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 HNAA2020111200313Skin · crackedRT EXTERNAL UPPER FUSELAGE SKIN CRACKED AT RIVETS 2 EA FR 79. INSTALLED SERVICEABLE RIVET AND REPAIR SKIN BUSHING AT FR 79 BETWEEN STR 3R-4R, IAW EO1-53-20-0406.SDR DALA2020111203690Skin · dentedDURING INITIAL INSPECTION FOUND DENT ON EXTERNAL FUSELAGE BETWEEN STA 377 TO STA 395 AND STG 13R TO STR 14R . REPAIRED PER SRM.SDR JJBA20201109007Skin · damagedDURING REMOVAL OF REPAIR DOUBLER LOCATED ON RT CENTER FUSE 1 BETWEEN FRAME 19-20 AND STR 18-19R. RT CENTER FUSELAGE I BETWEEN FR 19-20 AND BETWEEN STR 18R-20R DAMAGE TO SKIN REPAIRED.SDR SWIA202053967Skin · bentLOWER SKIN (P/N 601R10871-3 SRM ITEM 8) BETWEEN WS 371.00 WS 377.00 IS BENT 0.250" UPWARD ALONG 3.50" SPANWISE & 1.00? CHORDWISE. CLASSIFIED AS MAJOR REPAIR M-337 INITIATED. FILED CLOSED. REPAIR OF LOWER SKIN PERFORMED BY MHIRJ MRT PERSONNEL, PER REO. COMPSDR AALA202011119018Skin · corrodedAIRCRAFT IN BASE MAINTENANCE. CORROSION OF FUSELAGE SKIN AT STA 917 BETWEEN STR 21L AND STR 22L, MEASURING L=4.0 IN, W=6.0 IN, D=0.032 IN. ACCOMPLISHED PERMANENT REINFORCING DOUBLER/TRIPLER REPAIR, IAW SRM 51-10-02 AND EA309614.SDR HNAA2020110900305Skin · chafedSMALL CHAFE BEHIND LT UPPER OVERWING FAIRING SUPPORT BETWEEN FR 42-43 AND STR 13L-14L. SMALL CHAFE BEHIND LT UPPER OVERWING FAIRING SUPPORT BETWEEN FR 42-43 AND STR 13L-14L, DRILLED OUT SMALL CHAFE AND INSTALLED SOLID RIVET AND WASHER AT LT UPPER OVERWING FAISDR HNAA2020110900199Skin · crackedFUSELAGE EXTERNAL SKIN HAS POSSIBLE CRACKS AT 1 RIVET ON FR 79 BETWEEN STR 8L/9L. EVALUATION COMPLETE: FUSELAGE EXTERNAL SKIN HAS POSSIBLE CRACKS AT 1 RIVET ON FR 79 BETWEEN STR 8L/9L. FABRICATED AND INSTALLED BUSHING ON FUSELAGE EXTERNAL SKIN AT FRAME 79 BSDR HNAA2020110900198Skin · dentedDENT FOUND ON SKIN, AT FRAME 3, BELOW THE LT LONGITUDINAL SKIN SPLICE. COMPLETE: CUT OUT ON BLEND NR 2, FABRICATED FILLER AND DOUBLER FOR DENT. INSTALALED REPAIR OVER DENT FWD OF FRAME 3 BELOW THE LT LONGITUNINAL SKIN, IAW ETD-2020-145-028955 AND EO1-53-20-0SDR FDEA202011072787Skin · corrodedEXTERIOR FUSELAGE SKIN HAS EVIDENCE OF CORROSION AND BULGED SKIN AT SPLICE ARE BS 1455-BS 1462 STR 30-STR 28R. REMOVED FASTENERS AT STA 1459 STR 28R TO 28L AND 1 EA SHEAR TIE AT STA 1459 STR 30-29R, IAW B757 SRM 51-40-02. REMOVED 1 EA SHEAR TIE STA 1459 STR SDR CALA2020110901255Doubler · damagedREMOVE AND REPLACE AFT FUSELAGE INTERNAL DOUBLER BETWEEN FR 73-FR 74 STR 33L-33R JACKING POINT AREA. EC/RA: 