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 V0XR202311150001Skin · corrodedAFT RADIO ALTIMETER BASE AND FUSELAGE SKIN CORRODED. COMPLETED REPAIR IAW EMBRAER ETD2023-145-023314 REV.:/ INTERNAL AND EXTERNAL DET INSPECTION REQUIRED AT THRESHOLD OF 7,173 FC WITH INTERVAL OF 7,173 FC.SDR SWAA2023100396039Access Panel · crackedLOWER FUSELAGE ACCESS PANEL 193D LOWER SKIN SURFACE HAS CRACKS AROUND FASTENER HOLES.<[01] APPLIED REPAIR. AT PANEL 193D PER B737 SRM 53-40-70-2R-1 ; B737 SRM<BR>51-70-04-2R-9 AND B737 SRM 51-70-04-2R-0 PARAGRAPH (4.L.7 & 4.N.2) TOOL USED TEMPERATURE CONTROL ISDR SWAA2023100396040Access Panel · damagedLOWER FUSELAGE ACCESS PANEL 193B LOWER SKIN SURFACE HAS SEVERAL ELONGATED HOLES.<[01] APPLIED REPAIR. AT PANEL 193B PER B737 SRM 53-40-70-2R-1 ; B737 SRM<BR>51-70-04-2R-9 AND B737 SRM 51-70-04-2R-0 PARAGRAPH (4.L.7 & 4.N.2) TOOL USED TEMPERATURE CONTROL ID 160SDR SWIA20230907831Unknown · dentedTRANSFER FROM EAML 1202516 : -1 AREA OF DENT DAMAGE TO EXISTING DOUBLERS REPAIR (GREO601R-53-21-180, REF) ON SKIN PANEL (DWG: 601R31062, REF) LOCATED BETWEEN STR 15 €“ STR 16 AND AT FS310.00. DENT AFFECTS ENTIRE STACKUP OF REPAIR AND MEASURES 0.5€? (L) X 0.2SDR DALA2023090507180Unknown · unknownLOWER SKIN PANEL ASSY 5911401-537 DAMAGED DRUING LANDING. REMOVED -537 SKIN ASSY PER DWG 5911401. LOCATED AND DRILLED NEW SKIN ASSY PER DWG 5911401. APPLIED TOP COAT TO ASSEMBLY PARTS PER B717 SRM 51-22-01. INSTALLED DOUBLERS TO SKIN PER DWG 5911401. PRIMED EXSDR V0XR20231117AV1Skin · corrodedREAR FUSELAGE I LOWER SKIN AT RADIO ALTIMETER CORRODED BETWEEN FRAMES 65-66 REPAIRED IAW EMBRAER ETD2023-145-023822 REV.:/SDR YENA2023090101018Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION ON EXTERNAL FUSELAGE SKIN AND FASTENERS AT AREA COVERED BY LIVE TV RADOME; REMOVED CORROSION FROM AREA UNDER LIVE TV RADOME FOUND TO BE WITHIN ALLOWABLE LIMITS BUT CORROSION ON DOUBLER WAS FOUND OUT OF LIMITS. REMOVED AND RESDR YENA2023090101014Unknown · unknownDURING HEAVY MAINTENANCE: FUSELAGE / CTR FUSELAGE II / UPPER SKIN / LIVE TV RADOME AREA / BTW FR 63-64 / STGR 01L & STGR 02L / PREVIOUS DOUBLER / PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)SDR DALA2023083107109Unknown · unknownSHIP 3126 ELONGATED HOLE INTERNAL SKIN LOC FR 73 STR 31R TO 31L SHEAR TIE (4 EA) AND TIE CLIPS (4 E/A) IN THS COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE (4EA) AND CLIP (4EA) AND FASTENER LOC FRAME 73 AND STR 31R TO STR 31L ON THS COMPARTMENT AS PER A31SDR CALA2023100903005Skin · damagedREMOVED DAMAGED UPPER SKIN @ S-24-R AND APROX