# JASC 5341: Fuselage, Wing Attach Fittings

- Type: JASC system/component code (FAA)
- ATA chapter: 53 Fuselage
- Title in the code table: FUSELAGE, WING ATTACH FITTINGS
- Service difficulty reports: 489
- FAA code table: https://www.faa.gov/sites/faa.gov/files/JASC_Code.pdf#page=48
- Page: https://openairdocs.org/jasc/5341

## What it covers

For reports of the fittings on the fuselage used for the attachment of the wings.

## Service difficulty reports (489, newest 50)

- [SDR MASA20261001220](https://openairdocs.org/sdr/MASA20261001220), Sep 23, 2026: Emb ERJ170200LL. STRAP. INOPERATIVE. DURING HEAVY CHECK AFT WING TO FUSELAGE CORRODED ATTACHMENT STRAP BTWN FR 73 & FR 75, BTWN S23 - 28L REMOVED AND REPLACE (N88328)
- [SDR MASA20261001219](https://openairdocs.org/sdr/MASA20261001219), Sep 23, 2026: Emb ERJ170200LL. STRAP. INOPERATIVE. DURING HEAVY CHECK AFT WING TO FUSE, CORRODED ATTACHMENT STRAP BET FR 73 - 75, BTWN STR 23R & STR25R. REMOVED AND REPLAC (N88328)
- [SDR 2026FA0000624](https://openairdocs.org/sdr/2026FA0000624), Aug 6, 2026: Beech V35A. BOLT. CORRODED. PER BEECH SI 0572-031 AND BEECH SERVICE MANUAL, 35590096B, REISSUED: NOVEMBER 15, 1960; 35-590096B21, REVISED: AUGUST 29 (N7203N)
- [SDR 1Q2R2026080220061](https://openairdocs.org/sdr/1Q2R2026080220061), Jul 29, 2026: Cndair CL6002C10. FITTING. CHAFED. RT WING TO FUSELAGE ATTACHMENT FITTING AT FS797.00 HAS TWO CHAFED AREAS. PERFORMED PERMANENT REPAIR IN ACCORDANCE WITH R (N528EG)
- [SDR LR7A2026070103895](https://openairdocs.org/sdr/LR7A2026070103895), Jul 1, 2026: Lkheed 382G. DRAG ANGLE. CRACKED. DURING SCHEDULED B-2 CHECK UNDER SB 382-53-61, FOUND LH FUSELAGE TO WING DRAG ANGLE CRACKED AT FS477-617, LBL61, WL146.  (N407LC)
- [SDR 2026FA0000507](https://openairdocs.org/sdr/2026FA0000507), Jun 10, 2026: Cessna 414A. ANGLE. CRACKED. LEFT HAND UPPER ANGLE AT WING ROOT AND FUSELAGE CRACKS UNDER PRESSURIZATION/DEPRESSURIZATION WITH FLEX. (N512K)
- [SDR 2026FA0000506](https://openairdocs.org/sdr/2026FA0000506), Jun 10, 2026: Cessna 421C. ANGLE. CRACKED. LEFT HAND UPPER ANGLE AT WING ROOT AND FUSELAGE CRACKS UNDER PRESSURIZATION/DEPRESSURIZATION WITH FLEX. (N543PM)
- [SDR IPXA2026041526322](https://openairdocs.org/sdr/IPXA2026041526322), Mar 28, 2026: Boeing 75724APF. BRACKET. CORRODED. LH WING ROOT UPPER SIDE THROUGH ACCESS PANEL 191DL HAVE 4 BRACKETS WITH CORROSION . INSTALLED 2 NEW BRACKETS I.A.W. B757 (N430UP)
- [SDR 4GIA2026020206201](https://openairdocs.org/sdr/4GIA2026020206201), Jan 6, 2026: Cndair CL2156B11215. DRAG ANGLE. FAILED. LEFT FWD WING TO FUSELAGE DRAG ANGLE FOUND CRACKED. LT REAR WING TO FUSELAGE DRAG ANGLE CRACKED IN RH AFT WING DOULBLER  (N419BT)
- [SDR 2025FA0000819](https://openairdocs.org/sdr/2025FA0000819), Dec 11, 2025: Textrn TEXTRON700. ATTACH FITTING. CHAFED. FUSELAGE TO RT WING ATTACHMENT FITTING CHAFED. (N811QS)
- [SDR 2025FA0000779](https://openairdocs.org/sdr/2025FA0000779), Nov 21, 2025: Cessna 680CE. WING ROOT. CORRODED. CORROSION FOUND WHERE LT AND RT WING AND FUSELAGE MEET. (N313QS)
- [SDR COEA2026012102816](https://openairdocs.org/sdr/COEA2026012102816), Oct 17, 2025: Aerosp ATR72212. FRAME. DAMAGED. FUSELAGE WING ATTACHMENT FITTING, LT FWD INTERIOR FRAME 25 RIB 4 MIDDLE AFT HOLE HAS FLAW INDICATION. REPAIRED PER SRAS  (N816FX)