5351-01177-NR 929 2286. REMOVED AND REPLACED AFT FUSELAGE INTERNAL DOUBLER BETWEEN FR 73-FR 74, STR 33L-STR 33R AT JACKING POINT, IAW UNITED EC/RA 53SDR DALA2021080304391Skin · dentedSHIP 693 ERA 495296-14 REV B FUSELAGE/SKIN/FS 640 BTWN S-5L & S-6L/DENT. CORRECTIVE ACTION: REF ERA 495296-14 REV B AND REV C. (1650018)SDR SWIA202054732Skin · corrodedFUSELAGE SKIN AT STR 27, FS 978-982 HAS AREA WITH A CHAFE FROM A SCREW, AN AREA OF CORROSION AROUND THAT SCREW AND AN AREA EXTENDING FROM THAT CORROSION WITH MISSING PAINT THAT HAS BEEN POORLY BLENDED AND TREATED. C-CHECK RO 12/24/2020. REPAIRED FUSELAGE SKISDR SWIA202054465Skin · corrodedCORROSION DETECTED ON BELLY SKIN AT LOWER TCAS OMNIDIRECTIONAL ANTENNA CUT-OUT, MARKED. C-CHECK RO 12/04/2020. CUT OUT DAMAGED AREA ON BELLY SKIN AT LOWER TCAS OMNIDIRECTIONAL ANTENNA. FABRICATED AND INSTALLED REPAIR DOUBLER, REF REO. COMPLIED WITH SW TASKSDR CALA2020110901251Skin · damagedLT FUSELAGE SKIN FR 57-58 AT STR 37L HAS PREVIOUS DENT REPAIRED WITH INSTALLATION OF FASTENER THAT IS OUT OF LIMITS, IAW A320 SRM 53-00-11-283-005. SKIN REQUIRES REPAIR (SUPPORT TASK). REPAIR ACCOMPLISHED LT FUSELAGE EXTERIOR SKIN BETWEEN FR 57-58 AT STR SDR N6WA2020110602Skin · corrodedCORROSION ON INNER SKIN STRG 27-26 RT, FS 319.7-327.00. REPAIRED CORROSION ON INNER SKIN, IAW REO 670-53-21-1844.SDR CALA2020110601248Skin · dentedLT FUSELAGE SKIN FR 57-58 AT STR 37L HAS PREVIOUS DENT REPAIRED WITH INSTALLATION OF FASTENER THAT IS OUT OF LIMITS, IAW A320 SRM 53-00-11-283-005. SKIN REQUIRES REPAIR (SUPPORT TASK). GENERATED BY V061619 AT HAECO LCQ, PER NR 9292324. REPAIR ACCOMPLISHED SDR SWIA202055399Skin · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA59039-601R-53-00-743 N868ASMXCODEID51889-PR. THERE ARE TWO DENTS IN THE FUSELAGE, ONE LOCATED BETWEEN FS 295.0-FS 310.0 AT STR 21L AND THE OTHER LOCATED BETWEEN FS 409.00 AND FS 409.00+16 AND STR 16L-17L, PER REO 601RSDR SWIA202054896Skin · dentedADM# N787SK-5223. DENT LOCATED ON FUSELAGE APROXIMATELY 58" AFT OF THE SERVICE DOOR FS 349 61.5 FROM STRINGER 27. REMOVE ALL EVIDENCE OF THE DENT BY WAY OF STANDARD PRACTICES. C-CHECK RO 12/28/2020. REPAIRED DAMAGED AREA, REF MHIRJ REO, NO DEFECTS NOTED.SDR SWIA202054373Skin · corrodedINTERNAL SIDE OF EXTERNAL SKIN CORRODED AT DOOR DATUM 2 AND FS 329.5. C-CHECK RO 11/24/2020. REPAIRED PAX DOOR OUTER SKIN AT DATUM 2 AND FS 329.5, IAW MHIRJ REO. COMPLETED TASK CARD AND ATTACHED COMPLETED FORM 337. WEIGHT ADDED 0.18 LBS.SDR