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 DALA2020091903127Skin · damagedNICK EXTERNAL SKIN BETWEEN STRG 42L AND STRG 43L AND 4.5 INCH AHEAD OF FR 26 AT LOWER FUSELAGE (2 EA). CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN BETWEEN STR 42L AND STR 43L AND BETWEEN FR 23 TO FR 23 AT LOWER FUSELAGE, AS PER PRI 587690-1SDR SWIA202053639Doubler · corrodedMAIN AVIONICS BAY TCAS ANTENNA DOUBLER CORRODED BETWEEN FS 295.00 AND FS 310.00. C-CHECK RO 10/22/2020. REMOVED CORRODED TCAS ANTENNA DOUBLER BETWEEN FS 295 TO FS 310 AND INSTALLED NEW, REF CRJ700 SRM AND DWG. NO LEAKS NOTED. COMPLIED WITH TASK CARD. COMPSDR SWAA2020100619897Skin · dentedFUSELAGE SKIN HAS A DENT LOCATED AT BS 235+5'; 19' ABOVE S-17R. DENT MEASURES AT L=4'; W=2.5'; Y=.030'; W/Y=83. THE DAMAGE IS REPAIRED, PER EA 20-153-01901 REV IR (ATS ER 20-03299 REV IR). REFER TO NRC U213260 FOR TRACKING.SDR SWAA2020100619899Skin · dentedFUSELAGE SKIN HAS A DENT LOCATED AT BS 235+1'; 21.8' ABOVE S-17R. DENT MEASURES AT L=2'; W=3.8'; Y=.022'; W/Y=59. THE DAMAGE IS REPAIRED, PER EA 20-153-01901 REV IR (ATS ER 20-03299 REV IR). REFER TO NRC U213260 FOR TRACKING.SDR SWAA2020100516972Skin · corrodedCORROSION UPON REMOVAL OF AFT DRAIN MAST, FOUND EXTERNAL SKIN CORROSION. BS 992 TO BS 996 BETWEEN S-24L AND S-25L LBL 25. REPAIR ACCOMPLISHED, PER ATS ER NR 20-03297 REV IR & EA NR 20-153-01791 REV IR DATED 29-SEP.2020.SDR SWAA2020100519895Skin · dentedFUSELAGE SKIN DENT LOCATED AT BS 211+3'; 20' ABOVE S-17R. DENT MEASURES AT L=4.5'; W=4'; Y=.130; W/Y=30. REPAIRED FUSELAGE SKIN, PER EA 20-153-01905 REV IR (ATS ER 20-03304 REV IR).SDR SWAA2020100519896Skin · dentedFUSELAGE SKIN HAS A DENT LOCATED AT BS 224+4', 17' ABOVE S-17R. DENT MEASURES AT L=8'; W=3.8'; Y=.125'; W/Y=30. THE DAMAGE IS REPAIRED, PER EA 20-153-01901 REV IR (ATS ER 20-03299 REV IR).SDR SWAA2020100519898Skin · dentedFUSELAGE SKIN HAS A DENT LOCATED AT BS 243+1', 19.5' ABOVE S-17R. DENT MEASURES AT L=4.2'; W=1.7'; .Y=040'; W/Y=42. THE DAMGE IS REPAIRED, PER EA 20-153-01901 REV IR (ATS ER 20-03299 REV IR). REFER TO NRC U213260 FOR TRACKING.SDR SWAA2020100619066Skin · dentedFUSELAGE SKIN HAS DENT BS 440+6' 1' ABOVE STR 18L. REPAIRED PER SRM 53-00-01-2R-36 (REPAIR 36). UPON FURTHER INVESTIGATION DENT WAS FOUND TO BE A PREVIOUS BLEND. BLEND MEASURED 1. X .9' X .007' ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMITS, PER SRM 53-SDR DALA2020091603087Skin · dentedDURING INITIAL INSPECTION FOUND DENT AND PROTUBERANCE ON EXTERNAL FUSELAGE SKIN FS 620, S16L NEAR TO PREVIOUS REPAIR. EXTERNAL