JASC 5341
Service difficulty reports · 489
Reports filed under 5341 · Fuselage, Wing Attach Fittings, 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 = '5341' 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 = '5341' 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 SWAA2022081030381Intercostal · crackedINTERCOSTAL CRACKED AT FASTENER HOLE; STA 323; RBL31 / [01] REMOVED CRACKED INTERCOSTAL F.O.M.;[02] LOCATED AND DRILLED NEW INTERCOSTAL P/N:141A5410U140 AT STATION 323 AND RBL 31. ALL WORK REFERENCE TO SRM 51-20-02/0G01;[03] INSPECTION C/W.;[04] OK TO INSTALL.SDR SWAA2022081030384Intercostal · crackedINTERCOSTAL CRACKED AT FASTENER HOLE; STA 277; BL0 / [01] OK TO INSTALL.;[02] INSTALLED INTERCOSTAL PER SRM 51-40-02.;[03] C/W INSPECTIONSDR DALA2022071904971Web · crackedSHIP 3229 CRACK INDICATION FOUND ON FRAME WEB FR68 LH DOOR STOP FITTING 4. CORRECTIVE ACTION: PERFORMED REPAIR PER A320 SRM 53-41-12. (2325949)SDR DALA2022071904970Web · crackedSHIP 3229 CRACK INDICATION FOUND ON FRAME WEB FR68 LH DOOR STOP FITTING 6. CORRECTIVE ACTION: PERFORMED REPAIR PER A320 SRM 53-41-12. (2325942)SDR DALA2022071504907None · noneSHIP 3116 - FITTING FRAME 68 LOCATED BTW STR 22R TO STR 23R AFT PAX DOOR SILL. CORRECTIVE ACTION: FABRICATED FITTING FRAME 68 (1EA),LOCATED BTW STR 22R TO STR 23R AFT PAX DOOR SILL AT AFT GALLEY AREA, AS PER ER/A 600551. (2320229)SDR VQMA202207060001Attach Fitting · crackedMOUNTAIN AVIATION (CRS#: VQMR053W) COMPLETED THE WING ATTACH FITTING INSPECTION REQUIRED BY TEXTRON SERVICE LETTER SL750-57-07 AND FOUND CRACKS IN THE LH FWD (PN: 6710135-7) AND RH FWD (PN: 6710135-8) AUX SPAR CARRY THROUGH FITTING. THE WING ATTACH FITTING WASDR VQMA202207050001Attach Fitting · crackedTEXTRON AVIATION (CRS#: CNQR918C) COMPLETED THE WING ATTACH FITTING INSPECTION REQUIRED BY TEXTRON SERVICE LETTER SL750-57-07 AND FOUND CRACKS IN THE RH FWD (PN: 6710135-8), RH AFT (PN: 6710135-6), AND LH FWD (PN: 6710135-5) AUX SPAR CARRY THROUGH FITTINGS. TSDR VQMA202207010001Attach Fitting · crackedMOUNTAIN AVIATION (CRS#: VQMR053W) COMPLETED THE WING ATTACH FITTING INSPECTION REQUIRED BY TEXTRON SERVICE LETTER SL750-57-07 AND FOUND CRACKS IN THE RH FWD AUX SPAR CARRY THROUGH FITTING (PN: 6710135-8). THE WING ATTACH FITTING WAS REPLACED BY DEHAVILLAND ASDR VQMA202206280001Attach Fitting · crackedMOUNTAIN AVIATION (CRS#: VQMR053W) COMPLETED THE WING ATTACH FITTING INSPECTION REQUIRED BY TEXTRON SERVICE LETTER SL750-57-07 AND FOUND CRACKS IN THE LH FWD WING ATTACH FITTING (PN: 6710135-7). REPLACEMENT IS CURRENTLY UNDERWAY UNDER MOUNTAIN AVIATION WORK OSDR CALA2022062901603Skin · dentedUAL QC DISCOVERY DURING STORAGE, EXISTING DENT AND SCRATCH BETWEEN FRAMES 61 AND 62 JUST LEFT OF CENTER ON BELLY AFTER SMOOTHING PAINT SCRATCH STILL EXISTS, WILL