ASAA2020110533528Skin · dentedDENT OBSERVED FORWARD OF THE POTABLE WATER SERVICE DOOR. GROUNDED-YES. REPAIRED DENTED AREA WITH DOUBLER BETWEEN FR 64 AND FR 65 AND STR 36L AND STR 39L, REF A320 SRM 53-41-11-300-016 CLASS A REPAIR. LIMITED CUTOUT REPAIR. THIS CLEARS MDDR 73300, CONTACTEDSDR SWAA2020111229768Skin · cracked.75' CRACK AT CHEM MILL STOP AT S-10L AT STA 385 DEFECT WITH PART 6, 53-30-25 VERIFIED WITH PART 6, 53-30-07. COMPLIED WITH EA 20-153-02203 SEE NRC NR D352428.SDR SWAA2020111229771Skin · crackedFOUND CHEM MILL STEP CRACKED ACROSS STEP .75' LONG AT ST-10L AT STA 360 DETECTED WITH PART 6, 53-30-25. VERIFIED WITH PART 6, 53-30-09 AND PART 6, 51-00-00 PRO 23 INTERNALLY. COMPLIED WITH EA 20-153-02203 REFER TO N/R D352421 FOR LT TLD INFORMATION.SDR IPXA2020110562079Skin · delaminatedINSPECTION TYPE: SEG 4 AFT FUSELAGE SKIN FROM STA 1980 TO 1992.8 AND BETWEEN 15L AND 15R. ACCOMPLISHED REPAIR, PER AVENIR AVIATION EO AVR 53-80-01-04 REV.SDR A6WA202011067402Skin · dentedFUSELAGE SKIN AT FS 559 TO FS 559+16 AND BETWEEN STR 9R AND STR 10R DENTED. DENT DIMENSIONS L=3.75'' W=0.50'' AND D=0.046''. AIRCRAFT REMOVED FROM SERVICE. CUT-OUT DAMAGED SKIN AT FS 559 TO FS 559+16 AND BETWEEN STR 9R AND STR 10R, REF EA AWAC-CRJ253-01521 SDR A6WA202011067400Skin · dentedOUTWARD DENT IN SKIN AT FS 677 AND STR 23R + 2. AIRCRAFT REMOVED FROM SERVICE. EVALUATED DENT AT FS 677 AND STR 23R + 2. DENT MEASURES L=0.700'' W=0.600 D=0.015 FOUND TO BE OUT OF LIMITS, PER CRJ-200 SRM 53-00-31 REV 38 DIAL DEPTH GAUGE S/N X102407 CAL DUE SDR A6WA202011067398Skin · dentedFUSELAGE SKIN DENT AT FS 583 BETWEEN STR 25L AND STR 26L. AIRCRAFT REMOVED FROM SERVICE. PERFORMED HAND DRESS OF DENT BACK TO ORIGINAL CONTOUR OF FUSELAGE SKIN AT FS 583 BETWEEN STR 25L AND STR 26L, REF EA AWAC-CRJ253-01522 REV IR DATED 10/29/2020. PERFORMSDR SWAA2021081029766Skin · cracked.75' CRACK AT CHEM MILL STOP AT S-101 AT STA 385 DETECTED WITH PART 6; 53-30-25; VERIFIED WITH PART 6; 53-30-07 / TRANSFERED TO NR B352421SDR SWIA202054990Skin · dentedEXTERNAL FUSELAGE SKIN HAS 1 EA PROTRUDING DENT BETWEEN FS 202.75 AND FS 220, STR 18L TO STR 20L. C-CHECK RO 12/30/2020. REPAIRED EXTERNAL FUSELAGE SKIN BETWEEN FS 202.75 AND FS 220.00 STGR 18L TO STGR 20L, IAW REO. REFER TO CONTINUE CARD FOR WORK PERFORMEDSDR SWIA202054457Fastener · damagedEXTERNAL FASTENER DAMAGE INTO BASE METAL RESEMBLING A DRILL START IN DOUBLER REPAIR AT FS 977 AND STGR 27. C-CHECK RO 12/04/2020. REMOVED OLD REPAIR DOUBLER AND INSTALLED