FUSELAGE SKIN FS 620 S16L WAS REPAIRED PER ER/A 587829-14.SDR SWAA2021081616403Skin · corroded***CORROSION*** ON FUSELAGE SKIN UNDER DORSAL FIN BS887 - BS967 S-2L TO S-2R WL306. / REPAIRED DAMAGE ON FUSELAGE SKIN UNDER DORSAL FIN BS 887-967 STR 2L TO 2R; WL 306 PER ER 20-03307 REV IR AND EA 20-153-01902 REV IR.SDR SWIA202053756Fastener · missingFUSELAGE SKIN FASTENERS JUST FORWARD OF FS 202.75 AND BELOW WL 79.50 ON THE RT SIDE ONE (1 EA) FASTENER HEAD MISSING, THREE (3 EA) SUSPECTED TO BE LOOSE. C-CHECK RO 10/29/2020. THE LOOSE FUSELAGE SKIN RIVETS JUST FORWARD OF FS 202.75 HAVE BEEN REPLACED, REF SDR SWIA202053702Skin · dentedTHE FUSELAGE SKIN AT APPROXIMATELY FS 349, BETWEEN STGR 3L AND STGR 11L AT THE EDGE OF THE PAX DOOR CUT-OUT HAS A DENT THAT APPEARS TO ALSO BE GOUGED UNDER A PREVIOUS TOPCOAT OF PAINT. C-CHECK RO 10/29/2020. REMOVED DAMAGED SKIN AND PERFORMED A FLUSH REPAIR.SDR SWIA202053546Skin · corrodedEXTERIOR SKIN CORRODED BETWEEN STGRS 26L AND 25R AT FS 559+112, AS MARKED. C-CHECK RO 10/20/2020. BLENDED OUT EXTERIOR CORROSION ON EXTERIOR SKIN BETWEEN STGRS 26L AND 25R AT FS 559+112, AS MARKED, REF CRJ 200 SRM. REPAIRED EXTERIOR SKIN BETWEEN STGRS 26L ASDR SWIA202053340Skin · corrodedFS 559.00+80-FS 559.00+112 STRG 22RH TO 23RH, CORROSION ON EXTERIOR SKIN IN SEVERAL PLACES AROUND LAV SERVICE AREA, MARKED. C-CHECK RO 10/13/2020. CORROSION DAMAGE BLENDED/REMOVED FROM EXTERNAL FUSELAGE SKIN, AS MARKED. FS 559.0+112 STR 22R-23R, REF CRJ 200SDR SWIA202053326Skin · chafedLOWER CENTER WING PLANK EXTERIOR, APPROXIMATELY WS 45.0 LT AFT EDGE CHAFED, MARKED. C-CHECK RO 10/13/2020. REPAIRED LOWER WING PLANK AT LBL 45, AS MARKED REF REO. BLENDED AREA LOCATED WITHIN .150" OF A FASTENER. COMPLIED WITH TASK CARD.SDR SWAA2020100518821Skin · gougedFCD SKIN HAS A GOUGE LOCATED 24' FROM THE TOP EDGE AND 17' FROM AFT EDGE. REPAIRED FWD SKIN LOCATED 24' FROM THE TOP EDGE & 17' FROM AFT EDGE HFEC. NO DEFECT NOTED, IAW SRM 52-00-01-2R-2 REPAIR 2 & NDT 737 PART 6 51-00-00 PROC 23.SDR HNAA2020092400267Skin · damagedMULTIPLE RIVETS ON FR 78 BETWEEN STR 5L-8L HAVE POSSIBLE CRACKS (2 TOTAL). PERFORMED DYE PENETRANT INSPECTION, IAW EA SI NDTM 1. RELEVANT INDICATION NOTED SKIN CRACK ENDS, MARKED, RADIOMETER EASI 0452. COMPLETE: CUTOUT DAMAGE AREA ON FR 78 BETWEEN STR 6L-7LSDR YENA2020092200463Skin · dentedDURING HEAVY MAINTENANCE: DENT EXTERNAL SKIN BETWEEN FR 25-FR 26 AND BETWEEN STR 44-43, REF ARM W/O 2020-278/1 N/R 2020-270537. PERFORMED PERMANENT REPAIR DOUBLER LOCATED BETWEEN FR 25 TO FR 26 AND STRG 41L TO STRG 43L, IAW