REQUIRE ADDITIONAL EVALUATION IMENSIONS OF DENT: 2.4" L X 1.7" W X 0.42" D. FOUND TO BE OUT OF USESDR VQMA202206240001Attach Fitting · crackedMOUNTAIN AVIATION (CRS#: VQMR053W) COMPLETED THE WING ATTACH FITTING INSPECTION REQUIRED BY TEXTRON SERVICE LETTER SL750-57-07 AND FOUND CRACKS IN THE LH FWD (PN: 6710135-7), AND RH FWD (PN: 6710135-8) AUX SPAR CARRY THROUGH FITTINGS. THE WING ATTACH FITTING SDR UIEA2022062400654Web · corrodedCORROSION ON LOWER CHORD AND WEB OF WING TO BODY FAIRING FRAME ASSY (PN: 65B06749-50) AT STA 880 BETWEEN BL 0 LBL 40 REMOVED DAMAGE PARTS IAW SRM 51-40-02 REV 94. 2) REPAIRED DAMAGE AREA IAW SRM 53-00-71 REPAIR 2 REV 94 EI T2022A53M-1726 REV 1. 3) INSTALLED SDR GTIA2022062336491None · dentedDENT ON FUSELAGE- FRAME 53 + 14" STRINGER 40-41 LEFT. RAF-01 2964659-01 GENERATED.-REPAIRED DENT IN FUSELAGE SKIN FR 53+14 STR 40-41 LH PER A321 SRM 53-00-11-300-046. THIS IS CAT B REQUIRES REINSPECT AT 60,000FC/120,000FH SUBSIQUENT INSPECT TBD PER SRI 53-00-1SDR GTIA2022062336490Door Sill · corrodedR-4 PASSENGER DOOR SILL HAS CORROSION AROUND FASTENER HOLE AT FR 68 STR 23 RIGHT SIDE. RAF-01 2964658-02 WAS GENERATED FOR MAPPING PURPOSES ONLY.-REMOVED CORRODED SECTION AROUND NUT PLATE FASTENER HOLES AT R4 DOOR SILL FR68 IAW SRM 53-41-14-300-001 FIG 001. FASDR CALA2022062201553Torsion Box · corrodedAFT CARGO COMPARTMENT TORSION BOX UPPER SURFACE HAS MULTIPLE ARE A OF CORROSION SPEC # A3NB-05-3-6022 PER NR9290743/26743 GEN BY V077960 RMVD AND RPLD AFT CARGO COMPARTMENT TORSION BOX COVER IAW SRM 53 -41-49-283-004 FOUND TO BE OUT OF LIMITS MAX MAT. LOSS .01SDR AALA202207207255Attach Angle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED WING TO BODY FAIRING AND KEEL BEAM ATTACHMENT ANGLES, SHEAR PLATE WEB AT FR 42, -Y254 AND Z 2343.94. REPAIRED WEB PER EA 337185.SDR VQMA202206150001Attach Fitting · crackedMOUNTAIN AVIATION (CRS#: VQMR053W) COMPLETED THE WING ATTACH FITTING INSPECTION REQUIRED BY TEXTRON SERVICE LETTER SL750-57-07 AND FOUND CRACKS IN THE RH FWD AUX SPAR CARRY THROUGH FITTING (PN: 6710135-8). THE WING ATTACH FITTING WAS REPLACED BY DEHAVILLAND ASDR DALA2022062904534None · noneDURING PREFLIGHT. DENT DISCOVERED BETWEEN SERVICING DOORS UNDERSIDE OF AIRCRAFT. DENT LOCATED BETWEEN FRAME 65 & 66 AND BETWEEN 42R & 44 STRINGERS. PER A321 SRM 53-41-11-283-059 FIG 13 SHEET 2 OK TO DEFER FOR 200 F/C. A/C OK FOR SVC. EVALUATED DENT BETWEEN FRASDR VQMA202206100001Attach Fitting · crackedMOUNTAIN AVIATION (CRS#: VQMR053W) COMPLETED THE WING ATTACH FITTING INSPECTION REQUIRED BY TEXTRON SERVICE LETTER SL750-57-07 AND FOUND CRACKS IN THE LH FWD AUX SPAR CARRY THROUGH FITTING (PN: 6710135-7). THE WING ATTACH FITTING WAS REPLACED BY DEHAVILLAND ASDR CALA2022052301317None · corroded(A3NB-53-4-6179) AFT CARGO PIT DOOR SILL BETWEEN FR52/FR56 HAS C ORROSION IN SEVERAL LOCATIONS. DOT 52-69.