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 CALA2021112202152Stringer · corroded(A3NB-53-3-6299) R/H FR66-68 STR24R HAS CORROSION (REMOVE AND RE PLACE STRINGER OR REPAIR) REMOVED DAMAGED STRINGER SECTION 24R FR 64-67, INSTALLED NEW STR INGER SECTION 24R FR 64-67 P/N D5348004720801 AND AFT STR TIES A ND SHEAR TIES REMOVED TO FOM IAW SRM 51SDR CALA2021112202150Beam · corrodedABIN FLOOR STRUCTURE FRAME HAS CORROSION AT FRAME 66 -Y765 REMOVED CORROSION AT CABIN FLOOR STRUCTURE FRAME 66 -Y765 IAW SR MPLISHED BY V936054 ON WC 0018120 AT ST ENGINEERING BFM M 51-74-00. FOUND TO BE OUT OF LIMIT IAW SRM 53-00-14-283-002 FI G 001. REMOVED SDR CALA2021112202142Beam · corroded(A3NB-53-3-6222) FLOOR BEAM Y1162.5 BETWEEN FR 68/69 HAS CORROSI ON. 52-42 () FLOOR BEAM Y1162.5 BETWEEN FR68-FR69 REMOVED AND REPLACED IAW SR M 51-72-11. ACCOMPLISHED BY EMP#V933868 AT BFM ST AEROSPACE MOBI LE. NR#0015806SDR CALA2021112202141Door Sill · corroded(A3NB-53-3-6299) AFT RH DOOR SILL HAS CORROSION IN SEVERAL LOCAT IONS. DOT 52-45. REMOVED AND REPLACED AFT R2 DOOR SILL IAW SRM 51-42-11, DWG D534 80595. ACCOMPLISHED BY EMP#V935774 AT BFM ST AEROSPACE MOBILE. N R#0015809SDR WX0A1900010073975None · noneNRC 1000-0129: AFT CARGO DOOR STRUCTURE, CORROSION LOCATED ON UPPER SURFACE OF FR 55A AT FASTENERS HOLE BTW STR 39RH-38RH / AFT CARGO DOOR SURROUND STRUCTURE ON UPPER SURFACE OF FR55A AT FASTENERS HOLES (QTY.2) BTW STR38RH-39RH SHEET ASSY REPAIRED AS PER AIRBUSDR WX0A1900010073974None · noneNRC 1000-0095: 31594-12 FLOOR LEVEL, ON CARGO DOOR ENTRANCE BTW FRAMES 59 TO 55A, SURFACE CORROSION ON TOP AND UNDER THE FLOOR FRAME STRG 38RH TO 37RH / AT AFT CARGO DOOR ENTRANCE UNDER FLOOR LEVEL BTW FR55A-FR59 AND STR37-38RH AREA, DOORSILL BEAM REPLACED AS SDR CALA2021111802134Frame · corrodedCABIN FLOOR STRUCTURE FRAME HAS CORROSION AT FR68 -Y765 REMOVED CORROSION AT CABIN FLOOR STRUCTURE FRAME 68 - Y765 IAW S RM 51-74-00 FOUND TO BE OUT OF LIMITS. REMOVED CABIN FLOOR STRUC TURE FRAME 68 - Y765 IAW SRM 51-42-11. INSTALLED NEW FLOOR BEAM IAW SRM 51SDR CALA2021111802133Floor Mat · corrodedCABIN FLOOR STRUCTURE HAS CORROSION AT FR70 Y254 REMOVED AND REPLACED NEW CABIN FLOOR STRUCTURE FRAME 70 Y254 IAW SRM 51-42-11 AND SRM 51-72-11. REMOVED CORROSION AT CABIN FLOOR STRUCTURE FRAME 70 Y254 IAW SRM 51-74-00, FOUND TO BE OUT OF LI MIT IAW SRM 53-00-SDR CALA2021111702121Beam · corrodedCABIN FLOOR STRUCTURE HAS CORROSION AT FR70 Y254 REMOVED AND REPLACED NEW CABIN FLOOR STRUCTURE FRAME 70 Y254 IAW SRM 51-42-11 AND SRM 51-72-11. REMOVED CORROSION AT CABIN FLOOR STRUCTURE FRAME 70 Y254 IAW SRM 51-74-00, FOUND TO BE OUT OF LI MIT IAW SRM 53-00-SDR CALA2021111702120Beam · corrodedCABIN FLOOR STRUCTURE FRAME HAS CORROSION AT FR68 -Y765SDR CALA2021111502101Beam · corroded(A3NB-53-3-6186) SEAT TRACK OVER FLOOR BEAM Y1292 FR57 TO FR64 H AS SEVERAL SPOTS WITH CORROSION. DOT 52-51.