STA 216 TO 226 PER AVO11125 STEP 3. C/W AVO11125 REV A. VERIFIED REMOVED DAMAGED UPPER SKIN S-24-R AND APROX STA 216 TO PERFORMED 737 NDT PART 6, 51-00-00 TO VERIFY CRACK FREE AREA OF 226 PER AVO11125 STEP 3 IAW ASDR CALA2023100602986Skin · damagedREMOVED DAMAGED TO LOWER SKIN @ S-24-R AND STA 203-229 PER AVO11125 REV A. COMPLIED WITH ALL STEPS OF AVO11125 REV.A PER AVO11125 REV.C. STEP C.5. REMOVED LOWER LOBE SKIN FROM STA.178 TO STA.259.5. ACP. RII INSPECTION IAW GMM 09-25-05 & AVO11125. ACP STEP 11 CSDR CALA2023100602970Bear Strap · damagedBEAR STRAP AROUND NOSE GEAR DOORS AND FWD ACCESORY DOOR BENT AND DEORMED @ STA 224.8 AND BELOW S-24-R. C/W AVO11125 REV A. AVO 11152 STEP 4&5 ACCOMP RII HFEC SURFACE INSP OF EXPOSED BEAR STRAP PER NTM 6 51-00-00 PRO 23 NO CRACKS FOUND. STEP 5 ACCOMP RII HFEC SDR DALA2023090607255Unknown · unknownSHIP 1201 DT INSPECTIONS FOR DOUBLER INSTALLED BETWEEN STA 1395 / STA 1351 & STR 26R / STR 30R AND LAP SPLICE LOCATION AT STR 26R IN THE VICINITY OF THE REPAIR. CORRECTIVE ACTION: ADJUSTING THRESHOLD CYCLE LIMIT TO COUNT CYCLES FROM LP CREATION DATE 29AUG23. (SDR CALA2023090402706Bear Strap · deformedBEAR STRAP AROUND NOSE GEAR DOORS AND FWD ACCESORY DOOR BENT AND DEFORMED @ STA 224.8 AND BELOW S-24-R. C/W AVO11125 REV A. AVO 11152 STEP 4&5 ACCOMP RII HFEC SURFACE INSP OF EXPOSED BEAR STRAP PER NTM 6 51-00-00 PRO 23 NO CRACKS FOUND. STEP 5 ACCOMP RII HFECSDR CALA2023090402705Bear Strap · deformedBEAR STRAP AROUND NOSE GEAR DOORS AND FWD ACCESORY DOOR BENT AND DEFORMED @ STA 224.8 AND BELOW S-24-R. C/W AVO11125 REV A. AVO 11152 STEP 4&5 ACCOMP RII HFEC SURFACE INSP OF EXPOSED BEAR STRAP PER NTM 6 51-00-00 PRO 23 NO CRACKS FOUND. STEP 5 ACCOMP RII HFECSDR DALA2023090107131Unknown · unknownSHIP 1201 SKIN REPAIR TO BE ACCOMPLISHED PRIOR TO NEXT C CHECK PER SECTION III OF ER/A 546194-14 REV D BETWEEN STA1395/STA1351 & STR26R/ STR30R. CORRECTIVE ACTION: ACCOMPLISH SECTION III INSTRUCTIONS AT NEXT C CHECK FROM REVISION D APPROVAL DATE. (2942894)SDR DALA2023083007066Unknown · unknownCORROSION ON WASTE BOX DOUBLER RIGHT SIDE AND AFT SIDE. -M-. 001-0244:2021-2025/001 00020 COMPLIED WITH ER/A 611382-14 PRI REV 0, ER/ A 611382-14 PRI REV 1, ER/A 611382-14 PRI REV 2 AND FINAL ER/A 611382-14 REV OR IGINAL. CLOSING REQUIREMENTS RII: INSPECTOR 00SDR VNAA20230829001Skin · corrodedDISCREPANCY: FUSELAGE SKIN IS CORRODED UNDER FOOTPRINT OF PANEL 196DR AT STR 27.SDR VNAA202308290011Skin Splice · corrodedSKIN SPLICE STRAP IS CORRODED AT FS 333 BETWEEN STGR 27 AND STGR 26R.SDR SWIA20230920828Unknown · dentedTRANSFER