() REPLACED DOOR SILL SHEET IAW A320 SRM 51-42-11. P/N: D5347556521 200 BATCH: 0003946991. EMP# V934700 WORK ACCOMPLISHED AT ST ENGI NEERING AEROSPACE OF SDR CALA2022052001304None · corroded(A3NB-53-4-6179) AFT CARGO PIT DOOR SILL BETWEEN FR52/FR56 HAS CORROSION IN SEVERAL LOCATIONS. DOT 52-69.() REPLACED DOOR SILL SHEET IAW A320 SRM 51-42-11. P/N: D5347556521 200 BATCH: 0003946991. EMP# V934700 WORK ACCOMPLISHED AT ST ENGI NEERING AEROSPACE OF MSDR CALA2022052001289None · noneFR68 LHS AFT DOOR STOP FITTING #1 TO #7 HOLES FOUND BEYOND THE REQUIRED STARTING HOLE DIAMETER OF 8-1-N AS PER EA 5340-01724 REV.C, OPERATION 002 STEP 6.1 FIGURE 01 SHEET 02. ZONE 260, SEQ 1605, LTPR NR# 5001155215-0010. RPR IS CONSIDERED CAT B. REINSPECT IAW SDR CALA2022052001288None · noneFR68 RHS AFT DOOR STOP FITTING #1 TO #7 HOLES FOUND BEYOND THE REQUIRED STARTING HOLE DIAMETER OF 8-1-N AS PER EA 5340-01724 REV.C, OPERATION 002 STEP 6.2 FIGURE 01 SHEET 02. ZONE 260, SEQ 1605, LTPR NR# 5001155217-0010. RPR IS CONSIDERED CAT B. REINSPECT IAW SDR CALA2022052001287None · noneFR66 LHS AFT DOOR STOP FITTINGS #1 TO #7 HOLES FOUND BEYOND THE REQUIRED STARTING HOLE DIAMETER OF 8-1-N AS PER EA 5340-01724 REV.C OPERATION 001 STEP 6.1 FIGURE 01 SHEET 02. ZONE 260 SEQ:1602. LTPR NR 005001155209-0010. RPR IS CONSIDERED CAT B. REINSPECT IAW SDR CALA2022052001286None · noneFR66 RHS AFT DOOR STOP FITTING #1 TO #7 HOLES FOUND BEYOND THE REQUIRED STARTING HOLE DIAMETER OF 8-1-N AS PER EA 5340-01724 REV.C OPERATION 001 STEP 6.2 FIGURE 01 SHEET 02. ZONE:260 SEQ:1602. LTPR NR# 5001155213-0010. RPR IS CONSIDERED CAT B. REINSPECT IAW SRSDR CALA2022052001284Beam · corrodedDURING REMOVAL OF NTF ON AFT WET AREA, CORROSION FOUND ON PREVIOUS REPAIR OF L2 DOOR SILL BEAM, EVALUATION IS RECORDED UNDER LP# 8445827. PERFORMED INSTALLATION OF REPAIR PARTS OH LH DOOR 2 SILL BEAM FR.68 IAW A320-200 SRM 53-41-14-300-001 REV 140, AS NOTED ONSDR CALA2022051601261Fitting · noneFR68 RHS AFT DOOR STOP FITTING #1 TO #7 HOLES FOUND BEYOND THE REQUIRED STARTING HOLE DIAMETER OF 8-1-N AS PER EA 5340-01724 REV.C, OPERATION 002 STEP 6.2 FIGURE 01 SHEET 02. ZONE 260, SEQ 1605, LTPR NR# 5001155217-0010. RPR IS CONSIDERED CAT B. REINSPECT IAW SDR CALA2022051601260Frame · noneFR66 RHS AFT DOOR STOP FITTING #1 TO #7 HOLES FOUND BEYOND THE REQUIRED STARTING HOLE DIAMETER OF 8-1-N AS PER EA 5340-01724 REV.C OPERATION 001 STEP 6.2 FIGURE 01 SHEET 02. ZONE:260 SEQ:1602. LTPR NR# 5001155213-0010. RPR IS CONSIDERED CAT B. REINSPECT IAW SRSDR CALA2022051601259Frame · noneFR68 LHS AFT DOOR STOP FITTING #1 TO #7 HOLES FOUND BEYOND THE REQUIRED STARTING HOLE DIAMETER OF 8-1-N AS PER EA 5340-01724 REV.C, OPERATION 002 STEP 6.1 FIGURE 01 SHEET 02. ZONE 260, SEQ 