() REMOVED DAMAGED FLOOR SEAT TRACK FR47-64 IAW SRM 51-42-11. INSTA LLED NEW FLOOR SEAT TRACK P/N# D5397217620400 BATCH# 0003863708 IAW SRM 51-42-11. EMSDR CALA2021110102009Stringer · corrodedFOR SCEPTER TRACKING PURPOSE ONLY. DURING REINSTALLATION OF ELECTRICAL ACCESS FOR INCOMING REPAIR , MOD SKIN CORROSION , NEEDS TO BE EVALUATED. AS NOTED ON NR#5001106135-0010. DURING REINSTALLATION OF ELECTRICAL ACCESS FOR INCOMING REPAIR PERFORMERS IAW SRM 51SDR CALA2021102901995Plate · corrodedA3NB-53-4-6179 CORROSION FOUND IN AFT CARGO DOOR THRESHOLD FR52-55RH AND FRAME 55 UNDER TORSION BOX. AS NOTED ON LTPR NR#5001089366-0050SDR CALA2021102201956None · none(A3NB-53-3-6222) FLOOR BEAM -Y765 BETWEEN FR 66/70 HAS CORROSIO N. DOT 52-40 () REMOVED AND REPLACED FLOOR BEAM BETWEEN FR66 TO 70 AT -Y765 IAW A320 SRM 51-42-11. ACCOMPLISHED BY EMP#V933438 AT BFM ST AEROSPA CE MOBILE. NR 0015803SDR CALA2021102201950Beam · none(A3NB-53-3-6222) FLOOR BEAM Y254 BETWEEN FR 66/68 HAS CORROSION DOT 52-39 REMOVED AND REPLACED FLOOR BEAM Y254 BETWEEN FR 66/68 P/N D53472 17320100 IAW A320 SRM 51-42-11. ACCOMPLISHED BY EMP#V935833 AT S T AREORSPACE MOBILE. NR#0015802SDR CALA2021102201948Beam · none(A3NB-53-3-6222) FLOOR BEAM -Y765 BETWEEN FR 66/70 HAS CORROSIO N. DOT 52-40 () REMOVED AND REPLACED FLOOR BEAM BETWEEN FR66 TO 70 AT -Y765 IAW A320 SRM 51-42-11. ACCOMPLISHED BY EMP#V933438 AT BFM ST AEROSPA CE MOBILE. NR 0015803SDR CALA2021102001934Floorbeam · corroded(A3NB-53-3-6222) FLOOR BEAM Y254 BETWEEN FR 66/68 HAS CORROSION DOT 52-39 REMOVED AND REPLACED FLOOR BEAM Y254 BETWEEN FR 66/68 P/N D53472 17320100 IAW A320 SRM 51-42-11. ACCOMPLISHED BY EMP#V935833 AT S T AREORSPACE MOBILE. NR#0015802SDR SWAA2021101930438Fairing · crackedSUPPLEMENTAL INFORMATION: LEFT WING TO BODY FAIRINGS 191AL-191FL; SUPPORT ASSEMBLY CRACKED ; / [01] R&R LEFT WING TO BODY FAIRINGS 191AL-191FL; SUPPORT ASSEMBLY PER SRM 51-10-02 & SRM 51-40-02.SDR CALA2021101801887None · corrodedCORROSION ON BULK CARGO COMPT STGR 42R BETWEEN FR63 AND FR64 (A3 NB-53-3-6185) REMOVED CORROSION IAW SRM 51-74-00, CHECKED LIMITS L=18" D=.050" , OUT OF LIMITS IAW A320 SRM 53-41-13-283-002, REMOVED AND REPLA CED STRINGER 42R, BETWEEN FR60 TO FR64 P/N D5347041SDR CALA2021101401880Stringer · noneCORROSION ON BULK CARGO COMPT STGR41 LH BETWEEN FR63 AND FR64. REPLACED STRINGER 41L BETWEEN FR60 TO FR64. P/N: D5347041821600 BTCH: 0003849002 IAW A320 SRM 51-72-11-911-001 AND SRM 51-42-11. SFR# 1026673. MAINTENANCE ACCOMPLISHED BY V934700 ON WC 0014944 AT SSDR CALA2021101401879Stringer · noneCORROSION ON BULK CARGO COMPT