FROM EAML 1199891 : FOUND DENT TO MEASURE 7"L X 2.75"W X 0.080"D, WITH SEVERAL PAINT SCRATCHES ON FUSELAGE SKIN PANEL (DWG. 601R33010, 0.043" THK IN AFFECTED CHEM-MILL AREA, REF) BETWEEN FS265 - FS280 AND STR. 21L - STR.22L. DAMAGE IS OUT OF LIMITSDR CALA2023083002671Skin · damagedFUSELAGE SKIN FR73-FR74, STRINGER 31L TO 31R CREASED - INTERIM REPAIR ACCOMPLISHED REF EC/RA 5351-01212. OR BEFORE A/C REACHES 35,932 TOTAL FLIGHT CYCLES, 82,693 TOTAL INSP NOT TO EXCEED INTERVALS OF 120 FLIGHT CYCLES THEREAFTER. FLIGHT HRS OR 21-SEP-24 WHICHESDR SWIA202308290028Unknown · dentedTRANSFER FROM EAML 1199891 : FOUND DENT TO MEASURE 7"L X 2.75"W X 0.080"D, WITH SEVERAL PAINT SCRATCHES ON FUSELAGE SKIN PANEL (DWG. 601R33010, 0.043" THK IN AFFECTED CHEM-MILL AREA, REF) BETWEEN FS265 - FS280 AND STR. 21L - STR.22L. DAMAGE IS OUT OF LIMITSDR DALA2023082907027Unknown · unknownSHIP 3414 MTC IN CDG FOUND A DENT COMMON TO THE SKIN PANEL (P/N F5348704221000) JUST FORWARD OF FR 77 AND BETWEEN STR 43R AND 44R. THE DENT MEASURES 63.5MM FWD/AFT BY 45.7MM IN THE CIRCUMFERENTIAL DIRECTION, WITH A MAXIMUM DEPTH OF 6.3MM BEFORE PAINT REMOVAL. SDR HNAA2023101000360Unknown · unknownE993554 INTERNAL DOUBLER IS CORRODED BETWEEN FRAMES 61-62 STRINGERS 19L-20L. FABRICATED AND INSTALLED SERVICEABLE INTERNAL DOUBLER FOR INSTALLATION BTW FR 61-62 STGR 19L-20L IAW ETD# ETD2023-145-023886AND EO1-53-23-0290.SDR SWI2023F00305Unknown · damagedFORWARD FUSELAGE EXTERNAL SKIN HAS LIGHTNING STRIKE DAMAGE BETWEEN FRAME 10-11 AT STRINGER 12R. (C-CHECK RO 9/3/2023) PERFORMED PERMANENT DOUBLER REPAIR ON FWD FUSELAGE SKIN FR 10-11 STR 12R REF. SRM 53-10-01/REPAIR 15P. TOTAL WEIGHT OF DOUBLER REPAIR, SDR GTIA2023082837443Skin · damagedREF 3318852-1 DURING AIRCRAFT JACKING DENT CREATED AT AFT JACK SAFETY AREA FR 71-76. DAMAGE MEASUREMENTS FR73 BETWEEN STR 25L-25R 16", FR74 BETWEEN STR 25L-25R 25.5", STR 32L 65", STR 32R 46.5". RAF CREATED-PERFORMED REPAIR IN AFT JACK SAFETY AREA FR 71-76 IAWSDR R61A2023082700459Skin · gougedDURING HEAVY CHECK, TEMP REPAIR ON L/H FUSE FR21 AND FR22 TO STR 14L AND 16L REQUIRES PERMANENT REPAIR WITHIN 7500FC PER ETD2021-170-025518 REV C. : L/H FUSE FR21 AND FR22 AND BETWEEN STR 14L AND 16L PERMANENT REPAIR HAS BEEN ACCOMPLISHED IAW ETD2021-170-02551SDR DALA2023082907040Unknown · unknownSHIP 0692 SECONDARY NRC IN REF NRC #00546: CRACK ON AFT LAV SERVICE PAN, CORRECTIVE ACTION: SUMMARY OF NRC 00585: AFT LAV SERVICE PAN WAS REPAIRED PER ER/A 611426-14. (2937766)SDR CALA2023082802656Skin · damagedRIGHT SIDE AIRCRAFT DAMAGED. DAMAGE IS LOCATED AT