NEW REPAIR AT FS 977.00 STGR 27, PER REO. COMPLIED WITH TASK CARD. PRESSURIZED LEAK CSDR FDEA202011042773Skin · corrodedEXTERIOR FUSELAGE UPPER ADF ANTENNA AREA STA 1116 HAS LIGHT PITTING. REMOVED CORROSION PITTING ORIGINAL MATERIAL .110, REMOVED .010, .100 REMAINING FOUND TO BE WITHIN LIMITS, IAW B757 SRM 53-00-01-1A. APPLIED CLEAR 1001 ALODINE, IAW B757 AMM 51-21-04-7.SDR JR2R20201104962Shim · corrodedACCESS PANEL 192CR SHIM FOUND CORRODED OUT OF LIMITS.SDR VNAA202011049995Doubler · corrodedANTENNA DOUBLER BETWEEN FS 295 AND FS 310 AT STGR 27 IS CORRODED. REMOVED CORRODED DOUBLER BETWEEN FS 295 AND FS 310 AT STGR 27 AND INSTALLED NEW SERVICEABLE DOUBLER P/N SH670-32364-7, IAW CRJ 700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.SDR SWAA2021081027878Filler · crackedLOWER FUSELAGE EXTERNAL ELECTRICAL POWER ACCESS DOOR CUTOUT HAS A CRACKED FILLER / REMOVED AND REPLACED LOWER FUSELAGE EXTERNAL ELECTRICAL POWER ACCESS DOOR CUTOUT FILLER IAW B737-700 SRM 53-10-15-2R-4; 51-40-02-0G-0 P/N 2024-T3-.040 ATAG A61559SDR SWIA202054775Doubler · corrodedTCAS OMNIDIRECTIONAL ANTENNA DOUBLER IS CORRODED AT CONNECTOR HOLE, MARKED. C-CHECK RO 12/26/2020. REMOVED AND REPLACED TCAS OMNIDIRECTIONAL ANTENNA DOUBLER, REF CRJ900 SRM AND DWG. COMPLIED WITH SKYWEST TASK CARD. COMPLETED FORM M-337. SEE CONTINUATION CSDR SWIA202054622Skin · chafedTHE FUSELAGE LOWER SKIN PANEL EXTERNAL REPAIR DOUBLER/TRIPLER BETWEEN FS 969 AND FS 985 AT STRINGER 27 IS CHAFED. C-CHECK RO 12/14/2020. REMOVED AND INSTALLED NEW REPAIR PARTS AT THE FUSELAGE LOWER SKIN PANEL BETWEEN FS 969 AND FS 985 AT STRINGER 27, REF REOSDR FDEA202011032903Skin · corrodedAFT FUSELAGE, RT SIDE STA 2163 LONG 33 NUTPLATE HOLE CORRODED OUT OF LIMITS. CONFIRMED WITH NDT. COMPLIED WITH FUSELAGE SKIN REPAIR, PER MD-10 SRM 53-20-00 PG 197-205 FIG 22.SDR SCNA20201117322Panel · damagedPANEL 192F AFT INSIDE EDGE OF PANEL HEAVILY WORN. REPAIRED DAMAGE TO AFT INSIDE EDGE OF PANEL 192F IAW SRM 51-70-05-2R-6 PER SRM 53-40-70-2R-1 PARA 4D(1) TABLE 202.SDR SCNA20201117320Panel · damagedPANEL 192HR HAS DAMAGED SCREW HOLES. REPAIRED DAMAGED SCREW HOLES ON PANEL 192HR, IAW SRM 51-70-05-2R-8 PER SRM 53-40-70-2R-1 PARA 4D(1) TABLE 202.SDR SCNA20201117318Panel · damagedPANEL 191FL HAS DAMAGED SCREW HOLES. REPAIRED DAMAGED SCREW HOLES ON PANEL 191FL, IAW 737 SRM 53-30-70-2R-1 AND SRM 51-70-05 REPAIR 8.SDR JJBA20201103006Skin · damagedSKIN DAMAGE ON RT FWD FUSE 2, BETWEEN FR 11-12 AND BETWEEN STR 17R-18R. SKIN