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.

SDR MASA20261001220Strap · inoperativeDURING HEAVY CHECK AFT WING TO FUSELAGE CORRODED ATTACHMENT STRAP BTWN FR 73 & FR 75, BTWN S23 - 28L REMOVED AND REPLACED WITH NEW IAW SRM 51-43-04 & SRM 51-41-02. NRC 450200-1000-0017, REV 45.Sep 23, 2026 · N88328 · Emb ERJ170200LLSDR MASA20261001219Strap · inoperativeDURING HEAVY CHECK AFT WING TO FUSE, CORRODED ATTACHMENT STRAP BET FR 73 - 75, BTWN STR 23R & STR25R. REMOVED AND REPLACED WITH NEW IAW SRM 51-43-04 AND SRM 51-41-02. NRG 4502700-1000-0016, REV 45.Sep 23, 2026 · N88328 · Emb ERJ170200LLSDR 2026FA0000624Bolt · corrodedPER BEECH SI 0572-031 AND BEECH SERVICE MANUAL, 35590096B, REISSUED: NOVEMBER 15, 1960; 35-590096B21, REVISED: AUGUST 29, 2003, PAGE 4-4M, THE WING BOLTS ARE TO BE MAGNETICALLY INSPECTED EVERY FIVE (5) YEARS AND REPLACED EVERY FIFTEEN (15) YEARS. SINCE MOST Aug 6, 2026 · N7203N · Beech V35ASDR 1Q2R2026080220061Fitting · chafedRT WING TO FUSELAGE ATTACHMENT FITTING AT FS797.00 HAS TWO CHAFED AREAS. PERFORMED PERMANENT REPAIR IN ACCORDANCE WITH RFTS-130158 REV. 0, DATED JULY 29, 2026, AND MHI RJ REO 670-57-11-265 REV. --, DATED JULY 29, 2026.Jul 29, 2026 · N528EG · Cndair CL6002C10SDR LR7A2026070103895Drag Angle · crackedDURING SCHEDULED B-2 CHECK UNDER SB 382-53-61, FOUND LH FUSELAGE TO WING DRAG ANGLE CRACKED AT FS477-617, LBL61, WL146. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1001392944.Jul 1, 2026 · N407LC · Lkheed 382GSDR 2026FA0000507Angle · crackedLEFT HAND UPPER ANGLE AT WING ROOT AND FUSELAGE CRACKS UNDER PRESSURIZATION/DEPRESSURIZATION WITH FLEX.Jun 10, 2026 · N512K · Cessna 414ASDR 2026FA0000506Angle · crackedLEFT HAND UPPER ANGLE AT WING ROOT AND FUSELAGE CRACKS UNDER PRESSURIZATION/DEPRESSURIZATION WITH FLEX.Jun 10, 2026 · N543PM · Cessna 421CSDR IPXA2026041526322Bracket · corrodedLH WING ROOT UPPER SIDE THROUGH ACCESS PANEL 191DL HAVE 4 BRACKETS WITH CORROSION . INSTALLED 2 NEW BRACKETS I.A.W. B757-200PF SRM 51-40-02. REVIEWEDMar 28, 2026 · N430UP · Boeing 75724APFSDR 4GIA2026020206201Drag Angle · failedLEFT FWD WING TO FUSELAGE DRAG ANGLE FOUND CRACKED. LT REAR WING TO FUSELAGE DRAG ANGLE CRACKED IN RH AFT WING DOULBLER BEHIND ANGLE IS CRACK: PERFORM AN EDDY CURRENT INSPECTION TO DETECT CRACKING OF THE FUSELAGE FRAME ANGLES AT THE WING FRONT AND REAR SPAR Jan 6, 2026 · N419BT · Cndair CL2156B11215SDR 2025FA0000819Attach Fitting · chafedFUSELAGE TO RT WING ATTACHMENT FITTING CHAFED.Dec 11, 2025 · N811QS · Textrn TEXTRON700SDR 2025FA0000779Wing Root · corrodedCORROSION FOUND WHERE LT AND RT WING AND FUSELAGE MEET.Nov 21, 2025 · N313QS · Cessna 680CESDR COEA2026012102816Frame · damagedFUSELAGE WING ATTACHMENT FITTING, LT FWD INTERIOR FRAME 25 RIB 4 MIDDLE AFT HOLE HAS FLAW INDICATION. REPAIRED PER SRAS S535R0181. 