JASC 5310
Service difficulty reports · 38,528
Reports filed under 5310 · Fuselage Main, Structure, 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 = '5310' 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 = '5310' 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 ASAA2022061038785Intercostal · crackedFWD WET AREA: INTERCOSTAL BETWEEN BS 312 AND 328, AT RBL 30 CRACKED. GROUNDED - YES. REMOVED CRACKED INTERCOSTAL BETWEEN BS 312 AND 328 AT RBL 30 AND REPLACED WITH NEW INTERCOSTAL IAW BOEING DWG 141A5400 SHEET 39 REV - AND B737-800 SRM 51-40-02.SDR IPXA2022062483432Floor Panel · damagedINSPECTION TYPE:CFWD CARGO FLOOR PNL 132 EDGE DAMAGEREPAIR IAW SREO A300-5320-42722-FSDR IPXA2022062483428Floor Panel · damagedINSPECTION TYPE:CFWD CARGO FLOOR PANEL 131BH EDGES DAMAGEDREPAIR IAW SREO A300-5320-42722-FSDR VNAA202206131111None · nonePERMANENT REPAIR DUE TO FUSELAGE SKIN BETWEEN FS 364.00 AND FS 379.00 AND STR 22R- STR 23R / COMPLIED WITH EDDY CURRENT OF CUT OUT SECTIONS OF REPAIR AREA SURROUNDING FS 364.00, FS 379.00, AND STR 22R-23R USING REO 690-53-21-1520 REV. P2 AND CRJ900 NDTM 51-20SDR CALA2022061301486Stiffener · crackedSUPPORT TASK - EA5310-07143 REV D OP002 RH NOSE WHEEL WELL VERTICAL STIFFENER ON STA287 BETWEEN WL159 TO 185 FOUND 2EA CRACKED. TRANSFER REF NON - ROUTINE WO.813498 AND ORIGINATED BY V914372 RH NOSE WHEEL WELL VERTICAL STIFFENER ON STA287 BETWEEN WL159 AND WL1SDR JR2R20220610745Shear Tie · corrodedSHEAR TIE CORRODED AT FR88 BETWEEN STR 28R AND 27RSDR SIMA20220609014Track · gougedLH CENTER SEAT TRACK IS GOUGED BTW FR. 33-34-C/A-PERFORMED SPLICE DEVICE REPAIR BY INSTALLING SPLICE DEVICE ON FR. 33-34 IAW EMB-175 SRM 53-00-10 REPAIR 02P.(MAJOR REPAIR)SDR ASAA2022060939022Intercostal · corrodedAFT WET AREA LAV G HARD POINT UNDER MOUNT CORRODED.MARKED IN RED. GROUNDED - YES. LAV MOUNT HARD POINT FOUND TO BE 50% CORRODED AND OUT OF LIMITS IAW B737-800 SRM 51-1A-1.REMOVED CORRODED HARD POINT IAW B737-800 SRM 51-40-02.LOCATED, DRILLED, AND INSTALLED NEWSDR ASAA2022060939021Floor Support · corrodedAFT WET AREA RBL 20 DLOOR BOARD SUPPORT SRUCTURE CORRODED.MARKED IN RED. GROUNDED - YES. SUPPORT STRUCTURE FOUND TO BE 50% MATERAL LOSS AND OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A-1.REMOVED CORRODED SUPPORTS IAW B737-800 SRM 51-40-02.LOCATED, DRILLED, AND ISDR ASAA2022060939020Floor Support · corrodedAFT WET AREA SUPPORT STRUCTURE UNDER LAV D CORRODED.AREAS MARKED IN RED. GROUNDED - YES. SUPPORT STRUCTURE PN: 147A5690-3, FOUND TO BE MORE THAN 50% CORRODED IAW B737-800 SRM 53-70-51-1A-1 AND OUT OF LIMITS.LOCATED DRILLED AND INSTALLED NEW SUPPORT STRUCTURE ISDR SIMA20220609011Track · corrodedSSI 52-23-005 LH CENTER SEAT TRACK IS CORRODED BTW FR 84-85 (MAJOR REPAIR) ( LEVEL 2 CORROSION)-C/A-FABRICATED AND INSTALLED FILLER AND REPAIR DOUBLER, EDGE SEALED AND APPLIED TOPCOAT TO REPAIR IAW ETD2022-170-021699, REV A, EMB 175 SRM 53-23-10 AND ERS-EJ-53MSDR AALA202207062645Angle · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION FOUND ON ANGLE LOCATED AT STA 550 AND LEFT BUTT LINE 44. INSTALLED NEW ANGLE ON LEFT BULKHEAD AT STA 500 PER AARD 51-00-05-1.SDR AALA202207061729None · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION FOUND ON LEFT TRANSITION PANEL LOCATED BETWEEN STA 727 AND STA 847, AND STR 25L. REMOVED AND REPLACED LEFT TRANSITION PANEL PER SRM 53-00-53-1A-2.SDR SIMA20220609010Panel Support · corrodedRIGHT HAND PANEL SUPPORT BETWEEN FRAME 89-90 CORRODED (LEVEL 2 CORROSION) -C/A-REMOVED, POSITIONED, DRILLED AND INSTALLED SERVICEABLE RIGHT HAND PANEL SUPPORT BETWEEN FRAME 89-90 IAW EMB 175 SRM 51-40-02SDR SIMA20220609007Floorbeam · corrodedGALLEY RH FLOOR BEAM CORRODED BETWEEN FR 12 AND FR 13. (LEVEL 2 CORROSION)-C/A-PERFORMED CUTOUT AS REQUIRED AND FABRICATED AND INSTALLED FILLER AND DOUBLER TO REPAIR FWD GALLEY RH FLOOR BEAM BETWEEN FR 12-13 IAW EMB-175 SRM 53-10-10 REPAIR 03P.SDR SIMA20220609008Shear Beam · corrodedRIGHT HAND SHEER PANEL BETWEEN FR 87 ? 88 CORRODED. (LEVEL 2 CORROSION)-C/A-RAR AFT GALLEY RH SHEAR PANEL IAW EMB-175 SRM 51-40-08.SDR SIMA20220609009Beam · corrodedRH FLOOR CROSS BEAM AT FR 84 IS CORRODED AT INBD END NEAR SEAT TRACK. (MAJOR REPAIR)(LEVEL 2 CORROSION) -C/A-REMOVED AND INSTALLED SERVICEABLE CROSSBEAM AT FR 84 IAW EMB 175 SRM 51-40-08SDR SIMA20220609006Nut Plate · brokenNUT PLATE BRACKET FORWARD OF RIGHT HAND SHEER PANEL ON FRAME 87 CORRODED. (LEVEL 2 CORROSION)-C/A-RAR NUT PLATE BRACKET FORWARD OF RIGHT HAND SHEER PANEL ON FRAME 87 IAW EMB-175 SRM 51-40-08SDR SIMA20220609004Door · gougedFWD PAX DOOR, THE SEAL DEPRESSOR IN THE CUTOUT HAS GOUGE / EROSION DAMAGE AT 7 LOCATIONS. (MAJOR REPAIR)-C/A-RAR FWD PAX DOOR CUTOUT AFT SEAL DEPRESSOR IAW EMB-175 SRM 51-40-08.SDR SIMA20220609005Track · corrodedLH CENTER SEAT TRACK IS CORRODED BTW FR 19 ? FR 20. (LEVEL 2 CORROSION) (MAJOR REPAIR) -C/A-PERFORMED CUTOUT TO REMOVE DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW ERS-EJ-53MR-4558.SDR AALA202206293427Floor Support · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT AFT FLOOR SUPPORT LOCATED AT BS 500I AND BL 44. REPLACED FLOOR SUPPORT PER AARD 51-00-05-1.SDR SIMA20220609002Floor Panel · corrodedGALLEY RH FLOOR SILL CORRODED BETWEEN FR 13/14. (LEVEL 2 CORROSION)-C/A-RAR FWD GALLEY RH FWD SILL IAW EMB-175 SRM 51-40-08SDR SIMA20220609003Beam · corrodedRH HAND SUPPORT BRACKET ON RH BEAM BETWEEN FR 89-90 CORRODED (LEVEL 2 CORROSION)-C/A-RAR RH SUPPORT BRACKET ON RH BEAM BETWEEN FR 89-90 IAW EMB-175 SRM 51-40-08.SDR ASAA2022060938823Floor Panel · delaminatedMAIN CABIN FLOOR BOARD DELAM P/N 141A5810-286. GROUNDED - YES. REPAIRED CABIN FLOOR BOARD PANEL P/N 141A5810-286 BY REMOVING DAMAGED AREA AND BONDING FIBERGLASS DOUBLER WET LAY UP REPAIR IAW B737-800 SRM 53-00-50-2R-4&1.SDR ASAA2022060938822Floor Panel · delaminatedCABIN FWD WET AREA FLOOR BOARD DELAM P/N 141A5810-236. GROUNDED - YES. REPAIRED CABIN FWD WET AREA FLOOR BOARD PANEL