SRM A320-53-00-11-300-029 PROCEDURESDR SWIA202053543Skin · dentedFS 559+112 TO FS 755.0 EXTERIOR BELLY SKIN HAS SEVERAL DENTS. C-CHECK RO 10/20/2020. REPAIRED FS 559+112 TO FS 755.0 EXTERIOR BELLY SKIN, REF MHI RJ REO AND PRESSURE CHECK GOOD. SEE CONTINUATION CARD FOR DETAILS.SDR MASA20200915062Skin · puncturedPUNCTURE/DAMAGE RT FUSE NOSE ADG SKIN. R & R UPPER RT SIDE SKIN PN-CC670-33107-2, UPPER CHANNEL PN-CC670-33260-3, INTERCOSTAL PN-CC670-3356-3, STIFFENER PN-CC670-3367-1 ADG SKIN PANEL CC670-33109-5 IAW SRM 51-42-06.SDR ABXR2020091400097Skin · corrodedCORROSION FOUND BETWEEN FS 1375 AND 1417 STR 35R AND 36R. BLENDED CORROSION BETWEEN STA 1375 TO 1417 STR 35R TO 36R. ORIGINAL THICKNESS .074", REMOVED .041", REMAINING T .033" FOUND TO BE OUT OF LIMITS. REQUESTED ENGINEERING SUPPORT. RECEIVED AMES DOC 4741SDR ABXR2020091400095Skin · damagedFUSELAGE SKIN IS CREASED AT STA 676 STRINGER 7L. FUSELAGE SKIN CREASED AT STA 676 7L FOUND TO BE OUT OF LIMITS, IAW B767 SRM 53-00-01 DETAIL III. REPAIRED AREA IAW AMES DOCUMENT #47416REA17.SDR ABXR2020091400094Skin · corrodedCORROSION ON INTERNAL FUSELAGE SKIN STA 783 ABOVE STRINGER 13R. REMOVED CORROSION FROM INTERNAL FUSELAGE SKIN AT STA 783 ABOVE STR 12R, IAW B767 200 SRM 53-00-01 AD 1. WITH 0.027" MAT LOSS, DAMAGE EXCEEDED 15% ALLOWED & FOUND TO BE OUT OF LIMITS. REPAIRED DSDR ABXR2020091400084Skin · corrodedBULGE IN SKIN AT FS 1395 AND STR 35L. REPAIRED SKIN AT FS 1395 S35L, IAW AMES REA 47416 REA 02 AND B767 SRM 53-00-01 REPAIR 12.SDR ABXR2020091400083Skin · corrodedCORROSION ON SKIN AT FASTENER FS 785 STR 38R. REMOVED CORROSION FROM SKIN AT FS 785 STR 38, IAW B767 200 SRM 53-00-01 FIG 1 DET II WITH ORIG MAT 0.150", MAT LOSS 0.052". FOUND TO BE OUT OF LIMITS, IAW B767 200 SRM 53-00-01. REPAIRED SKIN DAMAGE IAW 47416REASDR ABXR2020091400082Skin · corrodedDEFORMITY IN THE SKIN LEFT OF NLG DOOR ON FS 188.5 10" FROM DOOR OPENING. REMOVED DAMAGE AT STA 196.5 10" FROM DOOR OPENING AND REPAIRED, PER AMES DOCUMENT 47416REA07.SDR SWIA202053903Skin · corrodedFUSELAGE SKIN HAS CORROSION AROUND DRAIN HOLES BETWEEN BL 27-26 AT FS 559+14, +46 AND +94. C-CHECK RO 11/11/2020. REPAIR WAS ACCOMPLISHED IAW MHIRJ REO. NO CHANGE TO WEIGHT AND BALANCE, M-337 AND TASK CARD ATTACHED.SDR SWIA202053536Skin · dentedFUSELAGE DENT AT APPROXIMATELY FS 220 BETWEEN STR 22R AND STR 23R. C-CHECK RO 10/20/2020. REPAIRED FUSELAGE SKIN BETWEEN FS 220 BETWEEN STR 22R AND STR 23R, REF REO. SEE CONTINUATION CARD FOR DETAILS.SDR SWIA202053535Skin · dentedFUSELAGE DENT BETWEEN FS 250 AND FS 265 BETWEEN