26497 ISSUE A, DATED 11/19/2025.Oct 17, 2025 · N816FX · Aerosp ATR72212SDR VNAA20251015092Angle · corrodedWING TO FUSELAGE SUPPORT ANGLES AT RH SIDE AT FS939 PN SH670-39265-4 AND SH670-39265-6 HAS EXCESSIVE CORROSION REMOVED CORRODED ANGLES. LOCATED AND INSTALLED NEW ANGLES IAW REO 670-53-82-679 REV.--.Oct 17, 2025 · N501BG · Cndair CL6002C10SDR JJBA20251024078Attach Bracket · crackedRH WING TO FUSELAGE FAIRING ATTACH BRACKET SECOND FROM FDW SIDE OF WING CRACKED. INSTALLED NEW RH WING FAIRING ATTACH BRACKET AND DOUBLER.Jul 27, 2025 · N12135 · Emb EMB145XRSDR DALA2025052704021Structure · wornSHIP 9509 LT WING OUTBD-AIRFRAME-HINGE BOLT HOLE IS WORN. CORRECTIVE ACTION: ALL WORK C/W ON ERA 625207 -14 REV ORG. (0973047)May 18, 2025 · N950AT · Boeing 717200SDR EE4Y2025040722141Frame · crackedDURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-53-260-002 UPPER FUSELAGE AFT PAX CABIN CREW ENTRY DOOR FR66 RH DOOR STOP FITTING # 5 UPPER OUTBOARD HOLE WITH CRACK WAS FOUND. PERFORMED OVERSIZE BOLTS INSTALLATION ON AFT PAX CABIN ENTRY DOOR AT FRE66 RH DOOR Apr 7, 2025 · N272NV · Airbus A320214SDR HNAA2024050100297Attach Angle · scratchedSCRATCH ON SKIN AT WING TO FUSE ATTACHMENT ANGLE AT X15921. REPAIRED IAW ETD2025-145-905349 AND EO 1-53-25-0133Mar 26, 2025 · N686AE · Emb EMB145LRSDR IPXA2025041380559Angle · corrodedLEFT WING ROOT ON PANEL 191DL NUTPLACE BRACKET HAVE EEVIDENCE OF CORROSION DOT 07-034.REMOVED 4EA NUTPLATES ON BRACKET AT 191DL PANEL IAW B757-200 SRM 51-40-02-0G-0.BLENDED CORROSION ON BRACKET AT 191DL PANEL IAW B757-200 SRM 51-10-02-0G-0.REMOVED BRACKET ON 1Mar 26, 2025 · N443UP · Boeing 75724APFSDR EE4Y2024120221384Beam · mechanic errorDURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-ZL-171-01-2-001_P1-OP-UP-LF/005, REAR FUSELAGE PAX CABIN FR66 Y=254.0 BEAM WITH DOUBLE DRILLED HOLE PLUGGED WAS FOUND. AIRBUS WAS CONTACTED FOR REPAIR INSTRUCTIONS. AIRBUS PROVIDED REPAIR INSTRUCTIONS. THE PERMADec 2, 2024 · N286NV · Airbus A320214SDR YENA2024120201525String · corrodedDURING HEAVY MAINTENANCE: FUSELAGE / AFT FUSELAGE / STRINGER 37 LH BETWEEN FR 62-63 / CORROSION - PERMANENT REPAIR; REFERENCES: /1/ AEROMAN EA 53-9059-24 REV. 0 (COVER + PARTS 1 & 2) /2/ AIRBUS TD/81487525/006/2024#A /3/ AIRBUS RDAF 81487525/003/2024#A /4/ AIRNov 29, 2024 · N708JB · Airbus A320232SDR EE4Y2024021419447Frame · crackedDURING ACCOMPLISHMENT OF THE ALLEGIANT TASK 534123-01-2-001 FR 66 LH SIDE INNER CAP JOINT TO GUSSET PLATE AT STGR 15L FOUND SECOND HOLE (FROM UP TO DOWN) WITH CRACK. THE REPAIR WAS PERFORMED FOLLOWING THE REPAIR INSTRUCTIONS AS PER A319 SRM 53-41-12-300-018.THFeb 14, 2024 · N311NV · Airbus A319111SDR EE4Y2024021419445Frame · crackedDURING ACCOMPLISHMENT OF THE ALLEGIANT TASK 534123-01-2-001 FR 66 LH SIDE INNER CAP JOINT TO GUSSET PLATE AT STGR 12L FOUND SECOND HOLE (FROM UP TO DOWN) WITH CRACK. THE REPAIR WAS PERFORMED FOLLOWING THE REPAIR INSTRUCTIONS AS PER A319 SRM 53-41-12-300-018.THFeb 14, 2024 · N311NV · Airbus A319111SDR