- [SDR VNAA20251015092](https://openairdocs.org/sdr/VNAA20251015092), Oct 17, 2025: Cndair CL6002C10. ANGLE. CORRODED. WING TO FUSELAGE SUPPORT ANGLES AT RH SIDE AT FS939 PN SH670-39265-4 AND SH670-39265-6 HAS EXCESSIVE CORROSION REMOVED C (N501BG)
- [SDR JJBA20251024078](https://openairdocs.org/sdr/JJBA20251024078), Jul 27, 2025: Emb EMB145XR. ATTACH BRACKET. CRACKED. RH WING TO FUSELAGE FAIRING ATTACH BRACKET SECOND FROM FDW SIDE OF WING CRACKED. INSTALLED NEW RH WING FAIRING ATTACH BR (N12135)
- [SDR DALA2025052704021](https://openairdocs.org/sdr/DALA2025052704021), May 18, 2025: Boeing 717200. STRUCTURE. WORN. SHIP 9509 LT WING OUTBD-AIRFRAME-HINGE BOLT HOLE IS WORN. CORRECTIVE ACTION: ALL WORK C/W ON ERA 625207 -14 REV ORG. (09 (N950AT)
- [SDR EE4Y2025040722141](https://openairdocs.org/sdr/EE4Y2025040722141), Apr 7, 2025: Airbus A320214. FRAME. CRACKED. DURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-53-260-002 UPPER FUSELAGE AFT PAX CABIN CREW ENTRY DOOR FR66 RH DOOR ST (N272NV)
- [SDR HNAA2024050100297](https://openairdocs.org/sdr/HNAA2024050100297), Mar 26, 2025: Emb EMB145LR. ATTACH ANGLE. SCRATCHED. SCRATCH ON SKIN AT WING TO FUSE ATTACHMENT ANGLE AT X15921. REPAIRED IAW ETD2025-145-905349 AND EO 1-53-25-0133 (N686AE)
- [SDR IPXA2025041380559](https://openairdocs.org/sdr/IPXA2025041380559), Mar 26, 2025: Boeing 75724APF. ANGLE. CORRODED. LEFT WING ROOT ON PANEL 191DL NUTPLACE BRACKET HAVE EEVIDENCE OF CORROSION DOT 07-034.REMOVED 4EA NUTPLATES ON BRACKET A (N443UP)
- [SDR EE4Y2024120221384](https://openairdocs.org/sdr/EE4Y2024120221384), Dec 2, 2024: Airbus A320214. BEAM. MECHANIC ERROR. DURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-ZL-171-01-2-001_P1-OP-UP-LF/005, REAR FUSELAGE PAX CABIN FR66 Y=254.0 B (N286NV)
- [SDR YENA2024120201525](https://openairdocs.org/sdr/YENA2024120201525), Nov 29, 2024: Airbus A320232. STRING. CORRODED. DURING HEAVY MAINTENANCE: FUSELAGE / AFT FUSELAGE / STRINGER 37 LH BETWEEN FR 62-63 / CORROSION - PERMANENT REPAIR; REFE (N708JB)
- [SDR EE4Y2024021419447](https://openairdocs.org/sdr/EE4Y2024021419447), Feb 14, 2024: Airbus A319111. FRAME. CRACKED. DURING ACCOMPLISHMENT OF THE ALLEGIANT TASK 534123-01-2-001 FR 66 LH SIDE INNER CAP JOINT TO GUSSET PLATE AT STGR 15L FO (N311NV)
- [SDR EE4Y2024021419445](https://openairdocs.org/sdr/EE4Y2024021419445), Feb 14, 2024: Airbus A319111. FRAME. CRACKED. DURING ACCOMPLISHMENT OF THE ALLEGIANT TASK 534123-01-2-001 FR 66 LH SIDE INNER CAP JOINT TO GUSSET PLATE AT STGR 12L FO (N311NV)
- [SDR DALA2024011800745](https://openairdocs.org/sdr/DALA2024011800745), Jan 15, 2024: Airbus A320212. FASTENER. UNKNOWN. SHIP 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 RE (N371NW)
- [SDR 2024FA0000334](https://openairdocs.org/sdr/2024FA0000334), Jan 11, 2024: Piper PA46350P. LOCK FASTENER. LOOSE. AFT WING FITTING LOCK FASTENERS FOUND LOOSE ON LEFT AND RIGHT WING. ADDRESSED IN PIPPER SB820A BUT NOT APPLICABLE TO THI (N423JT)
- [SDR DALA2024010200058](https://openairdocs.org/sdr/DALA2024010200058), Dec 30, 2023: Airbus A330323. UNKNOWN. UNKNOWN. SHIP 3312 CORROSION FOUND AT LAV MOUNT 8" AFT OF FRAME 73 AT LBL 70. CORRECTIVE ACTION: REMOVED AND REPLACED BEAM. (0132 (N812NW)