REPAIRED ON RT FWD FUSELAGE 2, BETWEEN FR 11-12, BETWEEN STR 17R-18R.SDR IPXA2020110362001Skin · delaminatedINSPECTION TYPE: SEG 4 DENT 6 (TOP OF APU) 5.75" FWD OF BS 1963, 3.5" L OF BLO A=.125 Y=.008 A/Y=15.6 FOUND TO BE DELAMINATED. REPAIRED IAW B757 SRM 51-7010-2R, PER SRM 53-80-01-2R.SDR IPXA2020110362000Skin · delaminatedINSPECTION TYPE :SEG 4 DENT RIGHT OF CENTER TAILCONE (11.5" AFT OF BS 1896.20 10" R OF BLO) EVALUATED DEPTH TO BE .167" DOT 72/019. REPAIRED AREA IAW B757 SRM 51-70-10-2R, PER SRM 53-80-01-2R.SDR IPXA2020110361999Skin · delaminatedINSPECTION TYPE: SEG 4 DENT 4 (TOP OF APU) 8" AFT OF BS 1918.9 14" LOT BLO A=.187 Y=.015 A/Y=12.46 FOUND TO BE DELAMINATED. REPAIRED IAW B757 SRM 51-70-10-2R, PER SRM 53-80-01-2R.SDR IPXA2020110361998Skin · delaminatedINSPECTION TYPE: SEG 4 DENT (TOP OF APU) 16" R OF BLO A=/25 Y=.045 A/Y=5.5 FOUND TO BE DELAMINATED. REPAIRED AREA, IAW B757 SRM 51-70-10-2R PER EA 757-5380-27-A2515 REV- PER EO B757-5330-78319-A.SDR DALA2021031201416Paint · damagedSHIP 3302 PAINT DAMAGE IN CRITICAL RVSM AREA OF STATIC PORTS ON LEFT & RIGHT SIDE OF FUSELAGE. CORRECTIVE ACTION: APPLIED PAINT IN CRITICAL RVSM AREA OF STATIC PORTS ON LEFT AND RIGHT SIDE OF FUSELAGE ASPER A330 SRM 51-75. (7676910)SDR SWIA202056376Skin · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA56729-601R-53-61-7299 N246PS MXCODEID50918-PR - DURING ALLOWABLE DAMAGE INSPECTION; FOUND DENT AT FUSELAGE STA 626.3, ABOVE RT STR 21, MEASURING 1.34" DIAMETER BY .044" DEEP. COMPLIED WITH REO 601R-53-61-7299. PERMANSDR SWIA202055680Skin · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA55603-601R-53-11-3534 447SW MX CODE ID 50351 PR DENT AT FUSELAGE STATION 245.8 LT SIDE BETWEEN STRINGER 14L & 15L. DENT MEASURING 2.1" LONG, .9" WIDE & .095" DEEP. COMPLIED WITH TEMP REPAIR PER REO 601R-53-11-3534 RESDR SWAA2020113027686Skin · corrodedCORROSION, EXTERNAL FUSELAGE SKIN AT APPROXIMATELY BS 680-BS 700 STR 1-STR 2R BL 0-RBL 8, WL 306 HAS CORROSION AROUND ADF NO 1 ANTENNA MOUNT HOLES. REMOVED DAMAGE ON EXTERNAL FUSELAGE SKIN BS 680-700 STR 1-2 RT COMMON TO NR 1 ADF ANTENNA FASTENER HOLES. REPASDR SCNA20201117319Panel · damagedPANEL 192HL HAS DAMAGED SCREW HOLES. REPAIRED DAMAGED SCREW HOLES ON PANEL 192HL, IAW SRM 51-70-05-2R-8.SDR SCNA20201117317Panel · damagedPANEL 191FR HAS DAMAGED SCREW HOLES. REPAIRED DAMAGED SCREW HOLES ON PANEL 191FR, IAW 737 SRM 53-30-70-2R-1 AND SRM 51-70-04 REPAIR 9 AND 10.
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