DALA2024011800745Fastener · unknownSHIP 3271 DISC: REF LOG PAGE 1666423 PERM REPAIR C/W ON FASTENER ONE INCH FWD OF FR59 ON STR 38 PER A320 SRM 53-41-11 REF LOG #0646904. C/A: ER SRI 53-41-11 PAGE 233 REQUIRES REINSPECT AT 60000 FC /120000 FH FROM FIRST FLIGHT PER SRI 53-41-11-205-005 LOG-PAGE Jan 15, 2024 · N371NW · Airbus A320212SDR 2024FA0000334Lock Fastener · looseAFT WING FITTING LOCK FASTENERS FOUND LOOSE ON LEFT AND RIGHT WING. ADDRESSED IN PIPPER SB820A BUT NOT APPLICABLE TO THIS MODEL AIRCRAFT AND SHOULD BE.Jan 11, 2024 · N423JT · Piper PA46350PSDR DALA2024010200058Unknown · unknownSHIP 3312 CORROSION FOUND AT LAV MOUNT 8" AFT OF FRAME 73 AT LBL 70. CORRECTIVE ACTION: REMOVED AND REPLACED BEAM. (0132905)Dec 30, 2023 · N812NW · Airbus A330323SDR YENA2024010200010Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION: AFT LH LAVATORY FWD INBD FLOOR FITTING; REF EAMS NR-00200 W/O H9334: R & R AFT LAVATORY FLOOR FITTING PER SAFRAN CMM 25-42-06.Dec 29, 2023 · N198JB · Emb ERJ190100IGWSDR EE4Y2023121018948Door Frame · crackedDURING ACCOMPLISHMENT ALLEGIANT TASK CARD 53-260-003 AND AD 2022-22-04, IT WAS FOUND ATFR68 LHS DOOR STOP FITTING # 6 FASTENER HOLES AREA WITH CRACK INDICATION. THE PERMANENT REPAIRWAS ACCOMPLISHED IAW A320 SRM 53-41-12-300-008 AND SRM 53-41-12-300-009.THE REPDec 10, 2023 · N238NV · Airbus A320214SDR EE4Y2023112918887Frame · crackedDURING ALLEGIANT TASK INSPECTION 534123-01-3-001 FUSELAGE INTERNAL STRUCTURE FR666 RH SIDEINNER CAP JOINT TO GUSSET PLATE AT STGR 15RH LEVEL. FOUND THE HIGHEST HOLE & THE LOWESTHOLE CRACKED. COOPESA PERFORMED REPAIR IN ACCORDANCE A320 SRM TASK 53-41-12-300-018Nov 29, 2023 · N261NV · Airbus A320214SDR EE4Y2023092518460Frame · crackedDURING ALLEGIANT TASK INSPECTION 53-260-003 REAR FUSELAGE AFT PASS DOOR RH SIDE FR66 DOORSTOP FITTING # 1 LOWER I/B HOLE HAS BEEN FOUND WITH CRACK INDICATION. COOPESA PERFORMED REPAIR IN ACCORDANCE A320 SRM TASK 53-41-12-300-010. THIS REPAIR IS COVERED WITH CSep 25, 2023 · N259NV · Airbus A320214SDR DALA2023092907992Unknown · unknownSHIP 1702 THE CABIN ABOVE WING CENTER FOUND END FITTING CRACK AT STA927, LBL91. CORRECTIVE ACTION: DAMAGED REPAIRED PER ER/A:612062-14 (2983383)Sep 23, 2023 · N172DZ · Boeing 767332SDR IPXA2023091872753Unknown · unknown**SDR FILED OPEN**FAULT: AFT CARO PIT, SURFACE CORROSION ON R/H TRANSITION PANEL FROM FRS 1180 TO FRS 1310. CPCP AND SDR INFO RECORDED.Aug 29, 2023 · N433UP · Boeing 75724APFSDR HYIA20230724001Fitting · corrodedDURING MAINTENANCE A SPOT OF CORROSION WAS VISUALLY IDENTIFIED ON THE AFT FACE OF THE FWD RH UPPER FUSELAGE ATTACH FITTING PN: 0811350-9. THIS CORROSION MEASURES .275 WIDE, AND .226 TALL, WITH AN APPROXIMATE DEPTH OF .018 AND IS CONSISTENT WITH OTHER CORROSIONJul 20, 2023 · N160PB · Cessna 402CSDR EE4Y2023062717943Stringer · corrodedDURING INSPECTION TASK ZL-171-01-2-001 STRINGER 43 LEFT FLANGE UPPER CORROSION WAS FOUND.PERFORMED