STA. 344 BETWEEN STRINGERS 21R AND 22R. C/W AVO011117 REV. A STEP 8. PERFORMED HFEC INSPECTION ALONG THE TRIM EDGE REF. NDT PART 6, 51-00-00 PROC. 23. NO DAMAGE NOTED. TRIM-OUT DAMAGE AREA AND COMPLY WITH AVO11SDR CALA2023082802654Skin · dentedLOWER FUSELAGE EXTERNAL SKIN HAS 2 EA SMALL DENTS AT FR26 FR27 STR 42L STR 43L PER HAECO LCQ N/R 9296868/36868 DIM.1.5"X .875" AND RPR DBLR IAW SRM 53-21-11-300-076. REQUIRES EMBODIMENT IAW SRI 53-21-11-205-060 TABLE 1. THIS IS A CAT B INSP AT 60,000 FC/ 120,0SDR SWI2023F00304Unknown · damagedFWD FUSELAGE EXTERNAL SKIN HAS EVIDENCE OF LIGHTNING STRIKE DAMAGE AT FR 18; STR 5R-6R; IN BAY. (C-CHECK RO 9/3/2023) PERFORMED THROUGH HOLE REPAIR ON LIGHTNING STRIKE DAMAGE AT FR 18, STR 5R-6R REF. SRM 53-10-01/AD03. SEE CONTINUATION CARD FOR FURTHER SDR SWI2023F00303Unknown · damagedFWD FUSELAGE EXTERNAL SKIN HAS EVIDENCE OF LIGHTNING STRIKE DAMAGE AT FR 22; STR 4R-5R; IN BAY. (C-CHECK RO 9/3/2023) PERFORMED LIGHTNING STRIKE PERMANENT REPAIR ON FWD FUSELAGE SKIN FR 22, STR 4R-5R REF. SRM 53-00-00/REPAIR 03P. SEE CONTINUATION CARD SDR SWIA20230825Unknown · damagedFWD FUSELAGE EXTERNAL SKIN HAS EVIDENCE OF LIGHTNING STRIKE DAMAGE AT FR 13; STR 11R-12R; ON RIVET LINE. (C-CHECK RO 9/3/2023) PERFORMED LIGHTNING STRIKE PERMANENT REPAIR ON FWD FUSELAGE SKIN FR 13, STR 11R-12R REF. SRM 53-00-00/REPAIR 03P. SEE CONTINUASDR DALA2023082907047Unknown · unknownSHIP 0692 FUSELAGE / SKIN / ACCESS COVERS / AFT LAVATORY SERVICE PANEL PAN / BS 1681 TO BS 1701, STR 26R TO 29R / CRACKS. CORRECTIVE ACTION: REF ERA 611426-14. (2936748)SDR DALA2023082907024Unknown · unknownSHIP 3361 WHILE IN DTW, MTC REPORTED DAMAGE TO SKIN P/N F5347928020300, THE DAMAGE CONSISTS OF A DENT WITH GOUGE LOCATED BETWEEN FR72 AND FR73 AND STRINGERS 29R AND 30R. DAMAGED AREA WAS CUT OUT PER A330-200 SRM 53-41-11-300-015, AND FINAL CUT OUT AREA IS 4.0"SDR DALA2023082806942Unknown · unknownSHIP 3278 DENT EXTERNAL SKIN LOCATED FR8 TO FR9 8 INCHES ABOVE LOWER RH SIDE STRINGER LOWER FUSELAGE. CORRECTIVE ACTION: INSPECTED AND FOUND WITHIN LIMITS. CONTINUE ON REPEAT MONITOR. (2936582)SDR DALA2023082506925Unknown · unknownSHIP 3166 DAMAGE TO 191BB PANEL LEADING EDGE. CORRECTIVE ACTION: REPAIRED PER. A319 SRM 53-35-11-300-036. (4928074)SDR AALA202311130327Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TRAILING EDGE TOP SKIN PANEL UPPER SURFACE AT AILX 1157.630 AND RIB 24. REPAIRED SKIN PANEL PER EA 348318 .SDR SWAA2023092593244Skin · corrodedSURFACE CORROSION ON UPPER CROWN SKIN UNDER VERT STAB FUSELAGE STA 1016 TO STA 1040 AND FROM STRINGERS S-2AR TO S-2AL.