P/N 141A5810-236 BY REMOVED DAMAGED AREA AND BONDING FIBERGLASS DOUBLER WET LAY UP REPAIR IAW B737-800SRM 53-00-50-2R-4 &1.SDR ASAA2022060938821Floor Panel · delaminatedCABIN FWD WET AREA FLOOR PANEL DELAM P/N 141A5810-558. GROUNDED - YES. REPAIRED CABIN FWD WET ARA FLOOR PANEL IAW B737-800 SRM 53-00-50-2R-1.SDR ASAA2022060938820Floor Panel · delaminatedCABIN FWD WET AREA FLOOR PANEL DELAM P/N 141A5810-454. GROUNDED - YES. REPAIRED CABIN FWD WET AREA FLOOR PANEL P/N 141A5810-454 BY REMOVING DAMAGED AREA AND BONDING FIBERGLASS DOUBLER WET LAYUP REPAIR IAW B737-800SRM 53-00-50-2R-1.SDR ASAA2022060938819Floor Panel · delaminatedCABIN FWD WET AREA FLOOR PANEL DELAM P/N 141A5810-183. GROUNDED - YES. REPAIRED CABIN FWD WET AREA FLOOR PANEL P/N 141A5810-183 BY REMOVED DAMAGED AREA AND BONDING FIBERGLASS DOUBLER WET LAYUP REPAIR IAW B737-800 SRM 53-00-50-2R-1.SDR ASAA2022060938784Transition Panel · crackedFT PIT R/H TRANSITION PANEL STA 727H+15 HAS PUNCTURE. GROUNDED - YES. EVALUATED AFT PIT R/H TRANSITION PANEL STA 727H+15, PUNCTURE .400" IN DIAMETER , OUT OF LIMITS IAW B737-800 SRM 53-00-53-1A-2 PAR 4-A.(4). REMOVED AND FAB NEW REPAIR PART AND DOUBLER AND INSSDR ASAA2022060938783Shield · puncturedFWD PIT R/H FLOOR STRUCTURE SHILED STA 500 HSA PUNCTURE. GROUNDED - YES. EVALUATED FWD PIT SHIELD AT STA 500.ORIGINAL THICKNESS .032",MATERIAL REMOVED .032",REMAINING MATERIAL .000" DUE TO PUNCTURE MEASURING .300"FOUND TO BE OUT OF LIMITS PER B737-800 SRM 53-3SDR ASAA2022060938782Transition Panel · corrodedAFT PIT L/H TRANSITION PANEL STA 727+4 - 727E HAS CORROSION. GROUNDED - YES. EVALUATED AFT PIT LH TRANSITION PANEL STA 727+4 - 727E.ORIGINAL MAT .040"PER BAC DWG 1496-377MAT REMOVED .022"MAT' REMAINING .018"OUT OF LIMITS IAW ASA B737-800 SRM 53-00-53-1A-2 FIG SDR ASAA2022060938781Transition Panel · corrodedFWD PIT R/H TRANSITION PANEL STA 500B-500H+8 HAS NUMEROUS AREAS OF CORROSION. GROUNDED - YES. EVALUATED FWD PIT R/H TRANSITION PANEL SAT 500B - 500H+8,ORIG THICKNESS .040" PER BOEING DWG BAC 1496-444.MATERIAL REMOVED .014",REMAININT MATERIAL .026" TO BE OUT OFSDR ASAA2022060938780Shield · corrodedAFT CARGO R/H FLOOR SUPPORT SHIELD STA 767-787 HAS CORROSION. GROUNDED - YES. EVALUATED AFT PIT SHIELD STA 767 TO 787.ORIGINAL MAT'L .050REMAINING .019,MAT REMOVED .031FOUND TO BE OUT OF LIMITS IAW ASA B737-800 SRM 53-60-0I-1 AND SRM 53-60-15-1A-1 RECEIVED NEWSDR IPXA2022062483454Intercostal · crackedINSPECTION TYPE:3CR/H A/C BAY INTERCOSTAL IS CRACKED AT AFT UPPER CORNER LOCATED AT APPROX FS 553 RL31.REMOVED ,FABRICATED AND REPLACED THE CRACKED INTERCOSTAL IAW SRM 51-33-01 (MINOR)SDR JR2R20220609234Angle · crackedLH WHEEL WELL STUB ANGLE CRACKED FWD SIDE OF FR52 WEBSDR JR2R20220609522Web · crackedLH WHEEL WELL WEB AT FR52 CRACKEDSDR IPXA2022062283357Angle · crackedINSPECTION TYPE:3CAFT CARGO AT STA. 1841 AND LBL 25, VERTICAL STIFFNER IS CRACKED.REMOVED, FABRICATED AND REPLACED STIFFNER IAW DWG. 7170 AND SRM 51-33-01. (MINOR)SDR