1605, LTPR NR# 5001155215-0010. RPR IS CONSIDERED CAT B. REINSPECT IAW SDR CALA2022051601258Fitting · noneFR66 LHS AFT DOOR STOP FITTINGS #1 TO #7 HOLES FOUND BEYOND THE REQUIRED STARTING HOLE DIAMETER OF 8-1-N AS PER EA 5340-01724 REV.C OPERATION 001 STEP 6.1 FIGURE 01 SHEET 02. ZONE 260 SEQ:1602. LTPR NR 005001155209-0010. RPR IS CONSIDERED CAT B. REINSPECT IAW SDR CALA2022051601239None · corroded(A3NB-53-4-6179) AFT CARGO PIT BETWEEN FR56/FR59 STRG 42LH HAS CORROSION. DOT 52-72.() REPLACED STRINGER 42L BETWEEN FR53 TO FR60, IAW A320 SRM 51-42-1 1 P/N:DAN50B09 BATCH: 0003906803. ACCOMPLISHED BY EMP#V934585 AT ST BFM AEROSPACE MOBILE. NR#0029746SDR EE4Y2022051115555Frame · noneDURING THE INSPECTION STRUCTURE INSPECTION PER RDAS 80150308/002/2016 ISSUE B ROTO TEST INSPECTIONS, THERE WERE FOUND TOOL MARKS BETWEEN STRG 19LH AND STRG 20LH, DUE TO THIS FACT DETAILS WERE SENT TO AIRBUS ASKING FOR REPAIR INSTRUCTIONS AND FINAL APPROVAL. AFSDR VNAA202206269997Strap · corrodedCORROSION ON SETTLEMENT AREA LOWER SECTION OF WING-TO-FUSELAGE FAIRING AT FS STA 909.00.SDR CALA2022050901167None · corroded(A3NB-53-4-6179) AFT CARGO PIT UNDERFLOOR BAY BETWEEN FR53/FR59 STRG 42LH HAS CORROSION. DOT 52-43. () REMOVED CORROSION AT AFT CARGO PIT BETWEEN FR53-FR59 IAW SRM 51- 002. REMOVE AND REPLACED STRG 42LH BETWEEN FR53-FR60 IAW SRM 51- 74-00 AREA 1 BETWEEN FR53-5SDR VNAA202206269998Diaphragm · corrodedCORROSION ON DIAPHRAGM AT SETTLEMENT AREA LOWER SECTION OF WING-TO-FUSELAGE FAIRING BTW FS879.00/909.00 AND STR 24RH.SDR CALA2022042101042Stringer · corroded(A3NB-53-4-6179) AFT CARGO PIT UNDERFLOOR BAY BETWEEN FR64/FR65 STRG 43RH HAS CORROSION. DOT 52-36 () REMOVED CORROSION IAW 320 SRM 51-74-00 AND FOUND OUT OF LIMITS I BY EMP#V933870 AT BFM ST AEROSPACE MOBILE. NR#0027407 AW SRM 53-41-13-300-004 FIG 001 CHECKEDSDR DALA2022042002759Access Panel · elongatedSHIP 3234 ELONGATED HOLE ACCESS PANEL 540JB FUEL TANK CUT OUT LH WING. CORRECTIVE ACTION: REPAIRED PER A320 SRM 57-21-11. OK FOR SERVICE. (2201559)SDR CALA2022041801014Frame · corroded(A3NB-53-4-6179) AFT CARGO PIT UNDERFLOOR BAY BETWEEN FR64/FR65 STRG 43RH HAS CORROSION. DOT 52-36 () REMOVED CORROSION IAW 320 SRM 51-74-00 AND FOUND OUT OF LIMITS I BY EMP#V933870 AT BFM ST AEROSPACE MOBILE. NR#0027407 AW SRM 53-41-13-300-004 FIG 001 CHECKEDSDR EE4Y2022051115554Frame · crackedDURING THE INSPECTION STRUCTURE INSPECTION PER RDAS 80150308/002/2016 ISSUE A ROTO TEST INSPECTIONS, THERE WERE FOUND TWO HOLES WITH CRACK INDICATION AT FRAME 66, AT STOP FITTING #5 AREA, DUE TO THIS FACT DETAILS WERE SENT TO AIRBUS ASKING FOR REPAIR INSTRUCTSDR UIEA2022041200293Fitting · crackedCRACK-FOUND LH LONGERON EXTENSION FITTING HAS CRACK AT STA 1480. DIMENSION ABOUT 0.5"(<P>1. REPAIR THE LH SIDE LONGERON EXTENSION FITTING IAW