STR 24R AND STR 25R. C-CHECK RO 10/20/2020. REPAIRED FUSELAGE SKIN BETWEEN FS 250 AND FS 265 BETWEEN STR 24R AND STR 25R, REF REO. SEE CONTINUATION CARD FOR DETAILS.SDR SWIA202053534Skin · dentedFUSELAGE DENT BETWEEN FS 235 AND FS 250 BETWEEN STR 25L AND STR 26L. C-CHECK RO 10/20/2020. REPAIRED FUSELAGE SKIN BETWEEN FS 235 AND FS 250 BETWEEN STR 25L AND STR 26L, REF REO. SEE CONTINUATION CARD FOR DETAILS.SDR SWIA202053533Skin · dentedFUSELAGE 2 DENTS BETWEEN FS 250 AND FS 265 BETWEEN STR 24L AND STR 25L. C-CHECK RO 10/20/2020. REPAIRED FUSELAGE SKIN BETWEEN FS 250 AND FS 265 BETWEEN STR 24L AND STR 25L, REF REO. SEE CONTINUATION CARD FOR DETAILS.SDR SWIA202053532Skin · dentedFUSELAGE DENT BETWEEN FS 250 AND FS 265 BETWEEN STR 23L AND STR 24L. C-CHECK RO 10/20/2020. REPAIRED FUSELAGE SKIN BETWEEN FS 250 AND FS 265 BETWEEN STR 23L AND STR 24L, REF REO. SEE CONTINUATION CARD FOR DETAILS.SDR SWIA202053531Skin · dentedFUSELAGE DENT BETWEEN FS 265 AND FS 280 BETWEEN STR 23L AND STR 24L. C-CHECK RO 10/20/2020. REPAIRED FUSELAGE SKIN BETWEEN FS 265 AND FS 280 BETWEEN STR 23L AND STR 24L, REF REO. SEE CONTINUATION CARD FOR DETAILS.SDR SWIA202053530Skin · dentedFUSELAGE DENT BETWEEN FS 265 AND FS 280 BETWEEN STR 24L AND STR 25L. C-CHECK RO 10/20/2020. REPAIRED FUSELAGE SKIN BETWEEN FS 265 AND FS 280 BETWEEN STR 24L AND STR 25L, REF REO. SEE CONTINUATION CARD FOR DETAILS.SDR SWIA202053529Skin · dentedFUSELAGE DENT BETWEEN FS 265 AND FS 280 BETWEEN STR 25L AND STR 26L. C-CHECK RO 10/20/2020. REPAIRED FUSELAGE SKIN BETWEEN FS 265 AND FS 280 BETWEEN STR 25L AND STR 26L, REF REO. SEE CONTINUATION CARD FOR DETAILS.SDR DALA2020091103044Skin · gougedSHIP 3278, GOUGE EXTERNAL SKIN AT LEVEL OF FR23 AND STRG 23L ON UPPER FUSELAGE. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR INSTRUCTIONS ON EXTERNAL SKIN AT LEVEL OF STR.23L FR 23 ON UPPER FUSELAGE, AS PER PRI 587548-14 REV. 0 AND ER/A 587548-14 REV ORIGINASDR FXGA2020091402012Skin · corrodedCORRODED SKIN LAP AT F/STA 66, STRINGER 11L. TO REPAIR A CORRODED SKIN LAP AT F/STA 66, STRINGER 11L. CUT OUT DAMAGE AND REPAIR, PER EAC EO 0502, GENERIC REPAIR TO SKIN SAP SEAMS.SDR SWIA202053408Skin · corrodedFOUND CORROSION ON FUSELAGE EXTERNAL SKIN APPROXIMATELY FS 990 BETWEEN STGR 27 AND STGR 26L. C-CHECK RO 10/16/2020. COMPLIED WITH REO, ALL STEPS COMPLIED WITH ON FUSELAGE EXTERNAL SKIN APPROXIMATELY FS 990 STR 27-STR 26L.SDR SWAA2020092818356Skin · dentedFUSELAGE SKIN HAS A DENT AT BS 578+4.5'; 1.5' ABOVE S-4R. REPAIRED FUSELAGE SKIN DENT AT BS 578+4.5'; 1.5' ABOVE S-4R, PER