- [SDR YENA2024010200010](https://openairdocs.org/sdr/YENA2024010200010), Dec 29, 2023: Emb ERJ190100IGW. UNKNOWN. UNKNOWN. DURING HEAVY MAINTENANCE: CORROSION: AFT LH LAVATORY FWD INBD FLOOR FITTING; REF EAMS NR-00200 W/O H9334: R & R AFT LAVA (N198JB)
- [SDR EE4Y2023121018948](https://openairdocs.org/sdr/EE4Y2023121018948), Dec 10, 2023: Airbus A320214. DOOR FRAME. CRACKED. DURING ACCOMPLISHMENT ALLEGIANT TASK CARD 53-260-003 AND AD 2022-22-04, IT WAS FOUND ATFR68 LHS DOOR STOP FITTING # 6 FA (N238NV)
- [SDR EE4Y2023112918887](https://openairdocs.org/sdr/EE4Y2023112918887), Nov 29, 2023: Airbus A320214. FRAME. CRACKED. DURING ALLEGIANT TASK INSPECTION 534123-01-3-001 FUSELAGE INTERNAL STRUCTURE FR666 RH SIDEINNER CAP JOINT TO GUSSET PLAT (N261NV)
- [SDR EE4Y2023092518460](https://openairdocs.org/sdr/EE4Y2023092518460), Sep 25, 2023: Airbus A320214. FRAME. CRACKED. DURING ALLEGIANT TASK INSPECTION 53-260-003 REAR FUSELAGE AFT PASS DOOR RH SIDE FR66 DOORSTOP FITTING # 1 LOWER I/B HOLE (N259NV)
- [SDR DALA2023092907992](https://openairdocs.org/sdr/DALA2023092907992), Sep 23, 2023: Boeing 767332. UNKNOWN. UNKNOWN. SHIP 1702 THE CABIN ABOVE WING CENTER FOUND END FITTING CRACK AT STA927, LBL91. CORRECTIVE ACTION: DAMAGED REPAIRED PER  (N172DZ)
- [SDR IPXA2023091872753](https://openairdocs.org/sdr/IPXA2023091872753), Aug 29, 2023: Boeing 75724APF. UNKNOWN. UNKNOWN. **SDR FILED OPEN**FAULT: AFT CARO PIT, SURFACE CORROSION ON R/H TRANSITION PANEL FROM FRS 1180 TO FRS 1310. CPCP AND SDR (N433UP)
- [SDR HYIA20230724001](https://openairdocs.org/sdr/HYIA20230724001), Jul 20, 2023: Cessna 402C. FITTING. CORRODED. DURING MAINTENANCE A SPOT OF CORROSION WAS VISUALLY IDENTIFIED ON THE AFT FACE OF THE FWD RH UPPER FUSELAGE ATTACH FITTI (N160PB)
- [SDR EE4Y2023062717943](https://openairdocs.org/sdr/EE4Y2023062717943), Jun 27, 2023: Airbus A320214. STRINGER. CORRODED. DURING INSPECTION TASK ZL-171-01-2-001 STRINGER 43 LEFT FLANGE UPPER CORROSION WAS FOUND.PERFORMED PERMANENT REPAIR AT S (N289NV)
- [SDR YENA2023062200682](https://openairdocs.org/sdr/YENA2023062200682), Jun 21, 2023: Airbus A320232. UNKNOWN. UNKNOWN. DURING HEAVY MAINTENANCE: FUSELAGE / AFT FUSELAGE / CARGO COMPARTMENT AT FR56 & 62 STGR 32L / CORROSION. PERMANENT REPAI (N653JB)
- [SDR CALA2023040300962](https://openairdocs.org/sdr/CALA2023040300962), Mar 31, 2023: Airbus A319131. FLANGE. CRACKED. FR 68, STR 22 LH, FLANGE HAS CRACK AT LOWER RADIUS APPROX. 1.7 I NCHES LONG AND PENETRATES THROUGH TO IB FACE OF INNER C (N830UA)
- [SDR GTIA2023032337063](https://openairdocs.org/sdr/GTIA2023032337063), Mar 22, 2023: Airbus A321231. DOOR SILL. CORRODED. INSIDE CABIN AFT WET AREA- LEFT SIDE OF CABIN. DOOR SILL BEAM HAS CORROSION AROUND FASTENER HOLE. FRAME 68 STR 23L. RAF- (N674NK)
- [SDR WX0A2023040531746](https://openairdocs.org/sdr/WX0A2023040531746), Mar 15, 2023: Airbus A320214. UNKNOWN. UNKNOWN. NRC 1000-0004: (S/M 141-1) EXTERNAL FUSELAGE SKIN INTERNAL SURFACE, CORROSION FOUND BTW FR 64-65 AND BTW STGR 43L-43R. / (N284NV)
