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 DALA2023121310223Unknown · unknownSHIP 3358 DURING "C" CHECK IN MSP, THE F53273541203 FUSELAGE SKIN PANEL WAS FOUND WITH WEAR AT THE UPPER AFT CORNER AND UPPER EDGE OF THE #2 RH DOOR CUTOUT. SRM 53-21-11-283-005 EXCLUDES THE CORNER AREAS OF THE DOOR CUTOUT FOR REWORK LIMITS. REWORK RESULTED INSDR 2023FA0000823Unknown · unknownSEC 41, STA 347 TO STA 390, STR 36L TO STR 37L - SEVERAL BLEND OUTS ON FUSELAGE EXTERNAL SKINSDR VNAA202401220015Skin · damagedLIGHTNING STRIKE ON FUSELAGE SKIN BTW FS517.00 TO FS 533.00 AND BTW STGR13RH TO STGR14RH. LIGHTNING STRIKE ON FUSELAGE SKIN BTW FS517.00 TO FS 533.00 AND BTW STGR13RH TO STGR14RH WAS REPAIRED PER CRJ-900 SRM 53-00-00-201-003-A03SDR VNAA202401220014Skin · damagedLIGHTNING STRIKE ON FUSELAGE SKIN BTW FS549.00 TO FS 565.00 AND BTW STGR13RH TO STGR14RH. LIGHTNING STRIKE ON FUSELAGE SKIN BTW FS549.00 TO FS 565.00 AND BTW STGR13RH TO STGR 14RH WAS REPAIRED PER CRJ-900 SRM 53-00-00-201-003-A03SDR VNAA202401220002Skin · wornWEAR ON EXTERNAL FUSELAGE SKIN (2EAS) BTW FS 897.70 TO FS 927.00, BTW STGR 27 TO STGR 26LH. WEAR ON EXTERNAL FUSELAGE SKIN (2EAS) BTW FS 897.70 TO FS 927.00, BTW STGR 27 TO STGR 26LH WAS REPAIRED PER REO 690-53-51-393 REV --SDR SWAA2024010430618Panel · debondedPANEL 194CR OUTER SKIN IS DISBONDED. (MARKED)<[01] PANEL 194CR OUTER SKIN DISBONDED WAS REPAIRED IAW SRM 51-70-05-2R-2;[02] VERIFIED REPAIR OF PANEL 194CR PER SRM 51-70-05-2R-2SDR CALA2023122003688Skin · dentedFOUND 7" LONG B DENT @ LOWER FUS EXTDRNAL BELOW AFT CARGO BILGE BETWEEN S-26R AND S-27R STA 807 (REF AAR NR 9212566) INSTALLED DOUBLER AND FILLER REPAIR AT FUSELAGE SKIN BELOW AFT CARGO BILGE BETWEEN 526R AND S-27R STA 787+11.SDR SWI202402190136Skin · chafedDURING AUIDT OF 1C TASK CARD 53-150-502 (GENERAL VISUAL INSPECTION OF THE FORWARD BAGGAGE BAY DOOR, EXTERNAL SURROUND STRUCTURE AND FITTINGS €“ FS535.64 TO FS578.36, STGR19L TO STGR25L), FOUND CHAFFING ON FWD CARGO DOOR AREA, FUSELAGE SKIN UPPER EDGE. (C-CSDR SWAA2023121830941Skin · handler errorPROVO TRUCK COLLIDED WITH CAPT SIDE ENTRY AFT DOOR<[01] REPAIRED ON EA 23-153-03617 (N569WN - SWA - REPAIR - SECTION 47 FUSELAGE SKIN DAMAGE BETWEEN STA 914 - 937 AND BETWEEN STR 20L AND 21L) [TTG8Q00QBG9R]SDR DALA2023121310226Unknown · unknownSHIP 670 DTE, ERA 613497-14, MONITOR INSPECTION LOG REPAIR TO FUSELAGE SKIN BETWEEN STA 620 & STA 640, AND BETWEEN S -15L & S-16L. CORRECTIVE ACTION: REF ERA 613497-14. (0105557)SDR 7C7A2023121100064Skin · corrodedCORROSION FOUND UNDER #1 ADF ANTENNASDR DALA2023121110111Unknown · unknownBIRD STRIKE DAMAGE COMMON TO THE RHS OF THE NOSE FUSELAGE ABOVE THE AFT SKIN STRINGER AND BETWEEN FR13-FR14. TWO DENTS ARE PRESENT FWD OF FR13 AND FR14. