMED REPAIR 4--ELECTRICAL GROUND POWER RECEPTACLE SURROUND DOUBLER PER SRM 53-10-15-2R-4SDR U2RA2021061100021Skin · gougedFUSELAGE SKIN P/N 65B07657-8 AT BODY STATION 510, BETWEEN STRINGERS S22L AND S23L FOUND TO BE GOUGED. - ACCOMPLISHED INTERIM MAJOR REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING, INC ENGINEERING ORDER CONTROL NUMBER 21103-1 REVISION IR DATED 06/10/2021.SDR DALA2021061103195Skin · damaged(LOG 1836222) DURING INSPECTION FOUND TWO HOLES ON FUSELAGE SKIN WITH 0.093 IN OF DIAMETER LOCATED AT 0.031 IN TO THE HOLES PREVIOUSLY ADDED BY IDTV ANTENNA MODIFICATION AT FS 727E BTW STR 2L AND 2R. THE HOLES PREVIOUSLY ADDED BY IDTV ANTENNA MODIFICATION AT FSDR K11A2021081800064Skin · crackedCRACK IN FUSELAGE SKIN @ CHEM MILL AREA STA 518 BELOW STR 13LSDR SWIA2021081060209Skin · corrodedFS280-FS282.86 CIRCUMFERENTIAL JOINT HAS EVIDENCE OF CORROSION FROM STGR26R-STGR25R. (C-CHECK RO 8/6/2021) REPAIRED CIRCUNFERENTIAL JOINT AT FS 280.00 - FS 282.86 BETWEEN STGR 26R - STGR 25R REF REO 670-53-21-2066 REV -- DATED 2021-06-28 AND CRJ700 SRM SDR SWAA2021072681336Skin · crackedCRACK INDICATION LOCATED AROUND FASTENER HOLE ON FUSELAGE SKIN IN THE AREA UNDER THE DRAG LINK ASSEMBLY; COMMON TO THE BS540 BULKHEAD CHORD; BETWEEN S-21L AND S-22L. LOWER FUSELAGE. ; 2021-269663 / [01] ACCOMPLISHED EA 5331-E-14519-NG ON TTG8Q001PKAQ; [02] ACCSDR SWAA2021071981834Doubler · corrodedCORROSION ON SKIN DOUBLER AROUND BELLY DRAIN AT AREA AFT OF ACB BS949 BL0 WL174. ; / [01] REMOVED BELLY DRAIN SKIN DOUBLER AT BS949 BL0 WL174 IAW SRM 51-40-02-0G-0; [02] CORROSION DAMAGE ON SKIN DOUBLER AROUND BELLY DRAIN AT AREA AFT OF ACB BS949 BL0 WL174 WASSDR SWAA2021071981808Skin · corrodedCORROSION ON FUSELAGE SKIN AT AFT CARGO BAY BS727E+10 BL0 WL149. ; / [01] REMOVED DAMAGE IN ACB BS727E+10 BL0 WL149 IAW SRM 53-00-01-1A-5.[08] TRIMMED OUT DAMAGE IN ACB FUSELAGE SKIN BS727E+10 BL0 WL149 IN AN AREA OF 1.6'X 1.5' IAW SRM 51-10-02-0G-0; [09] VERISDR SWAA2021071981809Skin · corrodedCORROSION ON FUSELAGE SKIN AT AFT CARGO BAY BS727E+17 BL0 WL149. ; / [01] REMOVED DAMAGE ON FUSELAGE SKIN IN ACB BS 727E+17 BL0 WL149 IAW SRM 53-00-01-1A-5; [02] REMOVED DAMAGE IN AN AREA OF 1.5'X 1.3' IAW SRM 53-00-01-1A-5; [03] VERIFIED; [04] VERIFIED REMOVESDR SWAA2021071581785Doubler · corroded***CORROSION*** ON FRAME DOUBLER AT AREA AFT OF ACB BS952 S-19R WL193. ; / [01] REMOVED DAMAGE FROM FRAME DOUBLER BS 952; MATERIAL LOSS MORE THAN 10% FOUND TO BE OUT OF LIMIT PER SRM 53-70-15-1A-1 FIG 103; E. <BR><BR>REMOVED FRAME DOUBLER BS 952; RBL 42 PER SRSDR CALA2021061100829Skin · damagedAIRCRAFT FUSELAGE DAMAGE FROM GROUND EQUIPMENT AT STA 460 STR 36, 37L. REPAIRED REF ECRA 5330-06835 AND ENR # 000284628SDR CALA2021061100828Skin · damagedAIRCRAFT SUSTAINED FUSELAGE DAMAGE FROM GROUND EQUIPMENT AT STA 460 STR 36, 37L. REPAIRED REF ECRA 5330-06835 AND ENR # 000284628SDR 7C7A2012060900015Skin · damagedDAMAGE ON THE RH FUSE FWD OF THE RH EMERGENCY EXIT 1" AVOVE 23 FWD STA X201 REPAIRED RD8-53-17031SDR 7C7A2012060900014Skin · damagedEXTERNAL FUSELAGE RH SIDE STA X202 STR 21S SKIN NICKED REPAIRED RD8-53-4940SDR 7C7A2021060900012Skin · damagedRH EXT SKIN EDGE OF Y12 AND X115 RIVET LOOSE REPAIRED WITH RD 8-53-5099SDR 7C7A2021060900008Skin · dentedPERMANENT REPAIR FOR DENT RH FUSE 85310016 X182 -X201 STR 20S. REPAIRED RD8-53-16442SDR CALA2021060900822Skin · damagedB777-06-3-7176 - LH UPPER FUS STA212.5-STA220.5 AREA AFT OF FLIGHT COMPT WINDOW FOUND 1EA PREVIOUSLY BLEND. REF NR LP 9131391 LH UPPER FUSELAGE STA217 WL251.8 AFT AFT OF FLIGHT COMPT. WINDOW PREVIOUSLY BLEND AREA REPAIRED AS PER ECRA 5311-02578 REV- ATTAC H FOSDR SWIA202160729Skin · dented( ADM# N430SW-1750) 20 IN BELOW AFT SIDE OF CARGO DOOR MINOR DENT ROUGH MEASUREMENTS 2 IN L X 1 1/2 IN W X .02 IN D PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTICES. (C-CHECK RO 9/3/21SDR SWIA2021081060204Skin · corrodedFS280-FS282.86 CIRCUMFERENTIAL JOINT HAS EVIDENCE OF CORROSION FROM STGR25R-STGR23R. (C-CHECK RO 8/6/2021) REPAIRED CIRCUNFERENTIAL JOINT FS 280.00 - FS 282.86 BETWEEN STGR 23R - STGR 25R REF REO 670-53-21-2066 REV -- DATED 2021-06-28 AND CRJ700 SRM 51-SDR SWIA2021081060203Skin · corrodedFS280-FS282.86 CIRCUMFERENTIAL JOINT HAS EVIDENCE OF CORROSION FROM STGR24L-STGR23L. (C-CHECK RO 8/6/2021) REPAIRED CIRCUNFERENTIAL JOINT AT FS 280.00 BETWEEN STGR 24L - STGR 23L REF CRJ700 SRM 51-42-06-001-001-A01 AND CRJ700 SRM 51-21-06-001-001-A01 RESDR SWIA2021081060202Skin · corrodedFS280-FS282.86 CIRCUMFERENTIAL JOINT HAS EVIDENCE OF CORROSION FROM STGR26L-STGR26R. (C-CHECK RO 8/6/2021) REMOVED CORROSION AT FS280-FS282.86 CIRCUMFERENTIAL JOINT FROM STRG26L-STRG26R. FOUND TO BE WITHIN LIMITS PER MHIRJ REO 670-53-21-2066 REV -- DATESDR IXXA20210804044Skin · crackedIN COMPLIANCE OF TASK CARD 53-73-00-02 "GENERAL VISUAL INSPECTION OF EXTERNAL EXTERIOR SECTION 48 RIGHT SIDE" THE FOLLOWING FINDINGS WERE NOTED: AFT
RIGHT FUSELAGE SKIN SECTION 48 STATION 1654.5 ABOVE STRINGER 8R IS CRACKED. WORK IN PROGRESSSDR ASOA202107010182Skin · distortedDISCREPANCY - LEFT HAND SIDE FUSELAGE JUST AFT OF ENTRY DOOR AND FORWARD OF REPAIR HAS "OIL CANNING" AND DISTORTION THAT IS APPROXIMATELY 2 INCH'S SQUARE. CORRECTIVE ACTION - REPAIRED LEFT HAND SIDE FUSELAGE JUST AFT OF ENTRY DOOR IN ACCORDANCE WITH EMB 145 SRSDR R61A2021062800510Access Door · corrodedWASTE SERVICE ACCESS DOOR ASSY HAS CORROSION. WASTE SERVICE ACCESS DOOR REPLACED AS PER AMM 53-03-60.SDR JJBA20210608018Doubler · dentedAFTER DENT VISUAL INSPECTION, TOOL MARK AND RIVETS NOT PROPERLY INSTALLED ON PREVIOUS REPAIR DOUBLER AT FR 22-23, BTW STR 10R-12R. ON EXTERNAL SKIN AT FR 22-23, BTW STR 10R-12R LAYOUT COMPLETED FOR DOUBLER REPAIR. REPAIR DOUBLER AT FR 22-23, BTW 10R-12R. REPAISDR SWAA2021061481237Skin · gougedFUSELAGE SKIN GOUGED AT BS 847 - BS 852; 4IN BELOW STR 20R; WL 177 / ENTERED CALIBRATION INFO; APPLIED TOP FINISH TO REPAIR AREA. IAW AMM 51-21-00-100-801; VERIFIED APPLIED TOP FINISH TO REPAIR AREA. IAW AMM 51-21-00-100-801 <BR><BR>CARD COMPLETE
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