PERMANENT REPAIR AT STGR43L, BETWEEN FR64 AND FR66 I.A.W A320 SRM TASK 53-41-13-300-004 FIGURE 001 (SHEET 1), REV 144 DATED 02- 01-2023. THIS IS A MAJOR PERMANENJun 27, 2023 · N289NV · Airbus A320214SDR YENA2023062200682Unknown · unknownDURING HEAVY MAINTENANCE: FUSELAGE / AFT FUSELAGE / CARGO COMPARTMENT AT FR56 & 62 STGR 32L / CORROSION. PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)Jun 21, 2023 · N653JB · Airbus A320232SDR CALA2023040300962Flange · crackedFR 68, STR 22 LH, FLANGE HAS CRACK AT LOWER RADIUS APPROX. 1.7 I NCHES LONG AND PENETRATES THROUGH TO IB FACE OF INNER CAP APPROX . 1.0 INCH LONG VERTICALLY. "CONTACT ENGINEERING FOR REPAIR INST RUCTIONS BEFORE NEXT FLIGHT." AD RELATED SUPPORT TASK(AD 2022-15 Mar 31, 2023 · N830UA · Airbus A319131SDR GTIA2023032337063Door Sill · corrodedINSIDE CABIN AFT WET AREA- LEFT SIDE OF CABIN. DOOR SILL BEAM HAS CORROSION AROUND FASTENER HOLE. FRAME 68 STR 23L. RAF-01 CREATED.-REPAIRED AFT CABIN L4 DOOR SILL BEAM FR68 STR 23L PER A321 SRM 53-41-14-300-001 PRINCIPLE 5 CAT A REPAIR NO REINSPECTMar 22, 2023 · N674NK · Airbus A321231SDR WX0A2023040531746Unknown · unknownNRC 1000-0004: (S/M 141-1) EXTERNAL FUSELAGE SKIN INTERNAL SURFACE, CORROSION FOUND BTW FR 64-65 AND BTW STGR 43L-43R. / EXTERNAL FUSELAGE SKIN INTERNAL SURFACE BTW FR 64-65 AND BTW STGR 43L-43R NO DAMAGE ALLOWED ON INTERNAL SURFACE OF EXTERNAL SKIN AS PER PERMar 15, 2023 · N284NV · Airbus A320214SDR EE4Y2023031017408Unknown · corrodedDURING INSPECTION TASK 534150-01-2-001 LOWER FUSELAGE AFT CARGO DOOR CUTOUT BETWEEN FR55A AND FR59 AT LOWER SILL BELOW SHEET COVER WEB WITH NUT PLATE RUSTY AT SEVERAL PLACES WAS FOUND. THE SILL D5347715020200 WAS REPLACED IAW A319 SRM 51-72-11-911-001 REV 142 Mar 10, 2023 · N334NV · Airbus A319111SDR EE4Y2023031017407Frame · unknownDURING TASK INSPECTION 53-260-003 REAR FUSELAGE AFT PAX DOOR STOP FITTING # 1 CRACK WAS FOUND. PERMANENT REPAIR AT AFT ENTRY DOOR FRAME 68LH AT LOWER I/B HOLE DOOR STOP FITTING IAW A319 SRM TASK 53-41-12-300-011 PARAG 2.A TABLE 004 FIGURE 008 (SHEET 1,2,AND 3)Mar 10, 2023 · N312NV · Airbus A319111SDR EE4Y2023031017381Beam · corrodedDURING INSPECTION UPPER FUSELAGE AFT PAX CABIN FROM FR68 TO FR70 AT Y130 LONGITUDINAL BEAM WITH CORROSION WAS FOUND. THE LONGITUDINAL BEAM WAS REPLACED IAW A319 51-72-11-911-001 ATTACHED WITH HI-LOK IAW A319 SRM 51-42-11 PARAG 2F(2) REV140 DATED 02/01/2022 ANDMar 10, 2023 · N302NV · Airbus A319112SDR EE4Y2023031017378Floorbeam · corrodedDURING INSPECTION ON REAR FUSELAGE PAX CABIN FROM FR66+140MM TO FR 68 AT -Y 765 FLOOR BEAM WITH CORROSION WAS FOUND. THE AFFECTED FLOOR BEAM WAS REPLACED IAW A319 SRM 51-72-11-911-001 AND 51-72-11-911-002 REV140 DATED 02/01/2022 . THE REPAIR IS CAPTURED IN COOMar 10, 2023 · N314NV · Airbus A319111SDR EE4Y2023031017377Profile · noneDURING INSPECTION LOWER FUSELAGE AFT CARGO COMPARTMENT AT FR56, BETWEEN 260 