STGR 42L/H BETWEEN FR63 AND FR64 REPLACED STRINGER 42L, BETWEEN FR60 TO FR64, P/N: D5347041821800 BATCH: 0003848975 IAW A320 SRM 51-72-11-911-001 AND SRM 51-42-1 1. SFR# 1026673 MAINTENANCE ACCOMPLISHED BY V934585 ON WC 001494 3 ASDR CALA2021101101845None · corrodedCORROSION ON BULK CARGO COMPT STGR41 LH BETWEEN FR63 AND FR64.SDR CALA2021101101844None · corrodedCORROSION ON BULK CARGO COMPT STGR 42L/H BETWEEN FR63 AND FR64SDR CALA2021071901136Door Sill · corroded(A3NB-53-3-6186) CORROSION ON AFT L/H DOOR LOWER SILL AT FR68. REMOVED DAMAGE REPAIR AND INSTALLED NEW REPAIR IAW SRM 51-41-14- 300-001. REMOVED CORROSION ON AFT L/H DOOR LOWER SILL AT FR68 IA W SRM 51-74-00 L=1.1" W=0.73" D=0.063" NOMINAL MAT. THICKNESS 0. 06SDR CALA2021071901120Seat Track · corroded(A3NB-53-3-6356) CORROSION ON L/H CABIN SEAT TRACK Y765 BETWEEN FR61 AND FR63 REMOVED CORROSION ON LH CABIN SEAT TRACK Y765, IAW SRM 51-74-00, SEAT TRACK FOUND TO BE OUT LIMITS BETWEEN FR61 AND FR62 IAW SRM 53-41-15-283 FIG 1. SEAT TRACK SECTION Y765 REPAIRED SDR CALA2021071601113Floorbeam · corroded(A3NB-53-3-6186) CORROSION ON AFT CABIN FLOOR BEAM Y-765 AT FR66 REMOVED CORROSION ON AFT CABIN FLOOR BEAM Y-765 AT FR66 IAW SRM 51-74-00, FOUND TO BE OUT LIMITS IAW SRM 53-41-14. REMOVED AND R EPLACED AFT CABIN FLOOR BEAM FROM FR64 TO 66 IAW SRM 51-42-11. M ASDR CALA2021071601103Beam · corroded(A3NB-53-3-6186) CORROSION ON AFT CABIN FLOOR BEAM Y160.5 BETWEE N FR68 AND FR70 BLENDED CORROSION AREA IAW SRM 57-74-00 REMOVED AND REPLACED NEW FLOOR BEAM P/N D5347209600000 BATCH# 00024944875 I.A.W A320 SRM 51-42-11, BLEND OUT FOUND TO BE OUT LIMITS IAW SRMSDR CALA2021071601104Beam · corroded(A3NB-53-3-6186) CORROSION ON AFT CABIN FLOOR BEAM Y 254 AT FR66 AFT END BLENDED CORROSION AREA IAW SRM 57-74-00 REMOVED AND REPLACED NEW FLOOR BEAM P/N D5347277320000 BATCH# 0002836727 IAW A320 SRM 51 -42-11, BLEND OUT FOUND TO BE OUT LIMITS IAW SRM 53-00-14 SDR HYIA20210714001Attach Fitting · crackedDURING A 402-22 VISUAL WING ATTACHMENT FITTING INSPECTION, CORROSION WAS NOTED ON THE AFT VERTICAL PORTION OF THE LEFT HAND LOWER INBOARD WING ATTACH FITTING, JUST BEFORE THE AREA WHERE THE FITTING MOUNTS IN THE SPAR CAP. UPON REMOVAL OF THE FITTING, A LARGERSDR 1MYR20210701001Attach Fitting · corrodedFUSELAGE FRAME STATION 73 LEFT AND RIGHT WING ATTACH FITTING SEVERELY CORRODED DUE TO DISSIMILAR METAL CORROSION STEEL/ALUMINUM. PART IS CORRODED BEYOND ECONOMICAL REPAIR. REPLACEMENT IS REQUIRED. THIS IS FOLLOWING UP ON SPECIAL AIRWORTHINESS INFORMATIONAL BULSDR WX0A1900010073960None · noneNRC 1000-0110: 633-19 BULK CARGO DOOR CUTOUT LOWER SILL BEAM FR61 AND 62, NUT PLATE AREAS, CORROSION FOUND. / BULK CARGO DOOR CUTOUT LOWER SILL BEAM BTW FR 61 AND FR 62 