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0005:2000-2100/00SDR FDEA202312091934Skin · damagedPER WRI 53-30/0922, DURING BIRD STRIKE INSPECTION, FOUND DENTS LOCATED FWD OF CAPTAINS WINDSHIELD AFT OF RADOME. REPLACED SKIN PANEL 141T3830-18REF E.A. H-5330-T0377384 REV. C PT 2 AND SRM STANDARD PRACTICES. REF W.O. 87715 NR 52 FOR WORK ACCOMPLISHED.SDR DALA2023121310195Unknown · unknownSHIP 676 ATG4 ANTENNA REQUIRES REMOVAL TO C/W INSPECTION. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 002-0001:2330-01201-1601/001 00001 C/W ERA 614037-14 REV. A. (0101958)SDR SWI20240219000125Skin · gougedDURING AUDIT OF 1C TASK CARD 53-900-304 (EXTERNAL ZONAL INSPECTION OF THE REAR FUSELAGE - FS977.00 TO FS1098.20 BELOW WL72.50), FOUND A GOUGE IN THE EXTERNAL SKIN APPROXIMATELY 2" LONG AT STRG 27 JUST AFT OF FS977.00. (C-CHECK RO 2/19/2024) REPAIRED GOUGESDR DALA2023121310187Unknown · unknownSHIP 0670 IN REF NRC 00210, AFTER BLEND OUT BY CORROSION (UT) THICKNESS MEASUREMENT INSPECTION WAS ACCOMPLISHED ON SIDE PANEL LH BTW STA 1310-1350 AND STA 1410 TO STA 1530 ORIGINAL THICKNESS IS 0.063 IN AND MINIMUM REMAINING THICKNESS IS 0.029 IN, THEREFORE THSDR DALA2023121310186Unknown · unknownSHIP 0670 PROTUBERANCE ON EXTERNAL FUSELAGE SKIN BS 1440 BTW STGR 23LH AND 24LH. CORRECTIVE ACTION: SUMMARY OF NRC 00062 PROTUBERANCE ON EXTERNAL FUSELAGE SKIN BS 1440 BTW STGR 23LH AND 24LH WAS REPAIRED PER B757-200 SRM 53-00. (0101242)SDR DALA2023121210173Unknown · unknownSHIP 3303 DAMAGE TO SKIN JUST BELOW STR-40RH AT FRAME 20A. .875 X .875 AND TO FRAME 20A 10.5L X 4W X 1.3750 DEEP. CORRECTIVE ACTION: REPAIRED SKIN DAMAGE IAW ER/A 614093-14 AND PRI'S 614093-14. FRAME 20A REPAIRED IAW CR/A 613958-14 AND PRI'S 613958-14. (556303SDR DALA2023121110129Unknown · unknown(LOG 0101473) DURING MAJOR MAINTENANCE SERVICE ON MXA MRO AT MEX, WHILE PERFORMING DELTA TASK NO. 2020-9002 "CHECK - AIRCRAFT EXTERNAL DAMAGE IDENTIFICATION (ADF FILE) AND DENT RE-EVALUATION", A DENT WITH CREASE (LOG 0253353) WAS RE-EVALUATED ON RH FUSELAGE SKSDR 2023FA0000817Skin · crackedLH WING FLAP COVE SKIN FOUND CRACKED AT 5 RIVET LOCATIONS ALONG WING TRAILING EDGE AND 2 RIVET LOCATIONS AT LH W/S 36.5 FLAP COVE RIB. ALL TRAILING EDGE LOCATIONS EACH PROPAGATED BOTH INBOARD AND OUTBOARD OF RIVET NOT MORE THAN 