IPXA2022062283356Floor Support · crackedINSPECTION TYPE:3CAFT CARGO AT STA. 1841 AND RBL 25, VERTICAL STIFFNER IS CRACKED.REMOVED, FABRICATED AND REPLACED STIFFNER IAW DWG. AGA7170 AND SRM 51-33-01. (MINOR)SDR IPXA2022062283355Stiffener · crackedINSPECTION TYPE:3CAFT CARGO AT STA. 1841 RBL 36, VERTICAL STIFFNER IS CRACKED.REMOVED, FABRICATED AND REPLACED STIFFNER IAW DWG. AGA7170 AND SRM 51-33-01. (MINOR)SDR IPXA2022061783197Angle · crackedINSPECTION TYPE:3CFWD. CARGO PANEL SUPPORT ANGLE IS CRACKED AT STA. 6-10 R/H SIDE.REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG. ADA0130 AND SRM 51-33-01. (MINOR)SDR IPXA2022061783196Angle · crackedINSPECTION TYPE:3CFWD. CARGO PANEL SUPPORT ANGLE IS CRACKED AT STA. 939 L/H SIDE.REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG. ADA0130 AND SRM 51-33-01. (MINOR)SDR IPXA2022061783195Angle · crackedINSPECTION TYPE:3CCENTER CARGO PANEL SUPPORT ANGLE IS CRACKED AT STA. 1681 L/H SIDE.REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG. ADA0130 AND SRM 51-33-01. (MINOR)SDR IPXA2022061783194Angle · crackedINSPECTION TYPE:3CFWD. CARGO COMP. PANEL SUPPORT ANGLE IS CRACKED AT STA. 1099 L/H SIDE.REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG. ADA0130 AND SRM 51-33-01. (MINOR)SDR IPXA2022061783193Angle · crackedINSPECTION TYPE:3CFWD. CARGO COMP. PANEL SUPPORT ANGLE IS CRACKED AT STA. 1119 R/H SIDE.REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG. ADA0130 AND SRM 51-33-001. (MINOR)SDR IPXA2022061783192Angle · crackedINSPECTION TYPE:3CFWD. CARGO PANEL SUPPORT ANGLE IS CRACKED AT STA. 859 L/H SIDE.REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG. ADA0130 AND SRM 51-33-01. (MINOR)SDR AALA202206094437Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CAPTAIN'S #2 WINDOW FRAME CRACKED, LOCATED AT BS 217, WL 258. REPAIRED PER SB 737-53-1336 AND WORK CARD 5319J023-007.SDR EE4Y2022060815779Box Beam · crackedDURING THE STRUCTURAL INSPECTION PER WORK CARD Nº: 53-240-001 RELATED TO AD 2020-02-20, IT WAS FOUND ON SIDE BOX BEAM FLANGE AT LH SIDE IN S15 FR43 AREA (1 HOLE WITH CRACK INDICATION). A DAMAGE REPORT WAS SENT TO AIRBUS ASKING FOR REPAIR INSTRUCTIONS AND FINASDR EE4Y2022060815777Window Post · crackedDURING THE STRUCTURAL INSPECTION PER MPD WORK CARD Nº: 531135-01-2-001, IT WAS FOUND RH WINDSHIELD SIDE POST UPPER ATTACHMENT AT FRAME 4, ONE HOLE WITH CRACK INDICATION. A DAMAGE REPORT WAS SENT TO AIRBUS ASKING FOR REPAIR INSTRUCTIONS AND FINAL APPROVAL. AIRBSDR IXXA2022060806Frame · corrodedCORROSION ON LOWER SURFACE OF UPPER FRAME CHORD, FRAME 1395 AT THE ROLLER RAIL LBL42 TO RBL42SDR CALA2022060801471Floor Support · corrodedCABIN FLOOR SUPPORT STRUCTURE BTW FR64-FR70, Y160.5, BEAM WITH C ORROSION REMOVED CORROSION ON CABIN FLOORBEAM AND FOUND WITHIN LIMITS IA W A320 SRM 53-00-14-283-002 L=2" W=1", D=.014" (MAX DEPTH ALLOWE D=.016") AND COUPLINGS REMOVED AND REPLACED IAW A320 SRM
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