AT NUT PLATES AREAS (QTY.2) PERMANENTLY REPAIRED IAW SRM 53-41-49-300-003. REPAIR CATEGSDR QXEA2021030100081Channel · crackedCRACK ON UPPER CHANNEL OF LH UNDERWING TO FUSELAGE PANEL LANDING BETWEEN PANELS 263BL AND 263CL. CRACK DAMAGE AT FWD SECTION OF UPPER CHANNEL OF LH UNDER WING TO FUSELAGE PANELS REMOVED IAW RD84-53-10101. NDT CARRIED OUT BY SKY SERVICE (REF: WO# TWO33218) NO FSDR SWIA202157766Mount · corrodedEVIDENCE OF CORROSION FOUND AROUND NUTPLATE HOLES OF FWD WING TO FUSELAGE FAIRING MOUNTING JOINT STRAP (MARKED). (C-CHECK RO 4/22/2021) LOCATED, DRILLED AND INSTALLED NEW "T" SUPPORT PN: SH670-39063-1. REF CRJ 700 SRM 51-42-06-001-001-A01, 51-40-06-001-SDR A6WA202102177650Floorbeam · corrodedCORROSION COMMON TO PRESSURE FLOOR ANGLE AT FUSELAGE STATION 544.00 RBL 40 TO RBL 42. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION FS 544.00 RBL 40 TO RBL 42. .65 INCH WIDE X 2.0 INCH LONG PERFORMED HFEC, NO DEFECTS NOTED. PERFORMED UT THICKNESS CHESDR HYIA20210202001Fitting · corrodedDURING MAINTENANCE AN AREA OF CORROSION WAS VISUALLY IDENTIFIED ON THE LEFT HAND LOWER FUSELAGE ATTACH FITTING (P/N: 0811350-10) ON N763EA. THIS CORROSION MEASURES APPROXIMATELY .390 INCHES TALL, .429 WIDE, AND HAS A MAXIMUM DEPTH OF .056. IT IS LOCATED ON THESDR CALA2021012800100Door Sill · corrodedR2 SILL DOOR CENTER SHAPE SEAL HAS CORROSION FR 66-FR 68 A3NB-53 -3-6187-NR 9290511 (42511) AT HAECO LCQ. REMOVED AND REPLACED SHAPE SILL AT R-2 DOOR CENTER FR 66-FR 68, IAW A319 SRM 51-72-00-801 AND 51-42-11-801. REMOVED DOT.SDR GTIA2021012835571Threshold · damagedFOUND DURING TC 5001046727-0010 LIGHTNING STRIKE BETWEEB FR 58-59 STRINGER 34RT. RAF 2745921-2 CREATED. REVIEWED LTPR NRI 5001046727-0010. ACCOMPLISHED PERMANENT REPAIR IS CAT "B" REQ SUBSEQUENT INSP, IAW SRI 53-00-11-205-052 REV 135 INSP THRESHOLD FROM ADLSDR SWIA202056169Fitting · chafedL/H WING TO FUSELAGE FITTING - FS 473 - LOWER ATTACH FITTING SHOWS EVIDENCE OF CHAFFING ON EXTERIOR PANEL 2 PLACES AS MARKED (C-CHECK) RO 2/9/2021 REMOVED CHAFFING AT THE LH WING TO FUSELAGE FITTING FS.473 LOWER ATTACH FITTING REF CRJ 200 SRM 51-12-00 FOUNSDR FDEA202011182896Fitting · crackedLT WING ROOT FWD FACE FRAME 40 FWD FITTING STGR 32-33LT FOUND CRACK COMPLIED WITH EA: 6-5710-T0358132 P1. TITLE: WINGS-BASIC WING STRUCTURE-CRACK ON LT FR 40 FWD FITTING LOWER OUTBOARD RADIUS. REPAIRED THE LT WING ROOT FWD FACE- FRAME 40 FWD FITTING STGR 32SDR FE4R2020110917485Mount · damagedWHILE INVESTIGATING EXCESSIVE MOVEMENT BETWEEN THE LEFT WING AND FUSELAGE, BOTH WINGS WERE REMOVED FROM FUSELAGE. THE FORWARD LEFT WING ATTACH POINT BOLT HOLES FOUND ELONGATED TO TWICE THE BOLT DIAMETER. THE ATTACH BOLT WORN TO 75% NOMINAL DIAMETER. THE AFTSDR SWIA202054485Attach