1". ONE TRAILING EDGE LOCATIONSDR DALA2024120511473Skin · damagedERA 614059-14 ISSUED FOR BIRD STRIKE REPAIR TO FWD RH FUSELAGE S KIN FR13-14. DAMAGE TOLERANCE EVALUATION IS REQUIRED. ERA 614059-14 ISSUED AND IS LIMITED TO 12MONTHS AFTER SECTION I. SECTION I ACCOMPLISHED IN MSP 07DEC23. OPERATION BEYOND 12 MONTHS REQUIRES ASDR SWIA20231200007Unknown · chafedWHILE REMOVING AFT DRAIN MAST, FOUND FUSELAGE CHAFFED AND CORRODED DIRECTLY UNDER DRAIN MAST FLANGE. (FILED CLOSED)PERMANENTLY REPAIRED FUSELAGE SKIN BETWEEN FS605.00 - FS621.00 & STR25R - STR26R IN REFERENCE TO REO 601R-53-61-8125 REV-- DATED 2023-12-10.SDR AALA202312117714Doubler · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN ELECTRICAL GROUND POWER DOOR CUTOUT SURROUND DOUBLER AT BS 178, S19R. REPAIRED DOUBLER PER SRM 53-10-15-2R PROCEDURE 4.SDR DALA2023120810063Unknown · unknownSHIP 3120 NICK EXTERNAL SKIN LOCATED ACCESS DOOR 812 AT LOWER FUSELAGE. CORRECTIVE ACTION: REPAIRED PER ER/A 614003-14. (0099552)SDR DALA2023120810060Unknown · unknownCRACK ON UPPER AFT CORNER OF SKIN AT LH SLIDING WINDOW CUTOUT IN REF NRC 00408. SUMMARY OF NRC 00487: UPPER AFT CORNER OF SKIN AT LH SLIDING WINDOW CUTOUT WAS REPAIRED PER PRI 614087-14 REV 2 AND ER/A 614087-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIASDR SWI2024031200223Skin · crackedPOSSIBLE CRACK ON EXTERNAL SKIN AT FS235 RBL6 (NLG WHEEL WELL CUTOUT) (C-CHECK RO 3/9/2024) REPAIRED EXTERNAL SKIN (NLG WHEEL WELL CUTOUT) AT FS235 RBL6 REF REO 601R-53-11-048 REV. -D DATED 2015-06-10. COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECK GOOSDR SWI2024031200222Skin · crackedPOSSIBLE CRACK ON EXTERNAL SKIN AT FS235 LBL6 (NLG WHEEL WELL CUTOUT) (C-CHECK RO 3/9/2024) REPAIRED EXTERNAL SKIN (NLG WHEEL WELL CUTOUT) AT FS235 LBL6 REF REO 601R-53-11-048 REV. -D DATED 2015-06-10. COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECK GOOSDR CALA2023122003672Skin · crackedFUSELAGE SKIN HAS 2EA CRACKS ON VERTICAL FASTENER ROW MEASURING 1" LONG AND .250 LONG LOCATED AT LFS 1702, BETWEEN S-10L AND S-11L (VERI FIED WITH HFEC) REF AMES NR 165631-0300-0008 REMOVED DAMAGE. FABRICATED AND INST ALLED DOUBLER 1 AND FILLER 3 IAW SRM 53-00SDR DALA2023120810077Unknown · unknown(LOG 0098345) WHILE OVERNIGHT IN ATL, MTC ATTEMPTED TO REPAIR A DEFERRED LIGHTNING STRIKE DAMAGE TO THE FUSELAGE SKIN. THE DAMAGE IS LOCATED AT STA 370 AND STR 15L. DAMAGE REPAIRED PER ERA 614152-14.SDR DALA2023120810051Unknown · unknownSHIP 0670 FUSELAGE / EXTERNAL SKIN / FS508-520, S-28L TO S-28R / FORWARD