EI# T2022A07M-887 REV 0 & T2022A53M-954 REV 1 AND DWG # 65B15254 SH 10 REV G, 65B15254 SH 16 REV F, 65B01162 SH 14 REVSDR YENA2022041200360None · noneDURING HEAVY MAINTENANCE, (EA A22-218-01) FUSELAGE / REAR FUSELAGE/ UPPER SKIN PANEL/ FR 69/70 AT LEVEL OF STR 4L/ DENT- PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)SDR CALA2022040800933Frame · corrodedCORROSION ON AFT CABIN DR SILL BEAM AT FR.68 RH (A3NB-53-3-6187 ZONE 200 SEQ.618. LHT NR #5001115178-0010. CORROSION ON DR SILL BEAM FR66-FR68 STGR 23RH. PERFORMED REWORK REPLACEMENT OF RH DOOR SILL BEAM IS REQUIRED, PERFORMED ON DOOR SILL BEAM, THE REWORK ON SDR YENA2022040600343Shear Tie · corrodedDURING HEAVY MAINTENANCE, CORROSIÓN ON SHEARCLIP FR 75 BETWEEN STGR 22 & 23 LH ON AFT CARGO COMPARTMENT STRUCTURE; SUMMARY OF NRC 00123:CORROSION ON SHEARCLIP FR 75 BETWEEN STGR 22 & 23 LH ON AFT CARGO COMPARTMENT STRUCTURE WAS REMOVED AND EVALUATED ORIGINAL TSDR CALA2022040600893Floor Support · corrodedCORROSION ON AFT CABIN DR SILL BEAM AT FR.68 RH (A3NB-53-3-6187 ZONE 200 SEQ.618. LHT NR #5001115178-0010.SDR CALA2022033100858Floorbeam · corrodedCORROSION ON LH SIDE FLOOR SUPPORT BEAM Y-765 BETWEEN FR67-FR68 REMOVED CORROSION ON BEAM Y765 FR67-68 IN CABIN FLOOR IAW SRM 51 STA: ST ENG BFM SFR# 1028160 -74-00 BLENDED AREA MEASURES L=2.5" W=1" DEPTH=0.080" FOUND OUT OF LIMITS IAW SRM 53-00-14-283-002 FIGSDR CALA2022033100857Floorbeam · corrodedCORROSION ON RH SIDE FLOOR SUPPORT BEAM Y-1292 BETWEEN FR65-FR66 CORROSION ON RH SIDE FLOOR SUPPORT BEAM Y-1292 BTWN FR65-66 REMO LOCATED AND DRILLED IAW SRM 51-44-11 INSTALLED RH SIDE SUPPORT B VED IAW SRM 51-74-00, FOUND OUT OF LIMITS IAW SRM 53-00-14-283-0 SDR CALA2022033100856Fitting · corrodedCORROSION ON R2 DOOR CUTOUT LOWER FWD CORNER FITTING AFT OF FR66 RECEIVED NEW CORNER FITTING AFT FR60 PN D5348004220501 (OUT OF S EQUENCE ENTRY) REMOVED DAMAGE FITTING IAW SRM 51-42-11. INSTALLE D NEW CORNER FITTING IAW SRM 51-42-11. EMP: V934718 WC: 0024194 SSDR CALA2022033100855Floorbeam · corrodedCORROSION ON RH SIDE FLOOR SUPPORT BEAM Y-765 HAS CORROSION BETW EEN FR67-FR68 REMOVED CORROSION ON RH SIDE FLOOR SUPPORT BEAM Y-765 BTW FR67-6 (CALIPER T91558, DEPTH GAUGE T93985) REMOVED AND REPLACED FLOOR 8 IAW SRM 51-74-00. BLEND OUT FOUND OUT OF LIMITS IASDR A6WA202203308154None · crackedANGLE STIFFENER AT FS 516.00, ON LH BL 45.00 IS CRACKED AS MARKED ****AIRCRAFT REMOVED FROM SERVICE*** REMOVED CRACKED STIFFENER AND INSTALLED NEW ANGLE STIFFENER AT FS 516.00 ON LH BL 45.00 IAW ED# AWAC-CRJ253-01817SDR DALA2022033102159None · noneSHIP 3234 CORROSION LOWER SILL LOC BTW FR66 TO FR68 RH SIDE IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED LOWER SILL PER A320 SRM 51-42-11 AND 51-72-11. (2177484)
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