Fitting · corrodedRT WING STUB FAIRING ATTACHING GUIDE "FITTING", RT WING INBOARD TRAILING EDGE AREA, APPROXIMATELY WS 00.00, AFT OF FLAP TORQUE TUBE ANGLED GEAR BOX "CHAFED", FLAGGED. C-CHECK RO 12/04/2020. REPLACED RT WING STUB FAIRING ATTACHING GUIDE "FITTING", RT WING INSDR SWIA202054484Attach Fitting · chafedLT WING STUB FAIRING ATTACHING LUG/PLATE, LT WING TRAILING EDGE AREA, APPROXIMATELY WS 00.00, AFT OF FLAP TORQUE TUBE SHAFT ANGLED GEAR BOX MOUNT, CHAFED, FLAGGED. C-CHECK RO 12/04/2020. REPLACED LT WING STUB FAIRING ATTACHING LUG/PLATE, LT WING TRAILING EDGSDR LR7A2020100502535Attach Angle · corrodedDURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE RT FWD WING TO FUSELAGE FS 476 RBL 20 TO RBL 60 ATTACH ANGLE CORRODED. REPAIR BY REPLACEMENT ACCOMPLISHED, IAW LOCKHEED SMP583 SRM, CH 51-60 & 51-70. NR 6098.SDR 2020FA0000342Attach Fitting · looseWHILE PERFORMING UNRELATED MAINT MOVEMENT WAS NOTED IN THE WING ATTACHMENT AREAS. INVESTIGATION OF MOVEMENT REVEALED THAT THE NUT ASSEMBLY ON BOTH THE LEFT AND THE RIGHT WING ATTACHMENTS WERE INSTALLED BACKWARDS. TECH SUPPORT WAS CONTACTED, BOLTS REPLACED ANSDR SIMA202003094008Attach Angle · crackedLH WING-TO-FUSELAGE UPPER ATTACHMENT ANGLE. HAS EVIDENCE OF A CRACK APPROX. 1/2" LONG. JUST BELOW A RIVET AT FRAME 50.-C/A-RAR LH WING-TO-FUSELAGE UPPER ATTACHMENT ANGLE IAW SRM 51-40-02SDR SIMA202003026006Attach Angle · crackedLH WING-TO-FUSELAGE #2 LOWER ATTACHMENT ANGLE. HAS A 3/8" CRACK ON THE FWD END UP TO THE FIRST RIVET.-C/A-REMOVED AND REPLACED LH WING TO FUSELAGE #2 LOWER ATTACHMENT ANGLE IAW ETN-EM-53-142, AND SRM 51-40-02.SDR SIMA202003026004Attach Angle · crackedRH WING-TO-FUSELAGE LOWER ATTACHMENT ANGLE #1. HAS A 1/2" CRACK ON THE FWD END OF THE PREVIOUS REPAIR SPLICE. -C/A-REPLACED BOTH AREAS (REF TASK#1) WITH ONE REPAIR IAW ETN-EM-53-142R2.SDR SIMA202003026005Attach Angle · crackedLH WING-TO-FUSELAGE UPPER ATTACHMENT ANGLE. HAS EVIDENCE OF A CRACK APPROX. 1/2" LONG. JUST BELOW A RIVET AT FRAME 50. -C/A-REMOVED AND REPLACED LH WING TO FUSELAGE #2 LOWER ATTACHMENT ANGLE IAW ETN-53-142, AND SRM 51-40-02.SDR CALA2020022980520Attach Fitting · crackedMAIN CABIN CENTER WING ATTACHED FITTING CRACKS AT STA 540 AND RB L-41 MKD DOT (REF AAR NR 99876181) REMOVED AND REPLACED SUPPORT FITTING AT MAIN CABIN CENTER WING TANK AT STA 540 AND RBL-41 IAW B737 SRM 51-40-02. ADD EMP:V892418SDR XGNA202002060001Fitting · corrodedAIRCRAFT WAS IN MAINTENANCE FOR A ROUTINE 200 HOUR INSPECTION. MAINTENANCE WAS COMPLYING WITH MULTI-ENGINE OWNER ADVISORY MEL-57-02 WING- FORWARD LOWER CARRY-THRU SPAR CAP INSPECTION. DURING THIS INSPECTION CORROSION WAS NOTED ON THE CARRY-THRU SPAR LOWER FORW
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