- [SDR EE4Y2023031017408](https://openairdocs.org/sdr/EE4Y2023031017408), Mar 10, 2023: Airbus A319111. UNKNOWN. CORRODED. DURING INSPECTION TASK 534150-01-2-001 LOWER FUSELAGE AFT CARGO DOOR CUTOUT BETWEEN FR55A AND FR59 AT LOWER SILL BELOW S (N334NV)
- [SDR EE4Y2023031017407](https://openairdocs.org/sdr/EE4Y2023031017407), Mar 10, 2023: Airbus A319111. FRAME. UNKNOWN. DURING TASK INSPECTION 53-260-003 REAR FUSELAGE AFT PAX DOOR STOP FITTING # 1 CRACK WAS FOUND. PERMANENT REPAIR AT AFT E (N312NV)
- [SDR EE4Y2023031017381](https://openairdocs.org/sdr/EE4Y2023031017381), Mar 10, 2023: Airbus A319112. BEAM. CORRODED. DURING INSPECTION UPPER FUSELAGE AFT PAX CABIN FROM FR68 TO FR70 AT Y130 LONGITUDINAL BEAM WITH CORROSION WAS FOUND. THE (N302NV)
- [SDR EE4Y2023031017378](https://openairdocs.org/sdr/EE4Y2023031017378), Mar 10, 2023: Airbus A319111. FLOORBEAM. CORRODED. DURING INSPECTION ON REAR FUSELAGE PAX CABIN FROM FR66+140MM TO FR 68 AT -Y 765 FLOOR BEAM WITH CORROSION WAS FOUND. THE (N314NV)
- [SDR EE4Y2023031017377](https://openairdocs.org/sdr/EE4Y2023031017377), Mar 10, 2023: Airbus A319111. PROFILE. NONE. DURING INSPECTION LOWER FUSELAGE AFT CARGO COMPARTMENT AT FR56, BETWEEN 260 AND Y 680 PROFILES WITH ELONGATED HOLES WAS  (N314NV)
- [SDR EE4Y2023031017376](https://openairdocs.org/sdr/EE4Y2023031017376), Mar 10, 2023: Airbus A319111. STRINGER. CORRODED. DURING INSPECTION AT COOPESA MRO COORSION WAS REPORTED AT AFT CARGO COMPARTMENT STGR 42RH BETWEEN FR57-FR59 AND STGR43LH (N328NV)
- [SDR EE4Y2023031017375](https://openairdocs.org/sdr/EE4Y2023031017375), Mar 10, 2023: Airbus A319111. SHEAR PLATE. CORRODED. DURING MAINTENANCE AT COOPESA MRO CORROSION WAS REPORTED ON AFT CARGO COMPARTMENT SHEAR PLATES AT STGR-38RH AND FR52-FR6 (N328NV)
- [SDR EE4Y2023031017374](https://openairdocs.org/sdr/EE4Y2023031017374), Mar 10, 2023: Airbus A319111. INTERCOSTAL. CORRODED. AFT CARGO COMPARTMENT FROM FR47/51 TO FR65 BETWEEN 38LH AND 38RH NUT PLATES RUSTY AT SEVERAL PLACES WAS FOUND.AIRBUS WAS (N328NV)
- [SDR UIEA2023030900228](https://openairdocs.org/sdr/UIEA2023030900228), Mar 8, 2023: Boeing 74747UF. NONE. NONE. CORROSION - FOUND CORROSION ON SKIN INNER SURFACE TOTAL 26EA WHEN PERFORM SB 747-53A2898(<P>1. REMOVED THE AFFECTED FAST (N476MC)
- [SDR SWAA2023032010698](https://openairdocs.org/sdr/SWAA2023032010698), Feb 27, 2023: Boeing 7377H4. STRUCTURE. ELONGATED. COCKPIT DOOR SURROUND ATTACHMENT AT FRAME 277 BETWEEN STRINGER 1R-2R AFTER REMOVE BOLTS; FOUND ELONGATED HOLES AND GAUGE (N216WR)
- [SDR SWAA2023022403660](https://openairdocs.org/sdr/SWAA2023022403660), Feb 15, 2023: Boeing 7377H4. DOUBLER. OUT OF TOLERANCE. UPON REMOVAL OF EGPR INTERNAL SURROUND DOUBLER; FOUND EXISTING EXTERNAL DOUBLER AND TRIPLER WITH DEEP COUNTERSINKS.<[01] (N408WN)
- [SDR CALA2023021300413](https://openairdocs.org/sdr/CALA2023021300413), Feb 11, 2023: Airbus A320232. UNKNOWN. CRACKED. FUSELAGE FR68 (RH) CRACKED BETWEEN FRAME WEB AND FRAME STIFFENER (STR 22RH) AND CORROSION DAMAGE NOTED IN THE FRAME FWD  (N449UA)
- [SDR YENA2023021400159](https://openairdocs.org/sdr/YENA2023021400159), Feb 10, 2023: Airbus A320232. NONE. NONE. DURING HEAVY MAINTENANCE: FUSELAGE / REAR FUSELAGE / FR68 & STGR 22R HORIZONTAL FLANGE RADIUS & DOOR STOP FITTING #1 HOL (N508JL)