AND Y 680 PROFILES WITH ELONGATED HOLES WAS FOUND. THE AFFECTED PROFILES WERE REPLACED IAW A319 SRM 51-72-11-911-001 PARAG 2 REV 140 DATE 02-01-2022 AND DRAWING D53974965 ISSUE 5. THISMar 10, 2023 · N314NV · Airbus A319111SDR EE4Y2023031017376Stringer · corrodedDURING INSPECTION AT COOPESA MRO COORSION WAS REPORTED AT AFT CARGO COMPARTMENT STGR 42RH BETWEEN FR57-FR59 AND STGR43LH BETWEEN FR56-FR58 COOPESA ASSESSED THE DAMAGE AND COORDINATED A REPAIR WITH AIRBUS VIA TECH REQUEST DOSSIER # 810422127. AIRBUS ISSUED A REMar 10, 2023 · N328NV · Airbus A319111SDR EE4Y2023031017375Shear Plate · corrodedDURING MAINTENANCE AT COOPESA MRO CORROSION WAS REPORTED ON AFT CARGO COMPARTMENT SHEAR PLATES AT STGR-38RH AND FR52-FR60. COOPESA ASSESSED THE DAMAGE AND COORDINATED A REPAIR WITH AIRBUS VIA TECH REQUEST DOSSIER 81044409. AIRBUS ISSUED A REPAIR APPROVAL BY MEMar 10, 2023 · N328NV · Airbus A319111SDR EE4Y2023031017374Intercostal · corrodedAFT CARGO COMPARTMENT FROM FR47/51 TO FR65 BETWEEN 38LH AND 38RH NUT PLATES RUSTY AT SEVERAL PLACES WAS FOUND.AIRBUS WAS CONTACTED FOR REPAIR INSTRUCTIONS. AIRBUS PROVIDED REPAIR INSTRUCTIONS AND DAMAGE WAS REPAIRED IAW COOPESA EO COO-EO-2022-15305-R03 AND THEMar 10, 2023 · N328NV · Airbus A319111SDR UIEA2023030900228None · noneCORROSION - FOUND CORROSION ON SKIN INNER SURFACE TOTAL 26EA WHEN PERFORM SB 747-53A2898(<P>1. REMOVED THE AFFECTED FASTENERS IAW SRM 51-40-02-0G-0 REV96 2. PERFORMED EI NO T2023A53-135 REV0 3. PERFORMED EI NO T2023A53M-135 REV 1 4. PERFORMED EI NO. T2023A53M-Mar 8, 2023 · N476MC · Boeing 74747UFSDR SWAA2023032010698Structure · elongatedCOCKPIT DOOR SURROUND ATTACHMENT AT FRAME 277 BETWEEN STRINGER 1R-2R AFTER REMOVE BOLTS; FOUND ELONGATED HOLES AND GAUGES.<[01] INSTALLED PROTECTION EWIS AROUND FRAME 277 BETWEEN STRINGERS 1R-2R REF. BOEING 737 AMM 20-60-07-913-801;[02] REMOVED CHANEL AND ANGLFeb 27, 2023 · N216WR · Boeing 7377H4SDR SWAA2023022403660Doubler · out of toleranceUPON REMOVAL OF EGPR INTERNAL SURROUND DOUBLER; FOUND EXISTING EXTERNAL DOUBLER AND TRIPLER WITH DEEP COUNTERSINKS.<[01] PARTIALLY: STARTED FABRICATION OF THE EXTERNAL DOUBLER OF EGPR MATERIAL USED 2024T3 .063 IN AS PER SRM 53-10-15-2R-5 FIG 202 SHEET 1;[02] FFeb 15, 2023 · N408WN · Boeing 7377H4SDR CALA2023021300413Unknown · crackedFUSELAGE FR68 (RH) CRACKED BETWEEN FRAME WEB AND FRAME STIFFENER (STR 22RH) AND CORROSION DAMAGE NOTED IN THE FRAME FWD FACE & INNER CAP AREA BETWEEN STR23R-24R. REF HAECO LCQ NR 9296525 AND NR 9296374. BETWEEN STR23R-24R PER HAECO REO-L242211 REV IR AND ECRAFeb 11, 2023 · N449UA · Airbus A320232SDR YENA2023021400159None · noneDURING HEAVY MAINTENANCE: FUSELAGE / REAR FUSELAGE / FR68 & STGR 22R HORIZONTAL FLANGE RADIUS & DOOR STOP FITTING #1 HOLE 3 / CRACK - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)Feb 10, 2023 · N508JL · Airbus A320232
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