<[01] REMOVED FASTENERS BETWEEN BS1016- BS1040 FROM STR2AL-STR2AR IAW SRM 51-40-0<BR>1. ROIG; JOSUE (PENDING)<BR>01-SEP-2023 16:43:36<BR>EVALUSDR DALA2023082806972Unknown · unknown(LOG 2935049) DENT ON LH FUSLEAGE SKIN AT STA 367.25 AND 4" ABOVE STGR 27. DENT WAS REPAIRED IAW ERA 611057-14.SDR DALA2023082806971Unknown · unknown(LOG 2935042) DENT ON LH FUSELAGE SKIN AT STA 339.25 BETWEEN STGR 27/28. DENT WAS REPAIRED IAW ERA 611057-14.SDR DALA2023082806970Unknown · unknown(LOG 2935032) DENT ON LH FUSELAGE SKIN AT STA 349.75 AND 1" BELOW STGR 27. REPAIRED DAMAGE PER ERA 611057-14.SDR DALA2023082806969Skin · damaged(LOG 2934803) DAMGED FASTENER HOLE FOUND ON EXTERNAL FUSELAGE SKIN AT STA 500K +19, 2.5" BELOW STR 22R. C/W ER/A 611279-14 REV ORIGINAL.SDR DALA2023082506919Unknown · unknownSHIP 3274 INHIBIT INSPECTION BY EXISTING REPAIR (1EA) EXTERNAL FUSELAGE SKIN BTW FR47 TO FR70 FROM STR23 LH/RH TO BOTTOM CENTERLINE. CORRECTIVE ACTION: COMPLIED WITH ERA 611050-14AD, REV. ORIGINAL. (2934454)SDR DALA2023082506916Unknown · unknownSHIP 3274 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED BTW FR 63 TO FR 64 AND STR 21L TO STR 22L UPPER FUSELAGE. CORRECTIVE ACTION: REINSPECTED REPAIR. OK FOR SERVICE. (2934924)SDR DALA2023082506912Unknown · unknownC/W ERA 610811-14 INTERNAL DOUBLER FABRICATION DAMAGED DURING LANDING. C/W PRI 610811-14 REV 0. C/W ERA 610811-14 REV ORIG. PRI REV 0 MATCHES FINAL ERA. (LP #2934596)SDR VNAA202310080001Skin · dentedSEVERAL DENTS ON FUSELAGE SKIN, SETTLEMENT AREA OF LEFT AND RIGTH VENTRAL FIN FAIRING BTW FS 1069.75 TO REAR SPAR DATUM STABILIZER 67.5%. DENTS ON FUSELAGE SKIN, SETTLEMENT AREA OF LEFT AND RIGTH VENTRAL FIN FAIRING BTW FS 1069.75 TO REAR SPAR DATUM STABILIZESDR DALA2023082406894Unknown · unknownSHIP 3278 DENT EXTERNAL SKIN BTW FR 21 TO FR 23 AND BTW STR 24L TO STR 25L LOWER FUSELAGE. CORRECTIVE ACTION: FOUND TO BE WITHIN LIMITS. (2933330)SDR DALA2023082406885Unknown · unknownCRACK ON UPPER EXTERNAL SKIN PROTECTION STA Y=1200 (CANTED FRAME) AT PYLON OF RH ENGINE. SUMMARY OF NRC 00066; UPPER EXTERNAL SKIN PROTECTION STA Y=1200 (CANTED FRAME) AT PYLON OF RH ENGINE WAS REPAIRED PER B717-200 SRM 54-00-00-2R PROCEDURE 1 REPAIR 1. (LP #2SDR SWIA2023102300822Unknown · crackedPOSSIBLE CRACK PRENSENT ON SKIN AT LOWER LOWER FORWARD CORNER BELOW AFT LATCH OF LH FWD EQUIPMENT COMPARTMENT DOOR. (C-CHECK RO 10/21/2023) REMOVED AND INSTALLED NEW DOOR LAND SKIN PN 600-33052-145@.PER CRJ 200 SRM 51-42-06 , REO 601R-53-11-3887 REV -- DAT
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