LOWER ATG4 ANTENNA / INHIBITED INSPECTION. CORRECTIVE ACTION: REF ERA 613525-14. (0098690)SDR DALA2023120810050Unknown · unknown0673 SHIP FUSELAGE / SKIN / FWD LOWER ATG4 ANTENNA / REMOVAL. CORRECTIVE ACTION: REF ERA 614165-14. (0098603)SDR DALA2023120810049Unknown · unknownSHIP 6717 FUSELAGE / SKIN / FWD LOWER ATG4 ANTENNA / REMOVAL. CORRECTIVE ACTION: REF ERA 614166-14. (0098506)SDR DALA2023120810047Unknown · unknownSHIP 0670 DENT ON FUSELAGE SKIN ON BS 555 BTW STGR 23LH AND 24LH. CORRECTIVE ACTION: SUMMARY OF NRC 00057 PERMANENT REPAIR DENT ON FUSELAGE SKIN ON BS 555 BTW STGR 23LH AND 24LH. WAS PERFORMED PER ERA 613690-14. (0098572)SDR DALA2023120710024Unknown · unknown(LOG 0098446) COMPLY WITH PRI/ER/A 614152-14 LIGHTNING STRIKE REPAIR @ STA: 370 STR: 15L. C/W PRI 614152-14 REV. 3 (984172) (QC5290) C/W ER/A 614152-14 REV. ORIG SECTION I PERMANENT REPAIR.SDR DALA2023120710006Unknown · unknownBEND AND CRACK ON CUTOUT UPPER SIDE OF AIR STAIRWELL DOOR AT APPROX STA Y 160 AND BTW LONG 18LH AND LONG 19LH ON FUSELAGE. SUMMARY OF NRC 00126: CUTOUT UPPER SIDE OF AIR STAIRWELL DOOR AT APPROX STA Y 160 AND BTW LONG 18LH AND LONG 19LH ON FUSELAGE WAS REPAIRESDR DALA2023120710028Unknown · unknownSHIP 3303 DURING LINE OPERATIONS IN SJC, THE FWD CARGO DOOR SURROUND WAS HIT BY A CARGO LOADER. THE F53270600200 SKIN WAS FOUND DENTED AND GOUGED AT S-40R. THE A53772636006 FRAME 20A IS ALSO BUCKLED AT S-40R. DTE FOR REPAIR TO FWD CARGO SURROUND FRAME 20A DENTSDR DALA2023120610000Unknown · unknownSHIP 0676 FUSELAGE / SKIN / FS508-FS520, S-28L TO S-28R / FWD LOWER ATG4 ANTENNA / REMOVAL. CORRECTIVE ACTION: REF ERA 614037-14. (0096864)SDR DALA2023120609996Unknown · unknownSHIP 6813 DENTS #10, #12 AND #14 THEY ARE OUT LIMITS DUE TO DISTANCE TO SPLICE FASTENER ON UPPER SKIN FROM BSTA 740 TO BSTA 879 BTW S-4RH TO S- 10RH AT FUSELAGE. CORRECTIVE ACTION: REF ERA 614023-14. (0096908)SDR DALA2023120609995Unknown · unknownSHIP 6813 DENTS #11 0.762", Y=0.011", A/Y=69.509, #12 A= 0.935", Y=0.016", A/Y=57.147, #13 A=1.171", Y=0.019", A/Y=61.721, #45 A=1.055", Y=0.017", A/Y=60.622 AND #46 A=0.995", Y=0.010", A/Y= 99.991 OUT LIMITS DUE TO DISTANCE TO SPLICE FASTENER. CORRECTIVE ACTISDR DALA2023120609979Unknown · unknownELONGATED HOLES ON FUSELAGE BTW CANTED STA Y=1178 AND LOG PROJECT 14L AT AFT FUSELAGE. (IN REF TO NRC: 00238). SUMMARY OF NRC 00298: FUSELAGE BTW CANTED STA Y=1178 AND LOG PROJECT 14L AT AFT FUSELAGE WAS REPAIRED PER ER/A 613199-14 REV ORIGINAL, SECTION I: PERSDR SWIA20240319204Skin · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA82364-REO 601R-57-21-2702 MXCODEID65934-PR - DENT FOUND ON LT WING FWD LOWER PLANK BETWEEN WS65.75-WS85.50 AND BETWEEN STR 19-STR 20. PERMENANT REPAIR DUE WITHIN 2100 HOUR PER REO 601R-57-21-3702., PART NUMBER: - , SSDR DALA2023120409940Unknown · unknownSHIP 6710 FUSELAGE / SKIN / FS508-FS520, S-28L-S-28R / FORWARD LOWER ATG4 ANTENNAL / REMOVAL. CORRECTIVE ACTION: REF ERA 613975-14. (0094688)SDR DALA2023121810319Unknown · unknownSHIP 3245 DISC: DENT EXTERNAL SKIN LOC. FR 2 TO FR 3 UPPER STRINGER AND 16 INCHES BELO W LH SIDE AT LOWER FUSELAGE. C/A: EVALUATED DENT EXTERNAL SKIN LOC. FR 2 TO FR 3 UPPER STRINGER AND 16 INCHES BELOW ON LH SIDE AT LOWER FUSELAGE AND FOUND WITHINLIMITS AS PESDR VNAA202312140008Skin · dentedDESCRIPTION: SEVERAL DENTS ON FUSELAGE SKIN, SETTLEMNT AREA OF LEFT VENTRAL FIN FAIRING BTW FS 1069.75 TO REAR SPAR DATUM STABILIZER 67.5%, BTW STGR 22LH TO STGR 21LH. CORRECTIVE ACTION: SEVERAL DENTS ON FUSELAGE SKIN, SETTLEMNT AREA OF LEFT VENTRAL FIN FAIRINSDR DALA2023120409923Unknown · unknownSHIP 1011 JETWAY IMPACTED L/H SIDE OF AIRCRAFT LEAVING AN APPROX 11.0" X 9.0" DENT, BETWEEN FR21-FR22, STR 24L-25L. CORRECTIVE ACTION: REPAIRED PER ERA 613741-14. (0093806)SDR JR2R20231203248Skin · corrodedRH WING FIXED LEADING EDGE ABOVE PYLON CHAFED. REPAIREDSDR HNAA2024011700021Skin · gougedE012720 FUSELAGE INTERIOR SURFACE HAS A DENT AND GOUGE BETWEEN FR 59-60 AND STR 20R-19R. PERFORMED FUSELAGE SKIN REPAIR BTW FR 59-60 STGR 19R-20R IAW ETD# ETD2023-145-031986 AND EO1-53-23-0472.SDR DALA2023121810318Unknown · unknownSHIP 3273 DISC: DENT EXTERNAL SKIN LOCATED BETWEEN FR4 TO FR5 AND 8 INCH ABOVE OF RH LOWER SIDE STRINGER LOWER FUSELAGE. C/A: EVALUATED DENT LOC EXTERNAL SKIN LOC BTW FR4 TO FR5 AND 8 INCH ABOVE OF RH LOWER SIDE STRINGER LOWER FUSELAGE AND FOUND WITHINLIMITS, SDR DALA2023120409899Unknown · unknownCRACK ON EXTERNAL FUSELAGE SKIN Y=1022 BETWEEN LONGERONS L-8L AND L-7L. SUMMARY OF NRC 00368: EXTERNAL FUSELAGE SKIN Y=1022 BETWEEN LONGERONS L-8L AND L-7L WAS REPAIRED PER ER/A 613350-14 REV ORIGINAL SECTION I: TEMPORARY REPAIR. TIME OF ACCOMPLISHMENT ACCOMPLSDR SWIA202403041201Skin · gougedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA63874-690-53-21-1280 837SK MXCODEID53660-PR - GOUGE DAMAGE ON FUSELAGE SKIN AT FS349.00 AND BTW STR 4L AND 5L. COMPLIED WITH TEMPORARY REPAIR PER REO 690-53-21-1280 REV -- DATED 2020-11-17. PERMANENT REPAIR WITHIN 8000
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