EA 20-153-01719 REV IR AND ER 20-03260 REV IR.SDR SWIA2020091652495Skin · crackedFOUND CRACK INDICATION ASSOCIATED WITH THE DENT ON THE LT FUSELAGE JUST FWD OF FS 517.00 BETWEEN STGR 16L AND STGR 17L. FILED CLOSED. REPAIRED DENT ON THE LT FUSELAGE JUST FWD OF FS 517.00 BETWEEN STGR 16L AND STGR 17L IN ACCORDANCE WITH REO.SDR ABXR2020090900077Skin · corrodedCORROSION ON INTERNAL FUSELAGE SKIN AT BS 783, STRINGER 13 RIGHT.SDR SWIA202053633Skin · chafedAFT FUSELAGE EXTERNAL SKIN AT APPROXIMATEY FS 985.0 STGR 27 HAS 3 CHAFED AREAS, MARKED. C-CHECK RO 10/22/2020. BLENDED 3 CHAFED AREAS AFT FUSELAGE EXTERNAL SKIN AT APPROXIMATELY FS 985.0 STGR 27, REF REO. AREAS NR 1 & NR 2 ORIGINAL THICKNESS .118, NR 1 MATESDR SWIA202053499Skin · corrodedFOUND MINOR EXTERNAL SKIN CORROSION ON BELLY SKIN PANEL FS 559.00+92 TO FS 559.00+112 BETWEEN STGR 26L AND 26R. C-CHECK RO 10/18/2020. REPAIRED IAW REO. MAJOR REPAIR TASK & FORM M337 COMPLETED AND ATTACHED. NO MEASURABLE WEIGHT CHANGE. REFER TO CONTINUE SDR SWAA2020092417810Skin · dentedFUSELAGE SKIN HAS A DENT AT BS 203.8+4.5'; 4' BELOW S-17L. FUSELAGE SKIN DENT AT BS 203.8+4.5'; 4' BELOW S-17L. REPAIRED IAW ATS ER 20-03255 REV IR DATED 23-SEP-2020 AND PER EA NO:20-153-01830 REV IR. 55981U 23SEP20.SDR SWAA2020092417624Skin · dentedFUSELAGE SKIN HAS A DENT AT BS 827+8.5; 3.8' ABOVE S-7L. REPAIRED FUSELAGE SKIN DENT AT BS 827+8.5; 3.8' ABOVE S-7L, PER 737-700 SRM 53-00-01-2R-3 (REPAIR 3).SDR IPXA2020092160469Doubler · chafedINSPECTION TYPE: 2C LT UNDER WING FUSELAGE SKIN HAS CHAFE DAMAGE AT STA 1153 AND LONG 43L. REMOVED, FABRICATED, AND REPLACED DAMAGED DOUBLER AT STA 1153 AND LONG 43L, IAW SRM 53-40-01 REPAIR 2 FIG 202 (MAJOR).SDR A6WA202009187290Skin · damagedRT DME ANTENNA CUTOUT HAS SCRATCHES ON ANTENNA PAD AREA OF FUSELAGE SKIN. AIRCRAFT REMOVED FROM SERVICE. LOCATED AND BLENDED OUT DAMAGE WITH .001" MATERIAL REMOVED WITHIN REMAINING .054" MINIMUM SKIN THICKNESS CHECK. WITHIN ALLOWABLE LIMITS, REF AIR WISCONSSDR A6WA202009187289Skin · damagedLT DME ANTENNA CUTOUT HAS SCRATCHES ON ANTENNA PAD AREA OF FUSELAGE SKIN. AIRCRAFT REMOVED FROM SERVICE. LOCATED AND BLENDED OUT DAMAGE WITH .002" MATERIAL LOSS AND A MINIMUM REMAINING MATERIAL THICKNESS OF .054" WITHIN ALLOWABLE LIMITS, REF AIR WISCONSIN SUSDR EE4Y2020090721598Skin · dentedDURING ROUTINE MAINTENANCE AT MAINTENANCE FACILITY, THE LOWER FUSELAGE EXTERNAL SKIN JUST BELOW THE SERVICE DOOR, AT BS 301.5, BETWEEN STR-17 R AND STR-18 R WAS FOUND TO HAVE A SHALLOW DENT.
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