All 489: https://openairdocs.org/jasc/5341/reports.md

## Other codes in chapter 53

- [JASC 5300](https://openairdocs.org/jasc/5300): Fuselage Structure (General) (8,203 reports)
- [JASC 5301](https://openairdocs.org/jasc/5301): Aerial Tow Equipment (18 reports)
- [JASC 5302](https://openairdocs.org/jasc/5302): Rotorcraft Tail Boom (965 reports)
- [JASC 5310](https://openairdocs.org/jasc/5310): Fuselage Main, Structure (38,407 reports)
- [JASC 5311](https://openairdocs.org/jasc/5311): Fuselage Main, Frame (61,504 reports)
- [JASC 5312](https://openairdocs.org/jasc/5312): Fuselage Main, Bulkhead (20,041 reports)
- [JASC 5313](https://openairdocs.org/jasc/5313): Fuselage Main, Longeron/Stringer (36,267 reports)
- [JASC 5314](https://openairdocs.org/jasc/5314): Fuselage Main, Keel (2,917 reports)
- [JASC 5315](https://openairdocs.org/jasc/5315): Fuselage Main, Floor Beam (44,152 reports)
- [JASC 5320](https://openairdocs.org/jasc/5320): Fuselage Miscellaneous Structure (215,699 reports)
- [JASC 5321](https://openairdocs.org/jasc/5321): Fuselage Floor Panel (49,299 reports)
- [JASC 5322](https://openairdocs.org/jasc/5322): Fuselage Internal Mounting Structure (12,746 reports)
- [JASC 5323](https://openairdocs.org/jasc/5323): Fuselage Internal Stairs (98 reports)
- [JASC 5324](https://openairdocs.org/jasc/5324): Fuselage Fixed Partitions (40 reports)
- [JASC 5330](https://openairdocs.org/jasc/5330): Fuselage Main, Plate/Skin (79,225 reports)
- [JASC 5340](https://openairdocs.org/jasc/5340): Fuselage Main, Attach Fittings (22,382 reports)
- [JASC 5342](https://openairdocs.org/jasc/5342): Fuselage, Stabilizer Attach Fittings (573 reports)
- [JASC 5343](https://openairdocs.org/jasc/5343): Fuselage, Landing Gear Attach Fittings (1,946 reports)
- [JASC 5344](https://openairdocs.org/jasc/5344): Fuselage, Door Hinge (2,418 reports)
- [JASC 5345](https://openairdocs.org/jasc/5345): Fuselage, Equipment Attach Fittings (813 reports)
- [JASC 5346](https://openairdocs.org/jasc/5346): Fuselage, Powerplant Attach Fittings (921 reports)
- [JASC 5347](https://openairdocs.org/jasc/5347): Fuselage, Seat/Cargo Attach Fittings (66,268 reports)
- [JASC 5350](https://openairdocs.org/jasc/5350): Aerodynamic Fairings (6,107 reports)
- [JASC 5397](https://openairdocs.org/jasc/5397): Fuselage Main, Bulkhead Fuselage wiring (67 reports)

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